DE102004017392A1 - Pressure vessel for storing cryogenic fuels - Google Patents
Pressure vessel for storing cryogenic fuels Download PDFInfo
- Publication number
- DE102004017392A1 DE102004017392A1 DE200410017392 DE102004017392A DE102004017392A1 DE 102004017392 A1 DE102004017392 A1 DE 102004017392A1 DE 200410017392 DE200410017392 DE 200410017392 DE 102004017392 A DE102004017392 A DE 102004017392A DE 102004017392 A1 DE102004017392 A1 DE 102004017392A1
- Authority
- DE
- Germany
- 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- Withdrawn
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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
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
Die Erfindung betrifft einen doppelwandigen Druckbehälter zur Speicherung von kryogenem Kraftstoff in einem Kraftfahrzeug, dessen innerer Druckbehältermantel aus ersten Behälterteilen und dessen äußerer Behältermantel aus zweiten Behälterteilen zusammengesetzt ist, die jeweils mindestens in einer zu deren Mittellängsachse parallelen oder schiefen Ebene so abgeschnitten und an den Schnittstellen so miteinander verbunden sind, dass der innere Druckbehältermantel mindestens zwischen den ersten Behälterteilen mindestens eine konkave Einwölbung besitzt. Des Weiteren besitzt der den inneren Druckbehältermantel umgebende äußere Behältermantel nach innen gerichtete Abstützeinrichtungen, von denen sich jeweils eine in eine konkave Einwölbung des inneren Druckbehältermantels hineinerstreckt. Die Erfindung ist dadurch gekennzeichnet, dass die konkave Einwölbung des inneren Druckbehältermantels jeweils von mindestens einem Zugband überspannt ist und dass die Abstützeinrichtungen des äußeren Behältermantels an dem jeweiligen Zugband anliegen.The invention relates to a double-walled pressure vessel for storing cryogenic fuel in a motor vehicle, the inner pressure vessel shell of first container parts and the outer container shell is composed of second container parts, respectively cut off at least in a plane parallel to the central longitudinal axis or oblique plane and at the interfaces so connected to each other, that the inner pressure vessel shell has at least one concave curvature at least between the first container parts. Furthermore, the outer container jacket surrounding the inner pressure vessel jacket has inwardly directed support devices, one of which extends into a concave concavity of the inner pressure vessel jacket. The invention is characterized in that the concave concavity of the inner pressure vessel shell is spanned by at least one tension band and that the support means of the outer container shell abut the respective tension band.
Description
Die Erfindung betrifft einen Druckbehälter zur Speicherung von kryogenem Kraftstoff in einem Kraftfahrzeug, nach dem Oberbegriff des ersten Anspruchs.The The invention relates to a pressure vessel for storing cryogenic Fuel in a motor vehicle, after the generic term of the first Claim.
Aus
Bei einer Verwendung von solchen Rohr- und/oder Profilverbindern als Druckabstützungen, zur Fixierung des Druckbehälters im äußeren Behältermantel, wird das Nutzvolumen eingeschränkt, die Wärmeisolation beeinträchtigt und es sind mehr gasdichte Schweißnähte erforderlich.at a use of such pipe and / or profile connectors as Pressure supports, to Fixation of the pressure vessel in the outer container shell, is the useful volume restricted, the heat insulation impaired and more gas-tight welds are required.
Aufgabe der Erfindung ist es, eine Fixierung des inneren Druckbehälters in dessen äußerem Behältermantel bereitzustellen, deren Aufbau es ermöglicht, ohne die genannten Nachteile Speicher von gasförmigen oder kryogenen Kraftstoffen für Kraftfahrzeuge besser im Fahrzeugpackage zu integrieren.task The invention is a fixation of the inner pressure vessel in its outer container shell whose construction makes it possible without the said Disadvantages storage of gaseous or cryogenic fuels for To integrate motor vehicles better in the vehicle package.
Die Aufgabe wird mit den kennzeichnenden Merkmalen des Anspruchs 1 gelöst. Bevorzugte Ausführungsformen der Erfindung beschreiben die abhängigen Ansprüche.The The object is achieved with the characterizing features of claim 1. preferred embodiments of the invention describe the dependent claims.
Die Erfindung betrifft einen doppelwandigen Druckbehälter, zur Speicherung von kryogenem Kraftstoff in einem Kraftfahrzeug, dessen innerer Druckbehältermantel aus ersten Behälterteilen und dessen äußerer Behältermantel aus zweiten Behälterteilen zusammengesetzt ist, die jeweils mindestens in einer zu deren Mittellängsachse parallelen oder schiefen Ebene so abgeschnitten und an den Schnittstellen so miteinander verbunden sind, dass der innere Druckbehältermantel mindestens zwischen den ersten Behälterteilen mindestens eine konkave Einwölbung besitzt. Des weiteren besitzt der den inneren Druckbehältermantel umgebende äußere Behältermantel nach innen gerichtete Abstützeinrichtungen, von denen sich jeweils eine in eine konkave Einwölbung des inneren Druckbehältermantels hinein erstreckt. Die Erfindung ist dadurch gekennzeichnet, dass die konkave Einwölbung des inneren Druckbehältermantels jeweils von mindestens einem Zugband überspannt ist und dass die Abstützeinrichtungen des äußeren Behältermantels an dem jeweiligen Zugband anliegen.The The invention relates to a double-walled pressure vessel for storing cryogenic fuel in a motor vehicle whose inner pressure vessel shell from first container parts and its outer container shell from second container parts is composed, each at least in one of its central longitudinal axis parallel or inclined plane so cut off and at the interfaces are interconnected so that the inner pressure vessel shell at least one concave between the first container parts at least concavity has. Furthermore, it has the inner pressure vessel shell surrounding outer container casing inwardly directed support devices, one of which in each case into a concave curvature of the inner pressure vessel shell into it extends. The invention is characterized in that the concave concavity of the inner pressure vessel shell each is spanned by at least one tension band and that the support devices of the outer container jacket rest against the respective drawstring.
Das hat den Vorteil, dass Speichern von gasförmigen oder kryogenen Kraftstoffen aufgrund ihrer Formgebung eine bessere Integration im Fahrzeugpackage ermöglicht wird. Bauteilgewicht und Herstellkosten sind nicht wesentlich höher gegenüber zylindrischen Tanks. Die Fixierung des inneren Druckbehälters in dem äußeren Behältermantel ist dagegen, was Gewicht und Kosten betrifft, viel leichter und preiswerter herzustellen als mittels Rohr- und Profilverbindern, die mittels Durchführungen durch den Druckbehälter geführt werden müssen. Es sind weniger gasdichte Schweißnähte nötig und die Wärmeisolation ist effektiver. Die Zugbänder besitzen nur einen geringen Querschnitt und damit ist deren Wärmeleitungseffektivität sehr klein für minimierte Abdampfverluste. Außerdem sind alle für LH2-Speichersysteme notwendigen Funktionen, wie Rohrleitungen, Kupplung etc. mit diesem Konzept darstellbar.The has the advantage of storing gaseous or cryogenic fuels due to their shape a better integration in the vehicle package allows becomes. Component weight and manufacturing costs are not significantly higher compared to cylindrical Tanks. The fixation of the inner pressure vessel in the outer container shell is much easier and lighter in terms of weight and cost cheaper to produce than by means of pipe and profile connectors, by means of bushings through the pressure vessel guided Need to become. There are less gas-tight welds needed and the heat insulation is more effective. The drawstrings have only a small cross-section and thus their heat conduction efficiency is very small for minimized Evaporation losses. Furthermore are all for LH2 storage systems necessary functions, such as piping, coupling etc. with this Concept representable.
Bei einer vorteilhaften Ausführung der Erfindung ist der Zwischenraum zwischen dem Druckbehältermantel und dem äußeren Behältermantel im wesentlichen evakuiert und/oder mit einem Material zur Wärmeisolierung versehen, um Abdampfverluste so gering wie möglich zu halten.at an advantageous embodiment The invention is the space between the pressure vessel shell and the outer container shell essentially evacuated and / or with a material for thermal insulation provided to keep evaporation losses as low as possible.
Bei weiteren vorteilhaften Ausführungen der Erfindung ist die konkave Einwölbung des Druckbehältermantels umlaufend. Durch diesen geometrischen Aufbau kann in den Behälterwänden ein Membranspannungszustand erreicht werden. Aufgrund der belastungsgerechten Konstruktion können vorteilhafterweise geringe Wandstärken verwendet werden. Wenn dann die Abstützeinrichtungen des äußeren Behältermantels ebenfalls durch dessen konkave Einwölbung gebildet sind und wenn diese ebenfalls umlaufend ist, wird ein einfacher kostengünstiger Druckbehälteraufbau dadurch erreicht, dass die Zugbänder um den Druckbehältermantel umlaufend ausgebildet sind.In further advantageous embodiments of the invention, the concave curvature of the pressure vessel shell is circumferential. Through this geometric structure, a membrane voltage state can be achieved in the container walls. Due to the load-oriented design advantageously small wall thicknesses can be used. If then the support means of the outer container shell are also formed by its concave curvature and if this is also circumferential, a simple inexpensive pressure vessel structure is achieved in that the drawstrings around the pressure vessel shell circumferentially are formed.
So ist es möglich, auf einfache Weise, durch Anordnung von zum Beispiel drei Zugbändern, eines in einer Längsebene und zwei in je einer Querebene, eine stabile Auflage des Druckbehälters im äußeren Behältermantel zu erreichen. Werden weitere Abstützpunkte für den äußeren Behältermantel benötigt, so können diese vorteilhafterweise durch weitere, um den Druckbehältermantel umlaufende Zugbänder gebildet werden.So Is it possible, in a simple manner, by arranging, for example, three drawstrings, one in a longitudinal plane and two in a respective transverse plane, a stable support of the pressure vessel in the outer container shell to reach. If additional support points for the outer container shell needed, so can this advantageously by further to the pressure vessel shell circumferential drawstrings be formed.
Im
folgenden wird die Erfindung anhand eines bevorzugten Ausführungsbeispiels
weiter erläutert.
Die
Nach
der Erfindung kann die Form eines Druckbehälters zur Speicherung von kryogenem Kraftstoff,
zum Beispiel Wasserstoff, in einem Kraftfahrzeug, erzeugt werden,
indem dessen innerer
In
der Ausführung
von
Der äußere Behältermantel
Sind
nun umlaufende, gespannte Zugbänder
In
den
Claims (6)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410017392 DE102004017392A1 (en) | 2004-04-08 | 2004-04-08 | Pressure vessel for storing cryogenic fuels |
EP05102649A EP1584859A3 (en) | 2004-04-08 | 2005-04-04 | Pressure vessel for storing cryogen fuel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410017392 DE102004017392A1 (en) | 2004-04-08 | 2004-04-08 | Pressure vessel for storing cryogenic fuels |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102004017392A1 true DE102004017392A1 (en) | 2005-10-27 |
Family
ID=34895529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200410017392 Withdrawn DE102004017392A1 (en) | 2004-04-08 | 2004-04-08 | Pressure vessel for storing cryogenic fuels |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1584859A3 (en) |
DE (1) | DE102004017392A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7829240B2 (en) * | 2007-01-19 | 2010-11-09 | Gm Global Technology Operations, Inc. | Conical shaped fuel storage tank |
FR2919912B1 (en) * | 2007-08-06 | 2009-11-27 | Air Liquide | CRYOGENIC FLUID RESERVOIR AND VEHICLE COMPRISING SUCH A RESERVOIR |
AU2009300368A1 (en) | 2008-09-23 | 2010-04-08 | Aerovironment Inc. | Cryogenic liquid tank |
JP5646413B2 (en) * | 2011-08-24 | 2014-12-24 | 株式会社神戸製鋼所 | Pressure vessel |
US20220333739A1 (en) * | 2019-09-16 | 2022-10-20 | Third Shore Group, LLC | Thermal management in conformable tanks |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2339554A (en) * | 1941-12-02 | 1944-01-18 | Firestone Tire & Rubber Co | Container |
DE3026116A1 (en) * | 1980-07-10 | 1982-02-04 | Aeg Isolier- Und Kunststoff Gmbh, 3500 Kassel | Pressure container comprises several parallel communicating cylinders - esp. of glass fibre reinforced plastics giving form of flat rectangle |
FR2518217A1 (en) * | 1981-12-16 | 1983-06-17 | Ocean Phoenix Holdings Nv | RESERVOIR FOR STORAGE AND TRANSPORTATION OF A PRESSURIZED LIQUID |
DE3206430A1 (en) * | 1982-02-23 | 1983-09-08 | Daimler-Benz Ag, 7000 Stuttgart | High-pressure container |
DE4300484C1 (en) * | 1993-01-11 | 1994-01-05 | Silit Werke | High strength low weight pressure cylinder for recycling - consists of inner metal liner with rounded ends, annular stiffening ribs and outer tension bands |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2040430B (en) * | 1979-01-11 | 1983-02-02 | Ocean Phoenix Holdings Nv | Tanks for storing liquefied gases |
DE10217246A1 (en) * | 2002-04-15 | 2003-11-06 | Deutsch Zentr Luft & Raumfahrt | pressure tank |
-
2004
- 2004-04-08 DE DE200410017392 patent/DE102004017392A1/en not_active Withdrawn
-
2005
- 2005-04-04 EP EP05102649A patent/EP1584859A3/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2339554A (en) * | 1941-12-02 | 1944-01-18 | Firestone Tire & Rubber Co | Container |
DE3026116A1 (en) * | 1980-07-10 | 1982-02-04 | Aeg Isolier- Und Kunststoff Gmbh, 3500 Kassel | Pressure container comprises several parallel communicating cylinders - esp. of glass fibre reinforced plastics giving form of flat rectangle |
FR2518217A1 (en) * | 1981-12-16 | 1983-06-17 | Ocean Phoenix Holdings Nv | RESERVOIR FOR STORAGE AND TRANSPORTATION OF A PRESSURIZED LIQUID |
DE3206430A1 (en) * | 1982-02-23 | 1983-09-08 | Daimler-Benz Ag, 7000 Stuttgart | High-pressure container |
DE4300484C1 (en) * | 1993-01-11 | 1994-01-05 | Silit Werke | High strength low weight pressure cylinder for recycling - consists of inner metal liner with rounded ends, annular stiffening ribs and outer tension bands |
Also Published As
Publication number | Publication date |
---|---|
EP1584859A3 (en) | 2011-04-27 |
EP1584859A2 (en) | 2005-10-12 |
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