EP1584859A2 - Druckbehälter zur Speicherung von kryogenen Kraftstoffen - Google Patents
Druckbehälter zur Speicherung von kryogenen Kraftstoffen Download PDFInfo
- Publication number
- EP1584859A2 EP1584859A2 EP05102649A EP05102649A EP1584859A2 EP 1584859 A2 EP1584859 A2 EP 1584859A2 EP 05102649 A EP05102649 A EP 05102649A EP 05102649 A EP05102649 A EP 05102649A EP 1584859 A2 EP1584859 A2 EP 1584859A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure vessel
- shell
- inner pressure
- outer container
- concave
- 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.)
- Withdrawn
Links
Images
Classifications
-
- 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
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
-
- 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
- F17C2201/0147—Shape complex
-
- 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
- F17C2201/0147—Shape complex
- F17C2201/0152—Lobes
-
- 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
- F17C2201/054—Size medium (>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
- 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
- F17C2203/01—Reinforcing or suspension means
- F17C2203/011—Reinforcing means
- F17C2203/012—Reinforcing means on or in the wall, e.g. ribs
-
- 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
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
- F17C2203/016—Cords
-
- 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
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
-
- 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
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/228—Assembling processes by screws, bolts or rivets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/23—Manufacturing of particular parts or at special locations
- F17C2209/232—Manufacturing of particular parts or at special locations of walls
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/013—Reducing manufacturing time or effort
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
Definitions
- the invention relates to a pressure vessel for storing cryogenic Fuel in a motor vehicle, according to the preamble of the first claim.
- pressure vessel from cylinder, conical or frusto-conical container parts It is also known for storing cryogenic fuels double-walled, to use vacuum insulated containers.
- This is the pressure vessel of surrounded by an outer container shell and the space between the pressure vessel and the outer container shell is substantially evacuated and / or provided with a material for thermal insulation.
- the outer surface of the outer container shell is parallel to Outer surface of the pressure vessel by a so-called offset around the required isolation gap generated. It can also be sections different distances between the outer surface of the outer Container shell and the outer surface of the pressure vessel to be selected for example, to accommodate pipelines and valves.
- Pipe and / or profile connectors in application by means of feedthroughs are guided through the pressure vessel and this in the outer container shell to record a double-walled vacuum-insulated container.
- the object of the invention is to fix the inner pressure vessel in to provide its outer container shell whose structure it allows, without the mentioned disadvantages, storage of gaseous or cryogenic fuels for motor vehicles better in the vehicle package too integrate.
- the invention relates to a double-walled pressure vessel for storage of cryogenic fuel in a motor vehicle whose inner pressure vessel jacket from the first container parts and the outer container jacket is composed of second container parts, each at least in one to the central longitudinal axis parallel or inclined plane so cut off and connected to each other at the interfaces, that the inner pressure vessel shell at least between the first Container parts has at least one concave curvature. Furthermore has the outer container shell surrounding the inner pressure vessel shell inward-facing support devices, each of which one in a concave curvature of the inner pressure vessel shell into it extends.
- the invention is characterized in that the concave A concavity of the inner pressure vessel shell each of at least a tension band is spanned and that the support means of the outer container shell abut the respective drawstring.
- the gap between the pressure vessel shell and the outer container shell in essentially evacuated and / or with a material for thermal insulation provided to keep evaporation losses as low as possible.
- the concave Curvature of the pressure vessel shell surrounding Through this geometric Construction can in the container walls a membrane voltage state be achieved. Due to the load-oriented design can advantageously small wall thicknesses can be used. If then the Supporting the outer container shell also by the concave indentations are formed and if this is also circumferential, a simple, inexpensive pressure vessel construction is achieved by that the drawstrings around the pressure vessel jacket formed circumferentially are.
- FIG. 1 shows in a three-dimensional view a pressure vessel according to the invention.
- this pressure vessel is shown in longitudinal and cross-section.
- the shape of a pressure vessel for storage of cryogenic fuel, for example hydrogen, in a motor vehicle be generated by its inner 1 and outer Druckbe mboermantel 11 from container parts 5, 6, and 7, 8 is composed, at least in a plane parallel or inclined to its central longitudinal axis 2 cut off and connected to each other at the interfaces. And although so that both the inner 1, and the outer pressure vessel shell 11 between their respective container parts 5, 6, and 7, 8 a have concave concavity.
- the inner pressure vessel shell 1 composed of container parts 5, 6, which in one of their central longitudinal axis parallel plane 2 cut off and at the interfaces connected to each other. This creates the pressure vessel from at least two partially penetrating bodies, made up of circular Build up cross sections. At the interface of the two container parts 5, 6 is the inner pressure vessel shell 1 thus concave curved concave.
- the gap 10 ( Figures 2, 3) between the inner pressure vessel shell 1 and the outer container shell 11 is evacuated.
- the distance between inner Pressure vessel shell 1 and outer container shell 11 is selected so that the circumferential concave curvature of the outer container shell 11 at the interface of the two container parts 7, 8 in the circumferential concave Concave of the inner pressure vessel shell 1 at least as far protrudes into an imaginary, the concavity of the inner pressure vessel shell 1 bridging tangent to the container parts 5, 6 of the concave concavity of the outer container shell 11 is touched.
- FIGS. 2 and 3 the same terms and the same parts are used for the same parts Reference numeral used.
- FIG. 2 shows the inner pressure vessel jacket 1 in the outer container jacket 11, fixed by the longitudinal direction of the inner pressure vessel shell. 1 circumferential, tensioned drawstring 12. The encircling concave indentation the outer container shell 11 is supported on the drawstring 12, which in the evacuated gap 10 between the inner pressure vessel shell. 1 and the outer container shell 11 extends. From the outside is on the outer container shell 11, a its circumferential curvature filling Stiffening profile 15 applied.
- FIG. 3 shows the inner pressure vessel jacket 1 in the outer container jacket 11, fixed by the transversely around the inner pressure vessel shell. 1 circumferential, tensioned drawstring 13. The encircling concave indentation the outer container casing 11 is supported on the drawstring 13, which in the evacuated gap 10 between the inner pressure vessel shell. 1 and the outer container shell 11 extends. From the outside is on the outer container shell 11, a its circumferential curvature filling Stiffening profile 15 applied.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Description
Claims (6)
- Doppelwandiger Druckbehälter, zur Speicherung von kryogenem Kraftstoff in einem Kraftfahrzeug, dessen innerer Druckbehältermantel (1) aus ersten Behälterteilen (5, 6) und dessen äußerer Behältermantel (11) aus zweiten Behälterteilen (7, 8) zusammengesetzt ist, die jeweils mindestens in einer zu deren Mittellängsachse parallelen oder schiefen Ebene (2) so abgeschnitten und an den Schnittstellen so miteinander verbunden sind, dass der innere Druckbehältermantel (1) mindestens zwischen den ersten Behälterteilen (5, 6) mindestens eine konkave Einwölbung besitzt, wobei der den inneren Druckbehältermantel (1) umgebende äußere Behältermantel (11) nach innen gerichtete Abstützeinrichtungen besitzt, von denen sich jeweils eine in eine konkave Einwölbung des inneren Druckbehältermantels (1) hinein erstreckt, dadurch gekennzeichnet, dass die konkave Einwölbung des inneren Druckbehältermantels (1) jeweils von mindestens einem Zugband (12, 13, 14) überspannt ist und dass die Abstützeinrichtungen des äußeren Behältermantels (11) an dem jeweiligen Zugband (12, 13, 14) anliegen.
- Druckbehälter nach Anspruch 1, dadurch gekennzeichnet, dass der Zwischenraum (10) zwischen dem inneren Druckbehältermantel (1) und dem äußeren Behältermantel (11) im wesentlichen evakuiert und/oder mit einem Material zur Wärmeisolierung versehen ist.
- Druckbehälter nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die konkave Einwölbung des inneren Druckbehältermantels (1) umlaufend ist.
- Druckbehälter nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass die Abstützeinrichtungen des äußeren Behältermantels (11) ebenfalls durch dessen konkave Einwölbung gebildet sind.
- Druckbehälter nach Anspruch 4, dadurch gekennzeichnet, dass die konkave Einwölbung des äußeren Behältermantels (11) umlaufend ist.
- Druckbehälter nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass die Zugbänder (12, 13, 14) um den inneren Druckbehältermantel (1) umlaufend ausgebildet sind.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102004017392 | 2004-04-08 | ||
| DE200410017392 DE102004017392A1 (de) | 2004-04-08 | 2004-04-08 | Druckbehälter zur Speicherung von kryogenen Kraftstoffen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1584859A2 true EP1584859A2 (de) | 2005-10-12 |
| EP1584859A3 EP1584859A3 (de) | 2011-04-27 |
Family
ID=34895529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP05102649A Withdrawn EP1584859A3 (de) | 2004-04-08 | 2005-04-04 | Druckbehälter zur Speicherung von kryogenen Kraftstoffen |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP1584859A3 (de) |
| DE (1) | DE102004017392A1 (de) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2919912A1 (fr) * | 2007-08-06 | 2009-02-13 | Air Liquide | Reservoir de fluide cryogenique et vehicule comprenant un tel reservoir |
| CN102954214A (zh) * | 2011-08-24 | 2013-03-06 | 株式会社神户制钢所 | 压力容器 |
| US8960482B2 (en) | 2008-09-23 | 2015-02-24 | Aerovironment Inc. | Cryogenic liquid tank |
| DE102008004698B4 (de) * | 2007-01-19 | 2016-10-20 | GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) | Konisch geformter Brennstoffspeichertank |
| WO2021055319A1 (en) * | 2019-09-16 | 2021-03-25 | Third Shore Group, LLC | Thermal management in conformable tanks |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2339554A (en) * | 1941-12-02 | 1944-01-18 | Firestone Tire & Rubber Co | Container |
| GB2040430B (en) * | 1979-01-11 | 1983-02-02 | Ocean Phoenix Holdings Nv | Tanks for storing liquefied gases |
| DE3026116C2 (de) * | 1980-07-10 | 1985-01-31 | Aeg Isolier- Und Kunststoff Gmbh, 3500 Kassel | Druckbehälter |
| GB2111663B (en) * | 1981-12-16 | 1986-03-26 | Ocean Phoenix Holdings Nv | Tank for the storage and transport of pressurised fluid |
| DE3206430A1 (de) * | 1982-02-23 | 1983-09-08 | Daimler-Benz Ag, 7000 Stuttgart | Hochdruckbehaelter |
| DE4300484C1 (de) * | 1993-01-11 | 1994-01-05 | Silit Werke | Druckbehälter |
| DE10217246A1 (de) * | 2002-04-15 | 2003-11-06 | Deutsch Zentr Luft & Raumfahrt | Drucktank |
-
2004
- 2004-04-08 DE DE200410017392 patent/DE102004017392A1/de not_active Withdrawn
-
2005
- 2005-04-04 EP EP05102649A patent/EP1584859A3/de not_active Withdrawn
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008004698B4 (de) * | 2007-01-19 | 2016-10-20 | GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) | Konisch geformter Brennstoffspeichertank |
| FR2919912A1 (fr) * | 2007-08-06 | 2009-02-13 | Air Liquide | Reservoir de fluide cryogenique et vehicule comprenant un tel reservoir |
| WO2009019375A3 (fr) * | 2007-08-06 | 2009-04-09 | Air Liquide | Réservoir de fluide cryogénique et véhicule comprenant un tel réservoir |
| US8960482B2 (en) | 2008-09-23 | 2015-02-24 | Aerovironment Inc. | Cryogenic liquid tank |
| US9829155B2 (en) | 2008-09-23 | 2017-11-28 | Aerovironment, Inc. | Cryogenic liquid tank |
| US10584828B2 (en) | 2008-09-23 | 2020-03-10 | Aerovironment, Inc. | Cryogenic liquid tank |
| US11346501B2 (en) | 2008-09-23 | 2022-05-31 | Aerovironment, Inc. | Cryogenic liquid tank |
| CN102954214A (zh) * | 2011-08-24 | 2013-03-06 | 株式会社神户制钢所 | 压力容器 |
| CN102954214B (zh) * | 2011-08-24 | 2015-02-11 | 株式会社神户制钢所 | 压力容器 |
| WO2021055319A1 (en) * | 2019-09-16 | 2021-03-25 | Third Shore Group, LLC | Thermal management in conformable tanks |
| US12259090B2 (en) | 2019-09-16 | 2025-03-25 | Noble Gas Systems, Inc. | Thermal management in conformable tanks |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1584859A3 (de) | 2011-04-27 |
| DE102004017392A1 (de) | 2005-10-27 |
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