WO2020173690A1 - Composant de structure pour un cadre de châssis et procédé pour sa fabrication - Google Patents
Composant de structure pour un cadre de châssis et procédé pour sa fabrication Download PDFInfo
- Publication number
- WO2020173690A1 WO2020173690A1 PCT/EP2020/053233 EP2020053233W WO2020173690A1 WO 2020173690 A1 WO2020173690 A1 WO 2020173690A1 EP 2020053233 W EP2020053233 W EP 2020053233W WO 2020173690 A1 WO2020173690 A1 WO 2020173690A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- flange
- storage container
- groove
- structural component
- connecting element
- 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.)
- Ceased
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D21/00—Understructures, i.e. chassis frame on which a vehicle body may be mounted
- B62D21/02—Understructures, i.e. chassis frame on which a vehicle body may be mounted comprising longitudinally or transversely arranged frame members
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D21/00—Understructures, i.e. chassis frame on which a vehicle body may be mounted
- B62D21/16—Understructures, i.e. chassis frame on which a vehicle body may be mounted having fluid storage compartment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/001—Superstructures, understructures, or sub-units thereof, characterised by the material thereof characterised by combining metal and synthetic material
- B62D29/004—Superstructures, understructures, or sub-units thereof, characterised by the material thereof characterised by combining metal and synthetic material the metal being over-moulded by the synthetic material, e.g. in a mould
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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
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/084—Mounting arrangements for vessels for small-sized storage vessels, e.g. compressed gas cylinders or bottles, disposable gas vessels, vessels adapted for automotive use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D21/00—Understructures, i.e. chassis frame on which a vehicle body may be mounted
- B62D21/02—Understructures, i.e. chassis frame on which a vehicle body may be mounted comprising longitudinally or transversely arranged frame members
- B62D21/03—Understructures, i.e. chassis frame on which a vehicle body may be mounted comprising longitudinally or transversely arranged frame members transverse members providing body support
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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
- 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
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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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0123—Shape cylindrical with variable thickness or diameter
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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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/03—Orientation
- F17C2201/035—Orientation with substantially horizontal main axis
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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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
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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
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0604—Liners
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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
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0619—Single wall with two layers
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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
- F17C2203/066—Plastics
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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
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0103—Exterior arrangements
- F17C2205/0119—Vessel walls form part of another structure
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0153—Details of mounting arrangements
- F17C2205/0192—Details of mounting arrangements with external bearing means
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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
- F17C2209/2154—Winding
- F17C2209/2163—Winding with a mandrel
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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
- F17C2209/227—Assembling processes by adhesive means
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/031—Air
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0107—Single phase
- F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/035—High pressure (>10 bar)
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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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/012—Reducing weight
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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
- F17C2260/018—Adapting dimensions
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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
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
- F17C2270/0171—Trucks
Definitions
- the invention relates to a structural component for a chassis frame of a vehicle with at least one flange end for fastening the structural component to the chassis frame, and a storage container.
- the storage container is connected to the at least one flange end via a connecting element, a connecting area being formed between these elements.
- this connecting element there is at least one
- Adhesive connection provided.
- the invention also relates to a method for producing such a structural component.
- Chassis frames for vehicles usually have two longitudinal members and several cross members. Typically these are made from steel components.
- cross members were known which are made from material combinations, for example from steel components and fiber composite laminates.
- the stresses resulting from the different coefficients of thermal expansion are present in particular when the joining partners are joined entirely or partially with an adhesive joint in addition to the connection by means of a fiber composite laminate.
- the composite experiences high temperatures for curing over a certain period of time.
- the laminate hardens and the adhesive fully crosslinks. At this high temperature there is no tension in the structural component formed in this way.
- stresses form in the boundary layers and in the adhesive layer of the joining partners due to the different coefficients of thermal expansion. As already described, this can lead to disruptions in the transmission of loads and even failure of the entire structural component.
- the invention is now based on the object of proposing a structural component and a method for its production that allows functional integration and the use of different materials and joining techniques, while avoiding the damage caused by the stresses mentioned.
- a structural component for a chassis frame of a vehicle has at least one flange end and a storage container.
- the flange end is designed for fastening the structural component to the chassis frame.
- the storage container is a liner, that is to say a
- Hollow body that can take up, contain and release a medium.
- a storage container usually has at least one end at which or through which it can be placed in a receptacle provided for this purpose. For example, such a
- Storage container has a convex inner shape and an overall elongated outer contour, so that the two end faces of the shape of the storage container thus formed form the respective ends.
- the at least one flange end has a flange receptacle which loosely receives the storage container at the end.
- the device according to the invention consequently has at least one flange receptacle, which is why this formulation is also used synonymously in the following text. Accordingly, the end of the storage container is in the at least one
- Flange mount inserted, inserted or otherwise placed in it. Only a form fit is achieved, but no force-fit or material connection.
- the storage container is at least partially along its outer surface with an as
- Fiber composite laminate executed connecting element envelops, which at least partially surrounds the flange receptacle of the at least one flange end in a connection area.
- Under fiber composite laminate is a fiber plastic composite made of a
- Plastic matrix can be understood as bedding compound and reinforcing fibers, in particular carbon fibers, embedded in the bedding compound.
- the process used for this is usually also referred to as the wet winding process.
- the at least partial wrapping that is, the wrapping of at least a partial area of the outer surface of the storage container with the reinforcing fibers, is
- Connecting element formed. It is designed or configured in such a way that when the storage container is inserted into the at least one flange receptacle, it at least partially engages around, in other words, overlaps it. This area in which the overlap or encompassing is achieved is referred to below as the connection area.
- the connecting element By designing the connecting element as a fiber composite laminate, the design of the shape of the storage container is not limited to circular cylindrical geometries, but can be freely selected.
- the outer surface of the storage tank can also be completely or partially enveloped by means of the RTM process (abbreviation: Resin Transfer Molding).
- RTM process abbreviation: Resin Transfer Molding
- This is a resin injection process in which reinforcing fibers, in particular carbon fibers, are applied and only impregnated afterwards.
- Plastic matrix made of a thermosetting plastic is used as bedding material, such as polyester, epoxy or phenolic resin, in which reinforcing fibers are in turn embedded.
- bedding material such as polyester, epoxy or phenolic resin, in which reinforcing fibers are in turn embedded.
- the fibers used are almost completely utilized can.
- the fibers are deposited around a shaping core, which corresponds to the winding core of the wet winding process and specifies the shape of the component to be manufactured.
- the fibers are placed or braided around the shaping core in such a way that they form the contour of the component to be produced, with neither folds nor holes forming in the braid to be produced.
- the fibers are then injected, for example with an epoxy resin.
- connection element in particular if no storage container is required, or if the fiber composite laminate is to be manufactured with a constant cross section, is the pultrusion process, i.e. a drawing process for manufacturing the fiber composite laminate.
- connection area at least one groove for receiving an adhesive is provided on the surface of the at least one flange receptacle facing the connection element.
- at least one injection opening is made in the connection element, corresponding to the at least one groove. It is therefore provided that at least one injection opening is made in the connection area in the connection element, and at least one groove is also provided in the connection area on the surface of the at least one flange receptacle facing the connection element.
- the at least one injection opening and the at least one groove should correspond to one another, that is to say they should be arranged such that an adhesive can be introduced into the at least one groove through the at least one injection opening.
- Several injection openings can also be made in the connecting element, all of which correspond to one and the same groove. There can also be several grooves in one
- Connection area can be provided, each with one or more
- the adhesive is introduced into the at least one groove through the at least one injection opening and cured, so that the connecting element is fixed to the at least one flange end and thus the storage container is indirectly fixed to the at least one
- the Flange mount is connected.
- the connecting element is firmly connected, ie glued, to the at least one flange end by means of an adhesive that has been injected through at least one injection opening into at least one groove and cured there.
- the storage container is indirectly fixed to the flange receptacle at the same time.
- the storage container is thus arranged in a fixed position in the structural component, but is not directly connected to the flange receptacle, they are indirectly connected via the connecting element and the adhesive connection.
- the storage container can contract within the space available between the inner surface of the fiber composite laminate and its outer surface when the temperature drops and expand when the temperature increases.
- the structural component according to the invention and the storage container arranged therein form in their entirety a pressure tank.
- the storage container should be selected so that it can hold a medium and preferably have at least one opening for introducing and / or removing a medium at at least one of its ends, which opening corresponds to a corresponding opening in the associated flange end.
- the medium can be pressurized air, but also other gaseous or liquid media.
- the storage container represents a sealing layer, while the connecting element enveloping the storage container absorbs the pressure loads or the mass loads when the storage element is filled with a medium.
- the storage container can serve as an envelope core during the production of the structural component when the fiber composite laminate is applied, as will be explained below.
- the storage container can, for example, made of a plastic material, in particular a thermoplastic, particularly preferably made of polyethylene, polyamide or
- the flange end of the structural component can be made from one or more lightweight materials, such as aluminum.
- a very low weight is achieved, so that a structural component according to the invention also has only a low weight in its entirety.
- installation space can be created that previously had to be found outside the structural component.
- the structural component has the necessary stability and strength, while at the same time it has a low weight.
- the inside contour of the flange mount should therefore be shaped in such a way that it corresponds to the outer contour of the storage container to be received and a form fit is brought about when the storage container is positioned, i.e. inserted or plugged into the flange receptacle.
- the flange receptacle can be designed like a shell, and the outer contour of one end of the storage container can be designed to correspond to it, that is to say, for example, like a cap.
- the adhesive which is injected through the at least one injection opening into the at least one groove is based on acrylate, epoxy resin and / or based on polyurethane.
- the adhesive should therefore essentially be formed with acrylates, epoxy resins and / or polyurethane.
- reactive, two-component acrylate-based adhesives are ideal for bonding metals with coated surfaces and plastics.
- Epoxy resin adhesives are extremely strong.
- Polyurethane adhesives are suitable for bonding larger areas of a wide variety of materials, especially for components that are permanently or temporarily exposed to vibrations.
- the at least one groove is formed circumferentially around the flange receptacle. This is to be understood as meaning that the groove in the connection area is preferably continuous along the entire length of the
- Connecting element facing surface of the flange receptacle is formed. If, for example, the flange receptacle is designed to be rotationally symmetrical, in this preferred embodiment the groove is guided around the entire circumference of the surface of the flange receptacle facing the connecting element and thus forms one
- the width of the at least one groove is approximately 60% to 95% of the width of the connecting area.
- the overlap area between the at least one flange receptacle and the connecting element forms the connecting area.
- the amount by which the connecting element overlaps the flange mount is to be referred to as the width of the connecting area.
- the width of the groove should have the same orientation and denote the area which is within this connection area and in the same direction as the width of the
- Connection area indicates the dimension of the groove.
- the width of the groove is dependent on the geometric conditions and the loads that occur customized.
- the width of the groove, but also its length and depth, must be adapted to the respective conditions.
- the width of the groove should be in the range of about 60% to 95% of the width of the
- connection area The geometric dimensions of the groove can optionally be reduced or adapted if more than one groove is in / on one
- Flange mount is provided.
- At least one injection opening which corresponds to the at least one groove, must be provided in the connecting area of the connecting element.
- the number of injection openings can also vary and be adapted to suit the situation.
- the structural component is designed as a cross member in a chassis frame, the two flange ends with one each
- Chassis frame are arranged in a vehicle and is designed for this purpose. It has two flange ends, each one in turn
- the storage container is between the two
- Flange mounts arranged, these receiving the storage container loosely at its respective ends, so only by means of a form fit.
- the storage container the outer contour of which corresponds to the inner contours of the flange receptacles, is inserted into the latter.
- a connection area is thus formed between the respective flange receptacle and the connection element, in which one
- Flange mount at least partially encompassed by the connecting element
- the respective flange receptacle has at least one groove on the surface facing the connection element, and in the
- At least one injection opening is introduced in each case in the connection area corresponding to the at least one groove.
- a flange end with a flange receptacle is thus arranged in each end of the storage container, and at least one groove is provided in each of the two flange receptacles and at least one injection opening is in each case in the connecting areas in the
- Connecting element introduced. This ensures that the connecting element after Injecting and curing the adhesive is firmly connected to both flange ends and thus the storage container is indirectly firmly connected to the two flange receptacles.
- the structural component formed in this way can now be used as a cross member between the longitudinal members of a
- Chassis frame of a vehicle are installed, wherein the forces acting on the flange ends are advantageously transmitted via the connecting element, while the storage container stores the medium to be accommodated and thereby assumes a sealing function.
- the structural component according to the invention is carried out using a method with at least the following steps:
- Flange mount has at least one groove
- At least one flange end with a flange receptacle and the storage container are initially manufactured.
- the storage tank is finished, it is
- the at least one injection opening can be made in the area of the connecting element which, when all elements are joined together, the connecting area with the
- the at least one injection opening should be introduced into the connecting element in such a way that, after being inserted into the flange receptacle, it corresponds to the at least one groove of the flange receptacle. Subsequently, the storage container is plugged or inserted into the at least one flange receptacle, which the Storage container loosely takes up the end.
- the flange end and the storage container, which is at least partially enclosed by the connecting element are aligned with one another, that is, with one another, that the at least one groove of the at least one
- Flange receptacle correspond to the at least one injection opening of the connecting element.
- Flange mount is connected.
- each of these flange mounts having at least one groove.
- Fiber composite laminate introduced in each of the two resulting connecting areas at least one injection opening.
- the storage container is now inserted at the end into the two flange receptacles and loosely received by them.
- the flange ends and the storage container must be aligned with one another in such a way that the at least one injection opening per connection area in the connection element corresponds to the at least one groove of the respective flange receptacle.
- the adhesive can then be introduced into the respective injection openings and cured.
- the storage container Enveloping the storage container in a winding device, the storage container being arranged in, on and / or between two winding cores.
- the storage container is therefore used, for example, between two winding cores and then in the
- the connecting element enveloping the storage container is cut to size after hardening, that is, areas that are not required or that are made too large for joining with the at least one flange receptacle are separated. Also adjustments to special geometric Requirements can be realized by cutting, such as cutouts.
- the injection and curing of the adhesive is carried out at a temperature equal to or below 40 degrees Celsius, very particularly preferably below 25 degrees Celsius.
- the joining of the at least one flange end to the storage container and the gluing can thus take place at a temperature which approximately corresponds to the temperatures in the later state of use. This has the advantage of being joined and glued
- a structural component according to the invention and the method according to the invention for producing this structural component allow a functional integration in the form of a storage container that is located within a structural component, such as, for example, in a cross member for a
- Chassis frame of a vehicle is arranged, and so to save space and weight at the same time, and yet to meet the requirements of such a structural component in terms of stability and strength.
- the adhesive connection between the connecting element and the at least one flange receptacle is a particular advantage: on the one hand, this creates a firm connection between the connecting element and the flange end and, at the same time, an indirect, firm connection between the storage container and the flange receptacle, so that the storage container can move within the space available if the temperature increases expand and contract when the temperature drops.
- a temperature range can be selected independently of the lamination and curing of the fiber composite laminate, in which the risk of damage as a result of
- Figure 1 shows a chassis frame 100 of a utility vehicle N in a perspective
- FIG. 2 shows a sectional view of a cross member 1, T as a structural component 10 according to the prior art
- FIG. 3 shows a perspective illustration of the structural component 10 according to the invention in a production step
- FIG. 4 shows a perspective illustration of the structural component 10 according to the invention in a next production step
- FIG. 5 shows a perspective illustration of the structural component 10 according to the invention in a production step but one
- FIG. 6 shows a sectional illustration of the structural component 10 according to the invention in a further production step
- FIG. 7 shows a sectional illustration of a detail A from FIG.
- the direction lying in the vehicle is designated with “x”, the horizontal direction perpendicular to the x-direction is designated with “y” and the vertical direction perpendicular to the x-direction is designated with “z”.
- FIG. 1 shows a chassis frame 100 of a vehicle, in particular one
- the utility vehicle N comprises a plurality of wheel axles Y1, Y2 and Y3 which are arranged transversely to the longitudinal members 2 of the chassis frame 100.
- the chassis frame 100 has a plurality of cross members 1, T, at least one cross member 1, T being arranged parallel to a wheel axis Y2, Y3 at least close to an axle suspension.
- the extracted detail I shows a cross member 1, T, in the axial extension of which in the y-direction the axle suspension 3 is formed.
- the cross member marked T is designed without an axle suspension 3.
- a structural component 10 according to the invention can be designed as a cross member 1, 1 ′ for such a chassis frame 100 and can be designed with or without axle suspension 3.
- the cross member 1, 1 ‘shown in Figure 1 can be made in one piece from cast iron or as
- cross members 1, T were known in the prior art as structural components 10 with an integrated storage container 10E, as is shown by way of example in FIG.
- the structural component 10 shown in a section has a storage container 10E and two flange ends 10A, each with a flange receptacle 10A-2.
- the storage container 10E and the flange ends 10A are connected via a connecting element 10B, which as
- Fiber composite laminate is formed, at least partially enveloped.
- Fiber composite laminate takes place in the wet winding process, the storage container 10E being arranged between the flange ends 10A and then the flange ends 10A and the storage container 10E in their entirety being fed to the wet winding process.
- the structural component 10 formed in this way then experiences a curing process as a whole at elevated temperatures.
- the flange ends 10A can be glued to the storage container 10E.
- an adhesive 60 must be used before
- the fiber composite laminate and the adhesive 60 are cured and crosslinked at high temperatures. This creates a stress-free in this high temperature range
- the method according to the invention for producing a structural component 10 according to the invention is selected individually in a preferred embodiment as a cross member for a chassis frame 100 of a utility vehicle N
- two flange ends 10A which are later used to fasten the structural component 10 to the longitudinal members 2 of the chassis frame 100, are produced.
- the two flange ends 10A each have one
- Flange mount 10A-2 In these flange mounts 10A-2, in turn, is on the
- Connecting element 10B in the connecting region 40 which is then formed faces, each having a groove 50 formed.
- a storage container 10E which has at least one opening for filling and / or removing a medium.
- Storage container 10E corresponds to the inner contour of the flange receptacles 10A-2.
- FIG. 3 shows a perspective illustration of the structural component according to the invention in a production step.
- the previously manufactured storage container 10E is arranged at the end between two winding cores 80, each of which has an angular comb 20.
- This arrangement of storage container 10E and Wckelkern 80 is inserted into a Wckel device 70 (not shown) and there for example using the winding combs 20 with a wet winding process at least partially wrapped and cured with a fiber composite laminate.
- the coating can also be carried out using the RTM process (abbreviation: Resin Transfer Molding).
- FIG. 4 the storage container 10E, encased by the connecting element 10B, with the angular cores 80 is shown in a perspective view, as they are removed from the angular device 80 after the fiber composite laminate has hardened and cooled. Now protruding areas of the connecting element 10B forming
- Fiber composite laminate separated or trimmed This so-called waste is now removed and the angular cores 80 are removed.
- the angular cores 80 can first be removed and then the fiber composite laminate cut to size.
- this blank can also meet specific requirements for the geometry of the connecting element 10B, for example in the form of cutouts.
- FIG. 5 shows the cut connecting element 10B, which encloses the storage container 10E, in a perspective view. Two at least partially protruding areas can be seen, which after the storage container 10E has been inserted into the
- Flange receptacles 10A-2 for forming a cross member for a chassis frame 100 of a utility vehicle N form the connecting areas 40. At least one injection opening 30 is made in each of these connecting areas, for example by drilling. These injection openings 30 are introduced in such a way that, after the joining of the
- Storage container 10E with the flange ends 10A correspond to the grooves 50 provided on the flange receptacles 10A-2.
- FIG. 6 shows a sectional illustration of a structural component 10 according to the invention embodied as a cross member for a chassis frame 100 of a utility vehicle N.
- the sub-area marked “A” therein is shown in more detail in FIG.
- the storage container 10E covered with the connecting element 10B is inserted at the end into the flange receptacles 10A-2 of two flange ends 10A, where it is loosely received.
- the storage container 10E is aligned with the connecting element 10B surrounding it in such a way that the injection openings 30 in the connecting areas 40 correspond to the grooves 50 of the flange receptacles 10A-2.
- FIG. 7 the detail area marked "A" in FIG. 6 is shown enlarged. The corresponding arrangement of injection opening 30 and groove 50 can be seen.
- the width b of the groove 50 corresponds to approximately 60% to 95% of the width bv of the connecting area. According to the definition of the coordinate system given above, the width b and the width b are aligned along the y-direction. In order to ensure a secure and permanent bond between the connecting element 10B and the flange receptacles 10A-2, the groove 50 is on each of the two
- Flange receptacles 10A-2 are each formed circumferentially around the entire surface facing the connecting element 10B.
- An adhesive 60 which is formed on the basis of polyurethane, is introduced through the injection openings 30 and fills the groove 50 largely completely.
- the introduction of the adhesive 60 can advantageously take place at room temperature, that is to say below 25 degrees Celsius.
- Epoxy resin base can be used. After the adhesive 60 has cured, the connecting element 10B is fixed to the
- connection area (40) bv width of the connection area (40)
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Structural Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
L'invention concerne un composant de structure pour un cadre de châssis d'un véhicule, en particulier en forme d'une traverse, dans lequel un réservoir de stockage est intégré et un procédé pour sa fabrication. Selon l'invention, la surface enveloppante du réservoir de stockage est enveloppée au moins partiellement par un élément de connexion, qui est conçu comme un stratifié de composite de fibres, et le composant de structure est en outre collé au moins par zones. Pour la fabrication du composant de structure, au moins une extrémité à bride comprenant une réception de bride et un réservoir de stockage sont préfabriqués. Le réservoir de stockage est reçu de manière lâche par l'au moins une réception de bride et collé à celle-ci. Pour cela il est nécessaire que, dans la zone de connexion dans laquelle la liaison adhésive doit être réalisée, du côté de la réception de bride au moins une rainure pour la réception d'une colle et du côté de l'élément de connexion au moins une ouverture d'injection, qui correspond à la rainure, sont prévues ou introduites. Après l'assemblage de tous les composants, la colle peut être introduite dans l'au moins une rainure par l'au moins une ouverture d'injection et durcie. Cela crée une liaison fixe directe entre extrémité à bride et élément de connexion et, résultant de celle-ci, une connexion fixe indirecte entre réception de bride et réservoir de stockage.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102019202745.8A DE102019202745A1 (de) | 2019-02-28 | 2019-02-28 | Strukturbauteil für einen Fahrgestellrahmen und Verfahren zu seiner Herstellung |
| DE102019202745.8 | 2019-02-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2020173690A1 true WO2020173690A1 (fr) | 2020-09-03 |
Family
ID=69582098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2020/053233 Ceased WO2020173690A1 (fr) | 2019-02-28 | 2020-02-10 | Composant de structure pour un cadre de châssis et procédé pour sa fabrication |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE102019202745A1 (fr) |
| WO (1) | WO2020173690A1 (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11167961B2 (en) * | 2019-11-21 | 2021-11-09 | Oceaneering International, Inc. | Apparatus and method for assisting deployment of coiled tubing |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116293390B (zh) * | 2023-03-31 | 2025-02-11 | 一汽解放汽车有限公司 | 一种lng气瓶 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000193194A (ja) * | 1998-12-25 | 2000-07-14 | Mitsubishi Chemicals Corp | 耐圧容器及びその製造方法 |
| DE102017204658B3 (de) * | 2017-03-21 | 2018-08-16 | Volkswagen Aktiengesellschaft | Strukturbauteil eines Fahrzeugrahmens mit einem integrierten Speicherbehälter mit einem Verbindungselement aus Faserverbundlaminat |
| DE102017106024A1 (de) | 2017-03-21 | 2018-09-27 | Scania Cv Ab | Strukturbauteil eines Fahrzeugrahmens mit einem integrierten Speicherbehälter |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3940250A1 (de) * | 1989-12-06 | 1991-06-13 | Bayerische Motoren Werke Ag | Behaelter in einem fahrzeug |
| SE518935C2 (sv) * | 2001-06-19 | 2002-12-10 | Scania Cv Ab | Anordning vid fordonsram till ett tungt fordon |
| DE102017007308A1 (de) * | 2017-08-02 | 2019-02-07 | Audi Ag | Anordnung eines Betriebsstoffbehälters an einer Karosseriestruktur eines Fahrzeugs |
-
2019
- 2019-02-28 DE DE102019202745.8A patent/DE102019202745A1/de not_active Withdrawn
-
2020
- 2020-02-10 WO PCT/EP2020/053233 patent/WO2020173690A1/fr not_active Ceased
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000193194A (ja) * | 1998-12-25 | 2000-07-14 | Mitsubishi Chemicals Corp | 耐圧容器及びその製造方法 |
| DE102017204658B3 (de) * | 2017-03-21 | 2018-08-16 | Volkswagen Aktiengesellschaft | Strukturbauteil eines Fahrzeugrahmens mit einem integrierten Speicherbehälter mit einem Verbindungselement aus Faserverbundlaminat |
| DE102017106024A1 (de) | 2017-03-21 | 2018-09-27 | Scania Cv Ab | Strukturbauteil eines Fahrzeugrahmens mit einem integrierten Speicherbehälter |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11167961B2 (en) * | 2019-11-21 | 2021-11-09 | Oceaneering International, Inc. | Apparatus and method for assisting deployment of coiled tubing |
Also Published As
| Publication number | Publication date |
|---|---|
| DE102019202745A1 (de) | 2020-09-03 |
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