[go: up one dir, main page]

CN112192865B - A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor - Google Patents

A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor Download PDF

Info

Publication number
CN112192865B
CN112192865B CN202010969518.1A CN202010969518A CN112192865B CN 112192865 B CN112192865 B CN 112192865B CN 202010969518 A CN202010969518 A CN 202010969518A CN 112192865 B CN112192865 B CN 112192865B
Authority
CN
China
Prior art keywords
composite material
cutting
fiber
transverse
longitudinal
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CN202010969518.1A
Other languages
Chinese (zh)
Other versions
CN112192865A (en
Inventor
吕晓轩
智杰颖
袁立业
杨禹
宋英俊
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanxi Institute of Coal Chemistry of CAS
Original Assignee
Shanxi Institute of Coal Chemistry of CAS
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 Shanxi Institute of Coal Chemistry of CAS filed Critical Shanxi Institute of Coal Chemistry of CAS
Priority to CN202010969518.1A priority Critical patent/CN112192865B/en
Publication of CN112192865A publication Critical patent/CN112192865A/en
Application granted granted Critical
Publication of CN112192865B publication Critical patent/CN112192865B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/521Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement before the die
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/525Component parts, details or accessories; Auxiliary operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545Perforating, cutting or machining during or after moulding

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

本发明属于复合材料制备及无损监测领域,具体涉及一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺。该连续制造工艺包括光纤光栅前处理、碳纤维板材拉挤成型、成型复合材料的裁切以及光纤光栅传感器引线的后处理。该连续化制造工艺有效解决了拉挤成型连续化制造过程中光纤光栅传感器在预定长度上的引线接头难以引出的问题。在保证拉挤成型效率不明显降低的条件下,消除了内置接头方法对复合材料拉挤板材力学性能的不利影响。为智能化拉挤成型复合材料板材的制造及复合材料截面光纤引线的顺利引出提供了一种可靠稳定的方案。

Figure 202010969518

The invention belongs to the field of composite material preparation and non-destructive monitoring, and in particular relates to a continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor. The continuous manufacturing process includes fiber grating pre-processing, carbon fiber sheet pultrusion, cutting of the formed composite material, and post-processing of the fiber grating sensor leads. The continuous manufacturing process effectively solves the problem that the lead joint of the fiber grating sensor on a predetermined length is difficult to lead out during the continuous manufacturing process of pultrusion. Under the condition that the pultrusion efficiency is not significantly reduced, the adverse effect of the built-in joint method on the mechanical properties of the composite pultruded sheet is eliminated. A reliable and stable solution is provided for the manufacture of intelligently pultruded composite material sheets and the smooth lead-out of composite material cross-section optical fiber leads.

Figure 202010969518

Description

Continuous manufacturing process of pultrusion composite material plate internally implanted with FBG sensor
Technical Field
The invention belongs to the field of composite material preparation and nondestructive monitoring, and particularly relates to a continuous manufacturing process of a pultrusion composite material plate internally implanted with an FBG sensor.
Background
With the continuous acceleration of social economy and urbanization, the construction of national engineering facilities and urban infrastructure has been rapidly developed in the past period, and many buildings, bridges and engineering structures have been put into use for decades or even longer. As the use time of these infrastructures increases, the aging of the infrastructure and the safety risk of the infrastructure increases, so that the monitoring of the state of the infrastructure and the maintenance and repair of the infrastructure become important issues to be faced in the next social development.
The molding process of the carbon fiber reinforced composite material unidirectional plate is to impregnate fibers with resin, then solidify the fibers in a mold and continuously perform pultrusion molding. The carbon fiber reinforced composite material has the characteristics of high tensile strength, good corrosion resistance, good shock resistance, good impact resistance and the like, can give full play to the strength and the elastic modulus of the carbon fiber, and has wide application in the aspects of shear reinforcement and prestress reinforcement of bridges and tunnels. With the continuous progress of reinforcing and reinforcing technology and the continuous development of on-line monitoring technology, the implantation of sensors in the pultrusion composite material plate structure for the on-line monitoring of the structure health of facilities has become a key development direction in the field of building reinforcement.
The Fiber Bragg Grating (FBG) sensor has the characteristics of simple structure, strong electromagnetic interference resistance, convenience for implantation, easiness in forming a net and the like, and has obvious advantages in-situ online monitoring compared with metal strain gauges and other types of sensors. Of course, the FBG sensor has some disadvantages, the most important of which is that the optical fiber has poor shear resistance, and the grating region is used as a measurement sensitive component, which is fragile and easy to break, and once the grating region of the grating is broken, the monitoring signal is interrupted, which undoubtedly brings great difficulty to the implantation of the FBG sensor in the composite material pultruded plate, the sensor lead wire and the continuous production of the composite material unidirectional plate.
In order to solve the above problems, a series of researches have been carried out in recent years, and specifically, patent 200810217549.0 discloses a system and a method for embedding a fiber grating sensor in a fiber polymer composite material, wherein a single optical fiber is introduced into a fiber bundle from an introduction die and passes through a pultrusion die together. Such a solution does not allow for pre-tensioning of the FBG sensor fiber, which makes it difficult to precisely locate the FBG sensor in the composite material during the implantation process. Patent 200910057487.6 discloses a system and method for preparing an intelligent rib of a fiber grating composite material, the system and method combines the characteristics of pultrusion and compression molding, an FBG sensor is implanted into the middle position of two preformed bodies, and connectors are processed at two ends, on one hand, the production efficiency is reduced, on the other hand, when the system and method are applied to pultrusion plates, because the thickness of the plates is much smaller than the diameter of the rib, the minimum thickness is only 0.9mm-1.4mm, and embedded lead connectors are not easy to be embedded into two ends of an optical fiber. Patent 201710223794.1 discloses a system and method for continuously implanting fiber grating into pultruded composite material, which adds a pre-stretching device in the fiber grating implanting system to avoid the breaking of the optical fiber, but does not consider the problem that the fiber lead of the FBG sensor is led out from the cut end face of the composite material, and is difficult to realize the continuous manufacturing of the composite material pultruded plate with internally implanted long gauge length FBG sensor.
In summary, there is a need for a continuous manufacturing process and method for a pultrusion composite material plate with an FBG sensor built therein, which is significant for realizing stable implantation and continuous manufacturing and use of the FBG sensor in a pultrusion intelligent composite material.
Disclosure of Invention
The invention mainly aims to solve the key problem of providing a continuous manufacturing process of a pultrusion composite material plate with an internally-arranged FBG sensor, and the continuous manufacturing of the pultrusion intelligent composite material plate with the internally-arranged FBG sensor is realized on the premise of ensuring the smooth survival of the FBG sensor in the pultrusion process of the composite material.
In order to achieve the purpose, the invention adopts the following technical scheme:
a continuous manufacturing process of a pultrusion composite material plate internally implanted with FBG sensors comprises the following steps:
step 1, fiber grating pretreatment: according to the processing and manufacturing requirements of the pultrusion composite material plate, a plurality of grating areas are carved on continuous optical fibers in advance, the continuous optical fibers carved with the grating areas are soaked in a surface modifier for surface treatment and heating and drying, and after the surface modifier is completely dried, a self-lubricating coating is uniformly coated on the preset cutting position of each section of the pultrusion composite material plate;
step 2, pultrusion of the carbon fiber plate: leading the coiled carbon fiber material out of the fiber creel, sequentially passing through a fiber guide device and a resin impregnation device in sequence to ensure that the fiber bundle is uniformly impregnated with resin, and leading the carbon fiber material impregnated with the resin to pass through a fiber bundling plate through an optical fiber conveying device; leading out the continuous optical fiber carved with a plurality of grating areas from the optical fiber concentrator, passing through a guide hole at a preset position of the fiber bundling plate by an optical fiber conveyer, and uniformly surrounding the continuous optical fiber carved with a plurality of grating areas by a carbon fiber material; then the materials enter a heating forming die together for curing forming, and the formed composite material plate is continuously conveyed to a plate traction device;
step 3, cutting the formed composite material plate: after the composite material plate is conveyed to a preset cutting position of the optical fiber by the plate traction device, the composite material plate is cut, and the composite material plate is cut by adopting a two-stage cutting device:
firstly, performing transverse cutting, and controlling a cutter to cut from the edge of the composite material plate to the part in which the fiber bragg grating is implanted so as to ensure that the part in the middle of the composite material plate in which the optical fiber is implanted is still continuous; after the transverse cutting of the composite material plate is finished, continuously utilizing a longitudinal cutting tool to perform secondary cutting;
and 4, post-processing of the FBG sensor lead wires: and (3) carrying out post-treatment on the optical fiber outgoing lines at the sections of the two ends of the cut composite material plate, stripping the carbon fibers around the cut optical fibers by using a wire stripper, reserving the complete bare optical fiber outgoing lines, and after the bare optical fiber outgoing lines are welded with the FC/APC jumper, completing the implantation and continuous manufacturing of the FBG sensor in the pultruded composite material plate.
In the above steps, through the surface pretreatment of the optical fiber, the stable implantation of the FBG sensor, the continuous cutting and the post-treatment process, the damage of the mechanical property of the composite material plate caused by the implantation of the FBG sensor can be reduced to the maximum extent, and the interface bonding force between the optical fiber and the composite material is increased. Meanwhile, through a continuous cutting process, the preparation efficiency and stability are improved on the premise of not damaging the FBG sensor and the optical fiber lead.
Further, the difference of the central wavelengths of the grating regions in the step 1 is 10-15 nm, so that the central wavelengths of the intelligent carbon fiber composite material plate after the drift of the grating regions in the using process are prevented from overlapping, and the accuracy and precision of the strain test are effectively guaranteed.
Further, the surface modifier in the step 1 is a coupling agent, silica sol or a blending and compounding solution of the coupling agent and the silica sol, and the surface modifier is dissolved by an organic solvent before the continuous optical fiber engraved with a plurality of grating areas is immersed, so that the viscosity of the immersion solution is ensured to be proper, and the immersion uniformity of the surface modifier on the surface of the optical fiber is improved.
Further, in the step 1, the preset cutting position of the optical fiber is a position where the length of the optical fiber reaches the preset length of the composite material plate, the preset cutting position on the continuous optical fiber is marked, and cutting can be more accurate in a subsequent cutting process.
Further, the self-lubricating coating in the step 1 is made of polytetrafluoroethylene or ultra-high molecular weight polyethylene, the thickness of the self-lubricating coating is 0.2-0.4 mm, and the thickness of the self-lubricating coating is controlled, so that on one hand, small adhesion between an optical fiber lead and a composite material is ensured, on the other hand, good mechanical property of a cutting part of the composite material is ensured, and the optical fiber position of the cutting section is prevented from splitting; the length of the self-lubricating coating is 1-1.5 m, and the optical fiber leads with enough length are reserved on the cross sections of the two ends of the composite material plate.
Further, in the step 2, the preset position of the fiber bundling plate is determined according to the quantity of the optical fiber gratings to be implanted into the composite material plate, the implanted FBG sensors are symmetrically distributed along the central position of the fiber bundling plate, and the distance between two adjacent bundles of optical fibers is not less than 10 mm. If the distance between the two optical fibers is too close, it is difficult to simultaneously peel the two optical fibers from the cured and cut composite material, and the post-processing process increases the risk of breaking the FBG sensor leads.
Further, the two-stage cutting device in step 3 comprises: the device comprises a fixed frame, a lifting device, a longitudinal slide rail, a transverse cutting system and a longitudinal cutting system; the device fixing frame is used for fixing the cutting device and conveying the formed composite material; the lifting device is connected below the top surface of the fixed frame of the device and is used for controlling the feeding of the cutter assembly in the vertical direction; the longitudinal slide rail is connected below the lifting device and used for driving the cutter assembly to move in the front-back direction and feed and cut; the transverse cutting system is connected to the longitudinal slide rail and is used for transverse cutting of the pultrusion composite material perpendicular to the traction direction; the longitudinal cutting system is connected to the longitudinal sliding rail, arranged behind the transverse cutting system and used for longitudinally cutting the pultrusion composite material along the traction direction after the pultrusion composite material is transversely cut.
Still further, the device fixing frame comprises a fixing base, a frame upright post and an upper cover plate, wherein the fixing base is provided with a material conveying groove, and a material conveying guide roller is arranged in the material conveying groove; the lifting device is driven by electricity and comprises a front group of lifting upright posts and a rear group of lifting upright posts, wherein the two groups of lifting upright posts synchronously lift in the operation process and are provided with a descending limiting device.
Still further, the transverse cutting system comprises a primary transverse guide rail, a primary limiting device, a transverse extending arm, a transverse cutting knife wheel and a driving motor; the primary transverse guide rail is connected to the lower portion of the longitudinal slide rail, the primary limiting device is arranged below the primary transverse guide rail and can move towards the center along the edges of the two ends of the primary transverse guide rail, the primary limiting device limits the minimum distance between the two transverse cutting knife wheels to be 2mm, the transverse extending arm is connected with the primary limiting device through a transverse rotating shaft and can rotate around the transverse rotating shaft, the transverse cutting knife wheels and the driving motor are respectively arranged on the front side and the rear side of the transverse extending arm, the driving motor drives the transverse cutting knife wheels to rotate in the cutting process, the installation knife edges of the transverse cutting knife wheels are perpendicular to the conveying direction of the composite material, and the thickness of the knife edges of the transverse cutting knife wheels is 0.6-0.8 mm;
the longitudinal cutting system comprises a secondary transverse guide rail, a secondary limiting device, a longitudinal extending arm, a longitudinal cutting knife wheel and a driving motor; the two-stage transverse guide rail is connected to the lower portion of the longitudinal sliding rail, the left two-stage limiting device and the right two-stage limiting device are arranged on the two-stage transverse guide rail and used for adjusting the distance between the two longitudinal cutting knife wheels, the two-stage limiting device limits the minimum distance between the two longitudinal cutting knife wheels to be 2mm, the longitudinal extending arm is connected with the two-stage limiting device through a longitudinal rotating shaft, the longitudinal extending arm can rotate around the longitudinal rotating shaft, the longitudinal cutting knife wheels and the driving motor are respectively installed on two sides of the longitudinal extending arm, the driving motor drives the longitudinal cutting knife wheels to rotate in the cutting process, the installation knife edge direction of the longitudinal cutting knife wheels is parallel to the conveying direction of the composite material, and the thickness of the knife edge of the longitudinal cutting knife wheels is 0.6-0.8 mm.
Further, the transverse cutting in the step 3 is to stop cutting at a position 2-3 mm near the optical fiber lead, so that the section of the composite material plate is cut smoothly, and the part of the plate where the optical fiber lead is implanted is kept continuous. The minimum cutting distance can be set to reduce the content of fiber and resin coated around the optical fiber lead as much as possible on the premise of ensuring the optical fiber lead to be intact, and the optical fiber lead in the post-treatment process can be conveniently stripped.
Compared with the prior art, the invention has the following advantages:
the pultrusion device and the continuous manufacturing method of the composite material internally implanted with the FBG sensor effectively solve the problem that the lead joint of the fiber bragg grating sensor on the preset length is difficult to lead out in the pultrusion continuous manufacturing process. Under the condition of ensuring that the pultrusion efficiency is not obviously reduced, the adverse effect of a built-in joint method on the mechanical property of the composite material pultruded plate is eliminated. The device and the manufacturing process method can complete the implantation and lead wire of the FBG sensor only by simple pretreatment of the optical fiber and post-treatment of the formed composite material, and provide a reliable and stable scheme for manufacturing the intelligent pultrusion composite material plate.
Drawings
FIG. 1 is a view showing the structure of an apparatus according to the present invention;
FIG. 2 is a schematic view of a completed pultruded composite panel with an embedded fiber grating according to the present invention;
FIG. 3 is an overall schematic view of the two-stage cutting apparatus of the present invention;
FIG. 4 is a front view of the two-stage cutting apparatus of the present invention;
FIG. 5 is a side view of the two-stage cutting apparatus of the present invention;
the device comprises a base, a fiber guide device, a resin impregnation device, a fiber bundling plate, a continuous optical fiber bundle, a plate drawing device, a two-stage cutting device, a grating area, a carbon fiber bundle, a fiber guide device, a resin impregnation device, a fiber bundling plate, a continuous optical fiber bundle, a fiber concentrator, a fiber conveying device, a heating forming die, a plate drawing device, a two-stage cutting device, a grating area, a fiber bundle and a fiber splicing wire, wherein 6 is a carbon fiber material, 7 is a fiber creel, 8 is a fiber guide device, 9 is a resin impregnation device, 10 is a fiber bundling plate, 11 is a continuous optical fiber carved with a plurality of grating areas, 12 is an optical fiber concentrator, 13 is an optical fiber conveying device, 14 is a heating forming die, 15 is a plate drawing device, 16 is a two-stage cutting device, 17 is a grating area, 18 is a carbon fiber bundle, 19 is an FC/APC jumper wire, and 20 is an optical fiber outgoing wire; 1 is a device fixing frame, 2 is a lifting device, 3 is a longitudinal slide rail, 4 is a transverse cutting system, and 5 is a longitudinal cutting system; 101 is a fixed base, 102 is a frame upright post, 103 is an upper cover plate, 104 is a material conveying groove, and 105 is a material conveying guide roller; 201 is a lifting upright post, and 202 is a descending limiting device; 401 is a primary transverse guide rail, 402 is a primary limiting device, 403 is a transverse extending arm, 404 is a transverse cutting knife wheel, 405 is a driving motor, and 406 is a transverse rotating shaft; 501 is a secondary transverse guide rail, 502 is a secondary limiting device, 503 is a longitudinal extending arm, 504 is a longitudinal cutting knife wheel, 505 is a driving motor, and 506 is a longitudinal rotating shaft.
Detailed Description
The invention is further elucidated with reference to the drawing. The following description is given for the purpose of explanation and not limitation.
Example 1
A continuous manufacturing process of a pultrusion composite material plate internally implanted with FBG sensors comprises the following steps:
step 1, fiber grating pretreatment: according to the processing and manufacturing requirements of the pultrusion composite material plate, a plurality of grating areas 17 are carved on continuous optical fibers in advance, the continuous optical fibers 11 carved with the grating areas are soaked in a surface modifier for surface treatment and heating and drying, and after the surface modifier is completely dried, self-lubricating coatings are uniformly coated on the preset cutting positions of the continuous optical fibers carved with the grating areas according to the specified length of each section of pultrusion composite material plate;
the 3 grating grid regions are engraved on the continuous optical fiber, the central wavelength of each grating grid region is different, the central wavelength of each grating grid region is 1525nm, 1540nm and 1555nm, the central wavelengths of the intelligent carbon fiber composite material plate after the drift of each grid region are prevented from overlapping in the using process, and the accuracy and precision of the strain test are effectively guaranteed.
The surface modifier adopts a coupling agent, and is dissolved by acetone before the continuous optical fiber engraved with a plurality of grating areas is immersed, so that the viscosity of an immersion solution is ensured to be lower than 300mPa.s, and the immersion uniformity of the surface modifier on the surface of the optical fiber is improved.
The length of each section of pultruded composite material plate is 10m, the preset cutting position of the optical fiber is the position where the length of the optical fiber reaches the preset length of 10m of the composite material plate, and the preset cutting positions on the continuous optical fiber at intervals of 10m are marked.
The self-lubricating coating contains polytetrafluoroethylene, and the thickness of self-lubricating coating is 0.3mm, and the thickness of control self-lubricating coating guarantees on the one hand that optic fibre lead wire and combined material are less adhesion, and on the other hand guarantees the combined material and cuts the better mechanical properties in position, prevents to cut the optic fibre position of cross-section and takes place the splitting.
The length of the self-lubricating coating is 1.5m, and the optical fiber leads with enough length are reserved on the cross sections of the two ends of the composite material plate.
Step 2, pultrusion of the carbon fiber plate: the coiled carbon fiber material 6 is led out from a fiber creel 7 and sequentially passes through a fiber guide device 8 and a resin impregnation device 9 in sequence, and the carbon fiber material impregnated with resin passes through an optical fiber conveying device 13 and passes through a fiber bundling plate 10; leading out the continuous optical fiber 11 carved with a plurality of grating areas from an optical fiber concentrator 12, passing through a guide hole at a preset position of a fiber bundling plate 10 by an optical fiber conveying device 13, and uniformly surrounding the continuous optical fiber 11 carved with a plurality of grating areas 16 by a carbon fiber material impregnated with resin; after passing through the fiber bundling plate 10, the resin-impregnated carbon fiber material and the continuous optical fibers 11 engraved with the plurality of grating areas 16 enter a heating forming die 14 together for curing forming, and the formed composite material plate is continuously conveyed to a plate traction device 15;
the number of the optical fiber gratings to be implanted in the composite material pultrusion plate is 1, and the implanted optical fiber gratings are located in the center of the fiber bundling plate 10.
Step 3, cutting the formed composite material plate: after the composite material plate is conveyed to a preset cutting position of the optical fiber by the plate traction device 15, the composite material plate is cut, and the composite material plate is cut by adopting a two-stage cutting device 16:
firstly, performing transverse cutting, and controlling a cutter to cut from the edge of the composite material plate to the part in which the fiber bragg grating is implanted so as to ensure that the part in the middle of the composite material plate in which the optical fiber is implanted is still continuous; after the transverse cutting of the composite material plate is finished, continuously utilizing a longitudinal cutting tool to perform secondary cutting;
the two-stage cutting device 16 includes: the device comprises a device fixing frame 1, a lifting device 2, a longitudinal slide rail 3, a transverse cutting system 4 and a longitudinal cutting system 5; the device fixing frame 1 comprises a fixing base 101, a frame upright post 102 and an upper cover plate 103, wherein the fixing base 101 is provided with a material conveying groove 104, and a material conveying guide roller 105 is arranged in the material conveying groove and used for fixing the cutting device and conveying the formed composite material; the lifting device 2 is connected below the top surface of the device fixing frame 1 and used for controlling the feeding of the cutter assembly in the vertical direction, the driving mode of the lifting device 2 is electric driving and comprises a front group of lifting upright columns 201 and a rear group of lifting upright columns 201, the two groups of lifting upright columns 201 synchronously lift in the operation process, and a descending limiting device 202 is arranged; the longitudinal slide rail 3 is connected below the lifting device 2 and used for driving the cutter assembly to move in the front-back direction and feed and cut; the transverse cutting system 4 is connected to the longitudinal slide rail 3 and is used for transverse cutting of the pultruded composite material perpendicular to the traction direction, and the transverse cutting system 4 comprises a primary transverse guide rail 401, a primary limiting device 402, a transverse extending arm 403, a transverse cutting knife wheel 404 and a driving motor 405; the primary transverse guide rail 401 is connected to the lower portion of the longitudinal slide rail 3, the primary limiting device 402 is arranged below the primary transverse guide rail 401 and can move towards the center along the edges of two ends of the primary transverse guide rail 401, the primary limiting device 402 limits the minimum distance between the two transverse cutting knife wheels 404 to be 2mm, the transverse extending arm 403 is connected with the primary limiting device 402 through a transverse rotating shaft 406, the transverse extending arm 403 can rotate around the transverse rotating shaft 406, the transverse cutting knife wheels 404 and the driving motor 405 are respectively arranged on the front side and the rear side of the transverse extending arm 403, the driving motor 405 drives the transverse cutting knife wheels 404 to rotate in the cutting process, the installation knife edge direction of the transverse cutting knife wheels 404 is perpendicular to the composite material conveying direction, and the thickness of the cutting edge of the transverse cutting knife wheels 404 is 0.6-0.8 mm; the longitudinal cutting system 5 is connected to the longitudinal sliding rail 3, is arranged behind the transverse cutting system 4, and is used for longitudinally cutting the pultruded composite material along the traction direction after the transverse cutting, and the longitudinal cutting system 5 comprises a secondary transverse guide rail 501, a secondary limiting device 502, a longitudinal extending arm 503, a longitudinal cutting knife wheel 504 and a driving motor 505; the two-stage transverse guide rail 501 is connected to the lower portion of the longitudinal slide rail 3, the left two-stage limiting device 502 and the right two-stage limiting device 502 are arranged on the two-stage transverse guide rail 501 and used for adjusting the distance between the two longitudinal cutting knife wheels 504, the two-stage limiting device 502 limits the minimum distance between the two longitudinal cutting knife wheels 504 to be 2mm, the longitudinal extending arm 503 is connected with the two-stage limiting device 502 through a longitudinal rotating shaft 506 and can rotate around the longitudinal rotating shaft 506, the longitudinal cutting knife wheels 504 and a driving motor 505 are respectively arranged on two sides of the longitudinal extending arm, the driving motor 505 drives the longitudinal cutting knife wheels 504 to rotate in the cutting process, the installation blade direction of the longitudinal cutting knife wheels 504 is parallel to the conveying direction of the composite material, and the blade thickness of the longitudinal cutting knife wheels 504 is 0.6-0.8 mm.
And the transverse cutting is stopped at a position which is 3mm close to the optical fiber lead, so that the section of the composite material plate is smoothly cut, and the part of the plate, which is implanted with the optical fiber lead, is kept continuous.
And 4, post-processing of the fiber grating sensor lead: and (3) carrying out post-processing on the optical fiber outgoing lines 20 at the sections of the two ends of the cut composite material plate, stripping the carbon fiber bundles 18 around the cut optical fibers by using a wire stripper, reserving the complete bare optical fiber outgoing lines, and welding the bare optical fiber outgoing lines with an FC/APC jumper 19 to complete the implantation and continuous manufacturing of the fiber grating sensor in the pultruded composite material plate.

Claims (10)

1.一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,包括以下步骤:1. a continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor, is characterized in that, comprises the following steps: 步骤1,光纤光栅前处理:按照拉挤成型复合材料板材的加工制造需要,在连续的光纤上预先刻制多个光栅栅区(17),将刻制有多个光栅栅区的连续光纤(11)浸渍于表面改性剂中进行表面处理并加热烘干,待表面改性剂完全干燥之后,根据每段拉挤成型复合材料板材的规定长度,在刻制有多个光栅栅区(117)的连续光纤(11)的预定裁切位置均匀涂覆自润滑涂层;Step 1, fiber grating pretreatment: according to the processing and manufacturing needs of the pultruded composite material sheet, a plurality of grating grid regions (17) are pre-engraved on the continuous optical fiber, and the continuous optical fiber ( 11) Immerse in the surface modifier for surface treatment and heat drying. After the surface modifier is completely dried, according to the specified length of each pultruded composite material sheet, a plurality of grating grid regions (117 The predetermined cutting position of the continuous optical fiber (11) of ) is uniformly coated with a self-lubricating coating; 步骤2,碳纤维板材拉挤成型:成卷的碳纤维材料(6)从纤维纱架(7)引出,按顺序依次经过纤维导向装置(8)、树脂浸渍装置(9),浸渍树脂的碳纤维材料经过光纤输送装置(13),穿过纤维集束板(10);将刻制有多个光栅栅区的连续光纤(11)从光纤集线器(12)上引出,经过光纤传送器(13),从纤维集束板(10)预定位置的导向孔中穿过,使刻制有多个光栅栅区的连续光纤(11)被浸渍树脂的碳纤维材料均匀包围;浸渍树脂的碳纤维材料与刻制有多个光栅栅区的连续光纤(11)经过纤维集束板(10)之后,一起进入加热成型模具(14)进行固化成型,并将成型后的复合材料板材连续输送到板材牵引装置(15);Step 2, carbon fiber sheet pultrusion: the rolled carbon fiber material (6) is drawn out from the fiber creel (7), passes through the fiber guide device (8) and the resin impregnation device (9) in sequence, and the resin-impregnated carbon fiber material passes through the fiber guide device (8) and the resin impregnation device (9). The optical fiber conveying device (13) passes through the fiber bundle plate (10); the continuous optical fiber (11) engraved with a plurality of grating grid regions is led out from the optical fiber hub (12), and passes through the optical fiber transmitter (13), from the fiber The bundling plate (10) passes through a guide hole at a predetermined position, so that the continuous optical fiber (11) engraved with a plurality of grating grating regions is evenly surrounded by the resin-impregnated carbon fiber material; the resin-impregnated carbon fiber material is engraved with a plurality of gratings. After the continuous optical fibers (11) in the grid region pass through the fiber bundle plate (10), they enter the thermoforming mold (14) together for curing and forming, and the formed composite material sheet is continuously transported to the sheet pulling device (15); 步骤3,成型复合材料板材的裁切:复合材料板材经板材牵引装置(15)输送达到光纤的预定裁切位置之后,对复合材料板材进行切割,采用两级裁切装置(16)进行复合材料板材的裁切:Step 3, cutting of the formed composite material sheet: after the composite material sheet is conveyed by the sheet pulling device (15) to the predetermined cutting position of the optical fiber, the composite material sheet is cut, and the composite material sheet is cut by a two-stage cutting device (16). Cutting of the sheet: 首先进行横向裁切,控制刀具从复合材料板材边缘向内植光纤光栅的部位进行裁切,使复合材料板材中间部位内植有光纤的部分依然保持连续;复合材料板材横向裁切完成之后,继续利用纵向裁切刀具进行二次裁切;First, perform transverse cutting, and control the cutter to cut from the edge of the composite material sheet to the part where the fiber grating is implanted, so that the part where the optical fiber is implanted in the middle of the composite material sheet remains continuous; after the transverse cutting of the composite material sheet is completed, continue Use longitudinal cutting tool for secondary cutting; 步骤4,FBG传感器引线的后处理:对裁切完成后复合材料板材两端截面处的光纤引出线(20)进行后处理,将切割之后光纤周围碳纤维束(18)采用剥线器进行剥离,保留完整的裸光纤引出线,与FC/APC跳线(19)熔接之后,即完成FBG传感器在拉挤复合材料板材中的植入与连续制造。Step 4, post-processing of the FBG sensor leads: post-processing the optical fiber lead wires (20) at the cross-sections at both ends of the composite material sheet after the cutting is completed, and stripping the carbon fiber bundles (18) around the optical fibers after cutting with a wire stripper, After retaining the intact bare fiber lead-out wire and splicing with the FC/APC jumper (19), the implantation and continuous manufacturing of the FBG sensor in the pultruded composite material sheet are completed. 2.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤1中光栅栅区的中心波长相差10~15nm。2 . The continuous manufacturing process of a pultruded composite material sheet with built-in FBG sensor according to claim 1 , wherein in the step 1, the center wavelength of the grating grid region differs by 10-15 nm. 3 . 3.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤1中的表面改性剂为偶联剂、硅溶胶或两者的共混复配溶液,所述表面改性剂在刻制有多个光栅栅区的连续光纤(11)浸渍之前采用有机溶剂溶解。3. The continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor according to claim 1, wherein the surface modifier in the step 1 is a coupling agent, a silica sol or both The blending compound solution, the surface modifier is dissolved in an organic solvent before the continuous optical fiber (11) engraved with a plurality of grating grid regions is immersed. 4.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤1中预定裁切位置为刻制有多个光栅栅区的连续光纤(11)长度达到复合材料板材预定长度的位置,对刻制有多个光栅栅区的连续光纤(11)上的预定裁切位置进行标记。4 . The continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor according to claim 1 , wherein the predetermined cutting position in the step 1 is a continuous line engraved with a plurality of grating grid regions. 5 . When the length of the optical fiber (11) reaches the predetermined length of the composite material sheet, the predetermined cutting position on the continuous optical fiber (11) engraved with a plurality of grating grid regions is marked. 5.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤1中自润滑涂层为聚四氟乙烯或超高分子量聚乙烯,所述自润滑涂层的厚度为0.2~0.4mm,长度为1~1.5m。5. The continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor according to claim 1, wherein the self-lubricating coating in the step 1 is polytetrafluoroethylene or ultra-high molecular weight polyethylene , the thickness of the self-lubricating coating is 0.2-0.4 mm, and the length is 1-1.5 m. 6.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤2中纤维集束板预定位置根据复合材料板材中需要植入FBG传感器的数量进行确定,植入的光纤光栅沿纤维集束板的中心位置对称分布,相邻光纤光栅之间的距离不小于10mm。6 . The continuous manufacturing process of a pultruded composite material sheet with an implanted FBG sensor according to claim 1 , wherein in the step 2, the predetermined position of the fiber bundle plate is implanted according to the need to implant the FBG sensor in the composite material sheet. 7 . The number of fiber gratings is determined, the implanted fiber gratings are symmetrically distributed along the center of the fiber bundle plate, and the distance between adjacent fiber gratings is not less than 10mm. 7.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤3中两级裁切装置(16)包括:装置固定框架(1)、升降装置(2)、纵向滑轨(3)、横向裁切系统(4)、纵向裁切系统(5);所述装置固定框架(1)用于固定裁切装置并输送已成型复合材料;所述升降装置(2)连接在装置固定框架(1)顶面下方,用于控制刀具组件在竖直方向的进给;所述纵向滑轨(3)连接于升降装置(2)下方,用于驱动刀具组件沿前后方向运动及进给裁切;所述横向裁切系统(4)连接在纵向滑轨(3)上,用于拉挤成型复合材料垂直于牵引方向的横向裁切;所述纵向裁切系统(5)连接在纵向滑轨(3)上并置于所述横向裁切系统(4)后方,用于拉挤成型复合材料在横向裁切之后,沿牵引方向的纵向裁切。7. The continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor according to claim 1, wherein the two-stage cutting device (16) in the step 3 comprises: a device fixing frame (1 ), a lifting device (2), a longitudinal slide rail (3), a transverse cutting system (4), and a longitudinal cutting system (5); the device fixing frame (1) is used to fix the cutting device and transport the formed composite material; the lifting device (2) is connected under the top surface of the device fixing frame (1), and is used to control the feeding of the tool assembly in the vertical direction; the longitudinal slide rail (3) is connected under the lifting device (2) , used to drive the cutter assembly to move in the front-rear direction and feed cutting; the transverse cutting system (4) is connected to the longitudinal slide rail (3), and is used for transverse cutting of the pultruded composite material perpendicular to the pulling direction ; The longitudinal cutting system (5) is connected to the longitudinal slide rail (3) and placed behind the transverse cutting system (4), for the pultrusion composite material after transverse cutting, along the traction direction Crop lengthwise. 8.根据权利要求7所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述装置固定框架(1)包括固定基座(101)、框架立柱(102)以及上部盖板(103),所述固定基座(101)设有材料输送槽(104),所述材料输送槽内部设置有材料输送导辊(105);所述升降装置(2)驱动方式为电驱动,包括前后两组可升降立柱(201),运行过程中两组可升降立柱(201)同步升降,并设置有下降限位装置(202)。8 . The continuous manufacturing process of a pultruded composite material sheet with built-in FBG sensor according to claim 7 , wherein the device fixing frame ( 1 ) comprises a fixing base ( 101 ), a frame column ( 102 ) ) and an upper cover plate (103), the fixed base (101) is provided with a material conveying groove (104), and a material conveying guide roller (105) is arranged inside the material conveying groove; the lifting device (2) drives the The method is electric drive, including two groups of front and rear liftable uprights (201), the two groups of liftable uprights (201) are raised and lowered synchronously during operation, and a lowering limit device (202) is provided. 9.根据权利要求7所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述横向裁切系统(4)包括一级横向导轨(401)、一级限位装置(402)、横向伸臂(403)、横向裁切刀轮(404)以及驱动电机(405);所述一级横向导轨(401)连接在纵向滑轨(3)下部,所述一级限位装置(402)置于一级横向导轨(401)下方,可沿一级横向导轨(401)两端边缘向中心移动,一级限位装置(402)限制两横向裁切刀轮(404)之间的最小距离为2mm,横向伸臂(403)与一级限位装置(402)之间通过横向转轴(406)连接,横向伸臂(403)可绕横向转轴(406)转动,所述横向裁切刀轮(404)及驱动电机(405),分别安装在横向伸臂(403)的前后两侧,裁切过程中驱动电机(405)驱动横向裁切刀轮(404)转动,横向裁切刀轮(404)安装刀刃方向垂直于复合材料输送方向,所述横向裁切刀轮(404)的刃口厚度为0.6~0.8mm;9 . The continuous manufacturing process of a pultruded composite material sheet with built-in FBG sensor according to claim 7 , wherein the transverse cutting system ( 4 ) comprises a first-level transverse guide rail ( 401 ), a first-level transverse guide rail ( 401 ), a first-level transverse guide rail ( 401 ), A limiting device (402), a transverse outrigger (403), a transverse cutting wheel (404) and a drive motor (405); the first-level transverse guide rail (401) is connected to the lower part of the longitudinal slide rail (3), and the The first-level limiting device (402) is placed under the first-level transverse guide rail (401), and can move toward the center along the edges of both ends of the first-level transverse guide rail (401). The first-level limiting device (402) limits the two transverse cutting wheels The minimum distance between (404) is 2mm, the lateral outrigger (403) and the primary limiting device (402) are connected by a lateral shaft (406), and the lateral arm (403) can rotate around the lateral shaft (406) , the transverse cutting wheel (404) and the driving motor (405) are respectively installed on the front and rear sides of the transverse outrigger (403), and the driving motor (405) drives the transverse cutting wheel (404) during the cutting process Rotation, the direction of the installation of the blade edge of the transverse cutting blade wheel (404) is perpendicular to the conveying direction of the composite material, and the thickness of the blade edge of the transverse cutting blade wheel (404) is 0.6-0.8 mm; 所述纵向裁切系统(5)包括二级横向导轨(501)、二级限位装置(502)、纵向伸臂(503)、纵向裁切刀轮(504)及驱动电机(505);所述二级横向导轨(501)连接于纵向滑轨(3)下部,左、右两个二级限位装置(502)置于二级横向导轨(501)上,用于调整两个纵向裁切刀轮(504)之间的间距,二级限位装置(502)限制两纵向裁切刀轮(504)之间的最小距离为2mm,纵向伸臂(503)与二级限位装置(502)之间通过纵向转轴(506)连接,纵向伸臂(503)可绕纵向转轴(506)转动,所述纵向裁切刀轮(504)及驱动电机(505),分别安装在纵向伸臂的两侧,裁切过程中驱动电机(505)驱动纵向裁切刀轮(504)转动,纵向裁切刀轮(504)安装刀刃方向平行于复合材料输送方向,所述纵向裁切刀轮(504)的刃口厚度为0.6~0.8mm。The longitudinal cutting system (5) includes a secondary transverse guide rail (501), a secondary limiting device (502), a longitudinal extension arm (503), a longitudinal cutting wheel (504) and a drive motor (505); The secondary lateral guide rail (501) is connected to the lower part of the longitudinal slide rail (3), and the left and right secondary limiting devices (502) are placed on the secondary lateral guide rail (501) for adjusting the two longitudinal cuts The distance between the cutter wheels (504), the secondary limit device (502) limits the minimum distance between the two longitudinal cutting cutter wheels (504) to 2mm, the longitudinal outrigger (503) and the secondary limit device (502) ) are connected by a longitudinal axis (506), the longitudinal outrigger (503) can rotate around the longitudinal axis (506), and the longitudinal cutting wheel (504) and the drive motor (505) are respectively installed on the On both sides, the drive motor (505) drives the longitudinal cutting wheel (504) to rotate during the cutting process, and the longitudinal cutting wheel (504) is installed with the blade in a direction parallel to the direction of conveying the composite material. The longitudinal cutting wheel (504) ) of the edge thickness of 0.6 ~ 0.8mm. 10.根据权利要求1所述的一种内植FBG传感器的拉挤成型复合材料板材连续制造工艺,其特征在于,所述步骤3中横向裁切是在光纤引线附近2~3mm位置停止裁切。10 . The continuous manufacturing process of a pultruded composite material sheet with a built-in FBG sensor according to claim 1 , wherein the transverse cutting in the step 3 is to stop cutting at a position of 2-3 mm near the optical fiber lead. 11 . .
CN202010969518.1A 2020-09-15 2020-09-15 A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor Active CN112192865B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010969518.1A CN112192865B (en) 2020-09-15 2020-09-15 A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010969518.1A CN112192865B (en) 2020-09-15 2020-09-15 A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor

Publications (2)

Publication Number Publication Date
CN112192865A CN112192865A (en) 2021-01-08
CN112192865B true CN112192865B (en) 2021-10-15

Family

ID=74015125

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010969518.1A Active CN112192865B (en) 2020-09-15 2020-09-15 A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor

Country Status (1)

Country Link
CN (1) CN112192865B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024131748A1 (en) * 2022-12-21 2024-06-27 江苏神马电力股份有限公司 Pultrusion apparatus and pultrusion method
CN116001257B (en) * 2022-12-23 2025-03-25 卡本科技集团股份有限公司 Fiber Bragg grating built-in prestressed composite material and processing method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0561151A1 (en) * 1992-03-18 1993-09-22 Peguform-Werke Gmbh Method for producing beams of fibrereinforced plastics material for motorcar bumpers and such beams
HU0800256D0 (en) * 2008-04-24 2008-06-30 Szaplonczay Pal Method and instalation for fabrication of heat resistant transmission line having a thermo softening core
CN106808717A (en) * 2016-12-20 2017-06-09 中国科学院宁波材料技术与工程研究所 A kind of prepreg cuts lay product line device
CN106945310A (en) * 2016-11-09 2017-07-14 江苏九鼎新材料股份有限公司 A kind of glass fibre pultrusion grid continuous production line
CN107314783A (en) * 2017-06-19 2017-11-03 武汉理工大学 The device and method of fiber-optic grating sensor is drawn in a kind of central siphon from composite
CN108995251A (en) * 2018-07-30 2018-12-14 上伟(江苏)碳纤复合材料有限公司 It is a kind of suitable for the wind electricity blade girder production technology of carbon fiber pultrusion plate

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1238167A (en) * 1983-04-07 1988-06-21 James E. O'connor Process for preparing shaped objects of poly(arylene sulfide) and product thereof
JPS641526A (en) * 1987-04-27 1989-01-05 Toyo Cloth Kk Molding of composite material by means of ultra-violet ray curing
DE3810598A1 (en) * 1988-03-29 1989-10-12 Bayer Ag COMPOSITIONS CONTAINING METAL FIBERS AND THE USE THEREOF FOR PRODUCING MOLDED PARTS FOR SHIELDING ELECTROMAGNETIC RADIATION
US5006294A (en) * 1989-04-26 1991-04-09 E. I. Du Pont De Nemours And Company Process for making composites of stretch broken aligned fibers
DE19818379C1 (en) * 1998-04-24 1999-10-28 Rainer Lebmeier Construction of a multilayer prepreg preform for molding a fiber reinforced composite product
DE102007018052A1 (en) * 2007-04-17 2008-10-23 Airbus Deutschland Gmbh Pultrusion process for producing an endless profile
CN101738214B (en) * 2008-11-07 2013-01-02 深圳市海川实业股份有限公司 System and method for embedding optical fiber grating sensor in fiber high polymer composite material
CN101624790B (en) * 2009-05-22 2011-11-23 东南大学 A large-scale preparation process of distributed high-precision self-monitoring FRP tendons/cables based on optical fiber sensing
CN101930101B (en) * 2009-06-25 2013-06-19 上海启鹏工程材料科技有限公司 System and method for preparing optical fiber Bragg grating smart bar
KR20130112705A (en) * 2010-06-11 2013-10-14 티코나 엘엘씨 Structural member formed from a solid lineal profile
CN102947078B (en) * 2010-06-22 2015-07-08 提克纳有限责任公司 Method for forming reinforced pultruded profiles
US10358767B2 (en) * 2016-07-15 2019-07-23 GM Global Technology Operations LLC Carbon fiber pre-pregs and methods for manufacturing thereof
CN106404065B (en) * 2016-10-09 2019-05-07 山东大学 A composite material encapsulated fiber grating sensor and its manufacturing method
CN107053707B (en) * 2017-04-07 2019-06-28 武汉理工大学 A kind of fiber grating is continuously implanted into the system and method for molded through pultrusion of composite material
JP6834900B2 (en) * 2017-10-20 2021-02-24 トヨタ自動車株式会社 How to manufacture high pressure tank
CN210100754U (en) * 2019-06-10 2020-02-21 国塑机械(上海)有限公司 Molding equipment is used in production of thermoplasticity continuous fibers composite board

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0561151A1 (en) * 1992-03-18 1993-09-22 Peguform-Werke Gmbh Method for producing beams of fibrereinforced plastics material for motorcar bumpers and such beams
HU0800256D0 (en) * 2008-04-24 2008-06-30 Szaplonczay Pal Method and instalation for fabrication of heat resistant transmission line having a thermo softening core
CN106945310A (en) * 2016-11-09 2017-07-14 江苏九鼎新材料股份有限公司 A kind of glass fibre pultrusion grid continuous production line
CN106808717A (en) * 2016-12-20 2017-06-09 中国科学院宁波材料技术与工程研究所 A kind of prepreg cuts lay product line device
CN107314783A (en) * 2017-06-19 2017-11-03 武汉理工大学 The device and method of fiber-optic grating sensor is drawn in a kind of central siphon from composite
CN108995251A (en) * 2018-07-30 2018-12-14 上伟(江苏)碳纤复合材料有限公司 It is a kind of suitable for the wind electricity blade girder production technology of carbon fiber pultrusion plate

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
复合材料内传感光纤的埋置技术;杨建良等;《宇航材料工艺》(第06期) *

Also Published As

Publication number Publication date
CN112192865A (en) 2021-01-08

Similar Documents

Publication Publication Date Title
CN112192865B (en) A continuous manufacturing process of pultruded composite sheet with built-in FBG sensor
CN104819877B (en) A kind of method for making sample of unidirectional lamination tensile property test
CN1113139C (en) Truss structure
CN102658656B (en) Preparation method for glass fibre reinforced resin composite plate spring
CN103587111A (en) Surface treatment device of fiber enhanced composite material plain round rib for structural engineering
CN101598676A (en) Large-scale production process of distributed high-precision self-monitoring FRP tendons/cables based on optical fiber sensing
CN101624790B (en) A large-scale preparation process of distributed high-precision self-monitoring FRP tendons/cables based on optical fiber sensing
CN101930101A (en) System and method for preparing optical fiber Bragg grating smart bar
CN100363585C (en) Prestressed carbon fiber plate stretching method and device
CN110553926B (en) A Bending Creep Testing Device for Fiber Reinforced Composite Rods
CN110053278B (en) Forming device for producing high-insulativity lightweight composite material cross arm
CN107053707B (en) A kind of fiber grating is continuously implanted into the system and method for molded through pultrusion of composite material
WO2022016747A1 (en) Continuous deformation composite material profile and preparation method therefor
US6061902A (en) Method for recovering leads embedded within a composite structure
CN212603551U (en) Continuous cutting device for pultruded composite material with built-in FBG sensor
CN114193798A (en) A kind of continuous preparation method and anchoring method of FRP pultrusion profile
CN112060635A (en) Continuous cutting device and method for pultrusion composite material internally implanted with FBG (fiber Bragg Grating) sensor
CN112013781B (en) Pultrusion panel joint packaging device and method for embedded FBG sensor
CN204738169U (en) Single -strand fiber's manufacture equipment
CN110001083B (en) High-insulativity lightweight composite material cross arm production system
CN113246499B (en) Large-diameter fiber composite material pipe and preparation method and system thereof
CN106514862A (en) Reinforcing cage prestress tensioning device and making method of prestressed square pile
CN113442465A (en) Forming device and method for preparing composite material rod by utilizing thermoplastic prepreg tape
JP4283558B2 (en) Fiber reinforced plastic pipe manufacturing equipment
CN220198616U (en) FRP net piece preparation equipment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant