WO2003071181A1 - Pressurised container comprising a tubular connection - Google Patents
Pressurised container comprising a tubular connection Download PDFInfo
- Publication number
- WO2003071181A1 WO2003071181A1 PCT/CH2003/000126 CH0300126W WO03071181A1 WO 2003071181 A1 WO2003071181 A1 WO 2003071181A1 CH 0300126 W CH0300126 W CH 0300126W WO 03071181 A1 WO03071181 A1 WO 03071181A1
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- Prior art keywords
- pressure vessel
- vessel according
- oval
- stress
- connection
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/06—Closures, e.g. cap, breakable member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0617—Single wall with one layer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0646—Aluminium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/0663—Synthetics in form of fibers or filaments
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/0663—Synthetics in form of fibers or filaments
- F17C2203/0673—Polymers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/21—Shaping processes
- F17C2209/2109—Moulding
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/21—Shaping processes
- F17C2209/2109—Moulding
- F17C2209/2118—Moulding by injection
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/228—Assembling processes by screws, bolts or rivets
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0102—Applications for fluid transport or storage on or in the water
- F17C2270/0131—Submarines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
Definitions
- the present invention relates to a pressure container with at least one tubular connection at an opening in the container wall.
- a pressure vessel e.g. If an internal, pneumatic or hydraulic overpressure is applied, tensions occur in the container wall.
- pressure vessels are constructed as spherical or cylindrical as possible. If a connection is attached to such a container, the stresses concentrate in the area of the connection, as a result of which this area is subjected to higher loads and forms a weak point of the pressure container.
- the stresses for each point of the container wall can be described mathematically by stress tensor.
- the invariant of the stress tensor against coordinate transformations are three so-called main stresses, one of which is defined as the first main stress in the technical terminology of stress tensor mechanics.
- the first main stress corresponds to the greatest tensile stress. This term is also used in the following.
- main directions are assigned to the main stresses.
- WO 01/69187 A1 in relation to a pressure vessel which can be used in particular as a water meter housing, it is proposed to design the bottom part of the latter to be elliptical in order to reduce the voltage. It remains unclear which floor shape WO 01/69187 A1 is based on, since hemispherical or at least approximately elliptical floor shapes (so-called bobbin floors) have of course long been known in the prior art and would have at least equally good properties.
- WO 01/69187 A1 proposes to shift tensions away from weld seams in the area between two connections and the lower part of the housing, which is identical to the base part Make connections elliptical. 2 shows an example of this.
- WO 01/69187 A1 does not make any statements about which would allow an understanding of the stress shift claimed, nor does it make any statements about where the voltages are shifted to.
- the object of the present invention is to specify how the problems mentioned in the connection area of tubular connections can be reduced in the case of pressure vessels and thereby pressure vessels can be produced which can be loaded with a higher pressure difference or which have a higher safety reserve with the same load.
- the invention proposes ovalizing the connection in the connection area.
- the cross-sections of the opening and the tubular connection at this opening are oval and aligned with the major axis of the oval shape in the direction of the first main stress, which would result if the pressure vessel were subjected to an internal overpressure at the connection point without the opening and the connection ,
- the ovality O can be expressed by the ratio of the length of the large (D) and the small (d) axis of the oval shape and is, depending on the application and geometry, approximately in the range between 1, 1 and 3.0, preferably in the range between 1, 1 and 2.5, and particularly preferably in the range between 1, 1 and 1, 9.
- an essentially circular-cylindrical pressure vessel can be considered, in which stresses in the vessel wall result in internal pressure loading which are approximately twice as great in the circumferential direction as in the longitudinal direction.
- an oval shape is to be understood quite generally as an elongated round shape, of which e.g. an elliptical shape would represent a special case.
- the ovalization of the connection in the mentioned main voltage direction not only has a significant influence on the reduction of the maximum voltages that occur in the pressure vessel wall. They can be used to shift the voltages that occur to other areas, e.g. in those where there are no weld lines or sharp edges and where they have a less adverse effect.
- a certain disadvantage is the reduction in the cross-section available, for example, for a flow, which is associated with ovalization, if this is brought about from a circular cross-sectional shape by flattening this shape or by reducing an axis.
- it is sufficient to carry out the ovalization only directly in the connection area and to continuously change back to a circular tube shape within a relatively short distance.
- the length of this transition section L can e.g. are in the order of magnitude of the diameter of the circular shape of the connecting pipe, or may also be very short.
- Such a limited cross-sectional reduction only causes small pressure losses, which are usually negligible in relation to the losses of an overall system.
- the invention naturally also includes pressure vessels which are not flowed through and are under static pressure.
- pressure vessel and / or the tubular connection is to be understood very generally within the scope of the present invention.
- a pipe bend can be understood as a limit case of a cylindrical pressure vessel closed on one side and reduced in diameter with a pipe socket attached to the side at the closed end, whereby there is no longer even a difference between the part serving as pressure container and the part serving as pipe socket.
- a pipe bend can also be regarded as a one-armed T-piece.
- pressure vessel should not be interpreted restrictively in the sense that it always only has an internal overpressure compared to e.g. external normal pressure is loaded.
- inventive principle and the resulting geometry remain the same for every pressure difference situation and thus also for an external overpressure compared to e.g. an internal normal pressure, such as this e.g. in the case of submarines or the like. This means that it can be used both as an internal pressure vessel and as an external pressure vessel.
- the pressure container according to the invention can be a gas generator housing for at least one airbag, as is increasingly used in automobile construction.
- This is a pressure container through which a gaseous medium is directed into the corresponding air bags after the airbag has been triggered. This creates very high pressures in a very short time, which the housing has to withstand.
- Figure 1 is a perspective view of a cylindrical container with an oval pipe socket attached.
- Fig. 2 under a) in a sectional view the housing of a water meter with two opposite tubular connecting pieces, under b) a side view and under c) a top view of the same housing; 3 under a) - d) each quarter segments of a housing corresponding to that of Fig.
- FIG. 5 shows in a view and in several cross sections a T-piece ovalized according to the invention
- FIG. 6 shows a pipe bend ovalized according to the invention, cut open in a perspective view
- FIG. 9 sectional drawings through a gas generator housing for a head airbag system.
- a pressure vessel 1 shows, as a first simple example, a pressure vessel 1 with a circular cylindrical cross section, to which a pipe socket 2 is connected laterally to the lateral surface. If you think away the connection piece 2, then three main stresses can be specified at the connection point of the pipe socket for a load that occurs when the pressure vessel is placed under an internal overpressure. Under the junction of the For example, the raw connector should be understood to be the point of impact P of the connector axis A on the wall of the container 1. Because of the circular cylindrical shape of the pressure vessel 1, the tension in the circumferential direction is approximately twice as great as the tension in the longitudinal direction of the jacket.
- the pipe socket 2 oval in cross-section and by aligning the large axis of the oval shape in the circumferential direction of the container 1 and thus in the direction of the first main stress, a reduction of the stresses and a favorable distribution of the stresses, especially in the connection area of the Pipe socket 2 reached.
- the small axis of the oval shape is oriented perpendicular to the large axis and thus in the longitudinal direction of the jacket.
- Fig. 2 shows under a), b) and c) a pressure vessel 3, as e.g. used for water meters in three views.
- the pressure vessel 3 has an essentially cylindrical main body 4, which in the present example is closed at the bottom by a spherical cap.
- Two connecting pieces 5 and 6 are attached to the side of the cylindrical part 4.
- the connecting piece 5 is oval in the transition region L and the cut surface of its connection point and is therefore designed according to the present invention.
- the direction of the major axis of the oval shape is, as can be seen under b), oriented in the circumferential direction of the cylindrical part.
- the large axis corresponds to the circular diameter of the connecting pipe, as can also be seen in the top view under c).
- the maximum reference voltages occurring in the connection area are thereby reduced and at the same time shifted.
- the oval cross section changes into a circular cross section, as a result of which the connecting piece can be connected to other pipelines or the like much more easily, for example also by means of a screw connection.
- the transition length L between the oval shape and the circular shape is chosen so that there is a relatively smooth transition and no additional stresses are generated. In the example, the transition length L corresponds to approximately half the diameter of the circular shape.
- the connecting piece 6 is not ovalized and is therefore not designed according to the invention. It is used here only for a comparative representation of the state of the art.
- 3 shows under a) - d) each quarter segment 7 of a housing corresponding to that of FIG. 2 but with differently shaped connecting pieces 8.1. - 8.4, whereby the shading indicates the arithmetically resulting stress state with an internal pressure load.
- the connection stubs are designed to be closed only for computational reasons.
- the stress state calculation is based on a finite element model.
- the inherently multidimensional stress state is indicated by a scalar quantity, the so-called comparative or von Mieses stress ⁇ v , which can be derived from the stress state in a defined manner known to the person skilled in the art. This type of characterization of the stress state is also used in the context of FIGS. 4, 7 and 8 described below.
- Figure a shows the case with a connection piece with a circular cross-section as a reference, whereby a diameter of 40 mm was assumed for the calculation, which is a common pipe diameter e.g. of water pipes.
- High voltage concentrations can be seen in zones I and II (white areas in FIG. 3a)).
- a weld line also results approximately along the cutting edge designated 9 in the direction of flow behind the connecting piece 8.1 by the confluence of two melt streams in the injection mold. Since this coincides with zone II of high voltage, two unfavorable influencing factors with regard to the strength of the container accumulate here.
- the sequence of images b) - c) and d) shows how the tensions in areas I and II are reduced and also shifted.
- the ovality is 40:32
- the second number corresponds to the length of the small axis d in millimeters, while the large axis D was left at the aforementioned 40 mm of the circular reference cross section.
- the most favorable case is likely to be shown in Figure c), since there are hardly any stress concentrations and the stresses are fairly evenly distributed at a comparatively low level.
- a zone of high voltage has already formed again in area III.
- the influence of the nozzle ovality on the maximum comparison voltage is additionally shown in FIG. 4 in the form of a bar diagram, with additional ones in addition to FIG. 3 Ovalities are taken into account.
- the ovality varies along the horizontal axis, which is expressed on the one hand by the ratio D / d of the length D of the long axis to the length d of the short axis, for example in millimeters.
- the resulting ratio for the ovality O is also given in each case.
- the height of the hatched bars indicates, in relative unit ⁇ v, on the one hand the maximum reference stress occurring at I or II, referred to as local, while the height of the non-hatched bars indicates the maximum reference stress somewhere, referred to as global, in Figure d) e.g.
- the local maximum comparison voltage is identical to the global one.
- the local as well as the global maximum reference stress starting from the round cross-section (ovality 40:40 or 1), initially decreases with increasing ovality.
- the global maximum comparison voltage only increases again from the middle of the diagram, because from here a voltage zone begins to form in area III.
- the local maximum comparison voltage in areas I and II continues to decrease.
- the ovality is suitably dimensioned according to the voltage profiles shown in FIG. 4, an ovality in the range from 1.5 to 1.7 being suitable, for example. Taking into account the reduced material strength along the weld line of injection molded parts and if a maximum burst pressure for the component is to be reached, it may also make sense to choose the ovality in the range in which the global maximum reference stress is already rising again.
- the global as well as the local maximum comparison voltage can be reduced by more than 50%.
- FIG. 4 On the far right in FIG. 4, the case is shown for comparison, which would result for a round cross section without ovality with a diameter of 30.6 mm. With this diameter, the cross-sectional area is the same as in the case and 24 mm. It can be seen from the height of the bars in this case that a simple reduction in cross-section without simultaneous ovalization cannot achieve the effect of a well-known stress reduction which is desired according to the invention. Conversely, one could also say that the reduction in the maximum reference stress is primarily due to the ovalization and only to a small extent to the decrease in the free cross-section due to the reduction in the minor axis according to FIG. 4 (variant 40:24) , As a further application example for the teaching according to the invention, FIG.
- FIG. 5 shows a T-piece 10 with three ovalized connections 11, 12 and 13, which all lie in the same plane (drawing plane) and also have approximately the same cross section.
- the large axis of the oval shape of the three connections is selected according to the invention perpendicular to the plane mentioned.
- the opposite connections 11 and 12 could, for example, be equated with the container 1 of FIG. 1, the connection 13 in this case corresponding to the pipe socket 2.
- all three connections are ovalized here, as can also be seen from the cross sections BB and CC shown. In principle, however, it would also be possible to ovalize only two of the three connections, for example the connections 11 and 12, or only one of the connections, for example the connection 13.
- the oval cross-section of all three connections is converted back to their free ends over a relatively short distance into a round cross-sectional shape, so that in each case round pipes can be connected to the connections, for example via a screw connection.
- the round cross sections are denoted by AA or DD in FIG. 5.
- FIG. 6 shows a special case, namely a pipe bend 14 which can be produced by injection molding and is cut open in a perspective view, in which sharp edges result from the production.
- the two connecting pieces 15 and 16 are each ovalized. The big axis of the oval.
- the shape of both connections is perpendicular to the pipe bend plane. No use has been made of a transition to a round cross section towards its free ends. However, this would be possible and is preferred in itself.
- the connection 15 is shown closed again for purely computational reasons.
- FIG. 7 shows under a) - d) half shells of pipe elbows corresponding to that of FIG. 6 but with different ovality, the shading, as already shown in FIG. 3, identifying the resulting stress condition with an internal pressure load.
- Figure a) of Fig. 7 initially shows the case with a round, not as a reference ovalized cross section. Particularly high comparative stress concentrations can be seen in area I (white area).
- FIG. 8 shows the four cases of FIG. 7 in a bar diagram corresponding to FIG. 4, the local and global maximum comparison voltages also being shown next to one another as in FIG. 4.
- the diagram clearly shows that the optimal effect should be around 20:16.
- the global maximum comparison stress is reduced by approx. 47% compared to the round reference shape, and the local maximum comparison stress on the inside of the curve is even reduced by approx. 65%.
- FIG. 9 schematically shows an example of a gas generator housing of an airbag.
- This is a head airbag module.
- the ignition device and the gas source are integrated into the housing in the form of a gas cartridge via the installation position 19.
- the gas flows out of the gas cartridge through the oval opening 18 aligned according to the invention, and the gas flow is distributed over the outlets (sockets) 20 and 21, each of which has an airbag (“airbag”) attached a head airbag system for a front and font head airbag is shown schematically, as it is installed laterally in the top center of an automobile, such a gas generator housing could also have an outflow opening 18 for each outlet 20, 21.
- the invention can be used with particular advantage in the case of injection-molded parts, because in many geometric shapes, weld lines cannot be avoided precisely where the highest stresses occur due to the geometry.
- Suitable materials for the injection molding of the above-described molds include thermoplastic materials, in particular those made from a glass fiber reinforced polymer, the polymer advantageously being selected from the group of polyamides and copolyamides and having a melting point of at least 250 ° C., such as PA66 and PA46. It is particularly preferred to use a polymer which is a partially aromatic, partially crystalline copolyamide with a melting point in the range from 300 ° C. to 350 ° C. Such particularly well suitable polymer is available, for example under the name "GRIVORY ® HTV-5H1" by the company Ems-Chemie AG / Ems-Grivory, Domat / Ems, Switzerland, in the trade.
- PA 6T / 6I reinforced with 50% by weight glass fibers (based on the total weight) with a melting point of 325 ° C, i.e. a partially aromatic, partially crystalline copolyamide from the monomer components hexamethylenediamine, terephthalic acid and isophthalic acid.
- the material is generally particularly suitable for the production of extremely stiff, solid, heat-resistant and dimensionally accurate injection molded parts and is also characterized by very good chemical resistance.
- the melt temperature during injection molding is approx. 345 ° C.
- pressure vessels can not only be made from plastics, but in principle from all suitable materials.
- the invention can also be used in metal container construction.
- the invention can be used particularly advantageously in die-cast metal (eg aluminum).
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- External Artificial Organs (AREA)
- Air Bags (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Stackable Containers (AREA)
- Tubes (AREA)
- Closures For Containers (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020047012739A KR100718945B1 (en) | 2002-02-22 | 2003-02-20 | Pressure container with tube connection |
AU2003205485A AU2003205485A1 (en) | 2002-02-22 | 2003-02-20 | Pressurised container comprising a tubular connection |
DE50305953T DE50305953D1 (en) | 2002-02-22 | 2003-02-20 | PRESSURE CONTAINER WITH TUBULAR CONNECTION |
DK03702257T DK1476694T3 (en) | 2002-02-22 | 2003-02-20 | Pressure vessel with tubular connections |
JP2003570053A JP4257212B2 (en) | 2002-02-22 | 2003-02-20 | Pressurized container with tubular joint |
EP03702257A EP1476694B1 (en) | 2002-02-22 | 2003-02-20 | Pressurised container comprising a tubular connection |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10207613.8 | 2002-02-22 | ||
DE10207613A DE10207613C1 (en) | 2002-02-22 | 2002-02-22 | Injection molded pressure vessel, with a pipe connection at a side wall, has an oval shape for the wall opening and the end of the pipe at the connection for increased strength |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003071181A1 true WO2003071181A1 (en) | 2003-08-28 |
Family
ID=7713918
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CH2003/000126 WO2003071181A1 (en) | 2002-02-22 | 2003-02-20 | Pressurised container comprising a tubular connection |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP1476694B1 (en) |
JP (1) | JP4257212B2 (en) |
KR (1) | KR100718945B1 (en) |
AT (1) | ATE348288T1 (en) |
AU (1) | AU2003205485A1 (en) |
DE (2) | DE10207613C1 (en) |
DK (1) | DK1476694T3 (en) |
ES (1) | ES2279091T3 (en) |
WO (1) | WO2003071181A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008054103A1 (en) | 2008-10-31 | 2010-05-06 | Friatec Aktiengesellschaft | Component for applications in the service and / or wastewater sector and shut-off valve with such a device |
DE102009018056B4 (en) * | 2009-04-21 | 2011-01-20 | Qundis Gmbh | Water / heat meter with a transmitter housing and method for producing a transmitter housing |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3342209A (en) * | 1963-08-21 | 1967-09-19 | Hiltscher | Unsymmetrical connection-piece nozzle |
DE2224454A1 (en) * | 1972-05-19 | 1973-11-29 | Goeppner Kaiserslautern Eisen | ARRANGEMENT OF TUBULAR CONTAINERS |
EP0552710A1 (en) * | 1992-01-24 | 1993-07-28 | TECNO PLASTIC S.r.l. | Branch piece for plastics ducts or tanks |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR404634A (en) * | 1900-01-01 | |||
DE69108084T2 (en) * | 1990-04-20 | 1995-11-23 | Applied Materials Inc | Vacuum pressure container and its manufacturing process. |
-
2002
- 2002-02-22 DE DE10207613A patent/DE10207613C1/en not_active Expired - Fee Related
-
2003
- 2003-02-20 ES ES03702257T patent/ES2279091T3/en not_active Expired - Lifetime
- 2003-02-20 EP EP03702257A patent/EP1476694B1/en not_active Expired - Lifetime
- 2003-02-20 WO PCT/CH2003/000126 patent/WO2003071181A1/en active IP Right Grant
- 2003-02-20 DE DE50305953T patent/DE50305953D1/en not_active Expired - Lifetime
- 2003-02-20 DK DK03702257T patent/DK1476694T3/en active
- 2003-02-20 KR KR1020047012739A patent/KR100718945B1/en not_active Expired - Fee Related
- 2003-02-20 AT AT03702257T patent/ATE348288T1/en not_active IP Right Cessation
- 2003-02-20 JP JP2003570053A patent/JP4257212B2/en not_active Expired - Fee Related
- 2003-02-20 AU AU2003205485A patent/AU2003205485A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3342209A (en) * | 1963-08-21 | 1967-09-19 | Hiltscher | Unsymmetrical connection-piece nozzle |
DE2224454A1 (en) * | 1972-05-19 | 1973-11-29 | Goeppner Kaiserslautern Eisen | ARRANGEMENT OF TUBULAR CONTAINERS |
EP0552710A1 (en) * | 1992-01-24 | 1993-07-28 | TECNO PLASTIC S.r.l. | Branch piece for plastics ducts or tanks |
Also Published As
Publication number | Publication date |
---|---|
ES2279091T3 (en) | 2007-08-16 |
JP2005527415A (en) | 2005-09-15 |
EP1476694B1 (en) | 2006-12-13 |
DE50305953D1 (en) | 2007-01-25 |
JP4257212B2 (en) | 2009-04-22 |
EP1476694A1 (en) | 2004-11-17 |
KR100718945B1 (en) | 2007-05-16 |
DK1476694T3 (en) | 2007-04-10 |
KR20040105722A (en) | 2004-12-16 |
DE10207613C1 (en) | 2003-04-10 |
ATE348288T1 (en) | 2007-01-15 |
AU2003205485A1 (en) | 2003-09-09 |
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