EP3421864A1 - Flüssig-erdgastank für kraftfahrzeuge - Google Patents

Flüssig-erdgastank für kraftfahrzeuge Download PDF

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Publication number
EP3421864A1
EP3421864A1 EP18179109.6A EP18179109A EP3421864A1 EP 3421864 A1 EP3421864 A1 EP 3421864A1 EP 18179109 A EP18179109 A EP 18179109A EP 3421864 A1 EP3421864 A1 EP 3421864A1
Authority
EP
European Patent Office
Prior art keywords
container
tank
reinforcing
suspension
outer casing
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
Application number
EP18179109.6A
Other languages
English (en)
French (fr)
Other versions
EP3421864B1 (de
Inventor
Gwenaëlle CADO
Julien LALLOUET
Romain Sibarita
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ateliers Et Chantiers de la Grande Bruyere (acgb)
Original Assignee
Ateliers Et Chantiers de la Grande Bruyere (acgb)
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Publication date
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Publication of EP3421864A1 publication Critical patent/EP3421864A1/de
Application granted granted Critical
Publication of EP3421864B1 publication Critical patent/EP3421864B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C3/00Vessels not under pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • F17C2201/0157Polygonal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • F17C2201/0161Honeycomb
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • F17C2201/0166Shape complex divided in several chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • F17C2201/0171Shape complex comprising a communication hole between chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03Orientation
    • F17C2201/035Orientation with substantially horizontal main axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/056Small (<1 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/011Reinforcing means
    • F17C2203/012Reinforcing means on or in the wall, e.g. ribs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/011Reinforcing means
    • F17C2203/013Reinforcing means in the vessel, e.g. columns
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/014Suspension means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0308Radiation shield
    • F17C2203/032Multi-sheet layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0391Thermal insulations by vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0609Straps, bands or ribbons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0626Multiple walls
    • F17C2203/0629Two walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0646Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0123Mounting arrangements characterised by number of vessels
    • F17C2205/013Two or more vessels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0323Valves
    • F17C2205/0332Safety valves or pressure relief valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/2181Metal working processes, e.g. deep drawing, stamping or cutting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/219Working processes for non metal materials, e.g. extruding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/033Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04Indicating or measuring of parameters as input values
    • F17C2250/0404Parameters indicated or measured
    • F17C2250/0408Level of content in the vessel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/012Reducing weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/016Preventing slosh
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/018Adapting dimensions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0171Trucks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0176Buses

Definitions

  • the technical field of the present invention is that of liquefied gas tanks, such as liquefied natural gas (G.N.L), intended to equip motor vehicles.
  • liquefied gas tanks such as liquefied natural gas (G.N.L)
  • G.N.L liquefied natural gas
  • Liquefied natural gas is natural gas converted into liquid form. This liquid state is reached when the gas is cooled to a temperature of about -161 ° C at atmospheric pressure.
  • Liquefaction reduces the gaseous volume of natural gas and stores it in one or more tanks installed, for example, on the chassis of the truck.
  • the liquefied natural gas contained in the tank is regasified so as to feed the truck engine.
  • This fuel is less polluting than gasoline and diesel, and the autonomy of trucks using this fuel makes them suitable for long-distance road transport.
  • Liquefied natural gas tanks of trucks are designed to meet strict safety requirements, including pressure and maintaining a very low temperature, to maintain the gas in its liquid phase.
  • the tanks usually used have a cylindrical shape and have a double wall stainless steel between which are arranged an insulator multi-layer and vacuum classically. Their weight is therefore relatively important and their useful volume is reduced.
  • the tanks having this shape occupy a large space and are not adapted to the spaces / compartments of various shapes of the vehicle in which they are intended to be implanted.
  • the invention proposes for this purpose a tank for a motor vehicle intended to contain liquefied gas, such as liquefied natural gas.
  • the invention provides a tank of liquefied gas (LNG for example) double wall generally of substantially parallelepipedal shape comprising a container forming an inner wall and an outer envelope disposed around said container outer protective wall.
  • LNG liquefied gas
  • an intermediate space containing vacuum and / or an insulating material.
  • the fastening of the container to said outer envelope by suspension means allows to provide a degree of freedom between the two elements, so as to limit heat transfer by conduction and to compensate the thermal expansion / retraction due to the cooling of the internal container by limiting the stress inputs.
  • suspension means also allow mechanical movement of the container relative to said outer envelope.
  • the parallelepipedal shape of the container optimizes its storage capacity in liquefied gas and the parallelepipedal shape of the outer casing allows optimal integration of the reservoir to the vehicle architecture.
  • these suspension means allow a relative displacement of said container with respect to said outer envelope less than 10 mm, for example between 1 and 6 mm, and more specifically between 1 and 4 mm.
  • the thermal contraction of said container may be equal to 4 mm on each side of the container for example.
  • the suspension means thus make it possible to compensate for this retraction of the internal container.
  • the liquefied gas can be LNG (liquid methane), or liquid nitrogen for refrigerated trucks, for example.
  • said container is connected to a first lateral end of said outer envelope by suspension straps and to a second lateral end of said outer envelope by a suspension ring.
  • said suspension ring is attached to the inner surface of a side wall of said outer envelope and is fitted on a stud carried by the outer surface of a side wall of the container.
  • said suspension straps and said suspension ring are made of a thermally insulating material.
  • suspension means may alternatively be springs or silentblocs when these suspension means are insulating.
  • said container is connected to a first lateral end of said outer envelope by suspension straps and to a second lateral end of said outer envelope by suspension straps.
  • suspension straps are made of a thermally insulating material.
  • said internal reinforcing structure comprises a reinforcing framework secured to the inner wall of said container, the internal reinforcing structure comprising a plurality of reinforcing rings, substantially octagonal, spaced along the longitudinal axis of the container, and extending transversely to said longitudinal axis.
  • This reinforcing framework optimizes the mechanical strength of the container at the internal pressure of the liquefied gas and avoids the phenomena of inertia of the contained fluid.
  • a coiled cable could be used.
  • said reinforcing rings are mounted spaced apart on reinforcing bars extending parallel to the longitudinal axis and arranged around the periphery of the reinforcing rings, said reinforcing bars being each secured to a reinforcing rail fixed on the wall. internal of said container.
  • said internal reinforcing structure comprises a plurality of angle reinforcing plates fixed on the inner wall of said container and each connecting two adjacent inner faces of said container.
  • the container is made of aluminum.
  • said outer envelope is made of a fire-resistant material.
  • said outer envelope is covered on its surface exterior or interior of a fire resistant coating.
  • the outer shell can be made of aluminum or composite materials.
  • a fire resistant coating may be arranged alternatively or in addition to the outer surface of the container.
  • the internal reinforcing structure may be made of aluminum, or a composite material, for example.
  • the wall of the container and the wall of the outer casing are distant from each other, the space between these walls being filled with insulating means.
  • the space between the wall of the container and the wall of the outer casing is, for example, between 25 and 50 mm.
  • the internal reinforcing structure comprises a plurality of reinforcement plates spaced along the longitudinal axis of said container and extending transversely to said longitudinal axis.
  • said reinforcing plates are solid and have at least one orifice for passing the liquefied gas within said container.
  • the container comprises a reinforcing rod extending parallel to said longitudinal axis and connecting the side walls of the container through said reinforcing plates.
  • This reinforcing rod allows the maintenance of the bottoms, or side walls, of the container.
  • the internal reinforcing structure further comprises a reinforcement frame having a generally parallelepipedal shape and disposed against the inner wall of said container.
  • said reinforcing plates have a solid central portion from which extend several branches passing through the wall of said reinforcing framework.
  • the ends of the branches protruding from the outer surface of said reinforcement frame have a passage slot of a securing strip of the reinforcing plates to said reinforcement framework.
  • the securing strips extend in longitudinal grooves formed around the periphery of the outer surface of said reinforcing framework.
  • the invention also relates to a motor vehicle, such as a heavy vehicle, comprising at least one tank as described above.
  • the invention relates to a tank for a motor vehicle for containing liquefied gas, such as liquefied natural gas.
  • FIG. 1 in perspective, a container, according to a first embodiment, implemented in a motor vehicle tank according to the invention.
  • the inner space of the container 100 constitutes a sealed enclosure for the storage of liquefied natural gas under pressure (up to 20 bar, for example).
  • the container 100 is intended to be housed in an outer envelope (not shown) of the reservoir.
  • the container 100 and the outer envelope each have a generally parallelepipedal shape.
  • the container 100 is made of aluminum and has a length of two meters.
  • the container 100 extends longitudinally along the longitudinal axis Ax and its cross section to the axis Ax is a square whose corners are rounded (the cross section of the container could be rectangle).
  • the lateral faces 102, 103 located at the longitudinal ends of the container 100 are slightly curved or curved outwardly thereof in order to improve the distribution of the stresses related to the pressure of the liquefied natural gas under pressure.
  • the container 100 further comprises a plurality of reinforcing plates 110 planes or having reliefs, disposed within the container 100 and spaced along the longitudinal axis Ax.
  • the reinforcing plates 110 have a plurality of openings 111. Such openings allow the homogeneous distribution of the fluid under pressure throughout the container 100.
  • the container 100 comprises seven reinforcing plates 110 each having five openings 111, namely a central opening 112 and four peripheral openings 113.
  • each reinforcing plate 110 is aligned with the openings 111 of the adjacent reinforcing plates 110.
  • the parallelepipedal shape of the container 100 optimizes its fuel storage capacity and allows optimal integration with the vehicle architecture.
  • the figure 2 illustrates a container, according to a second embodiment, implemented in a motor vehicle tank according to the invention.
  • the container 200 extends longitudinally along the axis Ax and its cross section along the axis Ax is a square (or a rectangle) whose corners are rounded.
  • the container 200 is intended to be housed in an outer casing (not shown) of the reservoir.
  • the container 200 and the outer casing each have a generally parallelepipedal general shape.
  • the side faces 202, 203 at the longitudinal ends of the container 200 are slightly curved inwardly or curved outwardly therefrom.
  • the container 200 further comprises a plurality of plane reinforcing plates 210 disposed within the container 200 and spaced along the longitudinal axis Ax.
  • the reinforcing plates 210 have a single central opening 212.
  • the lateral faces 202, 203 of the container 200 each carry a plate 220, 230 respectively.
  • the plates 220, 230 are connected by a tube or rod 240 longitudinally through the container 200 passing through the central opening of each internal reinforcing plate 210.
  • the tube or the rod 240 protrudes from the outer surface of each of the plates 220, 230.
  • the tube or the rod 240 makes it possible to hold the bottoms or side walls of the container 200, and thus serves as a reinforcement.
  • the figure 3 illustrates a container, according to a third embodiment, implemented in a motor vehicle tank according to the invention.
  • the container 300 extends longitudinally along the axis Ax and its cross section along the axis Ax is a square (or a rectangle) whose corners are rounded.
  • the container 300 is intended to be housed in an outer shell (not shown) of the tank.
  • the container 300 and the outer casing each have a generally parallelepipedal general shape.
  • the side faces 302, 303 located at the longitudinal ends of the container 300 are flat.
  • the container 300 further comprises a plurality of flat 310 reinforcing plates disposed within the reservoir 300 and spaced along the longitudinal axis Ax. These plates extend transversely to the longitudinal axis Ax and their outer periphery comes into contact with the inner wall of the container 300.
  • the reinforcing plates 310 have a single central opening 312.
  • the recesses 305 have a semicircular section and extend transversely to the longitudinal axis Ax over the entire periphery of the container 300.
  • Such recesses 305 make it possible to improve the mechanical strength of the container 300 at the internal pressure of the liquefied natural gas.
  • the recesses have a different shape and / or that they extend partially around the periphery of the outer surface of the container.
  • the figure 4 illustrates a container, according to a fourth embodiment, implemented in a motor vehicle tank according to the invention.
  • the container 400 extends longitudinally along the axis Ax and its cross section along the axis Ax is a square (or a rectangle) whose corners are rounded.
  • the container 400 is intended to be housed in an outer shell (not shown) of the tank.
  • the container 400 and the outer envelope each have a generally parallelepipedal shape.
  • the container 400 comprises a plurality of flat reinforcing plates 410 disposed within the container 400 and spaced along the longitudinal axis Ax. These reinforcing plates 410 extend transversely to the longitudinal axis Ax and their outer periphery comes into contact with the inner wall of the container 400.
  • Each reinforcing plate 410 comprises a single central opening 412 and several lateral slots 414.
  • Such slots 414 allow the passage of reinforcing crosspieces 450 disposed against the inner wall of the container 400 and extending along the longitudinal axis Ax along the entire length of the container 400.
  • the tube or rod 440 protrudes from the outer surface of the side faces 402, 403, and serves as a reinforcement.
  • the Figure 5A illustrates a container, according to a fifth embodiment, implemented in a motor vehicle tank according to the invention, the Figure 5B being a detail view of the container.
  • the container 500 (shown without its side walls) is intended to be housed in an outer shell (not shown) of the tank.
  • the container 500 and the outer envelope each have a generally parallelepipedal general shape, the section of the container 500 being slightly smaller than that of the outer envelope so that it can be accommodated.
  • the square (or rectangular) section of the container 500 allows an increase in the useful volume of the latter.
  • the container 500 is made of aluminum, has a length of 2.30 m and a storage capacity of 584 liters of gas (188 kg of gas).
  • the tank has a weight of 329 kg.
  • the parallelepipedal aluminum tank of the invention Compared to a stainless steel tank of the same length and cylindrical section, the parallelepipedal aluminum tank of the invention has a reduced weight of the order of 3% and a useful volume of the container increased by 4%, which allows saving fuel and reducing CO2 emissions.
  • the parallelepipedal shape of the container 500 optimizes its fuel storage capacity and the parallelepipedal shape of the outer shell allows optimal integration of the tank with the vehicle architecture.
  • a tank according to the invention has a higher fuel storage capacity of the order of 12 to 25% compared to the cylindrical tanks of the prior art.
  • the ends 516 of the branches 515 pass through the slots in the grooves 551 of the reinforcement frame 550 and protrude from the bottom of the grooves (without exceeding the portions of the outer surface of the frame connecting the grooves).
  • Each of these projecting ends 516 has a slot 517 for the passage of a securing bar 560 of the reinforcing plates 510 to the reinforcement frame 550.
  • the securing strips 560 pass through the aligned slots of each of the reinforcing plates 510.
  • These securing strips 560 allow a distribution of stresses along the container 500 and the maintenance of the internal reinforcing plates 510.
  • the reinforcing plates 510 are disposed within the reinforcement framework 550 and are spaced along the longitudinal axis Ax.
  • These reinforcing plates 510 extend transversely to the longitudinal axis Ax and have a star structure.
  • the solid center portion section 510 'of the backing plate 510 is square, the corners being rounded. From each of these rounded angles extend three rectilinear branches 515 spaced from each other by an angle ⁇ of 45 ° in this example and whose central branch is aligned, or substantially aligned, with the diagonal of the central portion full 510 '.
  • a reinforcement tube or rod 540 extends parallel to the longitudinal axis Ax and passes through the reinforcing plates 510 in their middle.
  • the container 500, the reinforcement frame 550 and the reinforcing plates 510 are made of aluminum, for example, and that the reinforcement frame 550 and the reinforcement plates 510 are, for example, welded to each other. other.
  • the reinforcement frame 550 is a corrugated aluminum sheet welded around the reinforcing plates 510.
  • the reinforcement frame 550 is made of another material, such as a composite material.
  • the Figure 9A illustrates a container 900, according to a sixth embodiment implemented in a motor vehicle tank according to the invention.
  • the container 900 is intended to be housed in an external envelope (not shown) for protecting the reservoir.
  • the container 900 and the outer envelope each have a generally parallelepipedal shape, with rounded corners, the section of the container 900 being slightly smaller than that of the outer envelope so that it can be accommodated therein.
  • the substantially square section of the container 900 allows an increase in the useful volume of the latter.
  • the parallelepipedal shape of the container 900 optimizes its fuel storage capacity and the parallelepipedal shape of the outer shell allows optimal integration of the tank with the vehicle architecture.
  • the Figure 9B is a cross-sectional view of the container 900 showing the arrangement of a ring 940 of the backing frame 950, corner reinforcing plates 910, reinforcing rails 920, and reinforcing bars 930.
  • the Figure 9D is a detail view showing the attachment of several rings 940 on the reinforcement bars 930 of the reinforcement frame 950.
  • Successive rings 940 of substantially octagonal shape are thus fixed to several reinforcement bars 930, thus forming a group of rings spaced at regular intervals along the longitudinal axis Ax of the container 900.
  • This group of rings 940 is fixed to the inner wall of the container 900 by sliding reinforcing bars 930 in the grooves of the reinforcing rails 920 attached to the inner wall container 900.
  • the container 900, the elements constituting the reinforcement framework 950 (with the exception of the reinforcing rings 940) and the reinforcing plates 910 are made of aluminum, for example.
  • FIGS. 6A to 6D illustrate a reservoir 6 according to the invention comprising a container 600 and an outer casing 60, whose walls are spaced apart.
  • the space between the wall of the container and the wall of the outer casing is, for example, between 25 and 50 mm.
  • each have a generally parallelepipedal general shape, the section of the container 600 being slightly smaller than that of the outer casing 60 so that it can be accommodated therein.
  • the container 600 may be one of the containers of the six embodiments described above.
  • a multi-layer insulator and / or vacuum are arranged between the spaced walls of the container 600 and the outer casing 60 (which thus make it possible to avoid heat exchange by indirect contact between the container and the outer casing).
  • the reservoir 6 uses suspension means MS1, MS2 from the container 600 to the outer casing 60.
  • suspension means in particular make it possible to compensate for the thermal expansion / shrinkage of the internal container due to cooling by limiting the contribution of stresses.
  • the Figures 6A and 6B show the first means of suspension MS1 and the Figures 6C and 6D show the second suspension means MS2.
  • the height of the stud 606 is smaller than the thickness of the suspension ring 64.
  • the flat surface of the pad 606 is not in contact with the first internal lateral face of the outer casing 60.
  • the suspension ring 64 is made of a thermally insulating material to limit heat transfer by conduction.
  • the second suspension means MS2 comprise a plurality of straps 67 located on the side of the second external lateral face 603 of the container 600 and the second internal lateral face of the outer envelope 60 which are arranged facing each other.
  • Each of the straps 67 is made of a thermally insulating material to limit heat transfer by conduction.
  • a nut 634 which is mounted on a threaded rod 633 forming the base of the "Y” makes it possible to move in translation (in the directions of the double arrow of the Figure 6D ) the element 632 in the form of "Y” and thus to adjust the tension of the strap 67.
  • the tension of the straps 67 is chosen so as to minimize the sloshing of the container 600, even in the event of a collision of the vehicle.
  • the first and second suspension means may take other forms and be, for example, in the form of springs or silentblocs.
  • first and second suspension means MS1, MS2 comprise several straps 67 located on the side of each external lateral face 603 of the container 600 disposed opposite an internal lateral face of the outer envelope 60.
  • the suspension means offer a minimum degree of freedom and allow a movement of the container 600 relative to the outer casing 60.
  • This relative movement of the container 600 with respect to the outer envelope 60, along at least one of the three axes x, y and z ( Figure 6C ), is less than or equal to 10 mm and may be in particular between 1 and 6 mm, preferably between 1 and 4 mm.
  • the straps 67 of insulating material are disposed on the periphery of each side face of the container 600 (only one side face being visible in these figures).
  • the block element 635 and the support 631 each comprise an axis 637, 636 respectively around which is wound one end of the strap 67.
  • a ring 638 made of aluminum or stainless steel is positioned against a stop welded to the outer casing 60. This ring 638 makes it possible to wedge the bottom of the container 600. It is made of several mechanically welded parts.
  • the strap supports 631 are welded to the ring 638 and in the same material as the latter (aluminum or stainless steel).
  • the system for adjusting the tension of each strap 67 is carried by the corresponding block element 635 which has a generally "U" shape.
  • This block element 635 comprises fastening screws 639A of the block element 635 on the container 600, a first slider 640 on which is mounted the pin 637 of the strap 67 and a second slider 641 serving as a nut with two screws. 639B setting. It is possible to adjust the tension of the strap 67 by adjusting the position of the first slide 640 carrying the axis 637 in the direction of the double arrow F1 relative to the second slide 641. To do this, it acts on the adjusting screw 639B so as to move the second slide 641 in the direction of the double arrow F2, that is to say in a direction perpendicular to the direction of movement of the first slide 640. These movements of the slides in two perpendicular planes are provided by the implementation of inclined planes on each of the slides 640, 641 which are arranged vis-à-vis ( Figure 10C ).
  • the straps 67 of insulating material are disposed on the periphery of each side face of the container 600 (only one side face being visible in these figures).
  • the block element 635 and the support 631 each comprise an axis 637, 636 respectively around which is wound one end of the strap 67.
  • the system for adjusting the tension of each strap 67 is carried by the corresponding block element 635 which has a generally "U" shape.
  • This block element 635 comprises fixing screws 639A of the block element 635 on the container 600, a slide 640 on which is mounted the axis 637 of the strap 67 and adjustment screws 639B. It is possible to adjust the tension of the strap 67 by adjusting the position of the slide 640 carrying the axis 637 in the direction of the double arrow F1. To do this, one acts on the adjusting screws 639B on which come to rest the slide 640.
  • the straps 67 of insulating material are disposed on the periphery of each side face of the container 600 (only one side face being visible in these figures).
  • the supports 642, 643 each comprise an axis 636, 637 respectively around which is wound one end of the strap 67.
  • Two adjustment screws 639B which pass through the supports 643, 644 make it possible to move in translation (in the directions of the double arrow F1 of the figure 12C ) the support 643 movable relative to the fixed support 644 and thus to adjust the tension of the strap 67.
  • This particular approach implements, for each strap 67, two sliders 646 carrying the axis 636 of the strap 67, the sliders 646 being able to slide along the longitudinal axis of the container 600 in a rail 645 welded to the outer envelope 60.
  • Adjusting the tension of the strap 67 therefore requires adjusting the position of the two slides 646.
  • the figure 7 illustrates an example of installation of a tank according to the invention on a motor vehicle, in this case a truck, of which only the support frames 9, 9 'are visible.
  • a section through the wall of the tank 7 makes it possible to distinguish the different constituent elements of such a tank.
  • the structure of the reservoir 7 as shown corresponds to that of the reservoir of the embodiment illustrated in FIGS. Figures 5A and 5B .
  • Such a reservoir 7 thus comprises an outer envelope 70 surrounding a container 700, the latter comprising a reinforcement frame 750.
  • the branches 715 of the reinforcing plates 710 extend transversely to the longitudinal axis of the reservoir 7, and are secured to the reinforcement framework 750 by reinforcing bars 760.
  • a side and / or longitudinal wall of the reservoir 7 is mechanically and fluidly coupled to a technical box 8.
  • insulating means disposed in the space between the walls of the outer casing 70 and the container 700.
  • the outer shell of the tank may be made of any material adapted to withstand fire and possibly other safety constraints.
  • the outer surface of the outer envelope may be covered with at least one layer of material adapted to withstand fire.
  • It may be a fire-resistant paint or other type of coating that is applied to the outer and / or inner surface of the outer shell and / or the outer surface of the container.
  • the tank according to the invention can be installed on other types of motor vehicles, such as buses.
  • FIGS. 8a to 8m illustrate the section of different containers of a tank according to the invention obtained by an extrusion process.
  • the containers of Figures 8j and 8k have a curved and polygonal outer section respectively without internal reinforcement structure.
  • the container of the figure 8m has a four-leaf clover outer section with an internal reinforcing channel.
  • the reservoir of the invention can be assembled with other tanks of the same type.
  • the tank obtained by such an assembly can be housed in vehicle compartments of complex shapes.
  • the shape of the tank can be adapted to the volumes available on the chassis of the vehicle.
  • lateral faces located at the longitudinal ends of the container may be curved, curved or flat.
  • the longitudinal sides of the container may have a curve.
  • the reservoir of the invention can contain any type of liquefied gas, such as LNG (liquid methane), or liquid nitrogen for refrigerated trucks, for example.
  • LNG liquid methane
  • liquid nitrogen for refrigerated trucks
  • suspension straps is not limited to the examples illustrated.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
EP18179109.6A 2017-06-26 2018-06-21 Flüssig-erdgastank für kraftfahrzeuge Active EP3421864B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1755842A FR3068106B1 (fr) 2017-06-26 2017-06-26 Reservoir de gaz naturel liquefie pour vehicules automobiles

Publications (2)

Publication Number Publication Date
EP3421864A1 true EP3421864A1 (de) 2019-01-02
EP3421864B1 EP3421864B1 (de) 2020-01-29

Family

ID=59859273

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18179109.6A Active EP3421864B1 (de) 2017-06-26 2018-06-21 Flüssig-erdgastank für kraftfahrzeuge

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EP (1) EP3421864B1 (de)
FR (1) FR3068106B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022053585A1 (en) * 2020-09-09 2022-03-17 Xcience Ltd Pressure vessel liner, pressure vessel and methods
EP4124792A1 (de) * 2021-07-29 2023-02-01 Airbus Operations SAS Behälter, insbesondere für einen flüssigwasserstofftank, der mit innenschienen zum einbau eines gerätemoduls versehen ist

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3107747B1 (fr) * 2020-03-02 2022-02-11 Ateliers Et Chantiers De La Grande Bruyere Acgb Structure de renfort d’un réservoir de fluide cryogénique, tel que du gaz naturel liquéfié, pour véhicules automobiles
EP4150243A1 (de) 2020-05-12 2023-03-22 Universal Hydrogen Co. Brennstoffspeichermodulanordnung
US11420757B2 (en) 2020-08-21 2022-08-23 Universal Hydrogen Co. Systems and methods for multi-module control of a hydrogen powered hybrid electric powertrain
CA3199672A1 (en) * 2020-10-30 2022-05-05 Universal Hydrogen Co. Systems and methods for storing liquid hydrogen

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2379126A (en) * 1943-05-11 1945-06-26 Glenn L Martin Co Surge plate
US3979005A (en) * 1974-05-13 1976-09-07 The Boeing Company Cryogenic tank and aircraft structural interface
US5263604A (en) * 1991-07-01 1993-11-23 Messerschmitt-Bolkow-Blohm AG Suspension arrangement for a tank
FR2781431A1 (fr) * 1998-07-21 2000-01-28 Giat Ind Sa Reservoir pour vehicule
FR2796010A1 (fr) * 1999-07-06 2001-01-12 Renault Reservoir en materiau composite destine au stockage de carburant liquefie sous pression
EP1128123A1 (de) * 2000-02-25 2001-08-29 Linde Aktiengesellschaft Speicherbehälter für kryogene Flüssigkeiten mit verstärkten Wandungen
FR2857082A1 (fr) * 2003-07-02 2005-01-07 Air Liquide Reservoir de fluide cryogenique et utilisation dans un vehicule automobile

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2379126A (en) * 1943-05-11 1945-06-26 Glenn L Martin Co Surge plate
US3979005A (en) * 1974-05-13 1976-09-07 The Boeing Company Cryogenic tank and aircraft structural interface
US5263604A (en) * 1991-07-01 1993-11-23 Messerschmitt-Bolkow-Blohm AG Suspension arrangement for a tank
FR2781431A1 (fr) * 1998-07-21 2000-01-28 Giat Ind Sa Reservoir pour vehicule
FR2796010A1 (fr) * 1999-07-06 2001-01-12 Renault Reservoir en materiau composite destine au stockage de carburant liquefie sous pression
EP1128123A1 (de) * 2000-02-25 2001-08-29 Linde Aktiengesellschaft Speicherbehälter für kryogene Flüssigkeiten mit verstärkten Wandungen
FR2857082A1 (fr) * 2003-07-02 2005-01-07 Air Liquide Reservoir de fluide cryogenique et utilisation dans un vehicule automobile

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022053585A1 (en) * 2020-09-09 2022-03-17 Xcience Ltd Pressure vessel liner, pressure vessel and methods
EP4124792A1 (de) * 2021-07-29 2023-02-01 Airbus Operations SAS Behälter, insbesondere für einen flüssigwasserstofftank, der mit innenschienen zum einbau eines gerätemoduls versehen ist
FR3125857A1 (fr) * 2021-07-29 2023-02-03 Airbus Operations Cuve, en particulier pour réservoir à hydrogène liquide, pourvu de rails internes pour la mise en place d’un module d’équipements.

Also Published As

Publication number Publication date
FR3068106B1 (fr) 2020-10-09
FR3068106A1 (fr) 2018-12-28
EP3421864B1 (de) 2020-01-29

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