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公开(公告)号：EP2393714B1
公开(公告)日：2018-09-12
申请号：EP10707603.6
申请日：2010-01-28
CPC分类号： B64G1/402 , B65D88/12 , F02K9/766 , F17C13/088 , F17C2223/0161 , F17C2270/0194 , Y10T137/86212 , Y10T137/86348
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公开(公告)号：EP2813433A2
公开(公告)日：2014-12-17
申请号：EP14171603.5
申请日：2014-06-06
申请人： Centre National d'Etudes Spatiales (C.N.E.S.) , L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE
发明人： Lienart, Thomas , Pfaab, Kilian , Bravais, Patrick
CPC分类号： F17C7/00 , B64G1/402 , F17C2205/0323 , F17C2223/0123 , F17C2223/035 , F17C2223/036 , F17C2227/0114 , F17C2260/025 , F17C2270/0194
摘要： L'invention concerne un procédé et un dispositif de vidange d'une enceinte d'engin spatial contenant une composition gazeuse sous une pression P1 supérieure à celle P2 régnant dans un environnement extérieur à l'engin spatial dans l'Espace, l'enceinte étant reliée à cet environnement extérieur de l'Espace par au moins une conduite (14) d'évacuation. La composition gazeuse circulant dans chaque conduite (14) d'évacuation traverse au moins un dispositif (20, 21) de détente initiale présentant au moins un étranglement de section à la sortie duquel la pression de la composition gazeuse se trouve à une troisième valeur Pi intermédiaire entre la première pression P1 dans l'enceinte et la deuxième pression P2 de l'environnement extérieur.
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公开(公告)号：EP2778500A1
公开(公告)日：2014-09-17
申请号：EP13159212.3
申请日：2013-03-14
CPC分类号： F17C5/06 , F17C7/00 , F17C13/04 , F17C2205/0326 , F17C2205/0335 , F17C2205/0338 , F17C2205/0341 , F17C2221/012 , F17C2223/0123 , F17C2223/036 , F17C2225/0123 , F17C2225/036 , F17C2250/032 , F17C2250/0605 , F17C2250/0626 , F17C2260/04 , F17C2265/065 , F17C2265/066 , F17C2270/0105 , F17C2270/0168 , F17C2270/0171 , F17C2270/0173 , F17C2270/0189 , F17C2270/0194 , Y02E60/321
摘要： Eine Verfahren zum Betreiben einer Drucktankvorrichtung umfassend einen Drucktank (1), einen Hochdruckeingang (2) zum Drucktank (1) und einen Niederdruckausgang (3) vom Drucktank (1), wobei im Niederdruckausgang (3) zumindest ein elektromechanisches Absperrventil (4) mit einem Absperrventilverschlusskörper und einem Absperrventilsitz angeordnet ist, wobei, zumindest am Beginn einer Betankung der Drucktankvorrichtung über den Hochdruckeingang (2), der Absperrventilverschlusskörper auf den Absperrventilsitz eine höhere Druckkraft aufbringt, als während einem Ruhebetrieb der Drucktankvorrichtung und eine solche Drucktankvorrichtung.
摘要翻译： 该方法包括在压力罐（1）的低压出口（3）中布置具有截止阀关闭体和截止阀的机电截止阀（4）。 在压力罐装置通过高压入口（2）开始加油期间，与在压力罐装置的空转操作期间相比，在截止阀关闭体上施加高压力，其中截止阀 在拆卸操作期间由打开方向由电磁线圈（6）驱动。 还包括压力罐装置的独立权利要求。
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4.发明公开
公开(公告)号：EP2724073A1
公开(公告)日：2014-04-30
申请号：EP12735481.9
申请日：2012-06-19
申请人： MT Aerospace AG
发明人： RADTKE, Wulf
CPC分类号： F17C1/14 , F17C1/06 , F17C1/16 , F17C2201/0109 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0641 , F17C2203/0643 , F17C2203/0648 , F17C2203/0663 , F17C2209/2181 , F17C2209/221 , F17C2209/232 , F17C2209/234 , F17C2221/011 , F17C2221/012 , F17C2223/0115 , F17C2223/0161 , F17C2223/035 , F17C2223/036 , F17C2260/011 , F17C2260/012 , F17C2270/0105 , F17C2270/0168 , F17C2270/0171 , F17C2270/0176 , F17C2270/0178 , F17C2270/0189 , F17C2270/0194 , Y02E60/321
摘要： The invention relates to a method for producing a pressurised container for receiving and storing cryogenic fluids, consisting of a metal container forming a liner (12) and a sheath (14) which is applied to the liner and consists of fibre-reinforced plastic, wherein the liner (12) is formed from a non-magnetic metal alloy having a fully austenitic, cubic-face-centred grid structure and is cold-stretched by up to approximately 25%, in particular by less than approximately 15%, to increase the elastic range before the sheath consisting of fibre-reinforced plastic is applied.
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5.发明公开
公开(公告)号：EP2724072A2
公开(公告)日：2014-04-30
申请号：EP12745410.6
申请日：2012-06-19
申请人： MT Aerospace AG
发明人： RADTKE, Wulf
CPC分类号： F17C1/00 , F17C2201/0109 , F17C2203/0604 , F17C2203/0648 , F17C2203/0663 , F17C2203/0675 , F17C2209/2181 , F17C2221/011 , F17C2221/012 , F17C2223/0115 , F17C2223/0161 , F17C2223/033 , F17C2260/011 , F17C2270/0105 , F17C2270/0131 , F17C2270/0165 , F17C2270/0168 , F17C2270/0171 , F17C2270/0176 , F17C2270/0178 , F17C2270/0189 , F17C2270/0194 , Y02E60/321
摘要： The invention relates to a pressure vessel for receiving and storing cryogenic fluids, in particular cryogenic liquids, said pressure vessel being composed of a metal vessel that forms a liner (12) and a reinforcement (14) made of fiber-reinforced plastic applied to the liner (12), wherein the liner (12) is made of a non-magnetic metal alloy having a fully austenitic face-centered cubic lattice structure and is subjected to a nitriding treatment by means of nitrogen or ammonia in order to expand the elastic range before the reinforcement (14) made of fiber-reinforced plastic is applied. The invention further relates to methods for producing said pressure vessel and to the use of said pressure vessel.
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公开(公告)号：EP1723364A4
公开(公告)日：2011-10-12
申请号：EP05710191
申请日：2005-02-08
申请人： SHOWA DENKO KK
发明人： SHIMADA TOSHIAKI , YOSHIDA YASUKI , KUWABARA HIROKAZU , OSAME YASUHIRO , KANNO YASUHARU , KAWAMATA YASUJI , YAMASAKI HIDEYO
IPC分类号： F17C1/02 , B60L11/18 , F02B43/00 , F02M21/02 , F17C1/06 , F17C1/08 , F17C1/14 , F17C1/16 , H01M8/04
CPC分类号： F17C1/06 , F17C1/08 , F17C1/14 , F17C1/16 , F17C2201/0109 , F17C2201/0119 , F17C2201/0166 , F17C2201/056 , F17C2203/013 , F17C2203/0604 , F17C2203/0619 , F17C2203/0646 , F17C2203/0648 , F17C2203/0665 , F17C2203/0668 , F17C2203/067 , F17C2205/0323 , F17C2205/0397 , F17C2209/222 , F17C2209/232 , F17C2209/234 , F17C2221/011 , F17C2221/012 , F17C2221/033 , F17C2223/0123 , F17C2223/035 , F17C2260/011 , F17C2260/012 , F17C2260/013 , F17C2265/07 , F17C2270/0168 , F17C2270/0184 , F17C2270/0194 , F17C2270/02 , F17C2270/05 , F17C2270/07 , F17C2270/0763 , Y02E60/321
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7.发明公开
公开(公告)号：EP2361196A1
公开(公告)日：2011-08-31
申请号：EP09795321.0
申请日：2009-12-01
申请人： MT Aerospace AG
发明人： SACHER, Hanno , SPIEGEL, Michael
IPC分类号： B64G1/40
CPC分类号： B64G1/402 , F02K9/44 , F02K9/605 , F17C2201/0109 , F17C2201/056 , F17C2201/058 , F17C2203/011 , F17C2203/0607 , F17C2203/0619 , F17C2203/0624 , F17C2203/0639 , F17C2203/0643 , F17C2203/0646 , F17C2203/0648 , F17C2203/0663 , F17C2203/0673 , F17C2203/0685 , F17C2209/221 , F17C2209/227 , F17C2209/228 , F17C2221/011 , F17C2221/012 , F17C2221/014 , F17C2221/08 , F17C2223/0161 , F17C2227/0192 , F17C2260/011 , F17C2260/012 , F17C2260/018 , F17C2260/027 , F17C2270/0105 , F17C2270/0131 , F17C2270/0168 , F17C2270/0171 , F17C2270/0178 , F17C2270/0189 , F17C2270/0194 , F17C2270/0197 , Y02E60/321
摘要： The invention relates to a tank for receiving, storing and discharging liquids and/or viscous substances, in particular fuel or propellant or drinking water, having a casing (12) and at least one baffle plate (16) which is arranged in an interior (14) of the tank (10), on the inner side (18) of the casing (12), and has one end (20) directed towards an outlet opening (22) of the tank (10), and extends into a region (24) which is adjacent to or adjoins the outlet opening (22) of the tank (10), characterized in that a flexible element (32) is arranged between the at least one baffle plate (16) and the inner side (18) of the casing (12) in order to cover (over) a gap, corner, interstice, or similar interspace (28) formed between the at least one baffle plate (16) and the inner side (18) of the casing (12), and also relates to a use of the same.
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公开(公告)号：EP1526324A3
公开(公告)日：2011-04-20
申请号：EP04256044.1
申请日：2004-09-30
IPC分类号： F17C1/06
CPC分类号： D04C1/06 , D10B2505/02 , F17C1/06 , F17C2201/0109 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0646 , F17C2203/0648 , F17C2203/066 , F17C2203/0665 , F17C2203/0673 , F17C2205/0397 , F17C2209/2118 , F17C2209/2127 , F17C2209/2154 , F17C2209/232 , F17C2221/012 , F17C2221/033 , F17C2223/0123 , F17C2223/036 , F17C2260/011 , F17C2260/013 , F17C2270/0178 , F17C2270/0194 , Y02E60/321
摘要： A pressure container manufacturing method by forming an outer shell of a fiber reinforced composite material on a periphery of a liner having a cylindrical portion, dome portions connected to both ends of the cylindrical portion, and a mouth piece disposed on one top of the dome portions, has: forming a body on the periphery by braiding fiber bundles provided from bobbins of a braider disposed in a circumferential direction of the liner, while moving the liner in an axial direction, wherein when body formation reaches a root portion of the mouth piece, a movement in a first direction of the liner is stopped, each bobbin is rotated approximately a half-turn in the circumferential direction, and thereafter formation of the body is continued while moving the liner in a second direction opposite to the first direction; and curing a resin impregnated in the fiber bundles, to form an outer shell.
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9.发明公开
公开(公告)号：EP2306066A1
公开(公告)日：2011-04-06
申请号：EP11000155.9
申请日：2009-03-13
发明人： Kawasaki, Haruo
CPC分类号： F17C13/088 , B64G1/402 , F17C13/026 , F17C13/028 , F17C2201/0109 , F17C2201/0119 , F17C2201/0128 , F17C2201/054 , F17C2201/056 , F17C2203/0304 , F17C2203/0308 , F17C2203/032 , F17C2221/08 , F17C2223/0153 , F17C2223/031 , F17C2227/0304 , F17C2227/0379 , F17C2250/032 , F17C2250/0408 , F17C2250/0426 , F17C2250/043 , F17C2250/0439 , F17C2250/0478 , F17C2250/0491 , F17C2250/0495 , F17C2250/0631 , F17C2260/024 , F17C2270/0194
摘要： Disclosed is an apparatus, which is capable of, even under a microgravity environment, determining a volume of the liquid, in a simple and accurate manner. The apparatus comprises a vessel adapted to contain therein a liquid, heating means provided on a wall surface of the vessel to heat the liquid contained in the vessel, temperature measuring means provided adjacent to the heating means to measure a temperature change occurring due to the heating by the heating means, and processing means operable, based on the temperature change measured by the temperature measuring means, to calculate a volume of the liquid contained in the vessel.
摘要翻译： 公开了一种即使在微重力环境下也能够以简单和准确的方式确定液体体积的装置。 该装置包括适于在其中容纳液体的装置，设置在容器的壁表面上的加热装置，以加热容纳在容器中的液体，设置在加热装置附近的温度测量装置，以测量由于加热而发生的温度变化 通过加热装置，以及基于由温度测量装置测量的温度变化可操作的处理装置，以计算容纳在容器中的液体的体积。
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10.发明公开
公开(公告)号：EP2173619A1
公开(公告)日：2010-04-14
申请号：EP08826964.2
申请日：2008-07-11
发明人： LACAPERE, Jérôme
CPC分类号： B64G1/402 , F17C3/00 , F17C2201/0109 , F17C2201/0147 , F17C2201/0166 , F17C2201/0171 , F17C2201/0185 , F17C2201/054 , F17C2203/0646 , F17C2203/0648 , F17C2221/01 , F17C2221/08 , F17C2223/0161 , F17C2223/033 , F17C2227/0121 , F17C2260/016 , F17C2260/027 , F17C2270/0194 , F17C2270/0197
摘要： Cryogenic tank intended for containing a cryogenic fluid, in particular a space launcher tank intended to contain a cryogenic propellant, comprising a wall (1 ) defining a storage volume for the cryogenic fluid, characterized in that it includes at least one partition (2) located in the storage volume, said partition (2) defining an upper volume (VS) and a lower volume (Vl) for the fluid in the tank (1) communicating via at least one opening (3) formed in the partition (2), in order, on the one hand, to allow the liquid to flow under gravity from the upper volume (VS) into the lower volume (Vl) and, on the other hand, to prevent the fluid from rising from the lower volume (Vl) into the upper volume (VS) under the action of acceleration forces.
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