US20120018314A1 - Pressure Vessel for Storing Gaseous Media Under Pressure - Google Patents
Pressure Vessel for Storing Gaseous Media Under Pressure Download PDFInfo
- Publication number
- US20120018314A1 US20120018314A1 US13/125,773 US200913125773A US2012018314A1 US 20120018314 A1 US20120018314 A1 US 20120018314A1 US 200913125773 A US200913125773 A US 200913125773A US 2012018314 A1 US2012018314 A1 US 2012018314A1
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- US
- United States
- Prior art keywords
- pressure vessel
- wrapping
- liner
- intermediate layer
- gas
- 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.)
- Abandoned
Links
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- 239000002657 fibrous material Substances 0.000 claims description 2
- 239000001257 hydrogen Substances 0.000 abstract description 51
- 229910052739 hydrogen Inorganic materials 0.000 abstract description 51
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 abstract description 46
- 239000007789 gas Substances 0.000 abstract description 21
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000009825 accumulation Methods 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
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- 239000000446 fuel Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000035699 permeability Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
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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
- 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
- F17C1/04—Protecting sheathings
- F17C1/06—Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0604—Liners
-
- 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
- F17C2203/0607—Coatings
-
- 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
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/0663—Synthetics in form of fibers or filaments
- F17C2203/0673—Polymers
-
- 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
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0305—Bosses, e.g. boss collars
-
- 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
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
-
- 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
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0388—Arrangement of valves, regulators, filters
- F17C2205/0394—Arrangement of valves, regulators, filters in direct contact with the pressure vessel
- F17C2205/0397—Arrangement of valves, regulators, filters in direct contact with the pressure vessel on both sides of the pressure vessel
-
- 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
- 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
- F17C2223/03—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)
-
- 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
- F17C2260/03—Dealing with losses
- F17C2260/035—Dealing with losses of fluid
- F17C2260/037—Handling leaked fluid
-
- 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
- F17C2260/04—Reducing risks and environmental impact
- F17C2260/042—Reducing risk of explosion
-
- 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
- F17C2270/0184—Fuel cells
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/32—Hydrogen storage
Definitions
- the invention relates to a pressure vessel for the storage of pressurized gaseous media.
- a pressure vessel of this type including a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner which gives the pressure vessel its dimensional stability.
- Such generic pressure vessels which are also referred to as composite pressure vessels, are known from EP 0 753 700 A1, for example. They comprise a liner defining an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability.
- the liner is usually made of a plastic material, while the wrapping is produced from a fibrous composite material.
- Pressure vessels of this type are for example used as hydrogen reservoirs in fuel cell systems and can store gaseous hydrogen at several hundred bars of excess pressure.
- DE 33 08 276 A1 discloses a multilayer pressure vessel for hot hydrogen, wherein hydrogen which penetrates through the innermost metal layer of the wall is vented from the space between the innermost metal layers in order to prevent a hydrogen attack and/or an embrittlement problem in the outer metal layers of the wall of the vessel.
- JP 2007-278482 A describes a composite pressure vessel with an inner tank and an outer tank.
- a continuous catalyst layer is provided between the inner and outer tanks, which converts the hydrogen into a stable compound.
- the present invention provides a solution to the problem of creating a composite pressure vessel of the type referred to above which excludes any risk to the environment posed by gases escaping at excessively high rates.
- This problem is solved by providing that an instantaneous escape of gaseous media at high rates during a discharge of the pressure vessel after a prolonged downtime is prevented by discharging gaseous media penetrating through the liner continuously and therefore at lower rates from the pressure vessel into the environment.
- the accumulation of gases penetrating through the liner in pockets between the liner and the wrapping and their instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel as a result of the separation between liner and wrapping are therefore avoided.
- a pressure vessel for the storage of pressurized gaseous media comprises a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability.
- the wrapping of the pressure vessel is designed to be at least partially gas-permeable, allowing the gas penetrating through the liner to escape from the pressure vessel through the wrapping.
- This structure of the pressure vessel with an at least partially gas-permeable wrapping has the result that the gas penetrating through the liner can be discharged continuously and at low rates from the pressure vessel into the environment. In this way, the accumulation of the gas penetrating through the liner between the liner and the wrapping, and its instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel, are prevented.
- the wrapping of the pressure vessel is designed to be at least partially porous.
- the wrapping of the pressure vessel may, for example, be made of a fibrous material bound with a resin material, the resin material being at least partially porous in the set state.
- the wrapping of the pressure vessel is provided at predetermined points with holes which connect the interior of the wrapping to its outside.
- the wrapping of the pressure vessel is provided on its outside with a coating (e.g., layer of paint) which is likewise designed to be gas-permeable at least in the gas-permeable regions of the wrapping.
- a coating e.g., layer of paint
- a pressure vessel for the storage of pressurized gaseous media comprises a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability.
- a gas-permeable intermediate layer is provided between the liner and the wrapping, this being connected to the outside of the wrapping in at least one region, so that the gas penetrating through the liner can escape from the pressure vessel through the intermediate layer.
- This structure of the pressure vessel with an at least partially gas-permeable intermediate layer between the liner and the wrapping has the result that the gas penetrating through the liner can be discharged continuously and at low rates from the pressure vessel into the environment. In this way, the accumulation of the gas penetrating through the liner between the liner and the wrapping, and its instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel, are prevented.
- the intermediate layer is at least partially porous.
- a gas treatment device which may, for example, be formed by impregnating the intermediate layer with a gas treatment medium is provided in the connecting region between the intermediate layer and the outside of the wrapping.
- the gas treatment device may for example comprise an oxidising catalyst. If the gaseous medium stored in the pressure vessel is hydrogen, the hydrogen flowing through the liner and through the intermediate layer is oxidized to water by the oxidizing catalyst and can be discharged without endangering the environment.
- the connecting region between the intermediate layer and the outside of the wrapping is provided in the region of a neck of the pressure vessel. This may be the region of a filling and/or discharge opening of the pressure vessel.
- FIG. 1 is a diagrammatic sectional view of a composite pressure vessel according to the present invention
- FIG. 2 is an enlarged part-section of a conventional composite pressure vessel before its discharge
- FIG. 3 is an enlarged part-section of a conventional composite pressure vessel after its discharge
- FIG. 4 is an enlarged part-section of a composite pressure vessel according to a first embodiment of the invention before its discharge;
- FIG. 5 is an enlarged part-section of a composite pressure vessel according to a first embodiment of the invention after its discharge.
- FIG. 6 is a diagrammatic sectional view of a composite pressure vessel according to a second embodiment of the present invention.
- the present invention is described below with reference to a pressure vessel for the storage of gaseous hydrogen at a pressure of, e.g., 700 bar, which may be used, for example, in fuel cell systems.
- the invention is, however, in no way restricted to this particular gaseous medium, this particular excess pressure in the interior of the pressure vessel and this particular application.
- FIG. 1 With reference to FIG. 1 , the basic structure of a composite pressure vessel to which the present invention can be applied is described in greater detail below.
- the composite pressure vessel 10 is formed from a liner 12 which defines an interior 14 for the accommodation of gaseous hydrogen.
- a plastic material may for example be used for the production of the liner 12 .
- the liner 12 is surrounded by a wrapping 16 which may, for example, be made of a fibrous composite material such as resin-impregnated carbon fibers and which gives the pressure vessel 10 the necessary dimensional stability.
- the materials for the production of the liner 12 and the wrapping 16 are, however, not restricted to those mentioned above.
- the invention is not restricted to a specific form of the wrapping 16 (e.g., axial and/or tangential and/or angled winding direction of the fibers) and to a specific thickness of the liner 12 and the wrapping 16 .
- the design of an embodiment fulfilling specific requirements e.g., type of gas, pressure, application, etc.
- the pressure vessel 10 has two neck regions (on top and at the bottom in FIG. 1 ), each of which is provided with an opening 22 sealed by a neck piece 18 and 20 , respectively.
- a valve 24 may be provided in the opening 22 which is not sealed by a neck piece (on top in the figure).
- the present invention is not restricted to a specific design of the neck pieces 18 , 20 .
- the two neck regions of the pressure vessel 10 may be provided with pole caps for the additional stabilization of the pressure vessel 10 .
- the pressure vessel 10 may optionally be provided with two openings 22 fitted with valves 24 .
- the shape of the pressure vessel 10 is moreover not restricted to that with two neck regions as shown in FIG. 1 .
- a coating 26 for example, a layer of paint, is further applied to the outside of the wrapping 16 .
- gaseous hydrogen may, for example, be stored at a pressure of approximately 700 bar. In the course of time, a certain amount of this hydrogen is diffused through the liner 12 (see arrow 28 in FIG. 2 ). This gaseous hydrogen which has penetrated through the liner 12 largely accumulates in pockets 30 between the liner 12 and the wrapping 16 . A small proportion of this hydrogen may reach the environment through pores or holes 32 in the wrapping 16 . A free access of this accumulated hydrogen to the few small holes 32 in the wrapping is greatly impeded by a macroscopically flush contact between the wrapping 16 and the liner 12 at high pressure in the interior 14 of the liner 12 .
- the hydrogen in the pockets 30 between the liner 12 and the wrapping 16 causes a build-up of pressure which may in extreme cases result in a deformation of the liner 12 .
- the hydrogen diffused through the liner instantaneously flows from the pressure vessel 10 at a comparatively high rate.
- the present invention proposes that the pressure build-up between the liner 12 and the wrapping 16 after a prolonged downtime of the pressure vessel 10 , which has been described above, should be avoided. For this purpose various measures are taken within the scope of the present invention.
- a first embodiment of a pressure vessel according to the invention is explained below with reference to FIGS. 4 and 5 .
- the pressure vessel 10 of this embodiment comprises a liner 12 which defines an interior 14 for the accommodation of a gaseous medium and a wrapping 16 encompassing the liner 12 .
- a high pressure in the interior 14 likewise causes the diffusion of a small quantity of hydrogen through the liner 12 (see arrows 28 in FIG. 4 ), the hydrogen initially accumulating in pockets 30 between the liner 12 and the wrapping 16 .
- the wrapping of the pressure vessel 10 of this embodiment is designed to be at least partially gas-permeable.
- the wrapping 16 may for example be porous.
- the wrapping 16 is provided at predetermined points with holes 34 which connect the interior of the wrapping 16 to its outside. In this way, the gaseous hydrogen penetrating through the liner 12 can be discharged continuously and at low rates through the wrapping 16 to the outside. Compared to the instantaneous release of the hydrogen at a high rate, the potential risk to the surroundings of the pressure vessel 10 posed by the escaping gaseous hydrogen is noticeably reduced.
- the wrapping 16 is designed to be gas-permeable at least in certain regions. In exemplary embodiments of the invention, however, the wrapping is designed to be gas-permeable substantially across all of its regions.
- this layer of paint 26 will have to be gas-permeable as well in this embodiment. This applies at least to the regions in which the wrapping 16 is designed to be gas-permeable.
- the porous wrapping 16 may for example be structured as follows.
- the wrapping 16 essentially consists of a fibrous composite material which may for example be made up from carbon fibers which give the wrapping its inherent compressive strength and of a resin for binding the carbon fibers. This resin has to be at least partially porous. The strength and stability under pressure of the wrapping 16 as a whole will nevertheless have to be ensured.
- the resin used for binding does not make any significant contribution to the stability of the pressure vessel 10 under pressure; the deciding factor is the carbon fiber bond.
- a resin may be used which, owing to high inner stresses, forms a sufficient number of micro-cracks in the setting process. These micro-cracks must, however, not result in a complete disintegration of the wrapping 16 . In addition, the micro-cracks have to form a continuous connection through the entire wrapping 16 , as they are required for the removal of the hydrogen into the environment.
- the gas-permeability of the wrapping 16 obviously varies with the gas in the interior 14 of the pressure vessel 10 .
- the gas permeability characteristics e.g., porosity and/or holes 34 , will have to be adapted accordingly.
- a second embodiment of a composite pressure vessel according to the present invention is described in greater detail below with reference to FIG. 6 .
- the pressure vessel 10 of this embodiment comprises a liner 12 which defines an interior 14 for the accommodation of a gaseous medium and a wrapping 16 encompassing the liner 12 .
- a high pressure in the interior 14 causes the diffusion of a small quantity of hydrogen through the liner 12 .
- the pressure vessel 10 of the embodiment shown in FIG. 6 is provided with a gas-permeable intermediate layer 36 between the liner 12 and the wrapping 16 .
- This intermediate layer 36 may be connected to the outside of the wrapping 16 , i.e., to the environment of the pressure vessel 10 , in the neck regions (right-and left-hand side in FIG. 6 ) of the pressure vessel 10 .
- the gaseous hydrogen which penetrates through the liner 12 can be discharged into the environment through the intermediate layer 36 continuously and at low rates.
- the potential risk to the surroundings of the pressure vessel 10 posed by the escaping gaseous hydrogen is noticeably reduced.
- the wrapping 16 itself may be gas-tight like in conventional pressure vessels and optionally provided with a coating 26 , for example a layer of paint.
- the intermediate layer 36 provided according to the invention is, for example, at least partially porous.
- a gas treatment device 38 is provided in the connecting regions between the intermediate layer 36 and the surroundings of the pressure vessel 10 , i.e., in the embodiment of FIG. 6 in the neck region of the pressure vessel 10 at the filling and/or discharge opening 22 .
- This gas treatment device 38 may, for example, be produced by impregnating the porous intermediate layer 36 with a suitable gas treatment medium.
- this gas treatment device 38 may comprise an oxidizing catalyst which oxidizes the hydrogen in the connecting regions described above into water.
- the water produced in this way is discharged as a liquid or vapor while hydrogen flows after it through the intermediate layer 36 . Any risk to the environment of the pressure vessel 10 posed by the discharge of hydrogen is completely avoided in this embodiment.
- the oxidative catalytically-acting part 38 of the porous intermediate layer 36 is restricted to the region where the intermediate layer 36 emerges into the environment of the pressure vessel 10 , where hydrogen would be discharged without the gas treatment device 38 .
- the catalytically-acting region 38 may for example be produced by impregnating the porous intermediate layer 36 with a liquid which contains the catalyst in a dissolved or suspended form. By means of a thermal after-treatment of this impregnated region 38 , the activity of the catalyst can be increased further. If the porous intermediate layer 36 has already been applied to the liner 12 , such a thermal after-treatment has obviously to be restricted to temperatures which will not damage the liner 12 .
- the oxidizing catalyst 38 is provided in the connecting region of the normal hydrogen outlet into the environment, there is sufficient access for the oxygen required for catalytic oxidation.
- a method for the application of the porous intermediate layer 36 to the liner 12 has to ensure that the free permeability of the porous intermediate layer 36 to hydrogen is maintained up to the catalytically-acting region 38 both in this process and during the subsequent application of the wrapping 16 , in order to ensure that the hydrogen penetrating through the liner 12 if fed to the gas treatment device 38 .
- the oxidising catalyst 38 at the free end of the porous intermediate layer 36 which may, for example, be produced by impregnation, in order to ensure an unimpeded discharge of the water produced in the catalyst 38 to the environment.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A pressure vessel for the storage of pressurized gaseous hydrogen includes a liner which defines an interior for the accommodation of the gaseous hydrogen and a wrapping encompassing the liner which gives the pressure vessel its dimensional stability. In order to prevent a discharge of gaseous hydrogen from the wrapping of the pressure vessel at a high rate if the pressure vessel is discharged after a prolonged downtime, the wrapping of the pressure vessel is designed to be at least partially gas-permeable, so that the gas penetrating through the liner can escape continuously through the wrapping of the pressure vessel.
Description
- The present application is a national stage of PCT International Application No. PCT/EP2009/007164, filed Oct. 6, 2009, and claims priority under 35 U.S.C. §119 to German Patent Application No. 10 2008 053 244.4, filed Oct. 25, 2008, the entire disclosures of which afore-mentioned documents are herein expressly incorporated by reference.
- The invention relates to a pressure vessel for the storage of pressurized gaseous media. In particular, it relates to a pressure vessel of this type, including a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner which gives the pressure vessel its dimensional stability.
- Such generic pressure vessels, which are also referred to as composite pressure vessels, are known from
EP 0 753 700 A1, for example. They comprise a liner defining an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability. The liner is usually made of a plastic material, while the wrapping is produced from a fibrous composite material. - Pressure vessels of this type are for example used as hydrogen reservoirs in fuel cell systems and can store gaseous hydrogen at several hundred bars of excess pressure.
- It has been observed that, in a discharge of such composite pressure vessels after a prolonged downtime, gaseous hydrogen escapes at a relatively high rate from the wrapping of the pressure vessel. There is therefore a demand for pressure vessels with a lower potential risk of hydrogen escape.
- DE 33 08 276 A1 discloses a multilayer pressure vessel for hot hydrogen, wherein hydrogen which penetrates through the innermost metal layer of the wall is vented from the space between the innermost metal layers in order to prevent a hydrogen attack and/or an embrittlement problem in the outer metal layers of the wall of the vessel.
- JP 2007-278482 A describes a composite pressure vessel with an inner tank and an outer tank. In order to protect the outer tank against attack by hydrogen penetrating through the inner tank and thereby to improve the durability of the pressure vessel, a continuous catalyst layer is provided between the inner and outer tanks, which converts the hydrogen into a stable compound.
- The present invention provides a solution to the problem of creating a composite pressure vessel of the type referred to above which excludes any risk to the environment posed by gases escaping at excessively high rates.
- This problem is solved by providing that an instantaneous escape of gaseous media at high rates during a discharge of the pressure vessel after a prolonged downtime is prevented by discharging gaseous media penetrating through the liner continuously and therefore at lower rates from the pressure vessel into the environment. The accumulation of gases penetrating through the liner in pockets between the liner and the wrapping and their instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel as a result of the separation between liner and wrapping are therefore avoided.
- According to a first aspect of the invention, a pressure vessel for the storage of pressurized gaseous media comprises a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability. According to the invention, the wrapping of the pressure vessel is designed to be at least partially gas-permeable, allowing the gas penetrating through the liner to escape from the pressure vessel through the wrapping.
- This structure of the pressure vessel with an at least partially gas-permeable wrapping has the result that the gas penetrating through the liner can be discharged continuously and at low rates from the pressure vessel into the environment. In this way, the accumulation of the gas penetrating through the liner between the liner and the wrapping, and its instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel, are prevented.
- In a variant of the invention, the wrapping of the pressure vessel is designed to be at least partially porous. The wrapping of the pressure vessel may, for example, be made of a fibrous material bound with a resin material, the resin material being at least partially porous in the set state.
- Alternatively or in addition, the wrapping of the pressure vessel is provided at predetermined points with holes which connect the interior of the wrapping to its outside.
- In a further development of the invention, the wrapping of the pressure vessel is provided on its outside with a coating (e.g., layer of paint) which is likewise designed to be gas-permeable at least in the gas-permeable regions of the wrapping.
- According to a second aspect of the invention, a pressure vessel for the storage of pressurized gaseous media comprises a liner which defines an interior for the accommodation of a gaseous medium and a wrapping encompassing the liner, which gives the pressure vessel its dimensional stability. According to the invention, a gas-permeable intermediate layer is provided between the liner and the wrapping, this being connected to the outside of the wrapping in at least one region, so that the gas penetrating through the liner can escape from the pressure vessel through the intermediate layer.
- This structure of the pressure vessel with an at least partially gas-permeable intermediate layer between the liner and the wrapping has the result that the gas penetrating through the liner can be discharged continuously and at low rates from the pressure vessel into the environment. In this way, the accumulation of the gas penetrating through the liner between the liner and the wrapping, and its instantaneous escape at high rates from the pressure vessel into the environment during a discharge of the pressure vessel, are prevented.
- In a variant of the invention, the intermediate layer is at least partially porous.
- In a further development of the invention, a gas treatment device which may, for example, be formed by impregnating the intermediate layer with a gas treatment medium is provided in the connecting region between the intermediate layer and the outside of the wrapping.
- The gas treatment device may for example comprise an oxidising catalyst. If the gaseous medium stored in the pressure vessel is hydrogen, the hydrogen flowing through the liner and through the intermediate layer is oxidized to water by the oxidizing catalyst and can be discharged without endangering the environment.
- In a further development of the invention, the connecting region between the intermediate layer and the outside of the wrapping is provided in the region of a neck of the pressure vessel. This may be the region of a filling and/or discharge opening of the pressure vessel.
- The above and further features and advantages of the present invention are understood more easily from a perusal of the following description of preferred embodiments with reference to the accompanying drawings.
-
FIG. 1 is a diagrammatic sectional view of a composite pressure vessel according to the present invention; -
FIG. 2 is an enlarged part-section of a conventional composite pressure vessel before its discharge; -
FIG. 3 is an enlarged part-section of a conventional composite pressure vessel after its discharge; -
FIG. 4 is an enlarged part-section of a composite pressure vessel according to a first embodiment of the invention before its discharge; -
FIG. 5 is an enlarged part-section of a composite pressure vessel according to a first embodiment of the invention after its discharge; and -
FIG. 6 is a diagrammatic sectional view of a composite pressure vessel according to a second embodiment of the present invention. - The present invention is described below with reference to a pressure vessel for the storage of gaseous hydrogen at a pressure of, e.g., 700 bar, which may be used, for example, in fuel cell systems. The invention is, however, in no way restricted to this particular gaseous medium, this particular excess pressure in the interior of the pressure vessel and this particular application.
- With reference to
FIG. 1 , the basic structure of a composite pressure vessel to which the present invention can be applied is described in greater detail below. - The
composite pressure vessel 10 is formed from aliner 12 which defines aninterior 14 for the accommodation of gaseous hydrogen. A plastic material may for example be used for the production of theliner 12. Theliner 12 is surrounded by a wrapping 16 which may, for example, be made of a fibrous composite material such as resin-impregnated carbon fibers and which gives thepressure vessel 10 the necessary dimensional stability. The materials for the production of theliner 12 and thewrapping 16 are, however, not restricted to those mentioned above. In the same way, the invention is not restricted to a specific form of the wrapping 16 (e.g., axial and/or tangential and/or angled winding direction of the fibers) and to a specific thickness of theliner 12 and the wrapping 16. As the basic structure of the pressure vessel is known to the expert from prior art, the design of an embodiment fulfilling specific requirements (e.g., type of gas, pressure, application, etc.) will not pose any problems for him or her. - In the embodiment of
FIG. 1 , thepressure vessel 10 has two neck regions (on top and at the bottom inFIG. 1 ), each of which is provided with an opening 22 sealed by a 18 and 20, respectively. In the opening 22 which is not sealed by a neck piece (on top in the figure), aneck piece valve 24 may be provided. The present invention is not restricted to a specific design of the 18, 20. In addition, the two neck regions of theneck pieces pressure vessel 10 may be provided with pole caps for the additional stabilization of thepressure vessel 10. Thepressure vessel 10 may optionally be provided with twoopenings 22 fitted withvalves 24. The shape of thepressure vessel 10 is moreover not restricted to that with two neck regions as shown inFIG. 1 . - A
coating 26, for example, a layer of paint, is further applied to the outside of the wrapping 16. - The problems of hydrogen escape from a conventional pressure vessel are explained below with reference to
FIGS. 2 and 3 . - In the
interior 14 of thepressure vessel 10, gaseous hydrogen may, for example, be stored at a pressure of approximately 700 bar. In the course of time, a certain amount of this hydrogen is diffused through the liner 12 (seearrow 28 inFIG. 2 ). This gaseous hydrogen which has penetrated through theliner 12 largely accumulates inpockets 30 between theliner 12 and the wrapping 16. A small proportion of this hydrogen may reach the environment through pores or holes 32 in the wrapping 16. A free access of this accumulated hydrogen to the fewsmall holes 32 in the wrapping is greatly impeded by a macroscopically flush contact between the wrapping 16 and theliner 12 at high pressure in theinterior 14 of theliner 12. - After a prolonged downtime of the
pressure vessel 10, the hydrogen in thepockets 30 between theliner 12 and the wrapping 16 causes a build-up of pressure which may in extreme cases result in a deformation of theliner 12. - If the
pressure vessel 10 is then discharged after a prolonged downtime, or if a defined quantity of hydrogen is taken from the interior 14, so that the pressure in the interior 14 is reduced significantly, an excess pressure is created by the hydrogen accumulated in thepockets 30 between theliner 12 and the wrapping 16. As illustrated inFIG. 3 , this excess pressure separates theliner 12 from the inside of the wrapping 16 and may also cause a deformation of theliner 12. This separation (see double-headed arrow inFIG. 3 ) creates a flow path for the gaseous hydrogen from thepockets 30 to the pores/holes 32 and thus to the outside of the wrapping 16, allowing hydrogen which has penetrated through theliner 12 to escape from thepressure vessel 10. - If the
pressure vessel 10 is then discharged after a prolonged downtime, the hydrogen diffused through the liner instantaneously flows from thepressure vessel 10 at a comparatively high rate. - In order to prevent a risk to the environment posed by the hydrogen escaping from the
pressure vessel 10 at a high rate, the present invention proposes that the pressure build-up between theliner 12 and the wrapping 16 after a prolonged downtime of thepressure vessel 10, which has been described above, should be avoided. For this purpose various measures are taken within the scope of the present invention. - A first embodiment of a pressure vessel according to the invention is explained below with reference to
FIGS. 4 and 5 . - Like the conventional pressure vessel, the
pressure vessel 10 of this embodiment comprises aliner 12 which defines an interior 14 for the accommodation of a gaseous medium and a wrapping 16 encompassing theliner 12. In this design of thepressure vessel 10, during prolonged downtimes a high pressure in the interior 14 likewise causes the diffusion of a small quantity of hydrogen through the liner 12 (seearrows 28 inFIG. 4 ), the hydrogen initially accumulating inpockets 30 between theliner 12 and the wrapping 16. - In contrast to the conventional composite pressure vessels described above, however, the wrapping of the
pressure vessel 10 of this embodiment is designed to be at least partially gas-permeable. For this purpose, the wrapping 16 may for example be porous. Alternatively or in addition, the wrapping 16 is provided at predetermined points withholes 34 which connect the interior of the wrapping 16 to its outside. In this way, the gaseous hydrogen penetrating through theliner 12 can be discharged continuously and at low rates through the wrapping 16 to the outside. Compared to the instantaneous release of the hydrogen at a high rate, the potential risk to the surroundings of thepressure vessel 10 posed by the escaping gaseous hydrogen is noticeably reduced. - Even if the
liner 12 in this case separates slightly from the wrapping 16 as thepressure vessel 10 is discharged, creating flow paths betweenindividual pockets 30 as shown inFIG. 5 , large quantities of hydrogen are no longer released in this state, because the hydrogen has already been discharged evenly through the wrapping 16 over a long period of time and has not been able to build up any significant pressure between theliner 12 and the wrapping 16. - The wrapping 16 is designed to be gas-permeable at least in certain regions. In exemplary embodiments of the invention, however, the wrapping is designed to be gas-permeable substantially across all of its regions.
- If, as
FIG. 1 shows, the wrapping 16 is coated with a layer ofpaint 26 or the like, this layer ofpaint 26 will have to be gas-permeable as well in this embodiment. This applies at least to the regions in which the wrapping 16 is designed to be gas-permeable. - The
porous wrapping 16 may for example be structured as follows. The wrapping 16 essentially consists of a fibrous composite material which may for example be made up from carbon fibers which give the wrapping its inherent compressive strength and of a resin for binding the carbon fibers. This resin has to be at least partially porous. The strength and stability under pressure of the wrapping 16 as a whole will nevertheless have to be ensured. The resin used for binding does not make any significant contribution to the stability of thepressure vessel 10 under pressure; the deciding factor is the carbon fiber bond. - To produce the
porous wrapping 16, a resin may be used which, owing to high inner stresses, forms a sufficient number of micro-cracks in the setting process. These micro-cracks must, however, not result in a complete disintegration of the wrapping 16. In addition, the micro-cracks have to form a continuous connection through theentire wrapping 16, as they are required for the removal of the hydrogen into the environment. - The same conditions apply to any outer layer of
paint 26 which may be provided. This can also be produced using the method described above and has to meet the same conditions with respect to hydrogen removal. - The provision of tailor-made
holes 34 in sufficient numbers at points previously determined does not require any detailed explanation. In principle, any suitable methods may be used. - The gas-permeability of the wrapping 16 obviously varies with the gas in the
interior 14 of thepressure vessel 10. Depending on the type of gaseous medium stored in thepressure vessel 10, the gas permeability characteristics, e.g., porosity and/or holes 34, will have to be adapted accordingly. - A second embodiment of a composite pressure vessel according to the present invention is described in greater detail below with reference to
FIG. 6 . - Like the conventional pressure vessel, the
pressure vessel 10 of this embodiment comprises aliner 12 which defines an interior 14 for the accommodation of a gaseous medium and a wrapping 16 encompassing theliner 12. In this design of thepressure vessel 10 as well, during prolonged downtimes a high pressure in the interior 14 causes the diffusion of a small quantity of hydrogen through theliner 12. - In contrast to the conventional composite pressure vessels described above, the
pressure vessel 10 of the embodiment shown inFIG. 6 is provided with a gas-permeableintermediate layer 36 between theliner 12 and the wrapping 16. Thisintermediate layer 36 may be connected to the outside of the wrapping 16, i.e., to the environment of thepressure vessel 10, in the neck regions (right-and left-hand side inFIG. 6 ) of thepressure vessel 10. In this way, the gaseous hydrogen which penetrates through theliner 12 can be discharged into the environment through theintermediate layer 36 continuously and at low rates. Compared to the instantaneous release of the hydrogen at a high rate, the potential risk to the surroundings of thepressure vessel 10 posed by the escaping gaseous hydrogen is noticeably reduced. - The wrapping 16 itself may be gas-tight like in conventional pressure vessels and optionally provided with a
coating 26, for example a layer of paint. Theintermediate layer 36 provided according to the invention is, for example, at least partially porous. - In addition, a
gas treatment device 38 is provided in the connecting regions between theintermediate layer 36 and the surroundings of thepressure vessel 10, i.e., in the embodiment ofFIG. 6 in the neck region of thepressure vessel 10 at the filling and/or dischargeopening 22. Thisgas treatment device 38 may, for example, be produced by impregnating the porousintermediate layer 36 with a suitable gas treatment medium. - If gaseous hydrogen is to be stored in the
interior 14 of thepressure vessel 10, thisgas treatment device 38 may comprise an oxidizing catalyst which oxidizes the hydrogen in the connecting regions described above into water. The water produced in this way is discharged as a liquid or vapor while hydrogen flows after it through theintermediate layer 36. Any risk to the environment of thepressure vessel 10 posed by the discharge of hydrogen is completely avoided in this embodiment. - The oxidative catalytically-acting
part 38 of the porousintermediate layer 36 is restricted to the region where theintermediate layer 36 emerges into the environment of thepressure vessel 10, where hydrogen would be discharged without thegas treatment device 38. The catalytically-actingregion 38 may for example be produced by impregnating the porousintermediate layer 36 with a liquid which contains the catalyst in a dissolved or suspended form. By means of a thermal after-treatment of this impregnatedregion 38, the activity of the catalyst can be increased further. If the porousintermediate layer 36 has already been applied to theliner 12, such a thermal after-treatment has obviously to be restricted to temperatures which will not damage theliner 12. - As the oxidizing
catalyst 38 is provided in the connecting region of the normal hydrogen outlet into the environment, there is sufficient access for the oxygen required for catalytic oxidation. - As the hydrogen penetrating through the
liner 12 is discharged continuously, excess pressure does not develop between theliner 12 and the wrapping 16 while the pressure vessel is discharged and pressure is reduced in theinterior 14 of the liner, so that an uneven deformation of theliner 12 is avoided. - In this context, a method for the application of the porous
intermediate layer 36 to theliner 12 has to ensure that the free permeability of the porousintermediate layer 36 to hydrogen is maintained up to the catalytically-actingregion 38 both in this process and during the subsequent application of the wrapping 16, in order to ensure that the hydrogen penetrating through theliner 12 if fed to thegas treatment device 38. - The same applies to the oxidising
catalyst 38 at the free end of the porousintermediate layer 36, which may, for example, be produced by impregnation, in order to ensure an unimpeded discharge of the water produced in thecatalyst 38 to the environment. - The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
Claims (20)
1. A pressure vessel for storing pressurised gaseous media, comprising:
a liner that defines an interior for accommodation of a gaseous medium; and
a wrapping encompassing the liner that gives the pressure vessel dimensional stability,
wherein the wrapping of the pressure vessel is at least partially gas-permeable, so that the gaseous medium penetrates through the liner and escapes from the pressure vessel through the wrapping.
2. The pressure vessel according to claim 1 , wherein the wrapping of the pressure vessel is at least partially porous and/or provided with holes (34) which connect the inside of the wrapping to its outside.
3. The pressure vessel according to claim 1 , wherein the wrapping of the pressure vessel is made of a fibrous material bound with a resin material, the resin material being at least partially porous in the set state.
4. The pressure vessel according to claim 1 , wherein the wrapping of the pressure vessel is provided with a coating on its outside, which is gas-permeable at least in the gas-permeable regions of the wrapping.
5. A pressure vessel for storing pressurised gaseous media, comprising:
a liner that defines an interior for accommodation of a gaseous medium; and
a wrapping encompassing the liner that gives the pressure vessel dimensional stability,
wherein a gas-permeable intermediate layer is connected to the outside of the wrapping in at least one region and is provided between the liner and the wrapping, so that the gaseous medium penetrates through the liner and escapes from the pressure vessel through the intermediate layer.
6. The pressure vessel according to claim 5 , wherein the intermediate layer is at least partially porous.
7. The pressure vessel according to claim 5 , wherein a gas treatment device is provided in a connecting region between the intermediate layer and the outside of the wrapping.
8. The pressure vessel according to claim 7 , wherein the gas treatment device comprises an oxidising catalyst.
9. The pressure vessel according to claim 7 , wherein the gas treatment device is produced by impregnating the intermediate layer with a gas treatment medium.
10. The pressure vessel according to claim 7 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a neck of the pressure vessel.
11. The pressure vessel according to claim 7 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a filling and/or discharge opening of the pressure vessel.
12. The pressure vessel according to claim 2 , wherein the wrapping of the pressure vessel is provided with a coating on its outside, which is gas-permeable at least in the gas-permeable regions of the wrapping.
13. The pressure vessel according to claim 3 , wherein the wrapping of the pressure vessel is provided with a coating on its outside, which is gas-permeable at least in the gas-permeable regions of the wrapping.
14. The pressure vessel according to claim 6 , wherein a gas treatment device is provided in a connecting region between the intermediate layer and the outside of the wrapping.
15. The pressure vessel according to claim 8 , wherein the gas treatment device is produced by impregnating the intermediate layer with a gas treatment medium.
16. The pressure vessel according to claim 8 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a neck of the pressure vessel.
17. The pressure vessel according to claim 9 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a neck of the pressure vessel.
18. The pressure vessel according to claim 8 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a filling and/or discharge opening of the pressure vessel.
19. The pressure vessel according to claim 9 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a filling and/or discharge opening of the pressure vessel.
20. The pressure vessel according to claim 10 , wherein the connecting region between the intermediate layer and the outside of the wrapping is provided in a region of a filling and/or discharge opening of the pressure vessel.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102008053244A DE102008053244A1 (en) | 2008-10-25 | 2008-10-25 | Pressure vessel for storing gaseous media under pressure |
| DE102008053244.4 | 2008-10-25 | ||
| PCT/EP2009/007164 WO2010046027A1 (en) | 2008-10-25 | 2009-10-06 | Pressure vessel for storing gaseous media under pressure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20120018314A1 true US20120018314A1 (en) | 2012-01-26 |
Family
ID=41528746
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/125,773 Abandoned US20120018314A1 (en) | 2008-10-25 | 2009-10-06 | Pressure Vessel for Storing Gaseous Media Under Pressure |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20120018314A1 (en) |
| JP (2) | JP5661636B2 (en) |
| DE (1) | DE102008053244A1 (en) |
| WO (1) | WO2010046027A1 (en) |
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| EP2910840A2 (en) | 2014-02-12 | 2015-08-26 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | Composite container and method for manufacturing same |
| CN109844398A (en) * | 2016-10-25 | 2019-06-04 | 宝马股份公司 | The pressure vessel of outlet with the fuel for accumulating between liner and fiber-reinforced layer |
| JP2019157864A (en) * | 2018-03-07 | 2019-09-19 | 本田技研工業株式会社 | High pressure tank device and its control method |
| US11117226B2 (en) | 2016-03-16 | 2021-09-14 | Hexagon Technology As | Vented fitting for pressure vessel boss |
| US11255483B2 (en) | 2017-12-25 | 2022-02-22 | Toyota Jidosha Kabushiki Kaisha | High pressure tank and method of manufacturing high pressure tank |
| US20230160535A1 (en) * | 2021-11-25 | 2023-05-25 | Airbus Sas | Hydrogen tank provided with a gaseous hydrogen capture system |
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| FR2956185B1 (en) * | 2010-02-11 | 2012-05-04 | Air Liquide | COMPOSITE TANK AND ASSEMBLY COMPRISING SUCH A RESERVOIR AND A GAS RECEIVER AND / OR DISPENSER ORGAN |
| DE102010033599A1 (en) * | 2010-08-06 | 2012-02-09 | Daimler Ag | Device for storing low molecular weight gases |
| DE102011108597B4 (en) | 2011-07-26 | 2013-09-12 | Daimler Ag | Device for storing low molecular weight gases |
| FR2995656B1 (en) * | 2012-09-17 | 2014-10-03 | Centre Nat Etd Spatiales | METHOD FOR SEALING A RESERVOIR OF COMPOSITE MATERIAL |
| FR3015629B1 (en) * | 2013-12-20 | 2016-01-29 | Eads Composites Aquitaine | RESERVOIR FOR STORING LIQUID OR GASEOUS MEDIA UNDER PRESSURE |
| JP6287872B2 (en) * | 2015-01-29 | 2018-03-07 | トヨタ自動車株式会社 | tank |
| DE102016208005B3 (en) * | 2016-05-10 | 2017-05-24 | Bayerische Motoren Werke Aktiengesellschaft | Pressure vessel with outgassing channels and manufacturing process |
| DE102017206338A1 (en) | 2017-04-12 | 2018-10-18 | Bayerische Motoren Werke Aktiengesellschaft | Method for pressure relief of a pressure vessel and pressure vessel |
| JP6741708B2 (en) * | 2018-03-07 | 2020-08-19 | 本田技研工業株式会社 | High pressure tank equipment |
| FR3087245B1 (en) * | 2018-10-11 | 2021-12-31 | Stelia Aerospace Composites | ANTI-COLLAPSE DEVICE FOR PRESSURIZED GAS STORAGE TANK |
| JP2020118288A (en) * | 2019-01-28 | 2020-08-06 | トヨタ自動車株式会社 | Hydrogen tank |
| EP3990819B1 (en) * | 2019-06-28 | 2024-03-13 | Linamar Corporation | Liner collapse mitigations for type iv conformable pressure vessels |
| DE102023128676A1 (en) * | 2023-10-19 | 2025-04-24 | Bayerische Motoren Werke Aktiengesellschaft | High-pressure container for storing hydrogen, vehicle with high-pressure container and method for producing a high-pressure container |
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| US3585052A (en) * | 1968-10-15 | 1971-06-15 | Jacob F Dannewald | Heat resistant paint |
| US4690295A (en) * | 1983-11-09 | 1987-09-01 | The British Petroleum Company P.L.C. | Pressure container with thermoplastic fusible plug |
| US20090236349A1 (en) * | 2006-09-16 | 2009-09-24 | Xperion Gmbh | Pressure vessel |
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| US11117226B2 (en) | 2016-03-16 | 2021-09-14 | Hexagon Technology As | Vented fitting for pressure vessel boss |
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| CN109844398B (en) * | 2016-10-25 | 2021-12-07 | 宝马股份公司 | Pressure vessel with a discharge opening for fuel accumulating between the inner liner and the fiber-reinforced layer |
| US11255483B2 (en) | 2017-12-25 | 2022-02-22 | Toyota Jidosha Kabushiki Kaisha | High pressure tank and method of manufacturing high pressure tank |
| JP2019157864A (en) * | 2018-03-07 | 2019-09-19 | 本田技研工業株式会社 | High pressure tank device and its control method |
| US20230160535A1 (en) * | 2021-11-25 | 2023-05-25 | Airbus Sas | Hydrogen tank provided with a gaseous hydrogen capture system |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2012506519A (en) | 2012-03-15 |
| JP2013238319A (en) | 2013-11-28 |
| JP5661636B2 (en) | 2015-01-28 |
| WO2010046027A1 (en) | 2010-04-29 |
| DE102008053244A1 (en) | 2010-04-29 |
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