EP3557117A2 - Pressure vessel and method for connecting a pressure vessel into a body structure - Google Patents
Pressure vessel and method for connecting a pressure vessel into a body structure Download PDFInfo
- Publication number
- EP3557117A2 EP3557117A2 EP19161168.0A EP19161168A EP3557117A2 EP 3557117 A2 EP3557117 A2 EP 3557117A2 EP 19161168 A EP19161168 A EP 19161168A EP 3557117 A2 EP3557117 A2 EP 3557117A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure vessel
- elements
- hollow cylindrical
- cylindrical extension
- winding
- 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.)
- Granted
Links
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- 238000004804 winding Methods 0.000 claims abstract description 53
- 239000000835 fiber Substances 0.000 claims description 11
- 238000003780 insertion Methods 0.000 claims description 11
- 230000037431 insertion Effects 0.000 claims description 11
- 239000004918 carbon fiber reinforced polymer Substances 0.000 claims description 10
- 239000011152 fibreglass Substances 0.000 claims description 8
- 229920003023 plastic Polymers 0.000 claims description 8
- 239000004033 plastic Substances 0.000 claims description 8
- 239000002131 composite material Substances 0.000 claims description 7
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 6
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 6
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 5
- 238000012546 transfer Methods 0.000 claims description 5
- 239000004917 carbon fiber Substances 0.000 claims description 4
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- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
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- 101710185324 GTP cyclohydrolase 1 feedback regulatory protein Proteins 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 3
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- 238000012805 post-processing Methods 0.000 claims description 2
- 238000006243 chemical reaction Methods 0.000 claims 1
- 229920001903 high density polyethylene Polymers 0.000 description 4
- 238000007493 shaping process Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000004046 wet winding Methods 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000000071 blow moulding Methods 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
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- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000003856 thermoforming Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Images
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
- 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
-
- 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
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
-
- 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
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0114—Shape cylindrical with interiorly 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
- F17C2203/0604—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
-
- 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
- F17C2203/0621—Single wall with three layers
-
- 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
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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
- F17C2205/0153—Details of mounting arrangements
-
- 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
- F17C2221/01—Pure fluids
- F17C2221/012—Hydrogen
-
- 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
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
-
- 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
-
- 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
- F17C2223/013—Single phase liquid
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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
- F17C2223/036—Very high pressure (>80 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
-
- 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
- F17C2270/0178—Cars
Definitions
- the invention relates to a pressure vessel according to the preamble of claim 1. Furthermore, the invention relates to a method for connecting such a pressure vessel in a body structure and a tool and a method for winding a hollow cylindrical extension of an outer shell of such a pressure vessel.
- Pressure vessels and corresponding methods for connecting such a pressure vessel in a body structure and tools and a method for winding a hollow cylindrical extension of an outer shell of such a pressure vessel are known in numerous variations.
- such pressure vessels can be filled, for example, with gases or pressure-liquefied gases and therefore store a considerable amount of energy. Due to the expansion of pressure vessels with very high filling pressures and the resulting change in length in the axial and radial directions during filling or pressurization, these pressure vessels are usually attached to the vehicle structure by means of flexible tank straps. These tank straps allow for tolerance compensation when filling the container, but provide no structural influence of the container stiffness on the body of the vehicle. As a result, the change in length of the pressure tank is not affected by the body and the transmission of the crash energy is carried out solely by the components or load paths of the body.
- connection concepts for pressure vessels in a body structure are already known, but these usually have a fixed and / or floating bearing for tolerance compensation and / or require due to the mounting accessibility a variety of additional holders for the realization of sufficient connection points to the vehicle structure.
- a generic pressure vessel which may be installed in a rear-side cargo space and / or underfloor in the region of a center tunnel of the vehicle body of a vehicle, preferably has a cylindrical design, in which a cylindrical pressure vessel shell is closed on both sides by curved outwardly, frontal bottoms.
- the pressure vessel wall may for example be constructed in three layers and comprise an inner layer, a middle layer of a fiber composite plastic and an outer layer of a further fiber composite plastic.
- the inner layer is a plastic liner made by blow molding or rotary / sintering method or thermoforming method.
- the plastic liner reinforcing middle layer is preferably wound in a wet winding process as a fiber winding on the plastic liner.
- the fiber winding consists of, for example, carbon, aramid, glass and / or boron fibers which are embedded in a matrix of thermosets or of thermoplastics.
- the fibers are applied to the plastic liner in different fiber orientations.
- the preferred impact-absorbing outer layer may also be a fiber winding which is wound on the middle layer in a wet winding process.
- the outer winding thus formed consists, for example, of carbon and / or glass fibers embedded in a matrix.
- the finished high-pressure container has, for example, on a front-side container bottom on an outwardly projecting neck piece, in which a valve is integrated. Otherwise, the high-pressure vessel is usually completely smooth on the outside. In its installed position, the high-pressure container is secured in position by means of clamping bands in conventional practice, which surround the smooth-surface cylinder wall of the high-pressure container.
- the fastening device is designed to connect the pressure vessel with a body of the motor vehicle.
- the fastening device comprises at least two connecting pins and at least two bearings.
- a connecting pin is connected to a bearing in a connection point.
- the connecting pins and / or the bearings are respectively connected to the pressure vessel in a pressure vessel connection area and extend away from the outer surface of the pressure vessel.
- the pressure tank connection areas each have an extension.
- the connecting pin and the bearing are at least partially formed and arranged in the connection point such that the extension E is guided kinematically by a movement of the bearing and / or the connecting pin with only one translational degree of freedom.
- a pressurizable container which comprises a cylindrical central part made of a fibrous plastic composite material at the ends of which a bottom part made of a fiber-plastic composite material is produced for closing the container.
- the middle part of the container is arranged on a winding mandrel of a wound body as a prefabricated middle part or produced by winding a roving.
- An inner surface of the bottom portion is defined by the winding mandrel of the bobbin and an end of the central portion adjacent to the bottom portion, and an outer surface of the bottom portion is defined by a plurality of shaping portions.
- the bottom part of the container is produced by winding a preferably unidirectional roving into a winding space defined by the winding mandrel and the shaping parts up to the end of the middle part, wherein the shaping parts are arranged successively from a winding axis of the winding body outwards on the winding axis, if an intermediate the winding mandrel and the respective previously arranged forming part formed part winding space is filled.
- Object of the present invention is to provide a pressure vessel and a method for connecting such a pressure vessel in a body structure and to provide a tool and a method for winding a hollow cylindrical extension of an outer shell of such a pressure vessel, which can be integrated in a simple manner as a stiffening element in the body structure and allows a level-independent tolerance compensation.
- hollow cylindrical extensions are at their open ends in each case as tension and / or pressure elastic compensation areas formed, which merge into several tensile and / or pressure elastic, strap-like compensation elements, at the end of each a fastener is formed, which are adapted to enter into a torsionally rigid connection with corresponding fasteners of a body structure.
- the pressure vessel comprises an outer shell which has a cylinder-like central region and two adjoining end regions. At both axial ends of the cylinder-like central region of the outer shell, in each case such a hollow cylindrical extension is formed, which projects beyond the respective end region.
- the corresponding body structure, to which the pressure vessel is to be integrated, has adapted to the shape and arrangement of the tab-like compensating elements counter elements.
- the fastening elements of the compensating elements and the counter-elements in an insertion position of the pressure vessel by a rotational movement of the pressure vessel about its longitudinal axis are slidable and thereby form a positive connection.
- the method for connecting such a pressure vessel in a body structure comprises the steps of: aligning the pressure vessel such that the pressure vessel is insertable from an open side of the body structure perpendicular to its longitudinal axis in the body structure, wherein the pressure vessel is rotated about its longitudinal axis to align the fasteners and the counter elements do not interfere with each other during insertion. Inserting the pressure vessel in the body structure until the insertion position is reached, and rotating the pressure vessel about its longitudinal axis such that a positive connection with the body structure is made.
- a tool for winding the hollow cylindrical extensions of the outer shell of the pressure vessel comprises a winding mandrel, through whose outer radius during winding an inner radius of the hollow cylindrical extension is predetermined.
- the mandrel can be converted from a first state having a predetermined winding radius and a resulting cross section into a second state having a smaller cross section.
- the mandrel can for example be made in several parts, wherein the transfer from the first to the second state then takes place by a decomposition.
- the method for winding the hollow cylindrical extension of the outer shell of the pressure vessel by means of such a tool comprises the steps: transfer of the winding mandrel in its first state, winding the hollow cylindrical extension, transferring the winding mandrel in its second state, and removing the winding mandrel from the hollow cylindrical extension.
- Embodiments of the pressure vessel according to the invention are characterized in that the structurally connected pressure vessel due to the interpretable in the fiber composite elastic compensation range allows tolerance compensation, but also forces from the vehicle structure, such as bending and torsional forces from the body stiffness and additional forces from Crashlast ton transferred, and thus can significantly contribute to increasing the lightweight construction and crash safety of the body.
- the compensation elements can be introduced by a machining post-processing, in particular by milling or cutting, in the hollow cylindrical extension.
- the compensation area and / or the lashing-like compensation elements can have regions of different stiffnesses.
- different fiber materials, fiber composites and / or laminate structures depending on the desired requirements, such as stiffness, strength, flexibility, elasticity, etc. can be used.
- the outer shell and the hollow cylindrical extensions for example, from a fiber-reinforced, preferably a continuous fiber reinforced plastic (CFRP, GRP) are made, for example, a carbon fiber reinforced, preferably a continuous carbon fiber reinforced plastic (CFRP), or a glass fiber reinforced, preferably an endless glass fiber reinforced plastic (GRP) ,
- the outer shell can surround a fluid-tight inner container made of metal or fiber-reinforced plastic or unreinforced plastic surface or form the fluid-tight inner container itself.
- a plurality of tab-like compensating elements with the fastening elements on the Circumference of the hollow cylindrical extension to be arranged equidistantly distributed.
- a further advantageous embodiment of the method for connecting such a pressure vessel in a body structure can be made between the fastening elements of the pressure vessel and the counter-elements of the body structure in addition a non-positive and / or material connection.
- the fastening elements and the counter-elements can for example be screwed together and / or glued and / or clipped.
- a pressure vessel 10 comprises an outer shell 12, which has a cylinder-like central region 14 and two adjoining end portions 16, 18. At both axial ends of the cylinder-like central region 14 of the outer shell 12, a hollow cylindrical extension 20 is formed, which projects beyond the respective end region 16, 18.
- the respective hollow cylindrical extension 20 is formed at its open end as tensile and / or compressive elastic compensation area 22, which merges into a plurality of tensile and / or pressure elastic, flap-like compensation elements 24, at the end of each a fastener 26 is formed, which is suitable are to enter into a torsionally rigid connection with corresponding fasteners 32 of a body structure 30.
- the fluid-tight inner container 11 can be made for example of metal or fiber-reinforced plastic (CFRP, GFRP) or unreinforced plastic.
- CFRP fiber-reinforced plastic
- the outer shell 12 itself may form the fluid-tight inner container 11.
- the outer shell 12 and the hollow cylindrical extension 20 are made of a fiber-reinforced, preferably a continuous fiber reinforced plastic (CFK, GRP), which, for example, a carbon fiber reinforced, preferably a continuous carbon fiber reinforced plastic (CFRP), and / or a glass fiber reinforced, preferably an endless glass fiber reinforced plastic (GRP) is.
- CFK continuous fiber reinforced plastic
- GRP glass fiber reinforced plastic
- the compensating elements 24 are introduced into the hollow cylindrical extension 20 by means of a machining operation.
- the compensation area 22 and / or the tab-like compensation elements 24 have regions of different stiffness in order to achieve the desired tensile and / or compressive elastic properties. How out 4 and 5 It can also be seen that the compensation area 22 and / or the tab-like compensating elements 24 allow expansion of the inner container 11 along its longitudinal axis LA and a cross-sectional enlargement perpendicular to the longitudinal axis.
- Fig. 1 to 8 How out Fig. 1 to 8 is further apparent, in the illustrated embodiment, four tab-like compensating elements 24 with the Fixing elements 26 arranged distributed over the circumference of the hollow cylindrical extension 20 equidistant.
- Fig. 6 to 8 The inventive method for connecting such a pressure vessel 10 in a body structure 30 is described below with reference to Fig. 6 to 8 described. How out Fig. 6 to 8 is further apparent, the body structure 30 on the shape and arrangement of the tab-like compensating elements 24 adapted counter elements 32. In this case, the fastening elements 26 of the compensating elements 24 and the counter-elements 32 are in an insertion position of the pressure vessel 10 by a rotational movement of the pressure vessel 10 about its longitudinal axis LA into one another and thereby form a positive connection. How out Fig. 6 and 7 it can be seen, the pressure vessel 10 is aligned such that the pressure vessel 10 is insertable from an open side of the body structure 30 perpendicular to its longitudinal axis LA in the body structure 30.
- Fig. 7 To align the pressure vessel 10 is rotated about its longitudinal axis LA so that the fasteners 26 and the counter-elements 32 do not interfere with each other during insertion, as from Fig. 7 is apparent. How out Fig. 7 Further, the pressure vessel 10 is inserted into the body structure 30 until the insertion position is reached. Then, the pressure vessel 10 is rotated about its longitudinal axis LA such that a positive connection with the body structure 30 is made, as shown Fig. 8 is apparent.
- fastening elements 26 of the pressure vessel 10 and the counter-elements 32 of the body structure 30, a non-positive and / or integral connection is produced.
- the fastening elements 26 and the counter-elements 32 for example, screwed together and / or glued and / or clipped.
- the tool for winding the hollow cylindrical extension 20 of the outer shell 12 of the pressure vessel 10 with the cylinder-like central region 14 and two adjoining end regions 16, 18 comprises a mandrel 40, by the outer radius of which during winding an inner radius of the hollow cylindrical extension 20 is predetermined.
- the winding mandrel 40 can be converted from a first state shown with a predetermined winding radius and a resulting cross section into a second state with a smaller cross section.
- the winding mandrel 40 is made of several parts and the transfer from the first to the second state is carried out by a disassembly of the winding mandrel 40 by first a first mandrel part 42 and then a second mandrel part 44 is removed from the wound extension 20.
- the method for winding the hollow cylindrical extension 20 of the outer shell 12 of the pressure vessel 10 by means of such a tool comprises the steps: transfer of the winding mandrel 40 in its first state, winding the hollow cylindrical extension 20, transferring the winding mandrel 40 in its second state, and removing the winding mandrel 40 from the hollow cylindrical extension 20th
Abstract
Die Erfindung betrifft einen Druckbehälter (10) sowie ein Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur und ein Werkzeug und ein Verfahren zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle (12) eines solchen Druckbehälters (10). Der Druckbehälter (10) umfasst eine Außenhülle (12), welche einen zylinderähnlichen Mittelbereich (14) und zwei sich daran anschließende Endbereiche (16, 18) aufweist, wobei an beiden axialen Enden des zylinderähnlichen Mittelbereichs (14) der Außenhülle (12) jeweils ein hohlzylindrischer Fortsatz (20) ausgebildet ist, welcher über den jeweiligen Endbereich (16, 18) übersteht. Erfindungsgemäß ist der jeweilige hohlzylindrische Fortsatz (20) an seinem offenen Ende als zug- und/oder druckelastischer Ausgleichsbereich (22) ausgebildet, welcher in mehrere zug- und/oder druckelastische, laschenähnliche Ausgleichselemente (24) übergeht, an deren Ende jeweils ein Befestigungselement (26) ausgebildet ist, welche dafür geeignet sind, mit entsprechenden Befestigungselementen (32) einer Karosseriestruktur (30) eine torsionssteife Verbindung einzugehen.The invention relates to a pressure vessel (10) and a method for connecting such a pressure vessel in a body structure and a tool and a method for winding a hollow cylindrical extension of an outer shell (12) of such a pressure vessel (10). The pressure vessel (10) comprises an outer shell (12) having a cylinder-like central region (14) and two adjoining end portions (16, 18), wherein at both axial ends of the cylinder-like central region (14) of the outer shell (12) in each case one hollow cylindrical extension (20) is formed, which projects beyond the respective end region (16, 18). According to the invention, the respective hollow cylindrical extension (20) is formed at its open end as tension and / or pressure-elastic compensation area (22), which merges into a plurality of tensile and / or pressure-elastic, tab-like compensating elements (24), at each of which a fastening element (24). 26) is formed, which are suitable for entering into a torsionally rigid connection with corresponding fastening elements (32) of a body structure (30).
Description
Die Erfindung betrifft einen Druckbehälter gemäß der Gattung des Patentanspruchs 1. Des Weiteren betrifft die Erfindung ein Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur sowie ein Werkzeug und ein Verfahren zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle eines solchen Druckbehälters.The invention relates to a pressure vessel according to the preamble of
Druckbehälter und korrespondierende Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur und Werkzeuge und ein Verfahren zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle eines solchen Druckbehälters sind in zahlreichen Variationen bekannt. Allgemein können solche Druckbehälter beispielsweise mit Gasen oder druckverflüssigten Gasen befüllt werden und daher eine erhebliche Energiemenge speichern. Aufgrund der Ausdehnung von Druckbehältern mit sehr hohen Fülldrücken und der daraus resultierenden Längenänderung in axialer sowie radialer Richtung während des Befüllens bzw. eine Druckbeaufschlagung werden diese Druckbehälter üblicherweise mittels flexibler Tankspannbänder an der Fahrzeugstruktur befestigt. Diese Tankspannbänder ermöglichen einen Toleranzausgleich beim Befüllen des Behälters, bieten jedoch keinen strukturellen Einfluss der Behältersteifigkeit auf die Karosserie des Fahrzeugs. Dadurch wird die Längenänderung des Drucktanks nicht durch die Karosserie beeinträchtigt und die Übertragung der Crashenergie erfolgt einzig durch die Bauteile bzw. Lastpfade der Karosserie.Pressure vessels and corresponding methods for connecting such a pressure vessel in a body structure and tools and a method for winding a hollow cylindrical extension of an outer shell of such a pressure vessel are known in numerous variations. In general, such pressure vessels can be filled, for example, with gases or pressure-liquefied gases and therefore store a considerable amount of energy. Due to the expansion of pressure vessels with very high filling pressures and the resulting change in length in the axial and radial directions during filling or pressurization, these pressure vessels are usually attached to the vehicle structure by means of flexible tank straps. These tank straps allow for tolerance compensation when filling the container, but provide no structural influence of the container stiffness on the body of the vehicle. As a result, the change in length of the pressure tank is not affected by the body and the transmission of the crash energy is carried out solely by the components or load paths of the body.
Zwar sind bereits mehrere Anbindungskonzepte für Druckbehälter in eine Karosseriestruktur bekannt, diese weisen jedoch in der Regel eine Fest- und/oder Loslageraufnahme zum Toleranzausgleich auf und/oder benötigen aufgrund der Montagezugänglichkeit eine Vielzahl von Zusatzhaltern zur Realisierung ausreichender Anbindungspunkte zur Fahrzeugstruktur.Although several connection concepts for pressure vessels in a body structure are already known, but these usually have a fixed and / or floating bearing for tolerance compensation and / or require due to the mounting accessibility a variety of additional holders for the realization of sufficient connection points to the vehicle structure.
Ein gattungsgemäßer Druckbehälter, welcher in einem heckseitigen Laderaum und/oder unterflurig im Bereich eines Mitteltunnels der Fahrzeugkarosserie eines Fahrzeugs verbaut sein kann, weist bevorzugt eine zylindrische Bauform auf, bei der ein zylindrischer Druckbehältermantel durch nach außen gewölbte, stirnseitigen Böden beidseitig verschlossen ist. Die Druckbehälterwand kann beispielsweise dreilagig aufgebaut sein und eine Innenlage, eine Mittellage aus einem Faserverbundkunststoff sowie eine Außenlage aus einem weiteren Faserverbundkunststoff umfassen. In einem sogenannten Typ-4-Hochdruckbehälter für Erdgas ist die Innenlage ein Kunststoff-Liner, der über Blasformen oder Rotations-/Sinter-Verfahren oder Thermoformverfahren hergestellt ist. Die den Kunststoff-Liner verstärkende Mittellage ist bevorzugt in einem Nasswickelverfahren als eine Faserwicklung auf den Kunststoff-Liner aufgewickelt. Exemplarisch besteht die Faserwicklung aus zum Beispiel Kohlenstoff-, Aramid-, Glas- und/oder Borfasern, die in einer Matrix aus Duromeren oder aus Thermoplasten eingebettet sind. Die Fasern sind in unterschiedlichen Faserorientierungen auf den Kunststoff-Liner aufgebracht. Die bevorzugt schlagabsorbierende Außenlage kann ebenfalls eine Faserwicklung sein, die in einem Nasswickelverfahren auf die Mittellage aufgewickelt wird. Die so gebildete Außenwicklung besteht beispielhaft aus Kohlenstoff- und/oder Glasfasern, die in einer Matrix eingebettet sind.A generic pressure vessel, which may be installed in a rear-side cargo space and / or underfloor in the region of a center tunnel of the vehicle body of a vehicle, preferably has a cylindrical design, in which a cylindrical pressure vessel shell is closed on both sides by curved outwardly, frontal bottoms. The pressure vessel wall may for example be constructed in three layers and comprise an inner layer, a middle layer of a fiber composite plastic and an outer layer of a further fiber composite plastic. In a so-called type 4 high pressure container for natural gas, the inner layer is a plastic liner made by blow molding or rotary / sintering method or thermoforming method. The plastic liner reinforcing middle layer is preferably wound in a wet winding process as a fiber winding on the plastic liner. By way of example, the fiber winding consists of, for example, carbon, aramid, glass and / or boron fibers which are embedded in a matrix of thermosets or of thermoplastics. The fibers are applied to the plastic liner in different fiber orientations. The preferred impact-absorbing outer layer may also be a fiber winding which is wound on the middle layer in a wet winding process. The outer winding thus formed consists, for example, of carbon and / or glass fibers embedded in a matrix.
Der fertiggestellte Hochdruckbehälter weist beispielsweise an einem stirnseitigen Behälterboden ein nach außen abragendes Halsstück auf, in das ein Ventil integriert ist. Ansonsten ist Hochdruckbehälter außenseitig meist komplett glattflächig ausgeführt. In seiner Einbaulage ist der Hochdruckbehälter in gängiger Praxis mittels Spannbänder lagegesichert, die die glattflächige Zylinderwand des Hochdruckbehälters umgreifen.The finished high-pressure container has, for example, on a front-side container bottom on an outwardly projecting neck piece, in which a valve is integrated. Otherwise, the high-pressure vessel is usually completely smooth on the outside. In its installed position, the high-pressure container is secured in position by means of clamping bands in conventional practice, which surround the smooth-surface cylinder wall of the high-pressure container.
Aus der
Aus der
Aufgabe der vorliegenden Erfindung ist es, einen Druckbehälter und ein Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur sowie ein Werkzeug und ein Verfahren zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle eines solchen Druckbehälters bereitzustellen, welcher in einfacher Weise als Versteifungselement in die Karosseriestruktur eingebunden werden kann und einen füllstandsunabhängige Toleranzausgleich ermöglicht.Object of the present invention is to provide a pressure vessel and a method for connecting such a pressure vessel in a body structure and to provide a tool and a method for winding a hollow cylindrical extension of an outer shell of such a pressure vessel, which can be integrated in a simple manner as a stiffening element in the body structure and allows a level-independent tolerance compensation.
Diese Aufgabe wird durch einen Druckbehälter mit den Merkmalen des Patentanspruchs 1, durch ein Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur mit den Merkmalen des Patentanspruchs 8 und durch ein Werkzeug zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle eines solchen Druckbehälters mit den Merkmalen des Patentanspruchs 11 sowie durch ein Verfahren zum Wickeln eines hohlzylindrischen Fortsatzes einer Außenhülle eines solchen Druckbehälters mit den Merkmalen des Patentanspruchs 13 gelöst. Vorteilhafte Ausgestaltungen mit zweckmäßigen Weiterbildungen der Erfindung sind in den abhängigen Patentansprüchen angegeben.This object is achieved by a pressure vessel having the features of
Um einen Druckbehälter sowie ein Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur bereitzustellen, welcher in einfacher Weise als Versteifungselement in die Karosseriestruktur eingebunden werden kann und einen füllstandsunabhängigen Toleranzausgleich ermöglicht, sind hohlzylindrische Fortsätze an ihren offenen Enden jeweils als zug- und/oder druckelastische Ausgleichsbereiche ausgebildet, welcher in mehrere zug- und/oder druckelastische, laschenähnliche Ausgleichselemente übergehen, an deren Ende jeweils ein Befestigungselement ausgebildet ist, welche dafür geeignet sind, mit entsprechenden Befestigungselementen einer Karosseriestruktur eine torsionssteife Verbindung einzugehen. Der Druckbehälter umfasst eine Außenhülle, welche einen zylinderähnlichen Mittelbereich und zwei sich daran anschließenden Endbereiche aufweist. An beiden axialen Enden des zylinderähnlichen Mittelbereichs der Außenhülle ist jeweils ein solcher hohlzylindrischer Fortsatz ausgebildet, welcher über den jeweiligen Endbereich übersteht.In order to provide a pressure vessel and a method for connecting such a pressure vessel in a body structure, which can be integrated in a simple manner as a stiffening element in the body structure and allows a filling level independent tolerance compensation, hollow cylindrical extensions are at their open ends in each case as tension and / or pressure elastic compensation areas formed, which merge into several tensile and / or pressure elastic, strap-like compensation elements, at the end of each a fastener is formed, which are adapted to enter into a torsionally rigid connection with corresponding fasteners of a body structure. The pressure vessel comprises an outer shell which has a cylinder-like central region and two adjoining end regions. At both axial ends of the cylinder-like central region of the outer shell, in each case such a hollow cylindrical extension is formed, which projects beyond the respective end region.
Die korrespondierende Karosseriestruktur, an welche der Druckbehälter eingebunden werden soll, weist an Form und Anordnung der laschenähnlichen Ausgleichselemente angepasste Gegenelemente auf. Hierbei sind die Befestigungselemente der Ausgleichselemente und die Gegenelemente in einer Einsatzposition des Druckbehälters durch eine Drehbewegung des Druckbehälters um seine Längsachse ineinander verschiebbar und bilden dadurch eine formschlüssige Verbindung aus. Das Verfahren zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur umfasst die Schritte: Ausrichten des Druckbehälters derart, dass der Druckbehälter von einer offenen Seite der Karosseriestruktur senkrecht zu seiner Längsachse in die Karosseriestruktur einführbar ist, wobei der Druckbehälter zum Ausrichten um seine Längsachse gedreht wird, dass sich die Befestigungselemente und die Gegenelemente beim Einführen nicht gegenseitig behindern. Einführen des Druckbehälters in die Karosseriestruktur bis die Einsatzposition erreicht ist, und Drehen des Druckbehälters um seine Längsachse derart, dass eine formschlüssige Verbindung mit der Karosseriestruktur hergestellt ist.The corresponding body structure, to which the pressure vessel is to be integrated, has adapted to the shape and arrangement of the tab-like compensating elements counter elements. In this case, the fastening elements of the compensating elements and the counter-elements in an insertion position of the pressure vessel by a rotational movement of the pressure vessel about its longitudinal axis are slidable and thereby form a positive connection. The method for connecting such a pressure vessel in a body structure comprises the steps of: aligning the pressure vessel such that the pressure vessel is insertable from an open side of the body structure perpendicular to its longitudinal axis in the body structure, wherein the pressure vessel is rotated about its longitudinal axis to align the fasteners and the counter elements do not interfere with each other during insertion. Inserting the pressure vessel in the body structure until the insertion position is reached, and rotating the pressure vessel about its longitudinal axis such that a positive connection with the body structure is made.
Ein Werkzeug zum Wickeln der hohlzylindrischen Fortsätze der Außenhülle des Druckbehälters umfasst einen Wickeldorn, durch dessen Außenradius beim Wickeln ein Innenradius des hohlzylindrischen Fortsatzes vorgegeben ist. Erfindungsgemäß ist der Wickeldorn von einem ersten Zustand mit einem vorgegebenen Wickelradius und einem sich daraus ergebenden Querschnitt in einen zweiten Zustand mit einem geringeren Querschnitt überführbar. Hierzu kann der Wickeldorn beispielsweise mehrteilig ausgeführt werden, wobei die Überführung vom ersten in den zweiten Zustand dann durch eine Zerlegung erfolgt.A tool for winding the hollow cylindrical extensions of the outer shell of the pressure vessel comprises a winding mandrel, through whose outer radius during winding an inner radius of the hollow cylindrical extension is predetermined. According to the invention, the mandrel can be converted from a first state having a predetermined winding radius and a resulting cross section into a second state having a smaller cross section. For this purpose, the mandrel can for example be made in several parts, wherein the transfer from the first to the second state then takes place by a decomposition.
Das Verfahren zum Wickeln des hohlzylindrischen Fortsatzes der Außenhülle des Druckbehälters mittels eines solchen Werkzeugs umfasst die Schritte: Überführung des Wickeldorns in seinen ersten Zustand, Wickeln des hohlzylindrischen Fortsatzes, Überführen des Wickeldorns in seinen zweiten Zustand, und Herausnehmen des Wickeldorns aus dem hohlzylindrischen Fortsatz.The method for winding the hollow cylindrical extension of the outer shell of the pressure vessel by means of such a tool comprises the steps: transfer of the winding mandrel in its first state, winding the hollow cylindrical extension, transferring the winding mandrel in its second state, and removing the winding mandrel from the hollow cylindrical extension.
Ausführungsformen des erfindungsgemäßen Druckbehälters zeichnen sich dadurch aus, dass der strukturell angebundene Druckbehälter aufgrund des im Faserverbund auslegbaren elastischen Ausgleichbereichs einen Toleranzausgleich ermöglicht, jedoch auch Kräfte aus der Fahrzeugstruktur, wie beispielsweise Biege- und Torsionskräfte aus der Karosseriesteifigkeit sowie zusätzliche Kräfte aus Crashlastfällen, übertragen und somit erheblich zur Erhöhung der Leichtbaugüte und Crashsicherheit der Karosserie beitragen kann.Embodiments of the pressure vessel according to the invention are characterized in that the structurally connected pressure vessel due to the interpretable in the fiber composite elastic compensation range allows tolerance compensation, but also forces from the vehicle structure, such as bending and torsional forces from the body stiffness and additional forces from Crashlastfällen transferred, and thus can significantly contribute to increasing the lightweight construction and crash safety of the body.
In vorteilhafter Ausgestaltung des Druckbehälters können die Ausgleichselemente durch eine spanabhebende Nachbearbeitung, insbesondere durch Fräsen oder Schneiden, in den hohlzylindrischer Fortsatz eingebracht werden.In an advantageous embodiment of the pressure vessel, the compensation elements can be introduced by a machining post-processing, in particular by milling or cutting, in the hollow cylindrical extension.
In weiterer vorteilhafter Ausgestaltung des Druckbehälters kann der Ausgleichsbereich und/oder die laschenähnlichen Ausgleichselemente bereichsweise unterschiedliche Steifigkeiten aufweisen. Bei der Herstellung des Ausgleichsbereichs und/oder der laschenähnlichen Ausgleichselemente und/oder der Befestigungselemente können verschiedene Faserwerkstoffe, Faserverbunde und/oder Laminatstrukturen in Abhängigkeit der gewünschten Anforderungen, wie beispielsweise Steifigkeit, Festigkeit, Flexibilität, Elastizität usw., verwendet werden. So können die Außenhülle und die hohlzylindrischen Fortsätze beispielsweise aus einem faserverstärkten, vorzugsweise einem endlosfaserverstärkten Kunststoff (CFK, GFK) gefertigt werden, der beispielsweise ein kohlefaserverstärkter, vorzugsweise ein endloskohlefaserverstärkter Kunststoff (CFK), oder ein glasfaserverstärkter, vorzugsweise ein endlosglasfaserverstärkter Kunststoff (GFK) ist.In a further advantageous embodiment of the pressure vessel, the compensation area and / or the lashing-like compensation elements can have regions of different stiffnesses. In the manufacture of the compensation area and / or the tab-like compensation elements and / or the fastening elements, different fiber materials, fiber composites and / or laminate structures depending on the desired requirements, such as stiffness, strength, flexibility, elasticity, etc., can be used. Thus, the outer shell and the hollow cylindrical extensions, for example, from a fiber-reinforced, preferably a continuous fiber reinforced plastic (CFRP, GRP) are made, for example, a carbon fiber reinforced, preferably a continuous carbon fiber reinforced plastic (CFRP), or a glass fiber reinforced, preferably an endless glass fiber reinforced plastic (GRP) ,
In weiterer vorteilhafter Ausgestaltung des Druckbehälters kann die Außenhülle einen fluiddichten Innenbehälter aus Metall oder aus faserverstärktem Kunststoff oder aus unverstärktem Kunststoff flächig umschließen oder den fluiddichten Innenbehälter selbst ausbilden.In a further advantageous embodiment of the pressure vessel, the outer shell can surround a fluid-tight inner container made of metal or fiber-reinforced plastic or unreinforced plastic surface or form the fluid-tight inner container itself.
In weiterer vorteilhafter Ausgestaltung des Druckbehälters können mehrere laschenähnliche Ausgleichselemente mit den Befestigungselementen über den Umfang des hohlzylindrischen Fortsatzes äquidistant verteilt angeordnet werden.In a further advantageous embodiment of the pressure vessel a plurality of tab-like compensating elements with the fastening elements on the Circumference of the hollow cylindrical extension to be arranged equidistantly distributed.
In weiterer vorteilhafter Ausgestaltung des Verfahrens zur Anbindung eines solchen Druckbehälters in eine Karosseriestruktur kann zwischen den Befestigungselementen des Druckbehälters und den Gegenelementen der Karosseriestruktur zusätzlich eine kraftschlüssige und/oder stoffschlüssige Verbindung hergestellt werden. Die die Befestigungselemente und die Gegenelemente können beispielsweise miteinander verschraubt und/oder verklebt und/oder verclipst werden.In a further advantageous embodiment of the method for connecting such a pressure vessel in a body structure can be made between the fastening elements of the pressure vessel and the counter-elements of the body structure in addition a non-positive and / or material connection. The fastening elements and the counter-elements can for example be screwed together and / or glued and / or clipped.
Die vorstehend in der Beschreibung genannten Merkmale und Merkmalskombinationen sowie die nachfolgend in der Figurenbeschreibung genannten und/oder in den Figuren alleine gezeigten Merkmale und Merkmalskombinationen sind nicht nur in der jeweils angegebenen Kombination, sondern auch in anderen Kombinationen oder in Alleinstellung verwendbar, ohne den Rahmen der Erfindung zu verlassen. Es sind somit auch Ausführungen als von der Erfindung umfasst und offenbart anzusehen, die in den Figuren nicht explizit gezeigt oder erläutert sind, jedoch durch separierte Merkmalskombinationen aus den erläuterten Ausführungen hervorgehen und erzeugbar sind.The features and feature combinations mentioned above in the description as well as the features and feature combinations mentioned below in the description of the figures and / or in the figures alone can be used not only in the respectively specified combination but also in other combinations or in isolation, without the scope of To leave invention. Thus, embodiments are also included and disclosed by the invention, which are not explicitly shown or explained in the figures, however, emerge and can be produced by separated combinations of features from the embodiments explained.
Ausführungsbeispiele der Erfindung sind in der Zeichnung dargestellt und werden in der nachfolgenden Beschreibung näher erläutert. In der Zeichnung bezeichnen gleiche Bezugszeichen Komponenten bzw. Elemente, die gleiche bzw. analoge Funktionen ausführen. Hierbei zeigen:
- Fig. 1
- eine schematische perspektivische Darstellung eines Ausführungsbeispiels eines erfindungsgemäßen Druckbehälters in einem ersten Zustand;
- Fig. 2
- eine schematische perspektivische Darstellung des Druckbehälters aus
Fig. 1 aus einem anderen Blickwinkel; - Fig. 3
- eine schematische perspektivische Darstellung des erfindungsgemäßen Druckbehälters aus
Fig. 1 und 2 in einem ausgedehnten zweiten Zustand; - Fig. 4
- eine Darstellung eines Details IV aus
Fig. 1 , - Fig. 5
- eine Darstellung eines Details V aus
Fig. 3 , - Fig. 6
- eine schematische Darstellung des erfindungsgemäßen Druckbehälters und einer korrespondierenden Karosseriestruktur vor dem Einführen des Druckbehälters;
- Fig. 7
- eine schematische Darstellung des erfindungsgemäßen Druckbehälters und der korrespondierenden Karosseriestruktur aus
Fig. 6 während des Einführens des Druckbehälters; - Fig. 8
- eine schematische Darstellung des erfindungsgemäßen Druckbehälters und der korrespondierenden Karosseriestruktur aus
Fig. 6 und7 nach dem Herstellen der formschlüssigen Verbindung; - Fig. 9
- eine schematische Darstellung eines Abschnitts des Druckbehälters aus
Fig. 1 bis 8 mit einem Wickelwerkzeug während eines Wickelvorgangs eines hohlzylindrischen Fortsatzes des Druckbehälters; und - Fig. 10
- eine Darstellung eines Details X aus
Fig. 9 .
- Fig. 1
- a schematic perspective view of an embodiment of a pressure vessel according to the invention in a first state;
- Fig. 2
- a schematic perspective view of the pressure vessel from
Fig. 1 from a different angle; - Fig. 3
- a schematic perspective view of the pressure vessel according to the invention
Fig. 1 and 2 in an extended second state; - Fig. 4
- a representation of a detail IV
Fig. 1 . - Fig. 5
- a representation of a detail V from
Fig. 3 . - Fig. 6
- a schematic representation of the pressure vessel according to the invention and a corresponding body structure prior to insertion of the pressure vessel;
- Fig. 7
- a schematic representation of the pressure vessel according to the invention and the corresponding body structure
Fig. 6 during insertion of the pressure vessel; - Fig. 8
- a schematic representation of the pressure vessel according to the invention and the corresponding body structure
Fig. 6 and7 after making the positive connection; - Fig. 9
- a schematic representation of a portion of the pressure vessel from
Fig. 1 to 8 with a winding tool during a winding operation of a hollow cylindrical extension of the pressure vessel; and - Fig. 10
- a representation of a detail X from
Fig. 9 ,
Wie aus
Erfindungsgemäß ist der jeweilige hohlzylindrische Fortsatz 20 an seinem offenen Ende als zug- und/oder druckelastischer Ausgleichsbereich 22 ausgebildet, welcher in mehrere zug- und/oder druckelastische, laschenähnliche Ausgleichselemente 24 übergeht, an deren Ende jeweils ein Befestigungselement 26 ausgebildet ist, welche dafür geeignet sind, mit entsprechenden Befestigungselementen 32 einer Karosseriestruktur 30 eine torsionssteife Verbindung einzugehen.According to the invention, the respective hollow
Wie aus
Die Ausgleichselemente 24 werden durch eine spanabhebende Nachbearbeitung in den hohlzylindrischer Fortsatz 20 eingebracht. Hierbei weisen der Ausgleichsbereich 22 und/oder die laschenähnlichen Ausgleichselemente 24 bereichsweise unterschiedliche Steifigkeiten auf, um die gewünschten zug- und/oder druckelastischen Eigenschaften zu erzielen. Wie aus
Wie aus
Das erfindungsgemäße Verfahren zur Anbindung eines solchen Druckbehälters 10 in eine Karosseriestruktur 30 wird nachfolgend unter Bezugnahme auf
Zusätzlich wird zwischen den Befestigungselementen 26 des Druckbehälters 10 und den Gegenelementen 32 der Karosseriestruktur 30 eine kraftschlüssige und/oder stoffschlüssige Verbindung hergestellt. Hierzu können die Befestigungselemente 26 und die Gegenelemente 32 beispielsweise miteinander verschraubt und/oder verklebt und/oder verclipst werden.In addition, between the
Wie aus
Wie aus
Das Verfahren zum Wickeln des hohlzylindrischen Fortsatzes 20 der Außenhülle 12 des Druckbehälters 10 mittels eines solchen Werkzeugs umfasst die Schritte: Überführung des Wickeldorns 40 in seinen ersten Zustand, Wickeln des hohlzylindrischen Fortsatzes 20, Überführen des Wickeldorns 40 in seinen zweiten Zustand, und Herausnehmen des Wickeldorns 40 aus dem hohlzylindrischen Fortsatz 20.The method for winding the hollow
- 1010
- Druckbehälterpressure vessel
- 1111
- Innenbehälterinner container
- 1212
- Außenhülleouter shell
- 1414
- Mittelbereichthe central region
- 16, 1816, 18
- Endbereichend
- 2020
- Fortsatzextension
- 2222
- zug- und/oder druckelastischer AusgleichsbereichTensile and / or pressure elastic compensation area
- 2424
- zug- und/oder druckelastisches Ausgleichselementtensile and / or pressure elastic compensation element
- 2626
- torsionssteifes Befestigungselementtorsionally rigid fastening element
- 3030
- Karosseriestrukturbody structure
- 3232
- karosserieseitige Gegenelementebody-side counter-elements
- 4040
- Wickeldornmandrel
- 4242
- erster Teildornfirst part of the mandrel
- 4444
- zweiter Teildornsecond part of the mandrel
- LALA
- Längsachselongitudinal axis
Claims (13)
dadurch gekennzeichnet,
dass der jeweilige hohlzylindrische Fortsatz (20) an seinem offenen Ende als zug- und/oder druckelastischer Ausgleichsbereich (22) ausgebildet ist, welcher in mehrere zug- und/oder druckelastische, laschenähnliche Ausgleichselemente (24) übergeht, an deren Ende jeweils ein Befestigungselement (26) ausgebildet ist, welche dafür geeignet sind, mit entsprechenden Befestigungselementen (32) einer Karosseriestruktur (30) eine torsionssteife Verbindung einzugehen.Pressure vessel (10) having an outer shell (12), which has a cylinder-like central region (14) and two adjoining end portions (16, 18), wherein at both axial ends of the cylinder-like central region (14) of the outer shell (12) each have a hollow cylindrical Extension (20) is formed, which projects beyond the respective end region (16, 18),
characterized,
in that the respective hollow-cylindrical extension (20) is formed at its open end as a tensile and / or pressure-elastic compensation area (22) which merges into a plurality of tensile and / or pressure-elastic, lashing-like compensating elements (24), at each of which a fastening element (22). 26) is formed, which are suitable for entering into a torsionally rigid connection with corresponding fastening elements (32) of a body structure (30).
dadurch gekennzeichnet, dass
die Ausgleichselemente (24) durch eine spanabhebende Nachbearbeitung in den hohlzylindrischen Fortsatz (20) eingebracht sind.Pressure vessel (10) according to claim 1,
characterized in that
the compensation elements (24) are introduced by a machining post-processing in the hollow cylindrical extension (20).
dadurch gekennzeichnet, dass
der Ausgleichsbereich (22) und/oder die laschenähnlichen Ausgleichselemente (24) bereichsweise unterschiedliche Steifigkeiten aufweisen.Pressure vessel (10) according to claim 1 or 2,
characterized in that
the compensation area (22) and / or the tab-like compensation elements (24) have regions of different stiffnesses.
dadurch gekennzeichnet, dass
die Außenhülle (12) und der hohlzylindrische Fortsatz (20) aus einem faserverstärkten, vorzugsweise einem endlosfaserverstärkten Kunststoff (CFK, GFK) gefertigt sind.Pressure vessel (10) according to one of claims 1 to 3,
characterized in that
the outer shell (12) and the hollow cylindrical extension (20) are made of a fiber-reinforced, preferably an endless-fiber-reinforced plastic (CFRP, GFRP).
dadurch gekennzeichnet, dass
der Faserverbundkunststoff ein kohlefaserverstärkter, vorzugsweise ein endloskohlefaserverstärkter Kunststoff (CFK) oder ein glasfaserverstärkter, vorzugsweise ein endlosglasfaserverstärkter Kunststoff (GFK) ist.Pressure vessel (10) according to claim 4,
characterized in that
the fiber composite plastic is a carbon fiber reinforced, preferably a continuous carbon fiber reinforced plastic (CFRP) or a glass fiber reinforced, preferably an endless glass fiber reinforced plastic (GRP).
dadurch gekennzeichnet, dass
die Außenhülle (12) einen fluiddichten Innenbehälter (11) aus Metall oder aus faserverstärktem Kunststoff (CFK, GFK) oder aus unverstärktem Kunststoff flächig umschließt oder den fluiddichten Innenbehälter (11) selbst ausbildet.Pressure vessel (10) according to one of claims 1 to 5,
characterized in that
the outer shell (12) encloses a fluid-tight inner container (11) made of metal or fiber-reinforced plastic (CFRP, GFRP) or unreinforced plastic or forms the fluid-tight inner container (11) itself.
dadurch gekennzeichnet, dass
mehrere laschenähnliche Ausgleichselemente (24) mit den Befestigungselementen (26) über den Umfang des hohlzylindrischen Fortsatzes (20) äquidistant verteilt angeordnet sind.Pressure vessel (10) according to one of claims 1 to 6,
characterized in that
a plurality of tab-like compensating elements (24) with the fastening elements (26) over the circumference of the hollow cylindrical extension (20) are arranged distributed equidistantly.
dadurch gekennzeichnet, dass
zwischen den Befestigungselementen (26) des Druckbehälters (10) und den Gegenelementen (32) der Karosseriestruktur (30) zusätzlich eine kraftschlüssige und/oder stoffschlüssige Verbindung hergestellt wird.Method according to claim 8,
characterized in that
between the fastening elements (26) of the pressure vessel (10) and the counter-elements (32) of the body structure (30) in addition a frictional and / or material connection is made.
dadurch gekennzeichnet, dass
die Befestigungselemente (26) und die Gegenelemente (32) miteinander verschraubt und/oder verklebt und/oder verclipst werden.Method according to claim 9,
characterized in that
the fastening elements (26) and the counter-elements (32) are screwed together and / or glued and / or clipped.
dadurch gekennzeichnet,
dass der Wickeldorn (40) von einem ersten Zustand mit einem vorgegebenen Wickelradius und einem sich daraus ergebenden Querschnitt in einen zweiten Zustand mit einem geringeren Querschnitt überführbar ist.Tool for winding a hollow cylindrical extension (20) of an outer shell (12) of a pressure vessel (10) with a cylinder-like central region (14) and two adjoining end portions (16, 18), with a winding mandrel (40), by its outer radius during winding an inner radius of the hollow cylindrical extension (20) is predetermined,
characterized,
in that the winding mandrel (40) can be converted from a first state having a predetermined winding radius and a resulting cross section into a second state having a smaller cross section.
dadurch gekennzeichnet, dass
der Wickeldorn (40) mehrteilig ausgeführt ist und die Überführung vom ersten in den zweiten Zustand durch eine Zerlegung erfolgt.Tool according to claim 11,
characterized in that
the winding mandrel (40) is designed in several parts and the transfer from the first to the second state is carried out by a decomposition.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102018204805.3A DE102018204805B4 (en) | 2018-03-28 | 2018-03-28 | Pressure vessel and method for connecting the pressure vessel and method for producing a hollow cylindrical extension of the outer shell |
Publications (3)
Publication Number | Publication Date |
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EP3557117A2 true EP3557117A2 (en) | 2019-10-23 |
EP3557117A3 EP3557117A3 (en) | 2020-01-08 |
EP3557117B1 EP3557117B1 (en) | 2022-07-20 |
Family
ID=65724220
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EP19161168.0A Active EP3557117B1 (en) | 2018-03-28 | 2019-03-07 | Pressure vessel and method for connecting a pressure vessel into a body structure |
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EP (1) | EP3557117B1 (en) |
DE (1) | DE102018204805B4 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022172032A1 (en) * | 2021-02-11 | 2022-08-18 | Viritech Ltd | Tanks for storing volatile gas under pressure and structures comprising such tanks |
Families Citing this family (1)
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DE102020122002B3 (en) | 2020-08-24 | 2021-08-26 | Audi Aktiengesellschaft | Pressure tank system with several standing pressure tanks and a motor vehicle with such a pressure tank system (I) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6565793B1 (en) * | 1998-09-11 | 2003-05-20 | Essef Corporation | Method for fabricating composite pressure vessels |
US8146948B2 (en) * | 2009-06-24 | 2012-04-03 | International Truck Intellectual Property Company, Llc | Structural air tank crossmember |
US8480131B2 (en) * | 2010-09-30 | 2013-07-09 | GM Global Technology Operations LLC | Integrated pressure vessels for vehicular applications |
US9102499B2 (en) * | 2011-02-21 | 2015-08-11 | Murata Machinery, Ltd. | Filament winding device |
FR3020323B1 (en) * | 2014-04-25 | 2017-09-15 | Technoboost | DEVICE FOR ELASTICALLY SUSPENDING A SET OF RESERVOIRS IN THE BASE OF A MOTOR VEHICLE |
DE102015206825A1 (en) * | 2015-03-17 | 2016-09-22 | Bayerische Motoren Werke Aktiengesellschaft | Pressure vessel for a motor vehicle |
DE102015106461B4 (en) * | 2015-04-27 | 2019-03-07 | Frauenthal Automotive Elterlein Gmbh | Polkappe, in particular for a pressure vessel and method for producing the pole cap and pressure vessel |
DE102015106463B4 (en) * | 2015-04-27 | 2022-11-03 | Frauenthal Automotive Elterlein Gmbh | Pressure vessel for storing pressurized fluids and method of manufacturing the pressure vessel |
DE102015007047B4 (en) * | 2015-05-29 | 2017-10-19 | Audi Ag | Method and device for producing a pressurizable container |
DE102016201477A1 (en) * | 2016-02-01 | 2017-08-03 | Bayerische Motoren Werke Aktiengesellschaft | Pressure vessel and method for producing a pressure vessel |
-
2018
- 2018-03-28 DE DE102018204805.3A patent/DE102018204805B4/en active Active
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2019
- 2019-03-07 EP EP19161168.0A patent/EP3557117B1/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2022172032A1 (en) * | 2021-02-11 | 2022-08-18 | Viritech Ltd | Tanks for storing volatile gas under pressure and structures comprising such tanks |
Also Published As
Publication number | Publication date |
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EP3557117B1 (en) | 2022-07-20 |
DE102018204805A1 (en) | 2019-10-02 |
EP3557117A3 (en) | 2020-01-08 |
DE102018204805B4 (en) | 2021-01-07 |
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