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WO2020017645A1 - Vehicle structural member - Google Patents

Vehicle structural member Download PDF

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Publication number
WO2020017645A1
WO2020017645A1 PCT/JP2019/028507 JP2019028507W WO2020017645A1 WO 2020017645 A1 WO2020017645 A1 WO 2020017645A1 JP 2019028507 W JP2019028507 W JP 2019028507W WO 2020017645 A1 WO2020017645 A1 WO 2020017645A1
Authority
WO
WIPO (PCT)
Prior art keywords
hollow member
hollow
longitudinal direction
reinforcing
bending
Prior art date
Application number
PCT/JP2019/028507
Other languages
French (fr)
Japanese (ja)
Inventor
孝博 相藤
Original Assignee
日本製鉄株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 日本製鉄株式会社 filed Critical 日本製鉄株式会社
Priority to JP2019559381A priority Critical patent/JP6693605B1/en
Publication of WO2020017645A1 publication Critical patent/WO2020017645A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D21/00Understructures, i.e. chassis frame on which a vehicle body may be mounted
    • B62D21/15Understructures, i.e. chassis frame on which a vehicle body may be mounted having impact absorbing means, e.g. a frame designed to permanently or temporarily change shape or dimension upon impact with another body
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • B62D25/08Front or rear portions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • B62D25/20Floors or bottom sub-units

Definitions

  • the present invention relates to a vehicle structural member.
  • the crushable zone of the front part there is a component called a front side member.
  • a load is input to the front side member mainly from the longitudinal direction (axial direction) of the member.
  • the front side member undergoes compression bending deformation.
  • compression bending deformation only the bent portion buckles and undergoes plastic deformation, but the other portions do not undergo much plastic deformation.
  • the axial crushing deformation in which buckling occurs continuously and deforms in a bellows-like manner has a wide plastic deformation region, and has higher energy absorption efficiency than bending deformation.
  • a member such as a front side member of the vehicle absorbs energy while performing compression bending deformation at the time of collision.
  • Patent Literature 1 discloses a plurality of ribs such that an inner space of a front portion of a hollow frame member is separated at regular intervals in a member longitudinal direction. A deployed technique is disclosed. Note that no rib is provided at the rear of the hollow frame member.
  • Patent Literature 2 discloses a welded structure closed-section frame that is used for an automobile body frame, a suspension frame, or the like and that prevents opening or breakage at a welded portion in a collision.
  • a plate-like metal reinforcing member is provided in a hollow member.
  • Patent Literature 3 discloses a configuration in which a plurality of reinforcing members are provided in a hollow member (strength member) having a closed cross-sectional structure, and discloses a technique using a synthetic resin as the reinforcing member.
  • Patent Document 4 discloses a technique of attaching a reinforcing member to the inner surface of a hollow member in a vehicle structural member, and discloses that the tensile strength of the hollow member is 980 MPa or more.
  • JP 2004-182189 A JP 2010-76762 A JP-A-11-342882 JP-A-2017-159896
  • Patent Document 1 with respect to the pitch of undulating buckling waves generated when a load is input (buckling mode pitch), the sum of the length of one side of the rectangular cross section of the hollow frame member and the length of the other side is constant. It is disclosed that if there is, even if the ratio of the length of one side to the length of the other side changes, the pitch of the buckling mode does not change. Patent Document 1 discloses that in the case of a square cross section, the length of one side and the pitch of the buckling mode are in a proportional relationship.
  • Patent Documents 2 to 4 disclose that the impact is efficiently absorbed when a load is input and that the load-bearing performance is improved and the weight is reduced.
  • the detailed conditions for causing deformation and improving the energy absorption performance are not sufficiently disclosed.
  • the detailed configuration such as the arrangement, spacing, number, and plate thickness of the reinforcing members has not been sufficiently disclosed, and there is room for further improving the energy absorption performance of structural members for vehicles.
  • the vehicle structural members such as the front side member, the rear side member, the crash box, and the extension have high energy absorption performance in a stable manner.
  • deformation occurs.
  • the present invention has been made in view of the above problems, and in a vehicle structural member, while achieving weight reduction, stably generate axial crush deformation at the time of a vehicle collision, and maintain or improve energy absorption performance. Aim.
  • a metal hollow member and each side are joined to an inner surface of the hollow member, and a member longitudinal direction of the hollow member is separated so as to separate an inner space of the hollow member.
  • the structural member for a vehicle wherein three or more sheets are arranged at an interval of 0.74 to 1.84 times the minimum width from the end of the vehicle, and the plate thickness of the reinforcing member is 0.7 to 3.0 mm.
  • the hollow member has a bending inducing portion in a part in the member longitudinal direction, and the interval between the reinforcing members arranged in the bending inducing portion is the interval between the reinforcing members arranged in portions other than the bending inducing portion. It may be narrower than.
  • the hollow member has a bending inducing portion in a part in the member longitudinal direction, and the thickness of the reinforcing member arranged in the bending inducing portion is a thickness of the reinforcing member arranged in a portion other than the bending inducing portion. It may be thicker than the plate thickness.
  • the hollow member has a bending inducing part in a part in the member longitudinal direction, and the tensile strength of the reinforcing member arranged in the bending inducing part is the reinforcing member arranged in a part other than the bending inducing part. May be greater than the tensile strength of the steel.
  • the FRP may be CFRP or GFRP.
  • the hollow member may have a tensile strength of 980 MPa or more.
  • the vehicle structural member may be any of a front side member, a rear side member, an extension, and a crash box.
  • axial crush deformation in a vehicle structural member, axial crush deformation can be stably generated at the time of a vehicle collision while maintaining weight reduction, and energy absorption performance can be maintained or improved.
  • FIG. 2 is a perspective view illustrating a schematic configuration of a vehicle frame according to the embodiment. It is a perspective view showing the shape of the reinforcing member concerning the embodiment.
  • FIG. 2 is a diagram showing a cross section of the vehicle frame according to the same embodiment, which is perpendicular to the member longitudinal direction of the hollow member.
  • FIG. 7 is a sectional view taken along line aa in FIG. 6.
  • FIG. 7 is a sectional view taken along line bb in FIG.
  • the vehicle body provided in a vehicle such as a general automobile can be classified into a front structure (FRONT), a rear structure (REAR), and a cabin structure (CABIN).
  • FRONT front structure
  • RRR rear structure
  • CABIN cabin structure
  • the front structure and the rear structure have a function of absorbing and mitigating a shock to the vehicle (shock absorbing function) by crushing the structure by itself during a vehicle collision. That is, in order to ensure the safety of the occupants in the cabin at the time of a vehicle collision, the front structure and the rear structure are required to have a structure that absorbs as much energy as possible due to the collision (collision energy). Therefore, the frames constituting the front structure and the rear structure are required to absorb a large amount of collision energy even when bending or crushing occurs during a collision.
  • the frames used for the front structure and the rear structure are, for example, front side members and rear side members.
  • the front side member includes a front side member rear that forms a rear end portion, and a front side member front that forms a portion on the front side of the rear end portion.
  • the rear side member includes a rear side member rear that constitutes a rear end, and a rear side member front that constitutes a portion on the front side of the rear end.
  • the strength and thickness of the steel sheet forming the vehicle body structure are being promoted.
  • the frames constituting the front structure, the rear structure, and the cabin structure are also being replaced with thinned high-strength steel plates.
  • the thickness of the frame formed by the high-strength steel sheet is made by the conventional steel sheet so that at least one of the collision energy absorption and the load-bearing performance is equivalent to the frame formed by the conventional steel sheet. It is set thinner than the frame to be formed. This makes it possible to reduce the weight of the frame while maintaining the collision performance of the high-strength frame equal to that of the conventional frame.
  • FIG. 1 is a perspective view showing a state in which a vehicle frame 1 according to one embodiment of the present invention and other members are joined.
  • FIG. 2 is a plan view of the state
  • FIG. 3 is a side view of the state.
  • the vehicle frame 1 in the examples shown in FIGS. 1 to 3 is a front side member, and the front end of the front side member is joined to a bumper beam 40 via a crash box 30.
  • two front side members are arranged symmetrically in front of the cabin portion, and FIGS. 1 to 3 show only one of the two front side members.
  • the vehicle frame 1 is an example of a vehicle structural member, and will be simply referred to as a frame 1 below.
  • the frame 1 is preferably applied to members having a front structure and a rear structure, but the vehicle frame 1 may be applied to a member having a cabin structure. Further, the vehicle structural member is applicable not only to automobiles but also to other vehicles and self-propelled machines. Other vehicles and self-propelled machines include, for example, motorcycles, heavy vehicles such as buses or towing vehicles, trailers, railway vehicles, construction machines, mining machines, agricultural machines, general machines, ships, and the like.
  • the frame 1 of the present embodiment includes a hollow member 10 made of metal and a plurality of reinforcing members 20 arranged inside the hollow member 10.
  • the hollow member 10 of the present embodiment is an example of a long structural member, and has a rectangular cross section perpendicular to the longitudinal direction of the member (the X direction in the present embodiment).
  • the hollow member 10 of the present embodiment is a square tubular member formed as an integral body, the hollow member 10 is configured by, for example, joining a flat closing plate and a member having a hat-shaped cross section. May be. That is, the configuration of the hollow member 10 is not particularly limited as long as the cross section perpendicular to the member longitudinal direction X is a closed cross section.
  • the shape of the hollow member 10 is a rectangular shape, which is an example of a polygonal shape.
  • the hollow member 10 may be a polygonal shape other than a rectangle.
  • the minimum width W min on the external dimensions is set to be 30% or more of the maximum width W max on the external dimensions. It is composed of
  • the hollow member 10 of the present embodiment has four flat portions 11a to 11d.
  • the plane part located on the upper side in FIG. 6 is the top part 11a
  • the plane part located on the right side is the side part 11b
  • the plane part located on the lower side is FIG.
  • the bottom portion 11c and the flat portion located on the left side are referred to as side portions 11d.
  • the connecting portion between the two flat portions 11a and 11b, which is the portion between the top surface portion 11a and the side surface portion 11b is a ridge line portion 11e
  • the two flat portion 11b which is the portion between the side surface portion 11b and the bottom surface portion 11c.
  • 11c are connected to the ridge 11f, and the connection between the flat portions 11c and 11d, which is the boundary between the bottom 11c and the side 11d, is connected to the ridge 11g, and the boundary between the side 11d and the top 11a.
  • the hollow member 10 is formed of a metal plate.
  • the type of the metal plate is not particularly limited, but is preferably formed of, for example, a metal plate such as a steel plate.
  • the plate thickness of the hollow member 10 is preferably 6.0 mm or less in a frame structure often used in large vehicles such as buses, and in a monocoque structure vehicle often used in vehicles of a normal size. It is preferable that it is 2 mm or less. If necessary, the lower limit of the plate thickness may be 0.8 mm, 1.0 mm, or 1.2 mm. Further, the tensile strength of the metal plate constituting the hollow member 10 (hereinafter, referred to as “the tensile strength of the hollow member 10”) is not particularly limited.
  • the tensile strength of the hollow member 10 is preferably 590 MPa or more. Further, the tensile strength of the hollow member 10 is more preferably 980 MPa or more. If necessary, the upper limit of the tensile strength of the hollow member 10 may be set to 2000 MPa or 1500 MPa.
  • the reinforcing member 20 is a plate-shaped FRP member. Flanges 21a to 21d are formed on each linear portion of the rectangular plate surface 20a.
  • the shape of the plate surface 20 a is similar to the shape of a cross section perpendicular to the member longitudinal direction X of the hollow member 10, and the plate surface 20 a is in the member longitudinal direction X of the hollow member 10. It is provided inside the hollow member 10 in a vertical direction.
  • the flange 21a of the reinforcing member 20 is on the inner surface of the top surface 11a of the hollow member 10, the flange 21b is on the inner surface of the side surface 11b of the hollow member 10, the flange 21c is on the inner surface of the bottom surface 11c of the hollow member 10, and the flange 21d is hollow. It is joined to the inner surface of the side surface portion 11d of the member 10, respectively. Thereby, the reinforcing member 20 is fixed to the hollow member 10.
  • the reinforcing member 20 fixed in this manner functions as a so-called bulkhead that covers the inner space of the hollow member 10 in a cross section perpendicular to the member longitudinal direction X. Note that the shape of the reinforcing member 20 is appropriately changed according to the shape of the hollow member 10, the method of joining the hollow member 10, and the like so that the reinforcing member 20 functions as a bulkhead.
  • the reinforcing member 20 is joined to the inner surface of the hollow member 10 via the flanges 21a to 21d formed on each linear portion (each side) of the rectangular plate surface 20a is illustrated and described.
  • the joining method and its mode are not limited to these.
  • the plate surface 20a may be directly joined to the inner surface of the hollow member 10 without forming a flange on each side of the reinforcing member 20 having the rectangular plate surface 20a.
  • the joining range does not necessarily have to be the entire circumference of the reinforcing member 20. For example, it is sufficient that 50% or more of the length of each side of the reinforcing member 20 is joined to the inner surface of the hollow member 10.
  • the FRP member used as the reinforcing member 20 means a fiber reinforced resin member made of a matrix resin and a composite reinforcing fiber material contained in the matrix resin.
  • the reinforcing fiber material for example, carbon fiber and glass fiber can be used.
  • a boron fiber, a silicon carbide fiber, an aramid fiber, or the like can be used as the reinforcing fiber material.
  • the reinforcing fiber substrate serving as the substrate of the reinforcing fiber material include a nonwoven fabric substrate using chopped fibers, a cloth material using continuous fibers, and a unidirectional reinforcing fiber substrate (UD). Material) etc. can be used.
  • These reinforcing fiber bases can be appropriately selected according to the necessity of the orientation of the reinforcing fiber material.
  • the CFRP member is an FRP member using carbon fiber as a reinforcing fiber material.
  • carbon fibers for example, PAN-based or pitch-based carbon fibers can be used. By using carbon fibers, strength against weight and the like can be efficiently improved.
  • the GFRP member is an FRP member using glass fiber as a reinforcing fiber material. Although it is inferior in mechanical properties to carbon fiber, it can suppress the electrolytic corrosion of the metal member.
  • thermosetting resin examples include an epoxy resin, an unsaturated polyester resin, and a vinyl ester resin.
  • thermoplastic resin examples include polyolefins (polyethylene, polypropylene, and the like) and their acid-modified products, polyamide resins such as nylon 6 and nylon 66, thermoplastic aromatic polyesters such as polyethylene terephthalate and polybutylene terephthalate, polycarbonate, and polyether sulfone.
  • styrene resins such as polyphenylene ether and modified products thereof, polyarylate, polyether ketone, polyether ether ketone, polyether ketone ketone, vinyl chloride and polystyrene, and phenoxy resins.
  • the matrix resin may be formed of a plurality of types of resin materials.
  • thermoplastic resin As the matrix resin from the viewpoint of workability and productivity. Furthermore, by using a phenoxy resin as the matrix resin, the density of the reinforcing fiber material can be increased. Further, the phenoxy resin has a heat structure similar to that of the epoxy resin because the molecular structure is very similar to that of the epoxy resin which is a thermosetting resin. Further, by further adding a curing component, application to a high-temperature environment becomes possible. When the hardening component is added, the addition amount may be appropriately determined in consideration of the impregnating property of the reinforcing fiber material, the brittleness of the FRP member, the tact time, the workability and the like.
  • Adhesive resin layer When the reinforcing member 20 is formed of an FRP member or the like, an adhesive resin layer is provided between the FRP member and the metal member (the hollow member 10 in the above embodiment), and the FRP member and the metal member are separated by the adhesive resin layer. They may be joined.
  • the type of the adhesive resin composition forming the adhesive resin layer is not particularly limited.
  • the adhesive resin composition may be either a thermosetting resin or a thermoplastic resin.
  • the types of the thermosetting resin and the thermoplastic resin are not particularly limited.
  • the thermoplastic resin polyolefins and acid-modified products thereof, polystyrene, polymethyl methacrylate, AS resin, ABS resin, thermoplastic aromatic polyesters such as polyethylene terephthalate and polybutylene terephthalate, polycarbonate, polyimide, polyamide, polyamide
  • the thermosetting resin for example, one or more selected from an epoxy resin, a vinyl ester resin, a phenol resin, and a
  • the adhesive resin composition can be appropriately selected according to the characteristics of the matrix resin constituting the FRP member, the characteristics of the reinforcing member 20, or the characteristics of the metal member. For example, by using a resin having a polar functional group or a resin subjected to acid modification or the like as the adhesive resin layer, the adhesiveness is improved.
  • the adhesion between the FRP member and the metal member can be improved.
  • the deformation followability of the FRP member when a load is input to the metal member can be improved. In this case, the effect of the FRP member on the deformed metal member can be more reliably exerted.
  • the form of the adhesive resin composition used to form the adhesive resin layer may be, for example, a liquid such as powder or varnish, or a solid such as a film.
  • a crosslinkable curable resin and a crosslinking agent may be blended with the adhesive resin composition to form a crosslinkable adhesive resin composition.
  • the heat resistance of the adhesive resin composition is improved, so that application in a high-temperature environment becomes possible.
  • the crosslinkable curable resin for example, a bifunctional or more functional epoxy resin or a crystalline epoxy resin can be used.
  • an amine, an acid anhydride, or the like can be used as a crosslinking agent.
  • various additives such as various rubbers, inorganic fillers and solvents may be blended in the adhesive resin composition as long as the adhesiveness and physical properties are not impaired.
  • the FRP member with the metal member is realized by various methods. For example, it is obtained by bonding an FRP to be an FRP member or an FRP molding prepreg that is a precursor thereof to a metal member with the above-described adhesive resin composition, and solidifying (or curing) the adhesive resin composition. . In this case, for example, by performing thermocompression bonding, the FRP member and the metal member can be combined.
  • the bonding of the FRP or the FRP forming prepreg to the metal member described above can be performed before, during or after forming the part.
  • FRP or a prepreg for FRP molding may be bonded to the metal member.
  • the composite material may be obtained by molding the workpiece to which the FRP member is bonded.
  • the matrix resin of the FRP member is a thermoplastic resin, it is possible to perform molding such as bending on the portion where the FRP member is bonded.
  • a composite batch molding in which the thermocompression bonding step and the molding step are integrated may be performed.
  • the joining method between the FRP member and the metal member is not limited to the above-described adhesion using the adhesive resin layer.
  • the FRP member and the metal member may be mechanically joined. More specifically, holes for fastening are formed at positions corresponding to the FRP member and the metal member, respectively, and these are fastened through the holes by fastening means such as bolts and rivets, so that the FRP member and the metal member are fastened.
  • the member may be joined.
  • the FRP member and the metal member may be joined by known joining means.
  • the FRP member and the metal member may be jointly joined by a plurality of joining means.
  • the bonding by the adhesive resin layer and the fastening by the fastening means may be used in combination.
  • the metal member according to the present invention may be plated. Thereby, corrosion resistance is improved.
  • the metal member is a steel material, it is more preferable.
  • the type of plating is not particularly limited, and known plating can be used.
  • a coated steel sheet steel material
  • the metal member may have a surface coated with a film called a chemical conversion treatment.
  • a chemical conversion treatment a generally known chemical conversion treatment can be used.
  • a zinc phosphate treatment, a chromate treatment, a chromate-free treatment, or the like can be used.
  • the above-mentioned film may be a known resin film.
  • the metal member may be a member to which a generally known coating is applied.
  • a generally known coating is applied.
  • a known resin can be used.
  • an epoxy resin, a urethane resin, an acrylic resin, a polyester resin, a fluororesin, or the like as a main resin can be used.
  • generally known pigments may be added to the coating, if necessary.
  • the coating may be a clear coating to which no pigment is added. Such coating may be applied to the metal member in advance before compounding the FRP member, or may be applied to the metal member after compounding the FRP member. Further, the metal member may be coated in advance, the FRP member may be composited, and then the coating may be performed.
  • the paint used for painting may be a solvent-based paint, a water-based paint, a powder paint, or the like.
  • a method for applying the coating a generally known method can be applied.
  • electrodeposition coating, spray coating, electrostatic coating, immersion coating, or the like can be used as a coating application method.
  • Electrodeposition coating is suitable for covering the end surfaces and gaps of metal members, and therefore has excellent corrosion resistance after coating.
  • a generally known chemical treatment such as zinc phosphate treatment or zirconia treatment to the surface of the metal member before coating, the adhesion of the coating film is improved.
  • each reinforcing member 20 in the present embodiment has an interval P from the front end 10 a to the rear end 10 b of the hollow member 10 so as to separate the inner space of the hollow member 10. It is arranged in.
  • the minimum width and the maximum width in the outer dimensions of the hollow member 10 in a cross section perpendicular to the member longitudinal direction X of the hollow member 10 are used as a reference.
  • the outer dimension on the short side of the substantially rectangular cross section shown in FIG. 6 is the minimum width W min
  • the outer dimension width on the long side of the substantially rectangular cross section is the maximum width W max .
  • a pair of opposed short sides and a pair of opposed long sides are configured to be equal to each other.
  • the minimum width W min on the external dimensions is configured to be 30% or more of the maximum width W max on the external dimensions.
  • the ratio of the minimum width W min and a maximum width W max of the outer shape dimension of the external dimensions relates, if the minimum width W min is not more than 30% of the length of the maximum width W max, hollow
  • the member 10 may not be stably deformed by axial crushing, and is not effective as a shock absorbing member. If necessary, the minimum width W min may be 35% or 40% or more of the maximum width W max . From the definition, the minimum width W min does not become larger than the maximum width W max .
  • the interval P between the reinforcing members 20 arranged inside the hollow member 10 is 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member 10.
  • each reinforcing member 20 extends along the member longitudinal direction X of the hollow member 10 at an interval P of 0.74 times to 1.84 times the minimum width W min on the external dimensions of the hollow member 10. Is arranged.
  • the minimum width W min is defined based on the cross-sectional shape of the hollow member 10 at a position where the area of the cross section perpendicular to the member longitudinal direction X is the smallest. .
  • the first reinforcement member 20 closest to the front end 10a is located at the position where the first reinforcement member 20 is arranged because the reinforcement effect is large at the position where the reinforcement member 20 is disposed.
  • the hollow member 10 is deformed in a portion forward of the hollow member 10. Thereafter, the deformation of the hollow member 10 proceeds toward the rear end 10b, and the deformation of the hollow member 10 where the first reinforcing member 20 is disposed is started. Since the FRP has low ductility, the first reinforcing member 20 breaks at this stage. That is, the reinforcing effect is lost at the place where the first reinforcing member 20 is arranged, and the hollow member 10 at the place is easily deformed.
  • the reinforcing members 20 are not broken, and thus the reinforcing effect is maintained without being lost. That is, at the place where the second and subsequent reinforcing members 20 are arranged, the hollow member 10 is in a state where it is difficult to deform. For this reason, until the deformation of the hollow member 10 at the location where the first reinforcing member 20 that has been broken is advanced sufficiently, the deformation amount of the hollow member 10 at the location where the second and subsequent reinforcing members 20 are located is It is getting smaller.
  • the deformation of the hollow member 10 where the second reinforcing member 20 is disposed starts.
  • the FRP has low ductility
  • the second reinforcing member 20 breaks at this stage. Thereby, the reinforcing effect is lost at the place where the second reinforcing member 20 is arranged, and the hollow member 10 at the place is easily deformed.
  • the interval P between the reinforcing members 20 does not satisfy 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member 10, stable axial crush deformation occurs in the hollow member 10. There is no fear. If the interval P is shorter than 0.74 times the minimum width W min of the external dimensions of the hollow member 10, the stiffness becomes too high, and there is a possibility that buckling does not occur between the reinforcing members 20. If the interval P is more than 1.84 times the minimum width W min of the external dimensions of the hollow member 10, the space between the reinforcing members 20 is too long, so that lateral bending deformation occurs at one location and does not result in axial crush deformation. There is fear.
  • the lower limit of the interval P between the reinforcing members 20 may be set to 0.80 times, 0.85 times, or 0.90 times the minimum width W min of the external dimensions of the hollow member 10.
  • the upper limit of the interval P between the reinforcing members 20 may be set to 1.60 times, 1.50 times, or 1.40 times the minimum width W min of the external dimensions of the hollow member 10.
  • the tensile strength of the FRP member constituting the reinforcing member 20 is preferably 100 MPa or more. If necessary, the upper limit of the tensile strength may be 2500 MPa or 2000 MPa. Further, as shown in the embodiments described later, the plate thickness of the reinforcing member 20 is preferably 0.7 to 3.0 mm. The lower limit of the plate thickness of the reinforcing member 20 may be 0.8 mm, 0.9, or 1.0 mm. The upper limit of the plate thickness may be 2.9 mm, 2.8 mm, 2.4 mm, or 2.0 mm.
  • the ductility of a metal plate such as a steel plate is generally good. For this reason, when the reinforcing member 20 is a metal plate, the reinforcing member 20 as described above does not break, so that high energy absorption performance cannot be stably obtained. For this reason, the reinforcing member 20 needs to be an FRP member.
  • each reinforcing member 20 may not be arranged over the entire region in the member longitudinal direction X.
  • the reinforcing member 20 has an end on the load input side (the front end 10 a in the present embodiment) among the front part and the rear part having the center position in the member longitudinal direction X of the hollow member 10 as a boundary. Located only on the front. Even in this case, in the area where the reinforcing member 20 is arranged, axial crush deformation can be stably generated when a load is input.
  • the reinforcing member 20 is preferably arranged within a range of 15%, 20%, or 30% from the end (front end 10a) on the load input side. More preferably, the number of the reinforcing members 20 is 4 or more, 5 or more, or 6 or more.
  • the interval P between the reinforcing members 20 is constant along the member longitudinal direction X of the hollow member 10, but the interval P is the minimum width W min in the outer dimensions of the hollow member 10. As long as it is within the range of 0.74 times to 1.84 times, the interval P may not be constant along the member longitudinal direction X as shown in FIG. In the example shown in FIG. 10, the interval between the reinforcing members 20 arranged at the front portion in the member longitudinal direction X of the hollow member 10 and the interval between the reinforcing members 20 arranged at the rear portion are different.
  • the shape of the hollow member 10 is appropriately changed depending on the use of the structural member for a vehicle.
  • the portion that is easily bent and deformed according to the shape of the hollow member 10 and the other portions are reinforced.
  • a portion where bending deformation is likely to occur may be mainly reinforced.
  • a portion where such bending deformation is likely to occur is referred to as a “bending inducing portion”.
  • the interval P between the reinforcing members 20 arranged in the bending inducing section is narrower than the interval P between the reinforcing members 20 arranged in portions other than the bending inducing section.
  • the reinforcing effect in the bending inducing portion is enhanced, and axial crush deformation can be more stably generated.
  • the plate thickness of the reinforcing member 20 arranged in the bending inducing portion is larger than the plate thickness of the reinforcing member 20 arranged in a portion other than the bending inducing portion.
  • the tensile strength of the reinforcing member 20 arranged in the bending inducing section is higher than the tensile strength of the reinforcing member 20 arranged in a portion other than the bending inducing section.
  • the methods for setting the interval P, the plate thickness, the tensile strength, and the like in the bending inducing section as described above may be appropriately combined.
  • Example of bending inducer> an example of the bending inducing section provided in the hollow member 10 will be described.
  • a hole, a concave portion, a convex portion, a plate thickness change portion, a different strength portion, and the like provided in the hollow member 10 realize a function as a bending inducing portion.
  • the portion provided with any one of the hole, the concave portion, the convex portion, and the plate thickness changing portion is a portion where the cross-sectional coefficient of the hollow member 10 changes in the member longitudinal direction X of the hollow member 10.
  • the bending stress generated in the hollow member 10 by the same bending moment changes, so that bending of the hollow member 10 is induced in the portion. More specifically, in a portion of the hollow member 10 having a relatively small section modulus in the longitudinal direction X of the member, the bending stress in the portion is relatively large, so that the portion is bent. Further, for a portion of the hollow member 10 having a relatively large section modulus in the member longitudinal direction X, the section modulus of a portion including the region before and after the hollow member 10 in the member longitudinal direction X is relatively small. . Therefore, bending occurs at the boundary between the region and the portion where the section modulus is relatively large.
  • the different strength portion is a portion where the yield strength of the hollow member 10 changes in the member longitudinal direction X of the hollow member 10.
  • plastic deformation of the hollow member 10 in the portion is induced.
  • plastic deformation in the portion occurs first in the hollow member 10, so that bending occurs in the portion.
  • the yield strength of the portion including the region before and after the hollow member 10 in the member longitudinal direction X is relatively small. . Therefore, bending occurs at the boundary between the region and the portion where the yield strength is relatively large.
  • the hollow member 10 does not include a hole, a concave portion, a convex portion, a plate thickness change portion, a different strength portion, and the like that realize the function as the bending inducing portion described above, the load applied to the hollow member 10
  • the direction of the input can be specified to some extent, there is a region where the bending moment is maximum in the hollow member under the influence of the constraint of the peripheral member joined to the hollow member 10, and bending occurs in the region. Therefore, when the bending moment generated in the hollow member 10 can be specified, the region where the bending moment is maximum also has a function as the bending inducing portion.
  • FIG. 11 is a cross-sectional view of the hollow member 10A for explaining an example of a hole provided in the hollow member 10A according to the present embodiment.
  • a hole 50 is provided in the side surface 11b.
  • the section modulus of the hollow member 10A in the portion where the hole 50 is provided is lower than the section modulus of the hollow member 10A in the portion before and after the portion where the hole 50 is provided. Therefore, when the collision load F shown in FIG. 11 is input to the hollow member 10A, the hollow member 10A bends at the portion where the hole 50 is provided so that the hole 50 is bent inside. That is, in the member longitudinal direction X of the hollow member 10A, a portion of the hollow member 10A where the hole 50 is provided becomes a bending inducing portion provided in the hollow member 10A.
  • 12 to 15 are schematic diagrams showing other examples of the hole provided in the hollow member 10A according to the present embodiment.
  • a circular hole 50a may be provided in the side surface 11b.
  • a plurality of holes 50b may be provided in the side surface 11b.
  • a plurality of holes 50b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10A. In this case, when the collision load is input, the hollow member 10A is easily bent and deformed toward the side surface 11b with the hole 50b as a starting point of bending.
  • a hole 50c extending in a direction transverse to the member longitudinal direction X of the hollow member 10A may be provided in the side surface 11b.
  • the hollow member 10A bends and deforms toward the side surface 11b with the hole 50c as a starting point of bending.
  • the shape of the hole 50c is not limited to the rounded rectangle shown in FIG. 14, and may be any shape.
  • the direction transverse to the member longitudinal direction X of the hollow member 10A described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10A as shown in FIGS.
  • the portion where the hole 50 is provided is not limited to the side surface 11b.
  • the hole 50 may be provided in the top surface 11a, the bottom surface 11c, or the side surface 11d.
  • a hole 50d may be provided in the ridge 11e.
  • the section modulus of the portion provided with the hole 50d in the member longitudinal direction X in the hollow member 10A is significantly reduced, the portion provided with the hole 50d is easily bent as a starting point of bending.
  • FIG. 16 is a cross-sectional view of the hollow member 10B for explaining an example of a bead portion provided in the hollow member according to the present embodiment.
  • the bead portion 51 is an example of a concave portion in the present embodiment.
  • a bead part 51 is provided on the side surface part 11b.
  • the section modulus of the hollow member 10B at the portion where the bead portion 51 is provided is lower than the section modulus of the hollow member 10B at the portion before and after the portion where the bead portion 51 is provided. Therefore, when the collision load F shown in FIG.
  • the hollow member 10B bends at the portion where the bead portion 51 is provided, such that the bead portion 51 is bent inside. That is, in the member longitudinal direction X of the hollow member 10B, a portion of the hollow member 10B where the bead portion 51 is provided serves as a bending inducing portion provided in the hollow member 10B.
  • the concave portion here means a concave portion such as an emboss or a bead provided in the side surface portion 11b of the hollow member 10B. As shown in FIG. 17, a circular concave portion 51a may be provided on the side surface portion 11b.
  • a plurality of recesses 51b may be provided on the side surface 11b.
  • a plurality of concave portions 51b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10B. In this case, when the collision load is input, the hollow member 10B is easily bent and deformed toward the side surface portion 11b with the plurality of concave portions 51b serving as a starting point of bending.
  • a bead portion 51c extending in a direction crossing the member longitudinal direction X of the hollow member 10B may be provided on the side surface portion 11b.
  • the hollow member 10B is bent and deformed toward the side surface 11b with the bead portion 51c as a starting point of bending.
  • the shape of the bead portion 51c is not limited to the rounded rectangle shown in FIG. 19, and may be any shape.
  • the direction crossing the member longitudinal direction X of the hollow member 10B described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10B as shown in FIG.
  • the portion where the concave portion 51 is provided is not limited to the side surface portion 11b.
  • the concave portion 51 may be provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d.
  • a concave portion 51d may be provided in the ridge line portion 11e.
  • the section modulus of the hollow member 10B in the member longitudinal direction X where the concave portion 51d is provided significantly changes, so that the portion provided with the concave portion 51d easily bends and deforms as a starting point of bending.
  • FIG. 21 is a schematic view showing another example of the recess provided in the hollow member 10B according to the present embodiment.
  • concave portions 51e and 51f extending in the member longitudinal direction X of the hollow member 10B may be provided side by side along the member longitudinal direction X of the hollow member 10B.
  • bending occurs in a portion 510 of the hollow member 10B between the concave portion 51e and the concave portion 51f in the member longitudinal direction X. That is, since the section of the hollow member 10B where the concave portions 51e and 51f are provided and the portion 510 between the concave portion 51e and the concave portion 51f have different sectional coefficients, the portion 510 is bent when the collision load is input.
  • the portion 510 may be formed with a concave portion, a convex portion described later, a thin portion, a different strength portion, or the like.
  • the concave portion 51e and the concave portion 51f do not necessarily have to be arranged in series as shown in FIG. Further, the concave portion 51e and the concave portion 51f do not necessarily need to extend in the member longitudinal direction X of the hollow member 10B.
  • FIG. 22 is a cross-sectional view of the hollow member 10C for explaining an example of a protrusion provided on the hollow member 10C according to the present embodiment.
  • a protrusion 52 is provided on the side surface 11b.
  • the section modulus of the hollow member 10C at the portion where the protrusion 52 is provided is higher than the section modulus of the hollow member 10C at the portion before and after the portion where the protrusion 52 is provided. Therefore, when the collision load F shown in FIG. 22 is input to the hollow member 10C, a portion of the region 6a or the region 6b before and after the convex portion 52 in the member longitudinal direction X of the hollow member 10C has a lowest section modulus.
  • the area 6a and the area 6b are areas where a change in the section modulus of the hollow member 10C in the Y direction occurs. That is, in the member longitudinal direction X of the hollow member 10C, a portion of the hollow member 10C including the convex portion 52 and the regions 6a and 6b before and after the convex portion 52 serves as a bending inducing portion provided in the hollow member 10C.
  • the protrusion 52 is provided on the side surface 11 b, but the protrusion 52 may be provided on, for example, the top surface 11 a, the bottom surface 11 c, or the side surface 11 d. More specifically, when the convex portion 52 is provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d on the same cross section in a part of the hollow member 10C in the member longitudinal direction X, the hollow member 10C Since the section modulus in the member longitudinal direction X changes at the portion where the convex portion 52 is provided, bending of the hollow member 10C may occur at the portion where the convex portion 52 is provided. Therefore, also in this case, the convex portion 52 becomes a bending inducing portion.
  • FIGS. 23 to 26 are schematic views showing other examples of the convex portion provided on the hollow member 10C according to the present embodiment.
  • the convex portion here is realized, for example, by processing the hollow member 10C. That is, such a convex portion may be provided by deforming a part of the steel plate constituting the hollow member 10C. As shown in FIG. 23, a circular convex portion 52a may be provided on the side surface portion 11b.
  • a plurality of protrusions 52b may be provided on the side surface 11b.
  • a plurality of convex portions 52b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10C.
  • any one of the regions before and after the plurality of protrusions 52b in the member longitudinal direction X of the hollow member 10C serves as a starting point of bending, and the hollow member 10C is easily bent and deformed toward the side surface 11b.
  • a protrusion 52c extending in a direction crossing the member longitudinal direction X of the hollow member 10C may be provided on the side surface 11b.
  • the hollow member 10C is bent and deformed toward the side surface portion 11b with any one of the regions before and after the convex portion 52c in the member longitudinal direction X of the hollow member 10C as a starting point of bending.
  • the shape of the projection 52c is not limited to the rounded rectangle shown in FIG. 25, and may be any shape.
  • the direction transverse to the member longitudinal direction X of the hollow member 10C described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10C as shown in FIG.
  • the portion where the convex portion 52 is provided is not limited to the side surface portion 11b.
  • the projection 52 may be provided on the top surface 11a, the bottom surface 11c, or the side surface 11d.
  • the projection 52d may be provided on the ridge 11e.
  • the section modulus of the portion of the hollow member 10C where the convex portion 52d is provided in the member longitudinal direction X changes remarkably, so that the portion where the convex portion 52d is provided easily bends as a starting point of bending.
  • FIG. 27 is a schematic view showing another example of the projection provided on the hollow member 10C according to the present embodiment.
  • the convex portions 52e and 52f extending in the member longitudinal direction X of the hollow member 10C may be provided side by side along the member longitudinal direction X of the hollow member 10C.
  • bending occurs in a portion 520 of the hollow member 10C between the convex portion 52e and the convex portion 52f in the member longitudinal direction X. That is, in the hollow member 10C, the section provided with the projections 52e and 52f and the section 520 between the projection 52e and the projection 52f have different cross-sectional coefficients. Bending deformation occurs with 520 as the starting point of bending.
  • the above-described concave portion, convex portion, or a thin portion or a different strength portion described later may be formed.
  • the convex part 52e and the convex part 52f do not necessarily need to be lined up in series, as shown in FIG.
  • the protrusion 52e and the protrusion 52f do not necessarily need to extend in the member longitudinal direction X of the hollow member 10C.
  • FIG. 28 is a schematic diagram illustrating an example of a plate thickness changing portion provided in the hollow member 10D according to the present embodiment.
  • the plate thickness change portion means a portion where the plate thickness changes in the member longitudinal direction X of the hollow member 10D.
  • the hollow member 10D includes a first thick part 111 and a second thick part 112.
  • the first thick part 111 is provided on the end side of the hollow member 10D, and the second thick part 112 is provided continuously with the first thick part 111 along the member longitudinal direction X of the hollow member 10D.
  • the thickness of the steel plate differs between the first plate thickness portion 111 and the second plate thickness portion 112.
  • the relationship between the plate thicknesses is not particularly limited.
  • the boundary between the first plate thickness portion 111 and the second plate thickness portion 112 becomes the plate thickness change portion 113.
  • the section modulus of the hollow member 10D in the member longitudinal direction X changes in the plate thickness changing portion 113. That is, the thickness change portion 113 corresponds to a bending inducing portion. Therefore, when a collision load is input to the hollow member 10D, the hollow member 10D bends at the plate thickness change portion 113.
  • FIG. 29 is a schematic diagram illustrating an example of a thin portion provided in the hollow member 10D according to the present embodiment.
  • a thin portion 114 having a relatively smaller thickness than other portions is provided on the side surface portion 11b in the longitudinal direction X of the hollow member 10D.
  • the section modulus of the hollow member 10D in the portion including the thin portion 114 is lower than the section modulus of the hollow member 10D in the portion before and after the portion in which the thin portion 114 is provided. That is, the portion of the hollow member 10D where the thin portion 114 is provided corresponds to the bending inducing portion. Therefore, when a collision load is input to the hollow member 10D, the hollow member 10D bends at the portion where the thin portion 114 is provided so that the thin portion 114 is bent inside.
  • the hollow member 10D having such a plate thickness change portion may be formed by, for example, a work plate made of cutting, pressing, and tailored blank.
  • a work plate may be a tailor weld blank (TWB) having a weld line.
  • the plate to be processed may be a tailor rolled blank (TRB) provided in a manner that the plate thickness is varied by a rolling roll.
  • TWB the difference thickness at the plate thickness change portion can be 0.2 mm or more.
  • the thickness change amount in the thickness change portion per the longitudinal direction of the member can be 0.1 mm / 100 mm or more.
  • FIG. 30 is a cross-sectional view of the hollow member 10E for explaining an example of the different strength portion provided in the hollow member 10E according to the present embodiment.
  • a different strength portion 53 is provided on the side surface portion 11b.
  • the different strength portion 53 is provided, for example, by partially performing heat treatment such as welding, quenching, or tempering on the hollow member 10E.
  • the yield strength of the hollow member 10E at the portion where the different strength portion 53 is provided is different from the yield strength of the hollow member 10E at the portion before and after the portion where the different strength portion 53 is provided. Therefore, when the collision load F shown in FIG.
  • the different-strength portion 53 is bent so as to be inside the different-strength portion 53 or in the vicinity of the different-strength portion 53. That is, in the member longitudinal direction X of the hollow member 10E, a portion including the different strength portion 53 of the hollow member 10E becomes a bending inducing portion provided in the hollow member 10E. This bending is a bending caused by plastic deformation of the different strength portion 53 or a region near the different strength portion 53.
  • the different strength portion 53 is provided on the side surface portion 11b, but the different strength portion 53 may be provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d, for example. . More specifically, when the different strength portion 53 is provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d on the same cross section in a part of the hollow member 10 in the member longitudinal direction X, In this case, the strength of the side surface portion 11b is lowest. Then, bending of the hollow member 10 ⁇ / b> E with the side surface portion 11 b bent inside may occur in the different strength portion 53. Therefore, also in this case, the different strength portion 53 becomes a bending inducing portion.
  • FIG. 31 and FIG. 32 are schematic diagrams illustrating another example of the different strength portion provided in the hollow member 10E according to the present embodiment.
  • the different strength portion here is realized by welding, heat treatment, or the like to the work plate forming the hollow member 10E.
  • different strength portions 120 are provided along the circumferential direction of the cross section with respect to the member longitudinal direction X of the hollow member 10E. Also in this case, the portion of the hollow member 10E where the different strength portion 120 is provided corresponds to the bending inducing portion. Therefore, when a collision load is input to the hollow member 10E, the hollow member 10E bends at the portion where the different strength portion 120 is provided so that the different strength portion 120 is bent inside.
  • the different strength portion may be partially provided on at least one of the wall portions constituting the cross section of the hollow member 10E, such as the side surface portion 11b. Even in such a case, when a collision load is input to the hollow member 10E, the hollow member 10E bends at a portion where the different strength portion 121 is provided so that the different strength portion 121 is bent inside.
  • FIG. 33 is a schematic diagram illustrating an example of a strength changing portion provided in the hollow member 10E according to the present embodiment.
  • the hollow member 10E includes a first strength part 122 and a second strength part 123.
  • the first strength portion 122 is provided on the end side of the hollow member 10E, and the second strength portion 123 is provided continuously with the first strength portion 122 along the member longitudinal direction X of the hollow member 10E.
  • the yield strength of the steel sheet differs between the first strength part 122 and the second strength part 123.
  • the magnitude relation of the yield strength is not particularly limited.
  • the boundary between the first strength part 122 and the second strength part 123 becomes the strength change part 124.
  • the strength changing portion 124 the yield strength of the hollow member 10E in the member longitudinal direction X changes. That is, the strength changing section 124 corresponds to a bending inducing section. Therefore, when a collision load is input to the hollow member 10E, the hollow member 10E bends at the strength changing portion 124.
  • a bending inducing portion may be realized by a combination of at least two or more of the above-described concave portion, convex portion, hole portion, plate thickness changing portion, thin portion, different strength portion, and strength changing portion.
  • the hollow member of the present embodiment can be applied to, for example, a front side member, a rear side member, an extension, a crash box, or the like, which is a vehicle structural member required to have an impact absorbing function.
  • the analysis model is composed of a bumper beam and a frame as shown in FIGS. 1 to 3, the cross section of the hollow member is rectangular, and the outer dimensions are 76 mm in width and 200 mm in height.
  • a plurality of analysis models are created under the conditions shown in Table 1 below.
  • the weight reduction rate in Table 1 is obtained by standardizing the weight of each structure by the weight of the structure 1.
  • Structures 1 and 2 in Table 1 above are structures in which the reinforcing member 20 is not provided, and structure 2 is a structure in which the thickness and thickness of the structure 1 are reduced.
  • Structures 3 to 10 are structures in which a plurality of reinforcing members 20 as shown in FIG. 4 are arranged along the member longitudinal direction X of the hollow member 10, the material of the reinforcing member 20 is CFRP, and its plate thickness is Is 0.8 mm. In the structure 3, the interval between the adjacent reinforcing members 20 is random, and the interval between the reinforcing members 20 is different from each other.
  • the reinforcing members 20 are arranged in the entire region of the hollow member 10 in the member longitudinal direction X, and the intervals between the reinforcing members 20 are constant.
  • the reinforcing members 20 are arranged only at the front part of the hollow member 10 in the member longitudinal direction X, and the intervals between the reinforcing members 20 are constant.
  • the reinforcing members 20 are arranged in the entire region in the member longitudinal direction X of the hollow member 10, but the spacing between the reinforcing members 20 arranged in front of the hollow member 10 and the hollow member The spacing between the reinforcing members 20 arranged at the rear of the 10 is different.
  • the structure 11 uses a steel plate as a material of the reinforcing member 20.
  • the structure 12 is a structure in which the thickness of the reinforcing member 20 is changed to 2.8 mm.
  • the structure 13 is a structure in which the thickness of the reinforcing member 20 is changed to 0.6 mm.
  • the structure 14 is a structure in which the thickness of the reinforcing member 20 is changed to 3.2 mm.
  • the structure 15 uses GFRP as a material of the reinforcing member 20.
  • the reinforcing members 20 are arranged only at the front part of the hollow member 10 in the member longitudinal direction X, and the number thereof is two.
  • CFRP used as the reinforcing member 20 in the structures 3 to 10, 12 to 14, and 16 are as follows.
  • Vf fiber content volume ratio
  • Young's modulus 102 GPa Breaking strength: 1500 MPa
  • Elongation at break 1.5%
  • the mechanical properties of the steel sheet used as the reinforcing member 20 in the structure 11 are as follows. Tensile strength: 440MPa Elongation at break: 28% The mechanical properties of the GFRP used as the reinforcing member 20 in the structure 15 are as follows. Vf (fiber content volume ratio): 50% Young's modulus: 13 GPa Breaking strength: 200MPa Elongation at break: 3.0%
  • This simulation simulates a frontal collision test of an automobile, and was performed by colliding a rigid wall having a mass of 200 kg with the bumper beam 40 shown in FIGS. 1 to 3 at 12 m / s.
  • the rear end 10b of the hollow member 10 in each analysis model is restricted.
  • Table 1 shows the deformation mode of each analysis model as a simulation result.
  • the “lateral bending” in the deformation mode shown in Table 1 is a deformation mode in which a horizontal bending deformation occurs from the initial deformation of the hollow member 10.
  • the “unstable axial crush” in the deformation mode shown in Table 1 means that the crushing deformation of the hollow member 10 is irregularly present in the member longitudinal direction X, and the crushing deformation occurs from the front end 10a of the hollow member 10. This is a deformation mode that is not continuous toward the rear end 10b.
  • “Stable axial crushing” in the deformation mode shown in Table 1 means that the crushing deformation of the hollow member 10 gradually progresses along the member longitudinal direction X, and the crushing deformation occurs continuously from the front end 10a to the rear end 10b. Mode.
  • FIG. 34 is a plan view showing a state in which the analysis model of the structure 1 is being deformed in the collision simulation
  • FIG. 35 is a plan view showing a state after the deformation of the analysis model of the structure 1 in the collision simulation.
  • FIG. 36 is a plan view showing a state in which the analysis model of the structure 4 is being deformed in the collision simulation
  • FIG. 37 is a plan view showing a state after deformation of the analysis model of the structure 4 in the collision simulation.
  • FIG. 38 is a plan view showing a state in which the analysis model of the structure 7 is being deformed in the collision simulation
  • FIG. 39 is a plan view showing a state after deformation of the analysis model of the structure 7 in the collision simulation.
  • the crush deformation is stably generated in the deformation process of the hollow member.
  • the deformation mode of the hollow member is lateral bending deformation
  • the plastic strain generated in the portion other than the horizontal bent portion of the hollow member is small, so the portion other than the horizontal bent portion hardly contributes to the improvement of the energy absorption performance.
  • the portion where plastic strain occurs increases, and the energy absorption performance can be improved.
  • Such deformation of the hollow member has also occurred in Structure 6, Structures 8 to 10, Structure 12, and Structure 15.
  • the energy absorption performance is improved as compared with the structure 1.
  • the weight reduction ratio with respect to the structure 1 is large. Therefore, according to the result of this simulation, when the interval between the reinforcing members is within the range of 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member, the weight is reduced. At the same time, it is possible to stably generate axial crush deformation and improve the energy absorption performance.
  • the deformation mode is stable axial crushing, whereas when the plate thickness of the reinforcing member is 0.6 mm. In some cases (Structure 13) or 3.2 mm (Structure 14), the deformation mode is unstable axial crush. That is, in the configuration according to the present invention, it can be said that the plate thickness of the CFRP member as the reinforcing member is preferably 0.8 mm to 2.8 mm.
  • GFRP is used as a material of the reinforcing member.
  • the deformation mode is stable axial crush, and the energy absorption performance is improved with respect to the structure 1. That is, in the configuration according to the present invention, it can be said that the use of GFRP as the material of the reinforcing member is also effective.
  • the number of reinforcing members arranged in the hollow member is two.
  • the deformation mode is lateral bending, and the energy absorption performance is not improved. That is, in the configuration according to the present invention, it can be said that the number of reinforcing members to be arranged is preferably three or more.
  • the present invention is applicable to structural members for vehicles.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Vibration Dampers (AREA)

Abstract

A vehicle structural member that is lighter weight, causes stable axial crush deformation at vehicle impact, and maintains or improves energy absorption performance. This vehicle structural member comprises a metal hollow member, and a plurality of plate-shaped reinforcement members formed from FRP, having each side thereof joined to the inner surface of the hollow member, and being disposed at intervals in the longitudinal direction of the hollow member so as to partition the inner space of the hollow member. In a cross section of the hollow member perpendicular to the longitudinal direction of the hollow member, the minimum width of the outer dimensions of the hollow member is at least 30% of the maximum width of the outer dimensions of the hollow member. Each reinforcement member is disposed such that the plate surface of the reinforcement member is oriented in a direction perpendicular to the longitudinal direction of the hollow member, and at least three reinforcement members are disposed from a longitudinal end section of the hollow member at intervals of 0.74 to 1.84 times the minimum width. Each reinforcement member has a plate thickness of 0.7 to 3.0 mm.

Description

車両用構造部材Vehicle structural members
(関連出願の相互参照)
 本願は、2018年7月20日に日本国に出願された特願2018-136982号に基づき、優先権を主張し、その内容をここに援用する。
(Cross-reference of related applications)
Priority is claimed on Japanese Patent Application No. 2018-136982, filed on July 20, 2018, the content of which is incorporated herein by reference.
 本発明は、車両用構造部材に関する。 The present invention relates to a vehicle structural member.
 近年、地球環境保護の観点から、自動車の燃費改善が要求されている。その一方で、車両の衝突安全性の維持または向上が要求されている。これらの要求を満足するために、高強度かつ軽量な車体構造の開発が進められている。車両用構造部材であり、車体の骨格を形成するフレームについても、従来の衝突性能を維持しつつ車体構造の軽量化を図るために、フレームを形成する鋼板の高強度化および薄肉化が進められている。 In recent years, from the viewpoint of global environmental protection, improvement of fuel efficiency of automobiles has been required. On the other hand, it is required to maintain or improve the collision safety of the vehicle. In order to satisfy these demands, the development of a high-strength and lightweight vehicle body structure has been promoted. The structural members for vehicles, and the frames that form the skeleton of the vehicle body, have also been strengthened and made thinner in the steel plates that form the frames in order to reduce the weight of the vehicle structure while maintaining the conventional collision performance. ing.
 また、車両の衝突安全性を向上させるためには、“クラッシャブルゾーン”とも呼ばれる車両のフロント部およびリア部のエネルギー吸収性能を向上させることが求められる。例えば、フロント部のクラッシャブルゾーンには、フロントサイドメンバと呼ばれる部品がある。例えば車両の前面衝突時においては、フロントサイドメンバに対し、主に部材長手方向(軸方向)から荷重が入力されることになるが、その際、フロントサイドメンバは、圧縮曲げ変形をする。一般的に圧縮曲げ変形は、曲げ部のみが座屈し、塑性変形するが、その他の部分はあまり塑性変形をしていない。それに対して、座屈が連続的に発生して蛇腹状に変形する軸圧潰変形は、塑性変形している領域が広く、曲げ変形に比べエネルギー吸収効率が高い。しかし、車両のように衝突時の荷重の入力方向が一意に定まらないような条件下において、軸圧潰変形を安定して発生させることは困難である。そのため、車両のフロントサイドメンバ等の部材は、衝突時に圧縮曲げ変形をしながらエネルギー吸収することがより好ましいとされる。 Also, in order to improve the collision safety of the vehicle, it is required to improve the energy absorption performance of the front part and the rear part of the vehicle, also called “crushable zone”. For example, in the crushable zone of the front part, there is a component called a front side member. For example, at the time of a frontal collision of a vehicle, a load is input to the front side member mainly from the longitudinal direction (axial direction) of the member. At that time, the front side member undergoes compression bending deformation. In general, in compression bending deformation, only the bent portion buckles and undergoes plastic deformation, but the other portions do not undergo much plastic deformation. On the other hand, the axial crushing deformation in which buckling occurs continuously and deforms in a bellows-like manner has a wide plastic deformation region, and has higher energy absorption efficiency than bending deformation. However, it is difficult to stably generate the axial crush deformation under the condition that the input direction of the load at the time of the collision is not uniquely determined as in a vehicle. Therefore, it is more preferable that a member such as a front side member of the vehicle absorbs energy while performing compression bending deformation at the time of collision.
 車両衝突時にエネルギー吸収性能を向上させることを目的とする技術として、特許文献1には、中空状フレーム部材前部の内方空間が、部材長手方向において一定間隔で区切られるように複数のリブが配置された技術が開示されている。なお、中空状フレーム部材の後部にはリブは配置されていない。 As a technique aimed at improving energy absorption performance at the time of a vehicle collision, Patent Literature 1 discloses a plurality of ribs such that an inner space of a front portion of a hollow frame member is separated at regular intervals in a member longitudinal direction. A deployed technique is disclosed. Note that no rib is provided at the rear of the hollow frame member.
 また、特許文献2には、自動車の車体フレームやサスペンションフレーム等に用いられ、衝突時に溶接部での開口や破壊を防止するような構成の溶接構造閉断面フレームが開示されている。この技術では、中空部材中に板状の金属製の補強部材を設けている。また、特許文献3には、閉断面構造の中空部材(強度部材)内に補強部材が複数設けられる構成が開示され、補強部材として合成樹脂を用いる技術が開示されている。また、特許文献4には、車両用構造部材において、中空部材の内面に補強部材を貼り付ける技術が開示され、中空部材の引張強度が980MPa以上であるとの開示もある。 Patent Literature 2 discloses a welded structure closed-section frame that is used for an automobile body frame, a suspension frame, or the like and that prevents opening or breakage at a welded portion in a collision. In this technique, a plate-like metal reinforcing member is provided in a hollow member. Patent Literature 3 discloses a configuration in which a plurality of reinforcing members are provided in a hollow member (strength member) having a closed cross-sectional structure, and discloses a technique using a synthetic resin as the reinforcing member. Patent Document 4 discloses a technique of attaching a reinforcing member to the inner surface of a hollow member in a vehicle structural member, and discloses that the tensile strength of the hollow member is 980 MPa or more.
特開2004-182189号公報JP 2004-182189 A 特開2010-76762号公報JP 2010-76762 A 特開平11-342862号公報JP-A-11-342882 特開2017-159896号公報JP-A-2017-159896
 特許文献1においては、荷重入力時に生じる波状の座屈の波のピッチ(座屈モードのピッチ)に関し、中空状フレーム部材の矩形断面の一辺の長さと、他辺の長さの和が一定であれば、一辺の長さと他辺の長さの割合が変化したとしても、座屈モードのピッチは変化しないことが開示されている。また、特許文献1には、正方形断面の場合に一辺の長さと座屈モードのピッチが比例関係にあることが開示されている。 In Patent Document 1, with respect to the pitch of undulating buckling waves generated when a load is input (buckling mode pitch), the sum of the length of one side of the rectangular cross section of the hollow frame member and the length of the other side is constant. It is disclosed that if there is, even if the ratio of the length of one side to the length of the other side changes, the pitch of the buckling mode does not change. Patent Document 1 discloses that in the case of a square cross section, the length of one side and the pitch of the buckling mode are in a proportional relationship.
 しかしながら、本発明者が特許文献1の開示内容について検討したところ、特許文献1に開示された辺の長さと座屈モードのピッチとの関係は静的荷重を付与した場合に成立するものであり、実際の自動車の衝突を模擬した動的荷重を付与した場合には成立しないとの知見が得られた。したがって、特許文献1の開示に基づいて中空状フレーム部材の内方にリブを配置しても、エネルギー吸収性能を十分に向上させることができない場合もある。 However, when the present inventor examined the disclosure content of Patent Document 1, the relationship between the length of the side and the pitch of the buckling mode disclosed in Patent Document 1 holds when a static load is applied. It has been found that this is not the case when a dynamic load simulating an actual car collision is applied. Therefore, even if the rib is arranged inside the hollow frame member based on the disclosure of Patent Document 1, the energy absorption performance may not be sufficiently improved in some cases.
 また、上記特許文献2~4においては、荷重入力時にその衝撃を効率的に吸収する旨や、耐荷重性能を向上させ軽量化を図る旨は開示されているが、部材に安定して軸圧潰変形を生じさせ、エネルギー吸収性能を向上させるための詳細な条件については十分に開示されているとはいえない。特に、補強部材の配置、間隔、枚数や板厚といった詳細な構成については十分な開示がされておらず、車両用構造部材に関し更なるエネルギー吸収性能の向上を図る余地がある。 In addition, Patent Documents 2 to 4 disclose that the impact is efficiently absorbed when a load is input and that the load-bearing performance is improved and the weight is reduced. The detailed conditions for causing deformation and improving the energy absorption performance are not sufficiently disclosed. In particular, the detailed configuration such as the arrangement, spacing, number, and plate thickness of the reinforcing members has not been sufficiently disclosed, and there is room for further improving the energy absorption performance of structural members for vehicles.
 具体的には、例えばフロントサイドメンバ、リアサイドメンバ、クラッシュボックス、エクステンションといった車両用構造部材において、高いエネルギー吸収性能を安定して得ることが求められ、そのためには、安定的に連続的な軸圧潰変形が生じることが好ましい。 Specifically, for example, it is required that the vehicle structural members such as the front side member, the rear side member, the crash box, and the extension have high energy absorption performance in a stable manner. Preferably, deformation occurs.
  本発明は、上記課題に鑑みてなされたものであり、車両用構造部材において、軽量化を図りつつ、車両衝突時に安定的に軸圧潰変形を発生させ、エネルギー吸収性能を維持または向上させることを目的とする。 The present invention has been made in view of the above problems, and in a vehicle structural member, while achieving weight reduction, stably generate axial crush deformation at the time of a vehicle collision, and maintain or improve energy absorption performance. Aim.
  上記課題を解決するため、本発明によれば、金属製の中空部材と、前記中空部材の内面に各辺が接合され、該中空部材の内方空間を隔てるように該中空部材の部材長手方向に沿って間隔をおいて複数配置された、FRPからなる板状の補強部材とを備え、前記中空部材の部材長手方向に垂直な断面において、該中空部材の外形寸法上の最小幅は、該中空部材の外形寸法上の最大幅の30%以上であり、各補強部材は、該補強部材の板面が前記中空部材の部材長手方向に垂直となる向きで、かつ前記中空部材の部材長手方向の端部から、前記最小幅の0.74倍~1.84倍の間隔でもって3枚以上配置され、前記補強部材の板厚は0.7~3.0mmである、車両用構造部材が提供される。 According to the present invention, in order to solve the above problems, a metal hollow member and each side are joined to an inner surface of the hollow member, and a member longitudinal direction of the hollow member is separated so as to separate an inner space of the hollow member. A plurality of plate-shaped reinforcing members made of FRP, which are arranged at intervals along with each other, and in a cross section perpendicular to the member longitudinal direction of the hollow member, the minimum width in external dimensions of the hollow member is 30% or more of the maximum width in the external dimensions of the hollow member, and each reinforcing member has a direction in which the plate surface of the reinforcing member is perpendicular to the longitudinal direction of the hollow member and the longitudinal direction of the hollow member. The structural member for a vehicle, wherein three or more sheets are arranged at an interval of 0.74 to 1.84 times the minimum width from the end of the vehicle, and the plate thickness of the reinforcing member is 0.7 to 3.0 mm. Provided.
 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、前記曲げ誘起部に配置された前記補強部材の間隔が、前記曲げ誘起部以外の部分に配置された前記補強部材の間隔よりも狭くても良い。 The hollow member has a bending inducing portion in a part in the member longitudinal direction, and the interval between the reinforcing members arranged in the bending inducing portion is the interval between the reinforcing members arranged in portions other than the bending inducing portion. It may be narrower than.
 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、前記曲げ誘起部に配置された前記補強部材の板厚が、前記曲げ誘起部以外の部分に配置された前記補強部材の板厚よりも厚くても良い。 The hollow member has a bending inducing portion in a part in the member longitudinal direction, and the thickness of the reinforcing member arranged in the bending inducing portion is a thickness of the reinforcing member arranged in a portion other than the bending inducing portion. It may be thicker than the plate thickness.
 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、前記曲げ誘起部に配置された前記補強部材の引張強さが、前記曲げ誘起部以外の部分に配置された前記補強部材の引張強さよりも大きくても良い。 The hollow member has a bending inducing part in a part in the member longitudinal direction, and the tensile strength of the reinforcing member arranged in the bending inducing part is the reinforcing member arranged in a part other than the bending inducing part. May be greater than the tensile strength of the steel.
 前記FRPは、CFRPまたはGFRPであっても良い。 The FRP may be CFRP or GFRP.
 前記中空部材の引張強さは、980MPa以上であっても良い。 中空 The hollow member may have a tensile strength of 980 MPa or more.
 上記車両用構造部材は、フロントサイドメンバ、リアサイドメンバ、エクステンション、クラッシュボックスのいずれかであっても良い。 The vehicle structural member may be any of a front side member, a rear side member, an extension, and a crash box.
 本発明によれば、車両用構造部材において、軽量化を図りつつ、車両衝突時に安定的に軸圧潰変形を発生させ、エネルギー吸収性能を維持または向上させることができる。 According to the present invention, in a vehicle structural member, axial crush deformation can be stably generated at the time of a vehicle collision while maintaining weight reduction, and energy absorption performance can be maintained or improved.
本発明の一実施形態に係る車両用フレームと他部材とが接合された状態を示す斜視図である。It is a perspective view showing the state where the frame for vehicles and other members concerning one embodiment of the present invention were joined. 同実施形態に係る車両用フレームと他部材とが接合された状態を示す平面図である。It is a top view showing the state where the frame for vehicles concerning the embodiment and other members were joined. 同実施形態に係る車両用フレームと他部材とが接合された状態を示す側面図である。It is a side view showing the state where the frame for vehicles and other members concerning the embodiment were joined. 同実施形態に係る車両用フレームの概略構成を示す斜視図である。FIG. 2 is a perspective view illustrating a schematic configuration of a vehicle frame according to the embodiment. 同実施形態に係る補強部材の形状を示す斜視図である。It is a perspective view showing the shape of the reinforcing member concerning the embodiment. 同実施形態に係る車両用フレームの、中空部材の部材長手方向に垂直な断面を示す図である。FIG. 2 is a diagram showing a cross section of the vehicle frame according to the same embodiment, which is perpendicular to the member longitudinal direction of the hollow member. 図6中のa-a断面図である。FIG. 7 is a sectional view taken along line aa in FIG. 6. 図6中のb-b断面図である。FIG. 7 is a sectional view taken along line bb in FIG. 6. 同実施形態に係る補強部材の配置例を示す図である。It is a figure showing an example of arrangement of a reinforcement member concerning the embodiment. 同実施形態に係る補強部材の配置例を示す図である。It is a figure showing an example of arrangement of a reinforcement member concerning the embodiment. 同実施形態に係る中空部材に設けられる穴部の例を説明するための中空部材の断面図である。It is sectional drawing of the hollow member for demonstrating the example of the hole provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる穴部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the hole provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる穴部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the hole provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる穴部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the hole provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる穴部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the hole provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられるビード部の例を説明するための中空部材の断面図である。It is sectional drawing of the hollow member for demonstrating the example of the bead part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凹部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the crevice provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる凹部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the crevice provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる凹部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the crevice provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる凹部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the crevice provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる凹部の他の例を示す模式図である。It is a mimetic diagram showing other examples of the crevice provided in the hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる凸部の例を説明するための中空部材の断面図である。It is sectional drawing of the hollow member for demonstrating the example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凸部の他の例を示す模式図である。It is a schematic diagram which shows the other example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凸部の他の例を示す模式図である。It is a schematic diagram which shows the other example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凸部の他の例を示す模式図である。It is a schematic diagram which shows the other example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凸部の他の例を示す模式図である。It is a schematic diagram which shows the other example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる凸部の他の例を示す模式図である。It is a schematic diagram which shows the other example of the convex part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる板厚変化部の一例を示す模式図である。It is a schematic diagram which shows an example of the board thickness change part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる薄肉部の一例を示す模式図である。It is a schematic diagram which shows an example of the thin part provided in the hollow member which concerns on the embodiment. 同実施形態に係る中空部材に設けられる異強度部の例を説明するための中空部材の断面図である。It is sectional drawing of the hollow member for demonstrating the example of the different strength part provided in the hollow member which concerns on the same embodiment. 同実施形態に係る中空部材に設けられる異強度部の他の例を示す模式図である。It is a mimetic diagram showing other examples of a different intensity part provided in a hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる異強度部の他の例を示す模式図である。It is a mimetic diagram showing other examples of a different intensity part provided in a hollow member concerning the embodiment. 同実施形態に係る中空部材に設けられる強度変化部の一例を示す模式図である。It is a schematic diagram which shows an example of the intensity | strength change part provided in the hollow member which concerns on the embodiment. 比較例(構造1)の車両用フレームの変形途中の状態を示す平面図である。It is a top view showing the state in the middle of the deformation of the vehicle frame of the comparative example (structure 1). 比較例(構造1)の車両用フレームの変形後の状態を示す平面図である。It is a top view showing the state after deformation of the vehicle frame of the comparative example (structure 1). 比較例(構造4)の車両用フレームの変形途中の状態を示す平面図である。It is a top view showing the state in the middle of the deformation of the vehicle frame of the comparative example (structure 4). 比較例(構造4)の車両用フレームの変形後の状態を示す平面図である。It is a top view showing the state after deformation of the vehicle frame of the comparative example (structure 4). 発明例(構造7)の車両用フレームの変形途中の状態を示す平面図である。It is a top view which shows the state in the middle of deformation | transformation of the vehicle frame of invention example (structure 7). 発明例(構造7)の車両用フレームの変形後の状態を示す平面図である。It is a top view which shows the state after deformation | transformation of the vehicle frame of invention example (structure 7). 衝突シミュレーションにおける各解析モデルのエネルギー吸収性能を比較した図である。It is the figure which compared the energy absorption performance of each analysis model in a collision simulation.
 以下、本発明の一実施形態について、図面を参照しながら説明する。なお、本明細書および図面において、実質的に同一の機能構成を有する要素においては、同一の符号を付することにより重複説明を省略する。 Hereinafter, an embodiment of the present invention will be described with reference to the drawings. In the specification and the drawings, elements having substantially the same function and configuration are denoted by the same reference numerals, and redundant description is omitted.
<1.車両用構造部材の適用対象>
 車両用構造部材の一例である車両用フレームの構成について説明する前に、当該車両用構造部材の適用対象について説明する。一般的な自動車等の車両に設けられる車体は、フロント構造(FRONT)、リア構造(REAR)、およびキャビン構造(CABIN)に分別することができる。
<1. Applicable objects of vehicle structural members>
Before describing the configuration of a vehicle frame, which is an example of a vehicle structural member, an application target of the vehicle structural member will be described. The vehicle body provided in a vehicle such as a general automobile can be classified into a front structure (FRONT), a rear structure (REAR), and a cabin structure (CABIN).
  フロント構造およびリア構造は、車両衝突時において当該構造が自ら圧潰することにより、車両に対する衝撃を吸収して緩和する機能(衝撃吸収機能)を担っている。すなわち、車両衝突時に、キャビンに搭乗する乗員の安全を確保するために、フロント構造およびリア構造は、衝突により生じるエネルギー(衝突エネルギー)を可能な限り吸収する構造であることが要求される。したがって、フロント構造およびリア構造を構成するフレームは、衝突時に曲げや潰れが生じた際においても衝突エネルギーを多く吸収することが求められる。当該フロント構造およびリア構造に用いられるフレームは、例えばフロントサイドメンバやリアサイドメンバ等である。フロントサイドメンバは、後端部を構成するフロントサイドメンバリア、および当該後端部よりも前側の部分を構成するフロントサイドメンバフロントを含む。リアサイドメンバは、後端部を構成するリアサイドメンバリア、および当該後端部よりも前側の部分を構成するリアサイドメンバフロントを含む。 (4) The front structure and the rear structure have a function of absorbing and mitigating a shock to the vehicle (shock absorbing function) by crushing the structure by itself during a vehicle collision. That is, in order to ensure the safety of the occupants in the cabin at the time of a vehicle collision, the front structure and the rear structure are required to have a structure that absorbs as much energy as possible due to the collision (collision energy). Therefore, the frames constituting the front structure and the rear structure are required to absorb a large amount of collision energy even when bending or crushing occurs during a collision. The frames used for the front structure and the rear structure are, for example, front side members and rear side members. The front side member includes a front side member rear that forms a rear end portion, and a front side member front that forms a portion on the front side of the rear end portion. The rear side member includes a rear side member rear that constitutes a rear end, and a rear side member front that constitutes a portion on the front side of the rear end.
  ところで、車両の衝突安全性の維持と軽量化とを両立させるために、車体構造を形成する鋼板の高強度化および薄肉化が進められている。上記のフロント構造、リア構造およびキャビン構造を構成するフレームについても、薄肉化された高強度鋼板に置き換えることが進められている。具体的には、衝突エネルギー吸収量および耐荷重性能の少なくともいずれかが、従来の鋼板により形成されるフレームと同等になるように、高強度鋼板により形成されるフレームの板厚が従来の鋼板により形成されるフレームよりも薄く設定される。これにより、高強度フレームの衝突性能を従来フレームと同等に維持しつつ、フレームの重量を低減させることができる。 鋼板 By the way, in order to maintain the collision safety of the vehicle and reduce the weight at the same time, the strength and thickness of the steel sheet forming the vehicle body structure are being promoted. The frames constituting the front structure, the rear structure, and the cabin structure are also being replaced with thinned high-strength steel plates. Specifically, the thickness of the frame formed by the high-strength steel sheet is made by the conventional steel sheet so that at least one of the collision energy absorption and the load-bearing performance is equivalent to the frame formed by the conventional steel sheet. It is set thinner than the frame to be formed. This makes it possible to reduce the weight of the frame while maintaining the collision performance of the high-strength frame equal to that of the conventional frame.
<2.車両用フレームの構成>
(フレームの構成要素)
  図1は、本発明の一実施形態に係る車両用フレーム1と他部材とが接合された状態を示す斜視図である。図2は、その状態の平面図であり、図3は、その状態の側面図である。図1~図3に示す例における車両用フレーム1はフロントサイドメンバであり、フロントサイドメンバの前端はクラッシュボックス30を介して、バンパービーム40に接合されている。通常、フロントサイドメンバは、キャビン部の前方に左右対称に2本配置されており、図1~図3では、2本の中の1本のみが図示されている。なお、車両用フレーム1は車両用構造部材の一例であり、以下単にフレーム1と記載する。フレーム1はフロント構造およびリア構造に係る部材に適用されることが好ましいが、車両用フレーム1をキャビン構造に係る部材に適用することも可能である。また、当該車両用構造部材は、自動車のみならず、他の車両および自走可能な機械にも適用可能である。他の車両および自走可能な機械には、例えば、二輪車両、バスまたは牽引車等の大型車両、トレーラー、鉄道車両、建設機械、鉱山機械、農業機械、一般機械、および船舶等が含まれる。
<2. Configuration of Vehicle Frame>
(Components of the frame)
FIG. 1 is a perspective view showing a state in which a vehicle frame 1 according to one embodiment of the present invention and other members are joined. FIG. 2 is a plan view of the state, and FIG. 3 is a side view of the state. The vehicle frame 1 in the examples shown in FIGS. 1 to 3 is a front side member, and the front end of the front side member is joined to a bumper beam 40 via a crash box 30. Usually, two front side members are arranged symmetrically in front of the cabin portion, and FIGS. 1 to 3 show only one of the two front side members. The vehicle frame 1 is an example of a vehicle structural member, and will be simply referred to as a frame 1 below. The frame 1 is preferably applied to members having a front structure and a rear structure, but the vehicle frame 1 may be applied to a member having a cabin structure. Further, the vehicle structural member is applicable not only to automobiles but also to other vehicles and self-propelled machines. Other vehicles and self-propelled machines include, for example, motorcycles, heavy vehicles such as buses or towing vehicles, trailers, railway vehicles, construction machines, mining machines, agricultural machines, general machines, ships, and the like.
 図4~図6に示すように本実施形態のフレーム1は、金属製の中空部材10と、中空部材10の内方に配置された複数の補強部材20を備えている。 As shown in FIGS. 4 to 6, the frame 1 of the present embodiment includes a hollow member 10 made of metal and a plurality of reinforcing members 20 arranged inside the hollow member 10.
 本実施形態の中空部材10は、長尺の構造部材の一例であり、部材長手方向(本実施形態ではX方向)に垂直な断面の形状が矩形状となった部材である。本実施形態の中空部材10は一体物として形成された角管状のものであるが、中空部材10は、例えば平板状のクロージングプレートと、断面がハット形状の部材とが接合されることで構成されていてもよい。すなわち、中空部材10は、部材長手方向Xに垂直な断面が閉断面となるように構成されていれば、その構成は特に限定されない。例えば本実施形態では中空部材10の形状が多角形状の一例である矩形状であったが、中空部材10は矩形以外の多角形状であってもよい。但し、後述するように、中空部材10の部材長手方向Xに垂直な断面において、その外形寸法上の最小幅Wminは、当該外形寸法上の最大幅Wmaxの30%以上の長さとなるように構成される。 The hollow member 10 of the present embodiment is an example of a long structural member, and has a rectangular cross section perpendicular to the longitudinal direction of the member (the X direction in the present embodiment). Although the hollow member 10 of the present embodiment is a square tubular member formed as an integral body, the hollow member 10 is configured by, for example, joining a flat closing plate and a member having a hat-shaped cross section. May be. That is, the configuration of the hollow member 10 is not particularly limited as long as the cross section perpendicular to the member longitudinal direction X is a closed cross section. For example, in the present embodiment, the shape of the hollow member 10 is a rectangular shape, which is an example of a polygonal shape. However, the hollow member 10 may be a polygonal shape other than a rectangle. However, as will be described later, in a cross section perpendicular to the member longitudinal direction X of the hollow member 10, the minimum width W min on the external dimensions is set to be 30% or more of the maximum width W max on the external dimensions. It is composed of
 図6に示すように、本実施形態の中空部材10は4つの平面部11a~11dを有している。以降の説明では、それらの4つの平面部11a~11dのうち、図6において上側に位置する平面部を天面部11a、右側に位置する平面部を側面部11b、下側に位置する平面部を底面部11c、左側に位置する平面部を側面部11dと称す。また、天面部11aと側面部11bとの境界となる部分である両平面部11a、11bの接続部を稜線部11e、側面部11bと底面部11cとの境界となる部分である両平面部11b、11cの接続部を稜線部11f、底面部11cと側面部11dとの境界となる部分である両平面部11c、11dの接続部を稜線部11g、側面部11dと天面部11aとの境界となる部分である両平面部11d、11aの接続部を稜線部11hと称す。 中空 As shown in FIG. 6, the hollow member 10 of the present embodiment has four flat portions 11a to 11d. In the following description, among the four plane parts 11a to 11d, the plane part located on the upper side in FIG. 6 is the top part 11a, the plane part located on the right side is the side part 11b, and the plane part located on the lower side is FIG. The bottom portion 11c and the flat portion located on the left side are referred to as side portions 11d. Also, the connecting portion between the two flat portions 11a and 11b, which is the portion between the top surface portion 11a and the side surface portion 11b, is a ridge line portion 11e, and the two flat portion 11b, which is the portion between the side surface portion 11b and the bottom surface portion 11c. , 11c are connected to the ridge 11f, and the connection between the flat portions 11c and 11d, which is the boundary between the bottom 11c and the side 11d, is connected to the ridge 11g, and the boundary between the side 11d and the top 11a. The connecting portion between the two flat portions 11d and 11a, which is a portion formed by the above, is referred to as a ridge portion 11h.
  中空部材10は、金属板により形成される。金属板の種類は特に限定されないが、例えば鋼板等の金属板により形成されることが好ましい。また、衝突性能の観点から中空部材10の板厚は、バス等の大型の車両で多く用いられるフレーム構造では6.0mm以下が好ましく、通常のサイズの車両で多く用いられるモノコック構造車両では3.2mm以下であることが好ましい。必要に応じて、板厚の下限を0.8mm、1.0mm又は1.2mmとしてもよい。また、中空部材10を構成する金属板の引張強さ(以下「中空部材10の引張強さ」という。)は特に限定されない。ただし、軽量化により低減し得るフレーム1の全体的な強度を補うために、中空部材10の引張強さは590MPa以上であることが好ましい。また、中空部材10の引張強さは980MPa以上であることがさらに好ましい。必要に応じて、中空部材10の引張強さの上限を、2000MPa又は1500MPaとしてもよい。 The hollow member 10 is formed of a metal plate. The type of the metal plate is not particularly limited, but is preferably formed of, for example, a metal plate such as a steel plate. Further, from the viewpoint of the collision performance, the plate thickness of the hollow member 10 is preferably 6.0 mm or less in a frame structure often used in large vehicles such as buses, and in a monocoque structure vehicle often used in vehicles of a normal size. It is preferable that it is 2 mm or less. If necessary, the lower limit of the plate thickness may be 0.8 mm, 1.0 mm, or 1.2 mm. Further, the tensile strength of the metal plate constituting the hollow member 10 (hereinafter, referred to as “the tensile strength of the hollow member 10”) is not particularly limited. However, in order to compensate for the overall strength of the frame 1 that can be reduced by weight reduction, the tensile strength of the hollow member 10 is preferably 590 MPa or more. Further, the tensile strength of the hollow member 10 is more preferably 980 MPa or more. If necessary, the upper limit of the tensile strength of the hollow member 10 may be set to 2000 MPa or 1500 MPa.
 補強部材20は、板状のFRP部材である。矩形状の板面20aの各直線部には、フランジ21a~21dが形成されている。本実施形態の補強部材20は、板面20aの形状が中空部材10の部材長手方向Xに垂直な断面の形状と相似形をなしており、板面20aが中空部材10の部材長手方向Xに垂直となる向きで、中空部材10の内方に設けられている。補強部材20のフランジ21aは中空部材10の天面部11aの内面に、フランジ21bは中空部材10の側面部11bの内面に、フランジ21cは中空部材10の底面部11cの内面に、フランジ21dは中空部材10の側面部11dの内面にそれぞれ接合されている。これにより補強部材20が中空部材10に対して固定されている。このように固定された補強部材20は、部材長手方向Xに垂直な断面における中空部材10の内方空間を覆う、いわゆるバルクヘッドとして機能する。なお、補強部材20の形状は、中空部材10の形状や、中空部材10との接合方法等に応じ、補強部材20がバルクヘッドとして機能するように適宜変更されるものである。 The reinforcing member 20 is a plate-shaped FRP member. Flanges 21a to 21d are formed on each linear portion of the rectangular plate surface 20a. In the reinforcing member 20 of the present embodiment, the shape of the plate surface 20 a is similar to the shape of a cross section perpendicular to the member longitudinal direction X of the hollow member 10, and the plate surface 20 a is in the member longitudinal direction X of the hollow member 10. It is provided inside the hollow member 10 in a vertical direction. The flange 21a of the reinforcing member 20 is on the inner surface of the top surface 11a of the hollow member 10, the flange 21b is on the inner surface of the side surface 11b of the hollow member 10, the flange 21c is on the inner surface of the bottom surface 11c of the hollow member 10, and the flange 21d is hollow. It is joined to the inner surface of the side surface portion 11d of the member 10, respectively. Thereby, the reinforcing member 20 is fixed to the hollow member 10. The reinforcing member 20 fixed in this manner functions as a so-called bulkhead that covers the inner space of the hollow member 10 in a cross section perpendicular to the member longitudinal direction X. Note that the shape of the reinforcing member 20 is appropriately changed according to the shape of the hollow member 10, the method of joining the hollow member 10, and the like so that the reinforcing member 20 functions as a bulkhead.
 なお、ここでは補強部材20は矩形状の板面20aの各直線部(各辺)に形成されたフランジ21a~21dを介して中空部材10の内面に接合される場合を図示し、説明したが、接合方法やその態様はこれに限定されるものではない。例えば、矩形状の板面20aを有する補強部材20の各辺にフランジを形成することなく、当該板面20aを直接中空部材10の内面に接合しても良い。また、接合範囲は必ずしも補強部材20の全周でなくても良く、例えば、補強部材20の各辺の長さの50%以上が中空部材10の内面に接合されていれば良い。 Here, the case where the reinforcing member 20 is joined to the inner surface of the hollow member 10 via the flanges 21a to 21d formed on each linear portion (each side) of the rectangular plate surface 20a is illustrated and described. However, the joining method and its mode are not limited to these. For example, the plate surface 20a may be directly joined to the inner surface of the hollow member 10 without forming a flange on each side of the reinforcing member 20 having the rectangular plate surface 20a. The joining range does not necessarily have to be the entire circumference of the reinforcing member 20. For example, it is sufficient that 50% or more of the length of each side of the reinforcing member 20 is joined to the inner surface of the hollow member 10.
(補強部材の例)
 補強部材20として用いられるFRP部材は、マトリックス樹脂と、該マトリックス樹脂中に含有され、複合化された強化繊維材料からなる、繊維強化樹脂部材を意味する。
(Example of reinforcing member)
The FRP member used as the reinforcing member 20 means a fiber reinforced resin member made of a matrix resin and a composite reinforcing fiber material contained in the matrix resin.
 強化繊維材料としては、例えば、炭素繊維、ガラス繊維を用いることができる。他にも、強化繊維材料として、ボロン繊維、シリコンカーバイド繊維、アラミド繊維等を用いることができる。FRP部材に用いられるFRPにおいて、強化繊維材料の基材となる強化繊維基材としては、例えば、チョップドファイバーを使用した不織布基材や連続繊維を使用したクロス材、一方向強化繊維基材(UD材)等を使用することができる。これらの強化繊維基材は、強化繊維材料の配向性の必要に応じて、適宜選択され得る。 As the reinforcing fiber material, for example, carbon fiber and glass fiber can be used. In addition, a boron fiber, a silicon carbide fiber, an aramid fiber, or the like can be used as the reinforcing fiber material. In the FRP used for the FRP member, examples of the reinforcing fiber substrate serving as the substrate of the reinforcing fiber material include a nonwoven fabric substrate using chopped fibers, a cloth material using continuous fibers, and a unidirectional reinforcing fiber substrate (UD). Material) etc. can be used. These reinforcing fiber bases can be appropriately selected according to the necessity of the orientation of the reinforcing fiber material.
 CFRP部材は、強化繊維材料として炭素繊維を用いたFRP部材である。炭素繊維としては、例えば、PAN系またはピッチ系のものが使用できる。炭素繊維を用いることにより、重量に対する強度等を効率よく向上させることができる。 The CFRP member is an FRP member using carbon fiber as a reinforcing fiber material. As the carbon fibers, for example, PAN-based or pitch-based carbon fibers can be used. By using carbon fibers, strength against weight and the like can be efficiently improved.
 GFRP部材は、強化繊維材料としてガラス繊維を用いたFRP部材である。炭素繊維よりも機械的特性に劣るが、金属部材の電蝕を抑制することができる。 The GFRP member is an FRP member using glass fiber as a reinforcing fiber material. Although it is inferior in mechanical properties to carbon fiber, it can suppress the electrolytic corrosion of the metal member.
 FRP部材に用いられるマトリックス樹脂として、熱硬化性樹脂および熱可塑性樹脂のいずれも使用することができる。熱硬化性樹脂としては、エポキシ樹脂、不飽和ポリエステル樹脂、並びにビニルエステル樹脂等があげられる。熱可塑性樹脂としては、ポリオレフィン(ポリエチレン、ポリプロピレン等)およびその酸変性物、ナイロン6およびナイロン66等のポリアミド樹脂、ポリエチレンテレフタラートおよびポリブチレンテレフタラート等の熱可塑性芳香族ポリエステル、ポリカーボネート、ポリエーテルスルホン、ポリフェニレンエーテルおよびその変性物、ポリアリレート、ポリエーテルケトン、ポリエーテルエーテルケトン、ポリエーテルケトンケトン、塩化ビニル、ポリスチレン等のスチレン系樹脂、並びにフェノキシ樹脂等があげられる。なお、マトリックス樹脂は、複数種類の樹脂材料により形成されていてもよい。 マ ト リ ッ ク ス As the matrix resin used for the FRP member, any of a thermosetting resin and a thermoplastic resin can be used. Examples of the thermosetting resin include an epoxy resin, an unsaturated polyester resin, and a vinyl ester resin. Examples of the thermoplastic resin include polyolefins (polyethylene, polypropylene, and the like) and their acid-modified products, polyamide resins such as nylon 6 and nylon 66, thermoplastic aromatic polyesters such as polyethylene terephthalate and polybutylene terephthalate, polycarbonate, and polyether sulfone. And styrene resins such as polyphenylene ether and modified products thereof, polyarylate, polyether ketone, polyether ether ketone, polyether ketone ketone, vinyl chloride and polystyrene, and phenoxy resins. Note that the matrix resin may be formed of a plurality of types of resin materials.
 金属部材への適用を考慮すると、加工性、生産性の観点から、マトリックス樹脂として熱可塑性樹脂を用いることが好ましい。さらに、マトリックス樹脂としてフェノキシ樹脂を用いることで、強化繊維材料の密度を高くすることができる。また、フェノキシ樹脂は熱硬化性樹脂であるエポキシ樹脂と分子構造が酷似しているためエポキシ樹脂と同程度の耐熱性を有する。また、硬化成分をさらに添加することにより、高温環境への適用も可能となる。硬化成分を添加する場合、その添加量は、強化繊維材料への含浸性、FRP部材の脆性、タクトタイムおよび加工性等とを考慮し、適宜決めればよい。 と Considering application to metal members, it is preferable to use a thermoplastic resin as the matrix resin from the viewpoint of workability and productivity. Furthermore, by using a phenoxy resin as the matrix resin, the density of the reinforcing fiber material can be increased. Further, the phenoxy resin has a heat structure similar to that of the epoxy resin because the molecular structure is very similar to that of the epoxy resin which is a thermosetting resin. Further, by further adding a curing component, application to a high-temperature environment becomes possible. When the hardening component is added, the addition amount may be appropriately determined in consideration of the impregnating property of the reinforcing fiber material, the brittleness of the FRP member, the tact time, the workability and the like.
(接着樹脂層)
 補強部材20がFRP部材等により形成される場合、FRP部材と金属部材(上記実施形態では中空部材10)との間に接着樹脂層が設けられ、該接着樹脂層によりFRP部材と金属部材とが接合されてもよい。
(Adhesive resin layer)
When the reinforcing member 20 is formed of an FRP member or the like, an adhesive resin layer is provided between the FRP member and the metal member (the hollow member 10 in the above embodiment), and the FRP member and the metal member are separated by the adhesive resin layer. They may be joined.
 接着樹脂層を形成する接着樹脂組成物の種類は特に限定されない。例えば、接着樹脂組成物は、熱硬化性樹脂、熱可塑性樹脂のいずれかであってもよい。熱硬化性樹脂および熱可塑性樹脂の種類は特に限定されない。例えば、熱可塑性樹脂としては、ポリオレフィンおよびその酸変性物、ポリスチレン、ポリメチルメタクリレート、AS樹脂、ABS樹脂、ポリエチレンテレフタラートやポリブチレンテレフタラート等の熱可塑性芳香族ポリエステル、ポリカーボネート、ポリイミド、ポリアミド、ポリアミドイミド、ポリエーテルイミド、ポリエーテルスルホン、ポリフェニレンエーテルおよびその変性物、ポリフェニレンスルフィド、ポリオキシメチレン、ポリアリレート、ポリエーテルケトン、ポリエーテルエーテルケトン、並びにポリエーテルケトンケトン等から選ばれる1種以上を使用することができる。また、熱硬化性樹脂としては、例えば、エポキシ樹脂、ビニルエステル樹脂、フェノール樹脂、およびウレタン樹脂から選ばれる1種以上を使用することができる。 種類 The type of the adhesive resin composition forming the adhesive resin layer is not particularly limited. For example, the adhesive resin composition may be either a thermosetting resin or a thermoplastic resin. The types of the thermosetting resin and the thermoplastic resin are not particularly limited. For example, as the thermoplastic resin, polyolefins and acid-modified products thereof, polystyrene, polymethyl methacrylate, AS resin, ABS resin, thermoplastic aromatic polyesters such as polyethylene terephthalate and polybutylene terephthalate, polycarbonate, polyimide, polyamide, polyamide Use one or more selected from imide, polyether imide, polyether sulfone, polyphenylene ether and modified products thereof, polyphenylene sulfide, polyoxymethylene, polyarylate, polyether ketone, polyether ether ketone, and polyether ketone ketone can do. Further, as the thermosetting resin, for example, one or more selected from an epoxy resin, a vinyl ester resin, a phenol resin, and a urethane resin can be used.
 接着樹脂組成物は、FRP部材を構成するマトリックス樹脂の特性、補強部材20の特性または金属部材の特性に応じて適宜選択され得る。例えば、接着樹脂層として極性のある官能基を有する樹脂や酸変性などを施された樹脂を用いることで、接着性が向上する。 The adhesive resin composition can be appropriately selected according to the characteristics of the matrix resin constituting the FRP member, the characteristics of the reinforcing member 20, or the characteristics of the metal member. For example, by using a resin having a polar functional group or a resin subjected to acid modification or the like as the adhesive resin layer, the adhesiveness is improved.
 このように、上述した接着樹脂層を用いてFRP部材を金属部材に接着させることにより、FRP部材と金属部材との密着性を向上させることができる。そうすると、金属部材に対し荷重が入力された際の、FRP部材の変形追従性を向上させることができる。この場合、金属部材の変形体に対するFRP部材の効果をより確実に発揮させることが可能となる。 Thus, by adhering the FRP member to the metal member using the above-described adhesive resin layer, the adhesion between the FRP member and the metal member can be improved. Then, the deformation followability of the FRP member when a load is input to the metal member can be improved. In this case, the effect of the FRP member on the deformed metal member can be more reliably exerted.
 なお、接着樹脂層を形成するために用いられる接着樹脂組成物の形態は、例えば、粉体、ワニス等の液体、フィルム等の固体とすることができる。 The form of the adhesive resin composition used to form the adhesive resin layer may be, for example, a liquid such as powder or varnish, or a solid such as a film.
 また、接着樹脂組成物に架橋硬化性樹脂および架橋剤を配合して、架橋性接着樹脂組成物を形成してもよい。これにより接着樹脂組成物の耐熱性が向上するため、高温環境下での適用が可能となる。架橋硬化性樹脂として、例えば2官能性以上のエポキシ樹脂や結晶性エポキシ樹脂を用いることができる。また、架橋剤として、アミンや酸無水物等を用いることができる。また、接着樹脂組成物には、その接着性や物性を損なわない範囲において、各種ゴム、無機フィラー、溶剤等その他添加物が配合されてもよい。 架橋 Alternatively, a crosslinkable curable resin and a crosslinking agent may be blended with the adhesive resin composition to form a crosslinkable adhesive resin composition. Thereby, the heat resistance of the adhesive resin composition is improved, so that application in a high-temperature environment becomes possible. As the crosslinkable curable resin, for example, a bifunctional or more functional epoxy resin or a crystalline epoxy resin can be used. In addition, an amine, an acid anhydride, or the like can be used as a crosslinking agent. Further, various additives such as various rubbers, inorganic fillers and solvents may be blended in the adhesive resin composition as long as the adhesiveness and physical properties are not impaired.
 FRP部材の金属部材への複合化は、種々の方法により実現される。例えば、FRP部材となるFRPまたはその前駆体であるFRP成形用プリプレグと、金属部材とを、上述した接着樹脂組成物で接着し、該接着樹脂組成物を固化(または硬化)させることで得られる。この場合、例えば、加熱圧着を行うことにより、FRP部材と金属部材とを複合化させることができる。 複合 Combining the FRP member with the metal member is realized by various methods. For example, it is obtained by bonding an FRP to be an FRP member or an FRP molding prepreg that is a precursor thereof to a metal member with the above-described adhesive resin composition, and solidifying (or curing) the adhesive resin composition. . In this case, for example, by performing thermocompression bonding, the FRP member and the metal member can be combined.
 上述したFRPまたはFRP成形用プリプレグの金属部材への接着は、部品の成形前、成形中または成形後に行われ得る。例えば、被加工材である金属材料を金属部材に成形した後に、FRPまたはFRP成形用プリプレグを該金属部材に接着しても良い。また、被加工材にFRPまたはFRP成形用プリプレグを加熱圧着により接着した後に、FRP部材が接着された該被加工材を成形して複合化された金属部材を得てもよい。FRP部材のマトリクス樹脂が熱可塑性樹脂であれば、FRP部材が接着された部分について曲げ加工等の成形を行うことも可能である。また、FRP部材のマトリクス樹脂が熱可塑樹脂である場合、加熱圧着工程と成形工程とが一体となった複合一括成形が行われてもよい。 The bonding of the FRP or the FRP forming prepreg to the metal member described above can be performed before, during or after forming the part. For example, after a metal material to be processed is formed into a metal member, FRP or a prepreg for FRP molding may be bonded to the metal member. Alternatively, after the FRP or the prepreg for FRP molding is bonded to the workpiece by heat and pressure bonding, the composite material may be obtained by molding the workpiece to which the FRP member is bonded. If the matrix resin of the FRP member is a thermoplastic resin, it is possible to perform molding such as bending on the portion where the FRP member is bonded. When the matrix resin of the FRP member is a thermoplastic resin, a composite batch molding in which the thermocompression bonding step and the molding step are integrated may be performed.
 なお、FRP部材と金属部材との接合方法は、上述した接着樹脂層による接着に限られない。例えば、FRP部材と金属部材とは、機械的に接合されてもよい。より具体的には、FRP部材と金属部材のそれぞれ対応する位置に締結用の孔が形成され、これらがボルトやリベット等の締結手段により当該孔を介して締結されることにより、FRP部材と金属部材とが接合されていてもよい。他にも公知の接合手段によってFRP部材と金属部材とが接合されてもよい。また、複数の接合手段により複合的にFRP部材と金属部材とが接合されてもよい。例えば、接着樹脂層による接着と、締結手段による締結とが複合的に用いられてもよい。 接合 The joining method between the FRP member and the metal member is not limited to the above-described adhesion using the adhesive resin layer. For example, the FRP member and the metal member may be mechanically joined. More specifically, holes for fastening are formed at positions corresponding to the FRP member and the metal member, respectively, and these are fastened through the holes by fastening means such as bolts and rivets, so that the FRP member and the metal member are fastened. The member may be joined. Alternatively, the FRP member and the metal member may be joined by known joining means. Further, the FRP member and the metal member may be jointly joined by a plurality of joining means. For example, the bonding by the adhesive resin layer and the fastening by the fastening means may be used in combination.
(金属部材およびその表面処理)
 本発明に係る金属部材は、めっきされていてもよい。これにより、耐食性が向上する。特に、金属部材が鋼材である場合は、より好適である。めっきの種類は特に限定されず、公知のめっきを用いることができる。例えば、めっき鋼板(鋼材)として、溶融亜鉛めっき鋼板、溶融合金化亜鉛めっき鋼板、Zn-Al-Mg系合金めっき鋼板、アルミニウムめっき鋼板、電気亜鉛めっき鋼板、電気Zn-Ni系合金めっき鋼板等が用いられ得る。
(Metal members and their surface treatment)
The metal member according to the present invention may be plated. Thereby, corrosion resistance is improved. In particular, when the metal member is a steel material, it is more preferable. The type of plating is not particularly limited, and known plating can be used. For example, as a coated steel sheet (steel material), a hot-dip galvanized steel sheet, a hot-dip galvanized steel sheet, a Zn-Al-Mg based alloy coated steel sheet, an aluminum plated steel sheet, an electro-galvanized steel sheet, an electric Zn-Ni based alloy-coated steel sheet, or the like can be used. Can be used.
 また、金属部材は、表面に化成処理とよばれる皮膜が被覆されていてもよい。これにより、耐食性がより向上する。化成処理として、一般に公知の化成処理を用いることができる。例えば、化成処理として、りん酸亜鉛処理、クロメート処理、クロメートフリー処理等を用いることができる。また、上記皮膜は、公知の樹脂皮膜であってもよい。 金属 The metal member may have a surface coated with a film called a chemical conversion treatment. Thereby, corrosion resistance is further improved. As the chemical conversion treatment, a generally known chemical conversion treatment can be used. For example, as the chemical conversion treatment, a zinc phosphate treatment, a chromate treatment, a chromate-free treatment, or the like can be used. Further, the above-mentioned film may be a known resin film.
 また、金属部材は、一般に公知の塗装が施されているものであってもよい。これにより、耐食性がより向上する。塗装として、公知の樹脂を用いることができる。例えば、塗装として、エポキシ樹脂、ウレタン樹脂、アクリル樹脂、ポリエステル樹脂またはふっ素系樹脂等を主樹脂としたものを用いることができる。また、塗装には、必要に応じて、一般に公知の顔料が添加されていてもよい。また、塗装は、顔料が添加されていないクリヤー塗装であってもよい。かかる塗装は、FRP部材を複合化する前に予め金属部材に施されていてもよいし、FRP部材を複合化した後に金属部材に施されてもよい。また、予め金属部材に塗装が施されたのちにFRP部材が複合化され、さらにその後塗装が施されてもよい。塗装に用いられる塗料は、溶剤系塗料、水系塗料または紛体塗料等であってもよい。塗装の施工方法として、一般に公知の方法が適用され得る。例えば、塗装の施工方法として、電着塗装、スプレー塗装、静電塗装または浸漬塗装等が用いられ得る。電着塗装は、金属部材の端面や隙間部を被覆するのに適しているため、塗装後の耐食性に優れる。また、塗装前に金属部材の表面にりん酸亜鉛処理やジルコニア処理等の一般に公知の化成処理を施すことにより、塗膜密着性が向上する。 金属 Also, the metal member may be a member to which a generally known coating is applied. Thereby, corrosion resistance is further improved. As the coating, a known resin can be used. For example, as the coating, an epoxy resin, a urethane resin, an acrylic resin, a polyester resin, a fluororesin, or the like as a main resin can be used. In addition, generally known pigments may be added to the coating, if necessary. The coating may be a clear coating to which no pigment is added. Such coating may be applied to the metal member in advance before compounding the FRP member, or may be applied to the metal member after compounding the FRP member. Further, the metal member may be coated in advance, the FRP member may be composited, and then the coating may be performed. The paint used for painting may be a solvent-based paint, a water-based paint, a powder paint, or the like. As a method for applying the coating, a generally known method can be applied. For example, electrodeposition coating, spray coating, electrostatic coating, immersion coating, or the like can be used as a coating application method. Electrodeposition coating is suitable for covering the end surfaces and gaps of metal members, and therefore has excellent corrosion resistance after coating. Further, by applying a generally known chemical treatment such as zinc phosphate treatment or zirconia treatment to the surface of the metal member before coating, the adhesion of the coating film is improved.
<3.補強部材の配置例>
 図4に示すように、複数の補強部材20は、中空部材10の部材長手方向Xの端部から部材長手方向Xの全域にわたって間隔をおいて配置されている。詳述すると、本実施形態における各補強部材20は、図7および図8に示すように中空部材10の前端10aから後端10bにかけて、中空部材10の内方空間を隔てるようにして間隔Pをおいて配置されている。
<3. Example of arrangement of reinforcing members>
As shown in FIG. 4, the plurality of reinforcing members 20 are arranged at intervals from the end of the hollow member 10 in the member longitudinal direction X to the entire region in the member longitudinal direction X. More specifically, as shown in FIGS. 7 and 8, each reinforcing member 20 in the present embodiment has an interval P from the front end 10 a to the rear end 10 b of the hollow member 10 so as to separate the inner space of the hollow member 10. It is arranged in.
 ここで、本明細書では、中空部材10の部材長手方向Xに垂直な断面における中空部材10の外形寸法上の最小幅と最大幅を基準として用いる。本実施形態の場合、図6に示す略矩形断面の短辺における外形寸法が最小幅Wminであり、略矩形断面の長辺における外形寸法幅が最大幅Wmaxとなる。本実施形態の中空部材10の断面においては、対向する一対の短辺、及び、対向する一対の長辺は互いに等しく構成されている。ここで、中空部材10の部材長手方向Xに垂直な断面において、その外形寸法上の最小幅Wminは、当該外形寸法上の最大幅Wmaxの30%以上の長さとなるように構成される。外形寸法上の最小幅Wminと該外形寸法上の最大幅Wmaxの比(即ち、断面の偏平比)に関し、最小幅Wminが最大幅Wmaxの30%以上の長さでない場合、中空部材10が安定して軸圧潰変形しない恐れがあり、衝撃吸収部材として有効でない。必要に応じて、最小幅Wminを最大幅Wmaxの35%又は40%以上としてもよい。なお、その定義から、最小幅Wminは最大幅Wmaxより大きくなることはない。 Here, in this specification, the minimum width and the maximum width in the outer dimensions of the hollow member 10 in a cross section perpendicular to the member longitudinal direction X of the hollow member 10 are used as a reference. In the case of the present embodiment, the outer dimension on the short side of the substantially rectangular cross section shown in FIG. 6 is the minimum width W min , and the outer dimension width on the long side of the substantially rectangular cross section is the maximum width W max . In the cross section of the hollow member 10 of the present embodiment, a pair of opposed short sides and a pair of opposed long sides are configured to be equal to each other. Here, in the cross section of the hollow member 10 perpendicular to the member longitudinal direction X, the minimum width W min on the external dimensions is configured to be 30% or more of the maximum width W max on the external dimensions. . The ratio of the minimum width W min and a maximum width W max of the outer shape dimension of the external dimensions (i.e., flat ratio of the section) relates, if the minimum width W min is not more than 30% of the length of the maximum width W max, hollow The member 10 may not be stably deformed by axial crushing, and is not effective as a shock absorbing member. If necessary, the minimum width W min may be 35% or 40% or more of the maximum width W max . From the definition, the minimum width W min does not become larger than the maximum width W max .
 中空部材10の内方に配置された各補強部材20の間隔Pは、中空部材10の外形寸法上の最小幅Wminの0.74倍~1.84倍の長さとなっている。すなわち、本実施形態においては、中空部材10の外形寸法上の最小幅Wminの0.74倍~1.84倍の間隔Pで、中空部材10の部材長手方向Xに沿って各補強部材20が配置されている。また、部材長手方向Xにおいて変化する形状の中空部材10の場合は、部材長手方向Xに垂直な断面の面積が最も小さい位置における中空部材10の断面形状を基準として上記最小幅Wminを定義する。 The interval P between the reinforcing members 20 arranged inside the hollow member 10 is 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member 10. In other words, in the present embodiment, each reinforcing member 20 extends along the member longitudinal direction X of the hollow member 10 at an interval P of 0.74 times to 1.84 times the minimum width W min on the external dimensions of the hollow member 10. Is arranged. In the case of the hollow member 10 having a shape that changes in the member longitudinal direction X, the minimum width W min is defined based on the cross-sectional shape of the hollow member 10 at a position where the area of the cross section perpendicular to the member longitudinal direction X is the smallest. .
 後述の実施例で示すように、各補強部材20の間隔Pが中空部材10の外形寸法上の最小幅Wminの0.74倍~1.84倍である場合、中空部材10の部材長手方向Xから高荷重が入力された際に、中空部材10に安定的に軸圧潰変形が生じる。このような変形が生じる理由は次の通りである。 As will be described later in the embodiment, when the interval P between the reinforcing members 20 is 0.74 times to 1.84 times the minimum width W min of the outer dimensions of the hollow member 10, the longitudinal direction of the hollow member 10 When a high load is input from X, axial crush deformation occurs in the hollow member 10 stably. The reason why such deformation occurs is as follows.
 補強部材20が配置された箇所においては補強効果が大きいことから、中空部材10の前端10aから高荷重が入力されると、まず、前端10aに最も近い1番目の補強部材20が配置された箇所よりも前方の部分において中空部材10が変形する。その後、中空部材10の変形が後端10bに向かって進行し、中空部材10の1番目の補強部材20が配置された箇所の変形が開始される。FRPは延性が低いため、この段階で1番目の補強部材20が破断する。すなわち、1番目の補強部材20が配置された箇所においては補強効果が失われ、当該箇所における中空部材10が変形しやすくなる。 When a high load is input from the front end 10a of the hollow member 10, the first reinforcement member 20 closest to the front end 10a is located at the position where the first reinforcement member 20 is arranged because the reinforcement effect is large at the position where the reinforcement member 20 is disposed. The hollow member 10 is deformed in a portion forward of the hollow member 10. Thereafter, the deformation of the hollow member 10 proceeds toward the rear end 10b, and the deformation of the hollow member 10 where the first reinforcing member 20 is disposed is started. Since the FRP has low ductility, the first reinforcing member 20 breaks at this stage. That is, the reinforcing effect is lost at the place where the first reinforcing member 20 is arranged, and the hollow member 10 at the place is easily deformed.
 一方、2番目以降の補強部材20が配置された箇所においては、補強部材20が破断していないことから、補強効果が失われずに維持されている。すなわち、2番目以降の補強部材20が配置された箇所においては、中空部材10が変形しにくい状態にある。このため、破断した1番目の補強部材20が配置された箇所における中空部材10の変形が十分に進行するまでは、2番目以降の補強部材20が配置された箇所の中空部材10の変形量は小さくなっている。そして、2番目の補強部材20が配置された箇所の前方領域の変形が十分に進行した後に、2番目の補強部材20が配置された箇所の中空部材10の変形が開始される。前述のようにFRPは延性が低いことから、この段階で、2番目の補強部材20が破断する。これにより、2番目の補強部材20が配置された箇所においては補強効果が失われ、当該箇所における中空部材10が変形しやすくなる。 On the other hand, at the places where the second and subsequent reinforcing members 20 are arranged, the reinforcing members 20 are not broken, and thus the reinforcing effect is maintained without being lost. That is, at the place where the second and subsequent reinforcing members 20 are arranged, the hollow member 10 is in a state where it is difficult to deform. For this reason, until the deformation of the hollow member 10 at the location where the first reinforcing member 20 that has been broken is advanced sufficiently, the deformation amount of the hollow member 10 at the location where the second and subsequent reinforcing members 20 are located is It is getting smaller. Then, after the deformation in the front region of the place where the second reinforcing member 20 is disposed has sufficiently progressed, the deformation of the hollow member 10 where the second reinforcing member 20 is disposed starts. As described above, since the FRP has low ductility, the second reinforcing member 20 breaks at this stage. Thereby, the reinforcing effect is lost at the place where the second reinforcing member 20 is arranged, and the hollow member 10 at the place is easily deformed.
 上記のような変形が3番目以降の補強部材20が配置された箇所においても繰り返し発生する。すなわち、本実施形態のフレーム1においては、中空部材10の部材長手方向Xに沿って配置された各補強部材20が、荷重入力側の端部から順々に破断しながら中空部材10の変形が進行する。これにより、中空部材10の部材長手方向Xからの荷重入力時において安定的に軸圧潰変形を発生させることができ、高いエネルギー吸収性能を安定して得ることができる。 (4) The above-described deformation occurs repeatedly even in the places where the third and subsequent reinforcing members 20 are arranged. That is, in the frame 1 of the present embodiment, the deformation of the hollow member 10 is caused while the reinforcing members 20 arranged along the member longitudinal direction X of the hollow member 10 are sequentially broken from the end on the load input side. proceed. Thereby, when a load is input from the member longitudinal direction X of the hollow member 10, axial crush deformation can be generated stably, and high energy absorption performance can be stably obtained.
 一方で、各補強部材20の間隔Pが中空部材10の外形寸法上の最小幅Wminの0.74倍~1.84倍を満たさない場合、中空部材10に安定的な軸圧潰変形は生じない恐れがある。間隔Pが中空部材10の外形寸法上の最小幅Wminの0.74倍よりも短い場合、剛性が高くなり過ぎるため、各補強部材20間で座屈が起こらない恐れがある。間隔Pが中空部材10の外形寸法上の最小幅Wminの1.84倍超である場合、各補強部材20間が長すぎるため1箇所での横折れ変形が生じ、軸圧潰変形とはならない恐れがある。必要に応じて、各補強部材20の間隔Pの下限を、中空部材10の外形寸法上の最小幅Wminの0.80倍、0.85倍又は0.90倍としてもよい。必要に応じて、各補強部材20の間隔Pの上限を、中空部材10の外形寸法上の最小幅Wminの1.60倍、1.50倍又は1.40倍としてもよい。 On the other hand, when the interval P between the reinforcing members 20 does not satisfy 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member 10, stable axial crush deformation occurs in the hollow member 10. There is no fear. If the interval P is shorter than 0.74 times the minimum width W min of the external dimensions of the hollow member 10, the stiffness becomes too high, and there is a possibility that buckling does not occur between the reinforcing members 20. If the interval P is more than 1.84 times the minimum width W min of the external dimensions of the hollow member 10, the space between the reinforcing members 20 is too long, so that lateral bending deformation occurs at one location and does not result in axial crush deformation. There is fear. If necessary, the lower limit of the interval P between the reinforcing members 20 may be set to 0.80 times, 0.85 times, or 0.90 times the minimum width W min of the external dimensions of the hollow member 10. If necessary, the upper limit of the interval P between the reinforcing members 20 may be set to 1.60 times, 1.50 times, or 1.40 times the minimum width W min of the external dimensions of the hollow member 10.
 また、エネルギー吸収性能についての重量効率を高める観点においては、補強部材20を構成するFRP部材の引張強さ(以下「補強部材20の引張強さ」という。)は100MPa以上であることが好ましい。必要に応じて、引張強さの上限を2500MPa又は2000MPaとしてもよい。また、後述の実施例で示すように、補強部材20の板厚は0.7~3.0mmであることが好ましい。補強部材20の板厚の下限を0.8mm、0.9又は1.0mmとしてもよい。板厚の上限を2。9mm、2.8mm、2.4mm又は2.0mmとしてもよい。
なお、鋼板などの金属板のその延性は、一般的に良好である。このため、補強部材20を金属板とした場合、上記のような補強部材20が破断することがないため、高いエネルギー吸収性能を安定して得ることができない。このため、補強部材20はFRP部材とする必要がある。
In addition, from the viewpoint of increasing the weight efficiency of the energy absorption performance, the tensile strength of the FRP member constituting the reinforcing member 20 (hereinafter, referred to as “the tensile strength of the reinforcing member 20”) is preferably 100 MPa or more. If necessary, the upper limit of the tensile strength may be 2500 MPa or 2000 MPa. Further, as shown in the embodiments described later, the plate thickness of the reinforcing member 20 is preferably 0.7 to 3.0 mm. The lower limit of the plate thickness of the reinforcing member 20 may be 0.8 mm, 0.9, or 1.0 mm. The upper limit of the plate thickness may be 2.9 mm, 2.8 mm, 2.4 mm, or 2.0 mm.
The ductility of a metal plate such as a steel plate is generally good. For this reason, when the reinforcing member 20 is a metal plate, the reinforcing member 20 as described above does not break, so that high energy absorption performance cannot be stably obtained. For this reason, the reinforcing member 20 needs to be an FRP member.
 以上、本実施形態に係る補強部材20の配置について説明したが、補強部材20の配置は図4に示した例に限定されない。例えば図9に示すように、各補強部材20は、部材長手方向Xの全域にわたって配置されていなくてもよい。図9に示す例では、中空部材10の部材長手方向Xの中央位置を境界とした前部と後部のうち、補強部材20は、荷重入力側の端部(本実施形態では前端10a)がある前部にのみ配置されている。この場合であっても、補強部材20が配置された領域においては、荷重入力時に安定的に軸圧潰変形を発生させることができる。荷重入力時に安定的に軸圧潰変形を発生させるとの観点からは、中空部材10の部材長手方向Xの前部において、荷重入力側の端部(前端10a)から間隔Pでもって3枚以上の補強部材20が配置されていれば良い。また、中空部材10の部材長手方向Xにおいて、荷重入力側の端部(前端10a)から長さ15%、20%、又は30%の範囲内に補強部材20が配置されることが好ましい。補強部材20の枚数を4枚以上、5枚以上又は6枚以上とすることがより好ましい。 Although the arrangement of the reinforcing members 20 according to the present embodiment has been described above, the arrangement of the reinforcing members 20 is not limited to the example illustrated in FIG. For example, as shown in FIG. 9, each reinforcing member 20 may not be arranged over the entire region in the member longitudinal direction X. In the example illustrated in FIG. 9, the reinforcing member 20 has an end on the load input side (the front end 10 a in the present embodiment) among the front part and the rear part having the center position in the member longitudinal direction X of the hollow member 10 as a boundary. Located only on the front. Even in this case, in the area where the reinforcing member 20 is arranged, axial crush deformation can be stably generated when a load is input. From the viewpoint of stably generating axial crushing deformation at the time of load input, three or more sheets at a distance P from the load input side end (front end 10a) at the front portion in the member longitudinal direction X of the hollow member 10. What is necessary is just to arrange the reinforcement member 20. Further, in the member longitudinal direction X of the hollow member 10, the reinforcing member 20 is preferably arranged within a range of 15%, 20%, or 30% from the end (front end 10a) on the load input side. More preferably, the number of the reinforcing members 20 is 4 or more, 5 or more, or 6 or more.
 また、前述の実施形態において、各補強部材20の間隔Pは、中空部材10の部材長手方向Xに沿って一定となっているが、間隔Pが中空部材10の外形寸法上の最小幅Wminの0.74倍~1.84倍の範囲内にあれば、間隔Pは図10に示すように部材長手方向Xに沿って一定でなくてもよい。図10に示す例では、中空部材10の部材長手方向Xにおける前部に配置された補強部材20の間隔と、後部に配置された補強部材20の間隔が異なっている。 In the above-described embodiment, the interval P between the reinforcing members 20 is constant along the member longitudinal direction X of the hollow member 10, but the interval P is the minimum width W min in the outer dimensions of the hollow member 10. As long as it is within the range of 0.74 times to 1.84 times, the interval P may not be constant along the member longitudinal direction X as shown in FIG. In the example shown in FIG. 10, the interval between the reinforcing members 20 arranged at the front portion in the member longitudinal direction X of the hollow member 10 and the interval between the reinforcing members 20 arranged at the rear portion are different.
 また、中空部材10の形状は、車両用構造部材の用途に応じて適宜変更されるものであるが、中空部材10の形状に応じて曲げ変形が生じやすい部分と、その他の部分とで、補強部材20の間隔Pや板厚、強度等を変えることによって曲げ変形が生じやすい部分を重点的に補強してもよい。これにより、従来、曲げ変形が発生し、必ずしもエネルギー吸収効率が高くなかった部位において、エネルギー吸収効率が高い軸圧潰変形を発生させることができる。本明細書においては、そのような曲げ変形が生じやすい部分を“曲げ誘起部”と称す。 The shape of the hollow member 10 is appropriately changed depending on the use of the structural member for a vehicle. However, the portion that is easily bent and deformed according to the shape of the hollow member 10 and the other portions are reinforced. By changing the interval P, the plate thickness, the strength, and the like of the members 20, a portion where bending deformation is likely to occur may be mainly reinforced. Thereby, it is possible to generate axial crush deformation having high energy absorption efficiency in a portion where bending deformation has conventionally occurred and energy absorption efficiency has not always been high. In this specification, a portion where such bending deformation is likely to occur is referred to as a “bending inducing portion”.
 曲げ誘起部に配置された補強部材20の間隔Pは、曲げ誘起部以外の部分に配置された補強部材20の間隔Pよりも狭いことが好ましい。これにより、曲げ誘起部における補強効果が高まり、より安定的に軸圧潰変形を発生させることができる。同様の理由で、曲げ誘起部に配置された補強部材20の板厚は、曲げ誘起部以外の部分に配置された補強部材20の板厚よりも厚いことが好ましい。また、同様の理由で、曲げ誘起部に配置された補強部材20の引張強さは、曲げ誘起部以外の部分に配置された補強部材20の引張強さよりも大きいことが好ましい。また、上記のような曲げ誘起部における間隔P、板厚および引張強さ等の設定方法は適宜組み合わせられていてもよい。 間隔 It is preferable that the interval P between the reinforcing members 20 arranged in the bending inducing section is narrower than the interval P between the reinforcing members 20 arranged in portions other than the bending inducing section. Thereby, the reinforcing effect in the bending inducing portion is enhanced, and axial crush deformation can be more stably generated. For the same reason, it is preferable that the plate thickness of the reinforcing member 20 arranged in the bending inducing portion is larger than the plate thickness of the reinforcing member 20 arranged in a portion other than the bending inducing portion. Further, for the same reason, it is preferable that the tensile strength of the reinforcing member 20 arranged in the bending inducing section is higher than the tensile strength of the reinforcing member 20 arranged in a portion other than the bending inducing section. In addition, the methods for setting the interval P, the plate thickness, the tensile strength, and the like in the bending inducing section as described above may be appropriately combined.
<4.曲げ誘起部の例>
 次に、中空部材10に設けられる曲げ誘起部の例について説明する。例えば中空部材10に設けられる穴部、凹部、凸部、板厚変化部、および異強度部等が、曲げ誘起部としての機能を実現する。穴部、凹部、凸部、および板厚変化部のいずれかが設けられた部分は、中空部材10の部材長手方向Xで中空部材10の断面係数が変化する部分である。中空部材10の部材長手方向Xで断面係数が変化する部分においては、同一の曲げモーメントにより中空部材10に生じる曲げ応力が変化するので、当該部分において中空部材10の曲げが誘起される。より具体的には、部材長手方向Xで中空部材10のうち断面係数が相対的に小さい部分については、当該部分における曲げ応力が相対的に大きくなるので、当該部分において屈曲が生じる。また、部材長手方向Xで中空部材10のうち断面係数が相対的に大きい部分については、当該部分の中空部材10の部材長手方向Xの前後における領域を含む部分の断面係数が相対的に小さくなる。したがって、当該領域と上記断面係数が相対的に大きい部分との境界部分において屈曲が生じる。
<4. Example of bending inducer>
Next, an example of the bending inducing section provided in the hollow member 10 will be described. For example, a hole, a concave portion, a convex portion, a plate thickness change portion, a different strength portion, and the like provided in the hollow member 10 realize a function as a bending inducing portion. The portion provided with any one of the hole, the concave portion, the convex portion, and the plate thickness changing portion is a portion where the cross-sectional coefficient of the hollow member 10 changes in the member longitudinal direction X of the hollow member 10. In a portion of the hollow member 10 where the section modulus changes in the member longitudinal direction X, the bending stress generated in the hollow member 10 by the same bending moment changes, so that bending of the hollow member 10 is induced in the portion. More specifically, in a portion of the hollow member 10 having a relatively small section modulus in the longitudinal direction X of the member, the bending stress in the portion is relatively large, so that the portion is bent. Further, for a portion of the hollow member 10 having a relatively large section modulus in the member longitudinal direction X, the section modulus of a portion including the region before and after the hollow member 10 in the member longitudinal direction X is relatively small. . Therefore, bending occurs at the boundary between the region and the portion where the section modulus is relatively large.
 また、異強度部は、中空部材10の部材長手方向Xで中空部材10の降伏強度が変化する部分である。中空部材10の部材長手方向Xで降伏強度が変化する部分においては、当該部分における中空部材10の塑性変形が誘起される。例えば、部材長手方向Xで中空部材10のうち降伏強度が相対的に小さい部分については、当該部分における塑性変形が中空部材10において最初に生じるため、当該部分において屈曲が生じる。また、部材長手方向Xで中空部材10のうち降伏強度が相対的に大きい部分については、当該部分の中空部材10の部材長手方向Xの前後における領域を含む部分の降伏強度が相対的に小さくなる。したがって、当該領域と上記降伏強度が相対的に大きい部分との境界部分において屈曲が生じる。 The different strength portion is a portion where the yield strength of the hollow member 10 changes in the member longitudinal direction X of the hollow member 10. In a portion of the hollow member 10 where the yield strength changes in the member longitudinal direction X, plastic deformation of the hollow member 10 in the portion is induced. For example, in a portion of the hollow member 10 where the yield strength is relatively small in the member longitudinal direction X, plastic deformation in the portion occurs first in the hollow member 10, so that bending occurs in the portion. Further, for a portion of the hollow member 10 where the yield strength is relatively large in the member longitudinal direction X, the yield strength of the portion including the region before and after the hollow member 10 in the member longitudinal direction X is relatively small. . Therefore, bending occurs at the boundary between the region and the portion where the yield strength is relatively large.
 また、中空部材10において、前述した曲げ誘起部としての機能を実現する穴部、凹部、凸部、板厚変化部、および異強度部等を含む部分がないとしても、中空部材10に加わる荷重入力の方向がある程度特定できる場合は、中空部材10と接合する周辺部材の拘束の影響を受けて、中空部材内に曲げモーメントが最大となる領域が存在し、当該領域で屈曲が生じる。そのため中空部材10に発生する曲げモーメントを特定できる場合は、曲げモーメントが最大となる領域も曲げ誘起部としての機能を有している。 Further, even if the hollow member 10 does not include a hole, a concave portion, a convex portion, a plate thickness change portion, a different strength portion, and the like that realize the function as the bending inducing portion described above, the load applied to the hollow member 10 When the direction of the input can be specified to some extent, there is a region where the bending moment is maximum in the hollow member under the influence of the constraint of the peripheral member joined to the hollow member 10, and bending occurs in the region. Therefore, when the bending moment generated in the hollow member 10 can be specified, the region where the bending moment is maximum also has a function as the bending inducing portion.
 以下、中空部材10に設けられる曲げ誘起部の具体例について説明する。 Hereinafter, a specific example of the bending inducing section provided in the hollow member 10 will be described.
 (穴部)
 図11は、本実施形態に係る中空部材10Aに設けられる穴部の例を説明するための中空部材10Aの断面図である。図11に示すように、側面部11bには穴部50が設けられている。穴部50が設けられた部分における中空部材10Aの断面係数は、穴部50が設けられた部分の前後における部分の中空部材10Aの断面係数よりも低い。したがって、図11に示す衝突荷重Fが中空部材10Aに入力された場合、中空部材10Aは、穴部50が設けられた部分において、穴部50が曲げ内側となるように屈曲する。すなわち、中空部材10Aの部材長手方向Xにおいて、中空部材10Aのうち穴部50が設けられた部分が、中空部材10Aに設けられる曲げ誘起部となる。
(Hole)
FIG. 11 is a cross-sectional view of the hollow member 10A for explaining an example of a hole provided in the hollow member 10A according to the present embodiment. As shown in FIG. 11, a hole 50 is provided in the side surface 11b. The section modulus of the hollow member 10A in the portion where the hole 50 is provided is lower than the section modulus of the hollow member 10A in the portion before and after the portion where the hole 50 is provided. Therefore, when the collision load F shown in FIG. 11 is input to the hollow member 10A, the hollow member 10A bends at the portion where the hole 50 is provided so that the hole 50 is bent inside. That is, in the member longitudinal direction X of the hollow member 10A, a portion of the hollow member 10A where the hole 50 is provided becomes a bending inducing portion provided in the hollow member 10A.
 また、穴部の形状および配置については、上述した例に限られない。図12~図15は、本実施形態に係る中空部材10Aに設けられる穴部の他の例を示す模式図である。図12に示すように、円形の穴部50aが側面部11bに設けられてもよい。また、図13に示すように、複数の穴部50bが側面部11bに設けられてもよい。この場合、例えば、複数の穴部50bが、中空部材10Aの部材長手方向Xに横切る方向に並んで設けられてもよい。この場合、衝突荷重の入力時において、穴部50bが曲げの起点として、中空部材10Aが側面部11b側に曲げ変形しやすくなる。 形状 Further, the shape and arrangement of the holes are not limited to the examples described above. 12 to 15 are schematic diagrams showing other examples of the hole provided in the hollow member 10A according to the present embodiment. As shown in FIG. 12, a circular hole 50a may be provided in the side surface 11b. Further, as shown in FIG. 13, a plurality of holes 50b may be provided in the side surface 11b. In this case, for example, a plurality of holes 50b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10A. In this case, when the collision load is input, the hollow member 10A is easily bent and deformed toward the side surface 11b with the hole 50b as a starting point of bending.
 また、図14に示すように、中空部材10Aの部材長手方向Xに横切る方向に延在する穴部50cが側面部11bに設けられてもよい。この場合、衝突荷重の入力時において、穴部50cが曲げの起点として、中空部材10Aが側面部11b側に曲げ変形する。なお、穴部50cの形状は、図14に示す角丸矩形に限定されず、あらゆる形状であってもよい。なお、上述した中空部材10Aの部材長手方向Xに横切る方向は、図12~図14に示すような、中空部材10Aの部材長手方向Xに直交する方向に限定されない。
また、穴部50の設けられる部分は側面部11bに限られない。例えば、天面部11a、底面部11c、または側面部11dに穴部50が設けられてもよい。
As shown in FIG. 14, a hole 50c extending in a direction transverse to the member longitudinal direction X of the hollow member 10A may be provided in the side surface 11b. In this case, when a collision load is input, the hollow member 10A bends and deforms toward the side surface 11b with the hole 50c as a starting point of bending. The shape of the hole 50c is not limited to the rounded rectangle shown in FIG. 14, and may be any shape. The direction transverse to the member longitudinal direction X of the hollow member 10A described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10A as shown in FIGS.
Further, the portion where the hole 50 is provided is not limited to the side surface 11b. For example, the hole 50 may be provided in the top surface 11a, the bottom surface 11c, or the side surface 11d.
 また、図15に示すように、穴部50dが稜線部11eに設けられてもよい。これにより、中空部材10Aのうち部材長手方向Xで穴部50dが設けられた部分の断面係数が顕著に低下するので、穴部50dが設けられた部分が曲げの起点として曲げ変形しやすくなる。 穴 Also, as shown in FIG. 15, a hole 50d may be provided in the ridge 11e. Thereby, since the section modulus of the portion provided with the hole 50d in the member longitudinal direction X in the hollow member 10A is significantly reduced, the portion provided with the hole 50d is easily bent as a starting point of bending.
(凹部)
 図16は、本実施形態に係る中空部材に設けられるビード部の例を説明するための中空部材10Bの断面図である。なお、ビード部51は、本実施形態における凹部の一例である。図16に示すように、側面部11bにはビード部51が設けられている。ビード部51が設けられた部分における中空部材10Bの断面係数は、ビード部51が設けられた部分の前後における部分の中空部材10Bの断面係数よりも低い。したがって、図16に示す衝突荷重Fが中空部材10Bに入力された場合、中空部材10Bはビード部51が設けられた部分において、ビード部51が曲げ内側となるように屈曲する。すなわち、中空部材10Bの部材長手方向Xにおいて、中空部材10Bのうちビード部51が設けられた部分が、中空部材10Bに設けられる曲げ誘起部となる。
(Recess)
FIG. 16 is a cross-sectional view of the hollow member 10B for explaining an example of a bead portion provided in the hollow member according to the present embodiment. Note that the bead portion 51 is an example of a concave portion in the present embodiment. As shown in FIG. 16, a bead part 51 is provided on the side surface part 11b. The section modulus of the hollow member 10B at the portion where the bead portion 51 is provided is lower than the section modulus of the hollow member 10B at the portion before and after the portion where the bead portion 51 is provided. Therefore, when the collision load F shown in FIG. 16 is input to the hollow member 10B, the hollow member 10B bends at the portion where the bead portion 51 is provided, such that the bead portion 51 is bent inside. That is, in the member longitudinal direction X of the hollow member 10B, a portion of the hollow member 10B where the bead portion 51 is provided serves as a bending inducing portion provided in the hollow member 10B.
 なお、凹部の形状および配置については、上述した例に限られない。図17~図20は、本実施形態に係る中空部材10Bに設けられる凹部の他の例を示す模式図である。ここでいう凹部とは、エンボスやビードなどの、中空部材10Bの側面部11b等に設けられる窪み部分を意味する。図17に示すように、円形の凹部51aが側面部11bに設けられてもよい。 Note that the shape and arrangement of the concave portions are not limited to the examples described above. 17 to 20 are schematic views showing other examples of the recess provided in the hollow member 10B according to the present embodiment. The concave portion here means a concave portion such as an emboss or a bead provided in the side surface portion 11b of the hollow member 10B. As shown in FIG. 17, a circular concave portion 51a may be provided on the side surface portion 11b.
 また、図18に示すように、複数の凹部51bが側面部11bに設けられてもよい。この場合、例えば、複数の凹部51bが、中空部材10Bの部材長手方向Xに横切る方向に並んで設けられてもよい。この場合、衝突荷重の入力時において、複数の凹部51bが曲げの起点として、中空部材10Bが側面部11b側に曲げ変形しやすくなる。 Also, as shown in FIG. 18, a plurality of recesses 51b may be provided on the side surface 11b. In this case, for example, a plurality of concave portions 51b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10B. In this case, when the collision load is input, the hollow member 10B is easily bent and deformed toward the side surface portion 11b with the plurality of concave portions 51b serving as a starting point of bending.
 また、図19に示すように、中空部材10Bの部材長手方向Xに横切る方向に延在するビード部51cが側面部11bに設けられてもよい。この場合、衝突荷重の入力時において、ビード部51cが曲げの起点として、中空部材10Bが側面部11b側に曲げ変形される。なお、ビード部51cの形状は、図19に示す角丸矩形に限定されず、あらゆる形状であってもよい。
なお、上述した中空部材10Bの部材長手方向Xに横切る方向は、図19に示すような、中空部材10Bの部材長手方向Xに直交する方向に限定されない。
また、凹部51の設けられる部分は側面部11bに限られない。例えば、天面部11a、底面部11c、または側面部11dに凹部51が設けられてもよい。
Further, as shown in FIG. 19, a bead portion 51c extending in a direction crossing the member longitudinal direction X of the hollow member 10B may be provided on the side surface portion 11b. In this case, when a collision load is input, the hollow member 10B is bent and deformed toward the side surface 11b with the bead portion 51c as a starting point of bending. Note that the shape of the bead portion 51c is not limited to the rounded rectangle shown in FIG. 19, and may be any shape.
Note that the direction crossing the member longitudinal direction X of the hollow member 10B described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10B as shown in FIG.
Further, the portion where the concave portion 51 is provided is not limited to the side surface portion 11b. For example, the concave portion 51 may be provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d.
 また、図20に示すように、凹部51dが稜線部11eに設けられてもよい。これにより、中空部材10Bのうち部材長手方向Xで凹部51dが設けられた部分の断面係数が顕著に変化するので、凹部51dが設けられた部分が曲げの起点として曲げ変形しやすくなる。 凹 部 Also, as shown in FIG. 20, a concave portion 51d may be provided in the ridge line portion 11e. Thus, the section modulus of the hollow member 10B in the member longitudinal direction X where the concave portion 51d is provided significantly changes, so that the portion provided with the concave portion 51d easily bends and deforms as a starting point of bending.
 図21は、本実施形態に係る中空部材10Bに設けられる凹部の他の例を示す模式図である。図21に示すように、中空部材10Bの部材長手方向Xに延在する凹部51e、51fが、中空部材10Bの部材長手方向Xに沿って並んで設けられてもよい。この場合、中空部材10Bのうち、部材長手方向Xにおける凹部51eと凹部51fとの間の部分510で曲げが生じる。すなわち、中空部材10Bのうち、凹部51e、51fが設けられた部分と、凹部51eと凹部51fとの間の部分510とでは断面係数が異なるので、衝突荷重の入力時において、当該部分510を曲げの起点として曲げ変形が生じる。また、当該部分510には、凹部、後述する凸部、薄肉部または異強度部等が形成されていてもよい。なお、凹部51eおよび凹部51fは、図21に示すように、必ずしも直列に並んでいなくてもよい。また、凹部51eおよび凹部51fは、必ずしも中空部材10Bの部材長手方向Xに延在していなくてもよい。 FIG. 21 is a schematic view showing another example of the recess provided in the hollow member 10B according to the present embodiment. As shown in FIG. 21, concave portions 51e and 51f extending in the member longitudinal direction X of the hollow member 10B may be provided side by side along the member longitudinal direction X of the hollow member 10B. In this case, bending occurs in a portion 510 of the hollow member 10B between the concave portion 51e and the concave portion 51f in the member longitudinal direction X. That is, since the section of the hollow member 10B where the concave portions 51e and 51f are provided and the portion 510 between the concave portion 51e and the concave portion 51f have different sectional coefficients, the portion 510 is bent when the collision load is input. Bending deformation occurs as a starting point of. In addition, the portion 510 may be formed with a concave portion, a convex portion described later, a thin portion, a different strength portion, or the like. In addition, the concave portion 51e and the concave portion 51f do not necessarily have to be arranged in series as shown in FIG. Further, the concave portion 51e and the concave portion 51f do not necessarily need to extend in the member longitudinal direction X of the hollow member 10B.
(凸部)
 図22は、本実施形態に係る中空部材10Cに設けられる凸部の例を説明するための中空部材10Cの断面図である。図22に示すように、側面部11bには凸部52が設けられている。凸部52が設けられた部分における中空部材10Cの断面係数は、凸部52が設けられた部分の前後における部分の中空部材10Cの断面係数よりも高い。したがって、図22に示す衝突荷重Fが中空部材10Cに入力された場合、中空部材10Cの部材長手方向Xにおける凸部52の前後の領域6aまたは領域6bのうち、最も断面係数が低くなる部分において、凸部52が曲げ内側となるように屈曲する。なお、この領域6aおよび領域6bは、Y方向における、中空部材10Cの断面係数の変化が生じる領域である。すなわち、中空部材10Cの部材長手方向Xにおいて、中空部材10Cのうち凸部52およびその前後の領域6aおよび領域6bを含む部分が、中空部材10Cに設けられる曲げ誘起部となる。
(Convex)
FIG. 22 is a cross-sectional view of the hollow member 10C for explaining an example of a protrusion provided on the hollow member 10C according to the present embodiment. As shown in FIG. 22, a protrusion 52 is provided on the side surface 11b. The section modulus of the hollow member 10C at the portion where the protrusion 52 is provided is higher than the section modulus of the hollow member 10C at the portion before and after the portion where the protrusion 52 is provided. Therefore, when the collision load F shown in FIG. 22 is input to the hollow member 10C, a portion of the region 6a or the region 6b before and after the convex portion 52 in the member longitudinal direction X of the hollow member 10C has a lowest section modulus. , So that the convex portion 52 is on the inside of the bend. The area 6a and the area 6b are areas where a change in the section modulus of the hollow member 10C in the Y direction occurs. That is, in the member longitudinal direction X of the hollow member 10C, a portion of the hollow member 10C including the convex portion 52 and the regions 6a and 6b before and after the convex portion 52 serves as a bending inducing portion provided in the hollow member 10C.
 なお、図22に示した例では、側面部11bに凸部52が設けられるとしたが、例えば、凸部52は、例えば天面部11a、底面部11cまたは側面部11dに設けられてもよい。より具体的に説明すると、凸部52が、中空部材10Cの部材長手方向Xの一部における同一断面上において天面部11a、底面部11c、または側面部11dに設けられた場合、中空部材10Cの部材長手方向Xにおける断面係数は、凸部52が設けられた部分で変化するので、中空部材10Cの曲げが、凸部52が設けられた部分において生じ得る。したがって、この場合においても、凸部52は曲げ誘起部となる。 In the example illustrated in FIG. 22, the protrusion 52 is provided on the side surface 11 b, but the protrusion 52 may be provided on, for example, the top surface 11 a, the bottom surface 11 c, or the side surface 11 d. More specifically, when the convex portion 52 is provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d on the same cross section in a part of the hollow member 10C in the member longitudinal direction X, the hollow member 10C Since the section modulus in the member longitudinal direction X changes at the portion where the convex portion 52 is provided, bending of the hollow member 10C may occur at the portion where the convex portion 52 is provided. Therefore, also in this case, the convex portion 52 becomes a bending inducing portion.
 また、凸部の形状および配置については、上述した例に限られない。図23~図26は、本実施形態に係る中空部材10Cに設けられる凸部の他の例を示す模式図である。ここでいう凸部は、例えば、中空部材10Cの加工等により実現される。すなわち、かかる凸部は、中空部材10Cを構成する鋼板の一部を変形させて設けられるものであってもよい。図23に示すように、円形の凸部52aが側面部11bに設けられてもよい。 Further, the shape and arrangement of the convex portions are not limited to the above-described example. FIGS. 23 to 26 are schematic views showing other examples of the convex portion provided on the hollow member 10C according to the present embodiment. The convex portion here is realized, for example, by processing the hollow member 10C. That is, such a convex portion may be provided by deforming a part of the steel plate constituting the hollow member 10C. As shown in FIG. 23, a circular convex portion 52a may be provided on the side surface portion 11b.
 また、図24に示すように、複数の凸部52bが側面部11bに設けられてもよい。この場合、例えば、複数の凸部52bが、中空部材10Cの部材長手方向Xに横切る方向に並んで設けられてもよい。この場合、衝突荷重の入力時において、中空部材10Cの部材長手方向Xにおける複数の凸部52bの前後の領域のいずれかが曲げの起点として、中空部材10Cが側面部11b側に曲げ変形しやすくなる。 Also, as shown in FIG. 24, a plurality of protrusions 52b may be provided on the side surface 11b. In this case, for example, a plurality of convex portions 52b may be provided side by side in a direction crossing the member longitudinal direction X of the hollow member 10C. In this case, at the time of input of a collision load, any one of the regions before and after the plurality of protrusions 52b in the member longitudinal direction X of the hollow member 10C serves as a starting point of bending, and the hollow member 10C is easily bent and deformed toward the side surface 11b. Become.
 また、図25に示すように、中空部材10Cの部材長手方向Xに横切る方向に延在する凸部52cが側面部11bに設けられてもよい。この場合、衝突荷重の入力時において、中空部材10Cの部材長手方向Xにおける凸部52cの前後の領域のいずれかが曲げの起点として、中空部材10Cが側面部11b側に曲げ変形される。なお、凸部52cの形状は、図25に示す角丸矩形に限定されず、あらゆる形状であってもよい。なお、上述した中空部材10Cの部材長手方向Xに横切る方向は、図25に示すような、中空部材10Cの部材長手方向Xに直交する方向に限定されない。また、凸部52の設けられる部分は側面部11bに限られない。例えば、天面部11a、底面部11c、または側面部11dに凸部52が設けられてもよい。 As shown in FIG. 25, a protrusion 52c extending in a direction crossing the member longitudinal direction X of the hollow member 10C may be provided on the side surface 11b. In this case, at the time of input of a collision load, the hollow member 10C is bent and deformed toward the side surface portion 11b with any one of the regions before and after the convex portion 52c in the member longitudinal direction X of the hollow member 10C as a starting point of bending. The shape of the projection 52c is not limited to the rounded rectangle shown in FIG. 25, and may be any shape. It should be noted that the direction transverse to the member longitudinal direction X of the hollow member 10C described above is not limited to the direction orthogonal to the member longitudinal direction X of the hollow member 10C as shown in FIG. Further, the portion where the convex portion 52 is provided is not limited to the side surface portion 11b. For example, the projection 52 may be provided on the top surface 11a, the bottom surface 11c, or the side surface 11d.
 また、図26に示すように、凸部52dが稜線部11eに設けられてもよい。これにより、中空部材10Cのうち部材長手方向Xで凸部52dが設けられた部分の断面係数が顕著に変化するので、凸部52dが設けられた部分が曲げの起点として曲げ変形しやすくなる。 凸 Also, as shown in FIG. 26, the projection 52d may be provided on the ridge 11e. Thereby, the section modulus of the portion of the hollow member 10C where the convex portion 52d is provided in the member longitudinal direction X changes remarkably, so that the portion where the convex portion 52d is provided easily bends as a starting point of bending.
 図27は、本実施形態に係る中空部材10Cに設けられる凸部の他の例を示す模式図である。図27に示すように、中空部材10Cの部材長手方向Xに延在する凸部52e、52fが、中空部材10Cの部材長手方向Xに沿って並んで設けられてもよい。この場合、中空部材10Cのうち、部材長手方向Xにおける凸部52eと凸部52fとの間の部分520で曲げが生じる。すなわち、中空部材10Cのうち、凸部52e、52fが設けられた部分と、凸部52eと凸部52fとの間の部分520とでは断面係数が異なるので、衝突荷重の入力時において、当該部分520を曲げの起点として曲げ変形が生じる。また、当該部分520には、上述した凹部、凸部または後述する薄肉部もしくは異強度部等が形成されていてもよい。なお、凸部52eおよび凸部52fは、図27に示すように、必ずしも直列に並んでいなくてもよい。また、凸部52eおよび凸部52fは、必ずしも中空部材10Cの部材長手方向Xに延在していなくてもよい。 FIG. 27 is a schematic view showing another example of the projection provided on the hollow member 10C according to the present embodiment. As shown in FIG. 27, the convex portions 52e and 52f extending in the member longitudinal direction X of the hollow member 10C may be provided side by side along the member longitudinal direction X of the hollow member 10C. In this case, bending occurs in a portion 520 of the hollow member 10C between the convex portion 52e and the convex portion 52f in the member longitudinal direction X. That is, in the hollow member 10C, the section provided with the projections 52e and 52f and the section 520 between the projection 52e and the projection 52f have different cross-sectional coefficients. Bending deformation occurs with 520 as the starting point of bending. Further, in the portion 520, the above-described concave portion, convex portion, or a thin portion or a different strength portion described later may be formed. In addition, the convex part 52e and the convex part 52f do not necessarily need to be lined up in series, as shown in FIG. In addition, the protrusion 52e and the protrusion 52f do not necessarily need to extend in the member longitudinal direction X of the hollow member 10C.
(板厚変化部・薄肉部)
 また、側面部11bには曲げ誘起部を実現する構成として板厚変化部が設けられてもよい。図28は、本実施形態に係る中空部材10Dに設けられる板厚変化部の一例を示す模式図である。ここでいう板厚変化部とは、中空部材10Dの部材長手方向Xにおいて板厚が変化する部分を意味する。図28に示すように、中空部材10Dは、第1板厚部111および第2板厚部112を備える。第1板厚部111は中空部材10Dの端部側に設けられ、第2板厚部112は、中空部材10Dの部材長手方向Xに沿って第1板厚部111と連続して設けられる。第1板厚部111と第2板厚部112との間では、鋼板の板厚が異なる。板厚の大小関係については特に限定されない。
(Thickness change part / thin part)
Further, the side surface portion 11b may be provided with a plate thickness changing portion as a configuration for realizing the bending inducing portion. FIG. 28 is a schematic diagram illustrating an example of a plate thickness changing portion provided in the hollow member 10D according to the present embodiment. Here, the plate thickness change portion means a portion where the plate thickness changes in the member longitudinal direction X of the hollow member 10D. As shown in FIG. 28, the hollow member 10D includes a first thick part 111 and a second thick part 112. The first thick part 111 is provided on the end side of the hollow member 10D, and the second thick part 112 is provided continuously with the first thick part 111 along the member longitudinal direction X of the hollow member 10D. The thickness of the steel plate differs between the first plate thickness portion 111 and the second plate thickness portion 112. The relationship between the plate thicknesses is not particularly limited.
 この場合、図28に示すように、第1板厚部111と第2板厚部112との境目の部分が板厚変化部113となる。この板厚変化部113において中空部材10Dの部材長手方向Xでの断面係数が変化する。すなわち、板厚変化部113が曲げ誘起部に相当する。したがって、衝突荷重が中空部材10Dに入力された場合、中空部材10Dは板厚変化部113において屈曲する。 In this case, as shown in FIG. 28, the boundary between the first plate thickness portion 111 and the second plate thickness portion 112 becomes the plate thickness change portion 113. The section modulus of the hollow member 10D in the member longitudinal direction X changes in the plate thickness changing portion 113. That is, the thickness change portion 113 corresponds to a bending inducing portion. Therefore, when a collision load is input to the hollow member 10D, the hollow member 10D bends at the plate thickness change portion 113.
 また、曲げ誘起部は、例えば、薄肉部により実現されてもよい。図29は、本実施形態に係る中空部材10Dに設けられる薄肉部の一例を示す模式図である。図29に示すように、側面部11bには、中空部材10Dの部材長手方向X前後において、他の部分よりも相対的に板厚が薄い薄肉部114が設けられている。薄肉部114を含む部分における中空部材10Dの断面係数は、薄肉部114が設けられた部分の前後における部分の中空部材10Dの断面係数よりも低い。すなわち、中空部材10Dのうち薄肉部114が設けられた部分が曲げ誘起部に相当する。したがって、衝突荷重が中空部材10Dに入力された場合、中空部材10Dは薄肉部114が設けられた部分において、薄肉部114が曲げ内側となるように屈曲する。 曲 げ The bending inducing section may be realized by, for example, a thin wall section. FIG. 29 is a schematic diagram illustrating an example of a thin portion provided in the hollow member 10D according to the present embodiment. As shown in FIG. 29, a thin portion 114 having a relatively smaller thickness than other portions is provided on the side surface portion 11b in the longitudinal direction X of the hollow member 10D. The section modulus of the hollow member 10D in the portion including the thin portion 114 is lower than the section modulus of the hollow member 10D in the portion before and after the portion in which the thin portion 114 is provided. That is, the portion of the hollow member 10D where the thin portion 114 is provided corresponds to the bending inducing portion. Therefore, when a collision load is input to the hollow member 10D, the hollow member 10D bends at the portion where the thin portion 114 is provided so that the thin portion 114 is bent inside.
  かかる板厚変化部を有する中空部材10Dは、例えば、切削、プレス、およびテーラードブランクからなる被加工板により形成されてもよい。かかる被加工板は、溶接線を有するテーラーウェルドブランク(Tailor  Welded  Blank;TWB)であってもよい。また、上記被加工板は、圧延ロールにより板厚を異ならせて設けられるテーラーロールドブランク(Tailor  Rolled  Blank;TRB)であってもよい。TWBにおいては、板厚変化部における差厚は0.2mm以上とすることが可能である。また、TRBにおいては、部材長手方向当たりの板厚変化部における板厚変化量は、0.1mm/100mm以上とすることが可能である。 中空 The hollow member 10D having such a plate thickness change portion may be formed by, for example, a work plate made of cutting, pressing, and tailored blank. Such a work plate may be a tailor weld blank (TWB) having a weld line. Further, the plate to be processed may be a tailor rolled blank (TRB) provided in a manner that the plate thickness is varied by a rolling roll. In the case of TWB, the difference thickness at the plate thickness change portion can be 0.2 mm or more. In the TRB, the thickness change amount in the thickness change portion per the longitudinal direction of the member can be 0.1 mm / 100 mm or more.
(異強度部・強度変化部)
 図30は、本実施形態に係る中空部材10Eに設けられる異強度部の例を説明するための中空部材10Eの断面図である。図30に示すように、側面部11bには異強度部53が設けられている。異強度部53は、例えば、中空部材10Eに対して部分的に溶接、焼き入れまたは焼き戻し等の熱処理等を行うことにより設けられる。異強度部53が設けられた部分における中空部材10Eの降伏強度は、異強度部53が設けられた部分の前後における部分の中空部材10Eの降伏強度とは異なる。したがって、図30に示す衝突荷重Fが中空部材10Eに入力された場合、異強度部53または異強度部53の近傍において、異強度部53が曲げ内側となるように屈曲する。すなわち、中空部材10Eの部材長手方向Xにおいて、中空部材10Eのうち異強度部53を含む部分が、中空部材10Eに設けられる曲げ誘起部となる。この屈曲は、異強度部53または異強度部53の近傍の領域が塑性変形することにより生じる屈曲である。
(Different strength part / Strength change part)
FIG. 30 is a cross-sectional view of the hollow member 10E for explaining an example of the different strength portion provided in the hollow member 10E according to the present embodiment. As shown in FIG. 30, a different strength portion 53 is provided on the side surface portion 11b. The different strength portion 53 is provided, for example, by partially performing heat treatment such as welding, quenching, or tempering on the hollow member 10E. The yield strength of the hollow member 10E at the portion where the different strength portion 53 is provided is different from the yield strength of the hollow member 10E at the portion before and after the portion where the different strength portion 53 is provided. Therefore, when the collision load F shown in FIG. 30 is input to the hollow member 10E, the different-strength portion 53 is bent so as to be inside the different-strength portion 53 or in the vicinity of the different-strength portion 53. That is, in the member longitudinal direction X of the hollow member 10E, a portion including the different strength portion 53 of the hollow member 10E becomes a bending inducing portion provided in the hollow member 10E. This bending is a bending caused by plastic deformation of the different strength portion 53 or a region near the different strength portion 53.
 なお、図30に示した例では、側面部11bに異強度部53が設けられるとしたが、異強度部53は、例えば天面部11a、底面部11c、または側面部11dに設けられてもよい。より具体的に説明すると、異強度部53が、中空部材10の部材長手方向Xの一部における同一断面上において天面部11a、底面部11c、または側面部11dに設けられた場合、当該断面上において側面部11bの強度が最も低くなる。そうすると、側面部11bを曲げ内側とする中空部材10Eの曲げが、異強度部53において生じ得る。したがって、この場合においても、異強度部53は曲げ誘起部となる。 In the example shown in FIG. 30, the different strength portion 53 is provided on the side surface portion 11b, but the different strength portion 53 may be provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d, for example. . More specifically, when the different strength portion 53 is provided on the top surface portion 11a, the bottom surface portion 11c, or the side surface portion 11d on the same cross section in a part of the hollow member 10 in the member longitudinal direction X, In this case, the strength of the side surface portion 11b is lowest. Then, bending of the hollow member 10 </ b> E with the side surface portion 11 b bent inside may occur in the different strength portion 53. Therefore, also in this case, the different strength portion 53 becomes a bending inducing portion.
 また、異強度部の配置については、上述した例に限られない。図31、図32は、本実施形態に係る中空部材10Eに設けられる異強度部の他の例を示す模式図である。ここでいう異強度部は、中空部材10Eを形成する被加工板に対する溶接または熱処理等により実現される。 配置 Also, the arrangement of the different strength portions is not limited to the example described above. FIG. 31 and FIG. 32 are schematic diagrams illustrating another example of the different strength portion provided in the hollow member 10E according to the present embodiment. The different strength portion here is realized by welding, heat treatment, or the like to the work plate forming the hollow member 10E.
 図31に示すように、中空部材10Eの部材長手方向Xに対する断面周方向に沿って異強度部120が設けられている。この場合も、中空部材10Eのうち異強度部120が設けられた部分が曲げ誘起部に相当する。したがって、衝突荷重が中空部材10Eに入力された場合、中空部材10Eは異強度部120が設けられた部分において、異強度部120が曲げ内側となるように屈曲する。 異 As shown in FIG. 31, different strength portions 120 are provided along the circumferential direction of the cross section with respect to the member longitudinal direction X of the hollow member 10E. Also in this case, the portion of the hollow member 10E where the different strength portion 120 is provided corresponds to the bending inducing portion. Therefore, when a collision load is input to the hollow member 10E, the hollow member 10E bends at the portion where the different strength portion 120 is provided so that the different strength portion 120 is bent inside.
 なお、かかる異強度部は、例えば、図32に示したように、側面部11b等、中空部材10Eの断面を構成する壁部の少なくともいずれかに部分的に設けられてもよい。かかる場合においても、衝突荷重が中空部材10Eに入力された場合、中空部材10Eは異強度部121が設けられた部分において、異強度部121が曲げ内側となるように屈曲する。 Note that, as shown in FIG. 32, the different strength portion may be partially provided on at least one of the wall portions constituting the cross section of the hollow member 10E, such as the side surface portion 11b. Even in such a case, when a collision load is input to the hollow member 10E, the hollow member 10E bends at a portion where the different strength portion 121 is provided so that the different strength portion 121 is bent inside.
 また、曲げ誘起部は、例えば、強度変化部により実現されてもよい。図33は、本実施形態に係る中空部材10Eに設けられる強度変化部の一例を示す模式図である。図33に示すように、中空部材10Eは、第1強度部122および第2強度部123を備える。第1強度部122は中空部材10Eの端部側に設けられ、第2強度部123は、中空部材10Eの部材長手方向Xに沿って第1強度部122と連続して設けられる。第1強度部122と第2強度部123との間では、鋼板の降伏強度が異なる。降伏強度の大小関係については特に限定されない。 曲 げ The bending inducing section may be realized by, for example, a strength changing section. FIG. 33 is a schematic diagram illustrating an example of a strength changing portion provided in the hollow member 10E according to the present embodiment. As shown in FIG. 33, the hollow member 10E includes a first strength part 122 and a second strength part 123. The first strength portion 122 is provided on the end side of the hollow member 10E, and the second strength portion 123 is provided continuously with the first strength portion 122 along the member longitudinal direction X of the hollow member 10E. The yield strength of the steel sheet differs between the first strength part 122 and the second strength part 123. The magnitude relation of the yield strength is not particularly limited.
 この場合、図33に示すように、第1強度部122と第2強度部123との境目の部分が強度変化部124となる。この強度変化部124において中空部材10Eの部材長手方向Xでの降伏強度が変化する。すなわち、強度変化部124が曲げ誘起部に相当する。したがって、衝突荷重が中空部材10Eに入力された場合、中空部材10Eは強度変化部124において屈曲する。 In this case, as shown in FIG. 33, the boundary between the first strength part 122 and the second strength part 123 becomes the strength change part 124. In the strength changing portion 124, the yield strength of the hollow member 10E in the member longitudinal direction X changes. That is, the strength changing section 124 corresponds to a bending inducing section. Therefore, when a collision load is input to the hollow member 10E, the hollow member 10E bends at the strength changing portion 124.
(組み合わせ)
 上記に示した曲げ誘起部の例が複数組み合わせられていてもよい。例えば、上述した凹部、凸部、穴部、板厚変化部、薄肉部、異強度部および強度変化部の少なくとも2つ以上の組み合わせにより、曲げ誘起部が実現されてもよい。
(combination)
A plurality of examples of the bending inducing section shown above may be combined. For example, a bending inducing portion may be realized by a combination of at least two or more of the above-described concave portion, convex portion, hole portion, plate thickness changing portion, thin portion, different strength portion, and strength changing portion.
(適用対象部材の例)
 本実施形態の中空部材は、例えば、衝撃吸収機能が求められる車両構造部材であるフロントサイドメンバ、リアサイドメンバ、エクステンション又はクラッシュボックスなどに適用することができる。
(Example of applicable material)
The hollow member of the present embodiment can be applied to, for example, a front side member, a rear side member, an extension, a crash box, or the like, which is a vehicle structural member required to have an impact absorbing function.
  以上、添付図面を参照しながら本発明の一実施形態について詳細に説明したが、本発明はかかる例に限定されない。本発明の属する技術の分野における通常の知識を有する者であれば、特許請求の範囲に記載された技術的思想の範疇内において、各種の変更例または修正例に想到し得ることは明らかであり、これらについても、当然に本発明の技術的範囲に属するものと了解される。 Although the embodiments of the present invention have been described in detail with reference to the accompanying drawings, the present invention is not limited to the embodiments. It is apparent that those skilled in the art to which the present invention pertains can conceive various changes or modifications within the scope of the technical idea described in the appended claims. It is understood that these also belong to the technical scope of the present invention.
 本発明に係るフレームのエネルギー吸収性能を評価するため、衝突シミュレーションを実施した。解析モデルは図1~図3に示すようなバンパービームとフレームで構成されており、中空部材の断面は矩形状であり、外形寸法は幅76mm、高さ200mmとなっている。また、解析モデルは下記表1に示す条件で複数作成されている。なお、表1中の軽量化率は、各構造の重量を構造1の重量で規格化したものである。 衝突 A collision simulation was performed to evaluate the energy absorption performance of the frame according to the present invention. The analysis model is composed of a bumper beam and a frame as shown in FIGS. 1 to 3, the cross section of the hollow member is rectangular, and the outer dimensions are 76 mm in width and 200 mm in height. In addition, a plurality of analysis models are created under the conditions shown in Table 1 below. The weight reduction rate in Table 1 is obtained by standardizing the weight of each structure by the weight of the structure 1.
Figure JPOXMLDOC01-appb-T000001
Figure JPOXMLDOC01-appb-T000001
 上記表1の構造1および構造2は、補強部材20が設けられていない構造であり、構造2は構造1に対して薄板化、およびハイテン化を図ったものである。構造3~構造10は、図4に示すような複数の補強部材20が中空部材10の部材長手方向Xに沿って配置された構造であり、補強部材20の素材はCFRPであり、その板厚は0.8mmである。構造3においては、隣り合う補強部材20の間隔がランダムとなっており、各補強部材20の間隔は互いに異なっている。構造4~構造8においては、補強部材20が中空部材10の部材長手方向Xの全域に配置されており、各補強部材20の間隔は一定間隔となっている。構造9においては、図9のように補強部材20が中空部材10の部材長手方向Xの前部にのみ配置されており、各補強部材20の間隔は一定間隔となっている。構造10においては、図10のように補強部材20が中空部材10の部材長手方向Xの全域に配置されているが、中空部材10の前部に配置された補強部材20の間隔と、中空部材10の後部に配置された補強部材20の間隔が異なっている。 構造 Structures 1 and 2 in Table 1 above are structures in which the reinforcing member 20 is not provided, and structure 2 is a structure in which the thickness and thickness of the structure 1 are reduced. Structures 3 to 10 are structures in which a plurality of reinforcing members 20 as shown in FIG. 4 are arranged along the member longitudinal direction X of the hollow member 10, the material of the reinforcing member 20 is CFRP, and its plate thickness is Is 0.8 mm. In the structure 3, the interval between the adjacent reinforcing members 20 is random, and the interval between the reinforcing members 20 is different from each other. In the structures 4 to 8, the reinforcing members 20 are arranged in the entire region of the hollow member 10 in the member longitudinal direction X, and the intervals between the reinforcing members 20 are constant. In the structure 9, as shown in FIG. 9, the reinforcing members 20 are arranged only at the front part of the hollow member 10 in the member longitudinal direction X, and the intervals between the reinforcing members 20 are constant. In the structure 10, as shown in FIG. 10, the reinforcing members 20 are arranged in the entire region in the member longitudinal direction X of the hollow member 10, but the spacing between the reinforcing members 20 arranged in front of the hollow member 10 and the hollow member The spacing between the reinforcing members 20 arranged at the rear of the 10 is different.
 また、構造11は、補強部材20の素材として鋼板を用いたものである。構造12は、補強部材20の板厚を2.8mmに変更した構造である。構造13は、補強部材20の板厚を0.6mmに変更した構造である。構造14は、補強部材20の板厚を3.2mmに変更した構造である。構造15は、補強部材20の素材としてGFRPを用いたものである。構造16は、補強部材20が中空部材10の部材長手方向Xの前部にのみ配置されており、その枚数は2枚である。 構造 The structure 11 uses a steel plate as a material of the reinforcing member 20. The structure 12 is a structure in which the thickness of the reinforcing member 20 is changed to 2.8 mm. The structure 13 is a structure in which the thickness of the reinforcing member 20 is changed to 0.6 mm. The structure 14 is a structure in which the thickness of the reinforcing member 20 is changed to 3.2 mm. The structure 15 uses GFRP as a material of the reinforcing member 20. In the structure 16, the reinforcing members 20 are arranged only at the front part of the hollow member 10 in the member longitudinal direction X, and the number thereof is two.
 構造3~10、12~14、16において補強部材20として用いられるCFRPの機械特性は以下の通りである。
 Vf(繊維含有体積率):50%
 ヤング率:102GPa
 破断強度:1500MPa
 破断伸び:1.5%
The mechanical properties of CFRP used as the reinforcing member 20 in the structures 3 to 10, 12 to 14, and 16 are as follows.
Vf (fiber content volume ratio): 50%
Young's modulus: 102 GPa
Breaking strength: 1500 MPa
Elongation at break: 1.5%
 また、構造11において補強部材20として用いられる鋼板の機械特性は以下の通りである。
 引張強さ:440MPa
 破断伸び:28%
 また、構造15において補強部材20として用いられるGFRPの機械特性は以下の通りである。
 Vf(繊維含有体積率):50%
 ヤング率:13GPa
 破断強度:200MPa
 破断伸び:3.0%
The mechanical properties of the steel sheet used as the reinforcing member 20 in the structure 11 are as follows.
Tensile strength: 440MPa
Elongation at break: 28%
The mechanical properties of the GFRP used as the reinforcing member 20 in the structure 15 are as follows.
Vf (fiber content volume ratio): 50%
Young's modulus: 13 GPa
Breaking strength: 200MPa
Elongation at break: 3.0%
  本シミュレーションは、自動車の正面衝突試験を模擬したものであり、質量200kgの剛体壁を図1~図3に示すバンパービーム40に12m/sで衝突させることで実施された。各解析モデルにおける中空部材10の後端10bは拘束されている。以下、シミュレーション結果について説明する。 This simulation simulates a frontal collision test of an automobile, and was performed by colliding a rigid wall having a mass of 200 kg with the bumper beam 40 shown in FIGS. 1 to 3 at 12 m / s. The rear end 10b of the hollow member 10 in each analysis model is restricted. Hereinafter, simulation results will be described.
 なお、上記表1には、シミュレーション結果として各解析モデルの変形モードを示している。表1に示す変形モードにおける“横折れ”とは、中空部材10の変形初期から横折れ変形が生じる変形モードである。表1に示す変形モードにおける“不安定軸圧潰”とは、中空部材10の圧潰変形の発生箇所が部材長手方向Xにおいて不規則に存在し、圧潰変形の発生箇所が中空部材10の前端10aから後端10bにかけて連続していない変形モードである。表1に示す変形モードにおける“安定軸圧潰”とは、中空部材10の圧潰変形が部材長手方向Xに沿って徐々に進行し、圧潰変形の発生箇所が前端10aから後端10bにかけて連続する変形モードである。 In addition, Table 1 shows the deformation mode of each analysis model as a simulation result. The “lateral bending” in the deformation mode shown in Table 1 is a deformation mode in which a horizontal bending deformation occurs from the initial deformation of the hollow member 10. The “unstable axial crush” in the deformation mode shown in Table 1 means that the crushing deformation of the hollow member 10 is irregularly present in the member longitudinal direction X, and the crushing deformation occurs from the front end 10a of the hollow member 10. This is a deformation mode that is not continuous toward the rear end 10b. “Stable axial crushing” in the deformation mode shown in Table 1 means that the crushing deformation of the hollow member 10 gradually progresses along the member longitudinal direction X, and the crushing deformation occurs continuously from the front end 10a to the rear end 10b. Mode.
 図34は衝突シミュレーションにおける構造1の解析モデルの変形途中の状態を示す平面図であり、図35は衝突シミュレーションにおける構造1の解析モデルの変形後の状態を示す平面図である。図34および図35に示すように、補強部材が設けられていない構造1においては、荷重が入力されると、中空部材に横折れが生じた。このような中空部材の変形は、構造2、構造3、構造11、構造16においても生じていた。 FIG. 34 is a plan view showing a state in which the analysis model of the structure 1 is being deformed in the collision simulation, and FIG. 35 is a plan view showing a state after the deformation of the analysis model of the structure 1 in the collision simulation. As shown in FIGS. 34 and 35, in the structure 1 in which the reinforcing member is not provided, when a load is input, the hollow member is horizontally bent. Such a deformation of the hollow member has also occurred in the structure 2, the structure 3, the structure 11, and the structure 16.
 図36は衝突シミュレーションにおける構造4の解析モデルの変形途中の状態を示す平面図であり、図37は衝突シミュレーションにおける構造4の解析モデルの変形後の状態を示す平面図である。図36に示すように、中空部材には、変形初期において、前端近傍以外に後端近傍にも圧潰変形が生じてしまい、変形モードが不安定軸圧潰となった。また、図37に示すように、中空部材の変形がさらに進行すると、中空部材の中央部に横折れが生じた。このような中空部材の変形は、構造5、構造13、構造14においても生じていた。 FIG. 36 is a plan view showing a state in which the analysis model of the structure 4 is being deformed in the collision simulation, and FIG. 37 is a plan view showing a state after deformation of the analysis model of the structure 4 in the collision simulation. As shown in FIG. 36, in the initial stage of deformation of the hollow member, crushing deformation occurred not only near the front end but also near the rear end, and the deformation mode became unstable axial crushing. Further, as shown in FIG. 37, when the deformation of the hollow member further progressed, the center portion of the hollow member was horizontally bent. Such deformation of the hollow member has also occurred in the structure 5, the structure 13, and the structure 14.
 一方、図38は衝突シミュレーションにおける構造7の解析モデルの変形途中の状態を示す平面図であり、図39は衝突シミュレーションにおける構造7の解析モデルの変形後の状態を示す平面図である。図38および図39に示すように、構造7では、中空部材の変形過程において安定的に圧潰変形が生じている。中空部材の変形モードが横折れ変形である場合、中空部材の横折れ部以外の部分に生じる塑性ひずみが小さいために、横折れ部以外の部分はエネルギー吸収性能の向上にほぼ寄与しないが、構造7のように変形モードが安定軸圧潰である場合には、塑性ひずみが生じる部分が多くなり、エネルギー吸収性能を向上させることが可能となる。このような中空部材の変形は構造6、構造8~10、構造12、構造15においても生じていた。 38, on the other hand, FIG. 38 is a plan view showing a state in which the analysis model of the structure 7 is being deformed in the collision simulation, and FIG. 39 is a plan view showing a state after deformation of the analysis model of the structure 7 in the collision simulation. As shown in FIGS. 38 and 39, in the structure 7, the crush deformation is stably generated in the deformation process of the hollow member. When the deformation mode of the hollow member is lateral bending deformation, the plastic strain generated in the portion other than the horizontal bent portion of the hollow member is small, so the portion other than the horizontal bent portion hardly contributes to the improvement of the energy absorption performance. In the case where the deformation mode is stable axial crushing as in 7, the portion where plastic strain occurs increases, and the energy absorption performance can be improved. Such deformation of the hollow member has also occurred in Structure 6, Structures 8 to 10, Structure 12, and Structure 15.
 次に、剛体壁を衝突させた際の荷重‐ストローク線図から、剛体壁の750mmストローク時におけるエネルギー吸収量を算出し、各解析モデルのエネルギー吸収性能を比較した。その結果を図40に示す。なお、図40のグラフの縦軸は、各構造におけるエネルギー吸収量と構造1のエネルギー吸収量との比である。 Next, from the load-stroke diagram when the rigid body wall collided, the amount of energy absorption at the time of the 750 mm stroke of the rigid body wall was calculated, and the energy absorption performance of each analysis model was compared. The result is shown in FIG. Note that the vertical axis of the graph in FIG. 40 is the ratio between the amount of energy absorbed in each structure and the amount of energy absorbed in Structure 1.
 図40に示すように、荷重入力時に安定して軸圧潰変形が生じていた構造6~構造10、構造12、15においては、構造1に対してエネルギー吸収性能が向上している。また、上記表1に示すように構造6~構造10においては、構造1に対する軽量化率も大きい。したがって、本シミュレーションの結果によれば、各補強部材の間隔が中空部材の外形寸法上の最小幅Wminの0.74倍~1.84倍の範囲内である場合には、軽量化を図りつつ、安定的に軸圧潰変形を発生させてエネルギー吸収性能を向上させることができる。 As shown in FIG. 40, in the structures 6 to 10, the structures 12, and 15 in which the axial crushing deformation is stably generated when a load is input, the energy absorption performance is improved as compared with the structure 1. Further, as shown in Table 1 above, in the structures 6 to 10, the weight reduction ratio with respect to the structure 1 is large. Therefore, according to the result of this simulation, when the interval between the reinforcing members is within the range of 0.74 times to 1.84 times the minimum width W min of the external dimensions of the hollow member, the weight is reduced. At the same time, it is possible to stably generate axial crush deformation and improve the energy absorption performance.
 また、上記表1に示すように、構造11においては、中空部材に横折れが生じたことに加え、構造1に対する軽量化率が低く、エネルギー吸収性能も向上していない。即ち、本発明に係る構成において、補強部材の素材として鋼板を用いるのは好ましくないといえる。 In addition, as shown in Table 1 above, in the structure 11, in addition to the horizontal bending of the hollow member, the weight reduction ratio with respect to the structure 1 was low, and the energy absorption performance was not improved. That is, in the configuration according to the present invention, it can be said that it is not preferable to use a steel plate as the material of the reinforcing member.
 また、構造12~14を比較すると、補強部材の板厚が2.8mmである場合(構造12)には変形モードが安定軸圧潰であるのに対し、補強部材の板厚が0.6mmである場合(構造13)や3.2mmである場合(構造14)には変形モードが不安定軸圧潰である。即ち、本発明に係る構成において、補強部材としてのCFRP部材の板厚は0.8mm~2.8mmが好ましいといえる。 When the structures 12 to 14 are compared, when the plate thickness of the reinforcing member is 2.8 mm (structure 12), the deformation mode is stable axial crushing, whereas when the plate thickness of the reinforcing member is 0.6 mm. In some cases (Structure 13) or 3.2 mm (Structure 14), the deformation mode is unstable axial crush. That is, in the configuration according to the present invention, it can be said that the plate thickness of the CFRP member as the reinforcing member is preferably 0.8 mm to 2.8 mm.
 また、構造15においては、補強部材の素材としてGFRPを用いている。この場合、変形モードは安定軸圧潰であり、構造1に対してエネルギー吸収性能が向上している。即ち、本発明に係る構成において、補強部材の素材としてGFRPを用いることも有効であると言える。 構造 In the structure 15, GFRP is used as a material of the reinforcing member. In this case, the deformation mode is stable axial crush, and the energy absorption performance is improved with respect to the structure 1. That is, in the configuration according to the present invention, it can be said that the use of GFRP as the material of the reinforcing member is also effective.
 また、構造16においては、中空部材に配置する補強部材の数を2枚としている。この場合、変形モードが横折れであり、エネルギー吸収性能も向上していない。即ち、本発明に係る構成において、配置する補強部材の数は3枚以上とすることが好ましいと言える。 構造 In the structure 16, the number of reinforcing members arranged in the hollow member is two. In this case, the deformation mode is lateral bending, and the energy absorption performance is not improved. That is, in the configuration according to the present invention, it can be said that the number of reinforcing members to be arranged is preferably three or more.
 本発明は、車両用構造部材に適用できる。 The present invention is applicable to structural members for vehicles.
1    フレーム
10   中空部材
10a  中空部材の前端
10b  中空部材の後端
11a  中空部材の天面部
11b、11d  中空部材の側面部
11c  中空部材の底面部
11e~11h  中空部材の稜線部
20   補強部材
20a  補強部材の板面
21a~21d  補強部材のフランジ
30   クラッシュボックス
40   バンパービーム
max   中空部材の外形寸法上の最大幅
min   中空部材の外形寸法上の最小幅
1 Frame 10 Hollow member 10a Front end 10b of hollow member Rear end 11a of hollow member Top surface 11b of hollow member 11d Side surface of hollow member 11c Bottom portions 11e to 11h of hollow member Ridge line portion of hollow member 20 Reinforcement member 20a Reinforcement member Plate surfaces 21a to 21d of the reinforcing member Flange 30 of the reinforcing member Crash box 40 Bumper beam W max Maximum width on the external dimensions of the hollow member W min Minimum width on the external dimensions of the hollow member

Claims (7)

  1. 金属製の中空部材と、
     前記中空部材の内面に各辺が接合され、該中空部材の内方空間を隔てるように該中空部材の部材長手方向に沿って間隔をおいて複数配置された、FRPからなる板状の補強部材とを備え、
     前記中空部材の部材長手方向に垂直な断面において、該中空部材の外形寸法上の最小幅は、該中空部材の外形寸法上の最大幅の30%以上であり、
     各補強部材は、該補強部材の板面が前記中空部材の部材長手方向に垂直となる向きで、かつ前記中空部材の部材長手方向の端部から、前記最小幅の0.74倍~1.84倍の間隔でもって3枚以上配置され、
     前記補強部材の板厚は0.7~3.0mmである、車両用構造部材。
    A metal hollow member,
    A plate-like reinforcing member made of FRP, each side of which is joined to an inner surface of the hollow member and a plurality of which are arranged at intervals along a member longitudinal direction of the hollow member so as to separate an inner space of the hollow member. With
    In a cross section perpendicular to the member longitudinal direction of the hollow member, the minimum width of the hollow member in external dimensions is 30% or more of the maximum width of the hollow member in external dimensions,
    Each reinforcing member has a direction in which the plate surface of the reinforcing member is perpendicular to the longitudinal direction of the hollow member, and is 0.74 times to 1. Three or more are arranged at 84 times interval,
    A structural member for a vehicle, wherein the reinforcing member has a plate thickness of 0.7 to 3.0 mm.
  2. 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、
     前記曲げ誘起部に配置された前記補強部材の間隔が、前記曲げ誘起部以外の部分に配置された前記補強部材の間隔よりも狭い、請求項1に記載の車両用構造部材。
    The hollow member has a bending inducing part in a part in the member longitudinal direction,
    The vehicle structural member according to claim 1, wherein an interval between the reinforcing members arranged in the bending inducing section is smaller than an interval between the reinforcing members arranged in a portion other than the bending inducing section.
  3. 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、
     前記曲げ誘起部に配置された前記補強部材の板厚が、前記曲げ誘起部以外の部分に配置された前記補強部材の板厚よりも厚い、請求項1または2に記載の車両用構造部材。
    The hollow member has a bending inducing part in a part in the member longitudinal direction,
    The structural member for a vehicle according to claim 1, wherein a thickness of the reinforcing member disposed in the bending inducing portion is larger than a thickness of the reinforcing member disposed in a portion other than the bending inducing portion.
  4. 前記中空部材は、部材長手方向における一部に曲げ誘起部を有し、
     前記曲げ誘起部に配置された前記補強部材の引張強さが、前記曲げ誘起部以外の部分に配置された前記補強部材の引張強さよりも大きい、請求項1~3のいずれか一項に記載の車両用構造部材。
    The hollow member has a bending inducing part in a part in the member longitudinal direction,
    4. The reinforcing member according to claim 1, wherein a tensile strength of the reinforcing member arranged at the bending inducing portion is larger than a tensile strength of the reinforcing member arranged at a portion other than the bending inducing portion. Vehicle structural member.
  5. 前記FRPは、CFRPまたはGFRPである、請求項1~4のいずれか一項に記載の車両用構造部材。 The vehicle structural member according to any one of claims 1 to 4, wherein the FRP is CFRP or GFRP.
  6. 前記中空部材の引張強さは、980MPa以上である、請求項1~5のいずれか一項に記載の車両用構造部材。 The structural member for a vehicle according to any one of claims 1 to 5, wherein the hollow member has a tensile strength of 980 MPa or more.
  7. フロントサイドメンバ、リアサイドメンバ、エクステンション、クラッシュボックスのいずれかである、請求項1~6のいずれか一項に記載の車両用構造部材。 The vehicle structural member according to any one of claims 1 to 6, which is any one of a front side member, a rear side member, an extension, and a crash box.
PCT/JP2019/028507 2018-07-20 2019-07-19 Vehicle structural member WO2020017645A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3901006A1 (en) * 2020-04-21 2021-10-27 Benteler Automobiltechnik GmbH Motor vehicle component

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102486799B1 (en) * 2020-11-18 2023-01-10 한국항공우주연구원 An impact absorption structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07228267A (en) * 1994-02-17 1995-08-29 Mitsubishi Motors Corp Strength member structure of car body
JP2003170860A (en) * 2001-12-05 2003-06-17 Nissan Motor Co Ltd Car body front part structure
JP2015174607A (en) * 2014-03-18 2015-10-05 本田技研工業株式会社 Vehicle body structure
JP2017159894A (en) * 2016-03-03 2017-09-14 新日鐵住金株式会社 Structural member for vehicle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07228267A (en) * 1994-02-17 1995-08-29 Mitsubishi Motors Corp Strength member structure of car body
JP2003170860A (en) * 2001-12-05 2003-06-17 Nissan Motor Co Ltd Car body front part structure
JP2015174607A (en) * 2014-03-18 2015-10-05 本田技研工業株式会社 Vehicle body structure
JP2017159894A (en) * 2016-03-03 2017-09-14 新日鐵住金株式会社 Structural member for vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3901006A1 (en) * 2020-04-21 2021-10-27 Benteler Automobiltechnik GmbH Motor vehicle component
US11492050B2 (en) 2020-04-21 2022-11-08 Benteler Automobiltechnik Gmbh Motor vehicle component

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