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公开(公告)号:US20180283611A1
公开(公告)日:2018-10-04
申请号:US15935436
申请日:2018-03-26
Applicant: Crompton Technology Group Limited
Inventor: James BERNARD , Jon PETHICK , Ian CHASE
IPC: F17C1/16
CPC classification number: F17C1/16 , F17C1/06 , F17C13/08 , F17C2201/0119 , F17C2201/0152 , F17C2201/0166 , F17C2201/0171 , F17C2201/035 , F17C2201/056 , F17C2203/012 , F17C2203/0619 , F17C2203/0621 , F17C2203/066 , F17C2203/0663 , F17C2203/0665 , F17C2203/0668 , F17C2205/0142 , F17C2205/0146 , F17C2209/2163 , F17C2209/22 , F17C2209/234 , F17C2221/011 , F17C2260/011 , F17C2260/012 , F17C2270/0189
Abstract: A pressure vessel includes front and rear end plates and a plurality of open-ended vessel structures constructed of fibre-reinforced polymer matrix composite material positioned adjacent to one another so that their longitudinal axes are parallel to a longitudinal direction extending between the front and rear end plates. The vessel also includes an outer reinforcement comprising polymer matrix composite material with continuous fibres extending longitudinally around the pressure vessel to secure the front and rear end plates to the vessel structures. At least one of the vessel structures has a partially curved cross section in a plane perpendicular to its longitudinal axis, such that one or more crevices are formed between the vessel structures, running longitudinally between the front and rear end plates and the front and rear end plates are shaped to allow the outer reinforcement to at least partially fill the one or more crevices between the vessel structures.
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公开(公告)号:US20180195669A1
公开(公告)日:2018-07-12
申请号:US15851845
申请日:2017-12-22
Applicant: TOYOTA JIDOSHA KABUSHIKI KAISHA
Inventor: Osamu SAWAI
CPC classification number: F17C1/02 , F17C1/00 , F17C1/06 , F17C1/14 , F17C1/16 , F17C13/06 , F17C13/083 , F17C13/084 , F17C2201/0104 , F17C2201/0109 , F17C2201/0119 , F17C2201/0138 , F17C2201/0166 , F17C2201/035 , F17C2201/056 , F17C2203/012 , F17C2203/0604 , F17C2203/0619 , F17C2203/0621 , F17C2203/0646 , F17C2203/066 , F17C2203/0663 , F17C2203/0665 , F17C2203/0668 , F17C2205/0142 , F17C2205/0146 , F17C2205/0157 , F17C2205/0323 , F17C2205/0394 , F17C2209/2154 , F17C2209/234 , F17C2221/012 , F17C2221/035 , F17C2223/0123 , F17C2223/0153 , F17C2223/036 , F17C2260/018 , F17C2270/0178 , F17C2270/0184 , Y02E60/321
Abstract: A high-pressure container includes a plurality of body parts arranged side by side, and each of the body parts has a cylindrical shape and has an opening at at least one of its axially opposite end portions. The high-pressure container also includes a cap configured to close the openings of the body parts as a unit, and a communication channel provided inside the cap for communicating interiors of the body parts with each other.
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公开(公告)号:US20180111475A1
公开(公告)日:2018-04-26
申请号:US15792090
申请日:2017-10-24
Applicant: Other Lab, LLC
Inventor: Jason Stein Wexler , Kevin Kai Morris , Jamie Marie LoBue
CPC classification number: B60K15/03006 , B60K15/01 , B60K15/013 , B60K2015/03315 , F17C1/005 , F17C1/16 , F17C13/04 , F17C13/083 , F17C2201/0104 , F17C2201/0109 , F17C2201/0123 , F17C2201/0138 , F17C2201/0166 , F17C2201/0195 , F17C2201/054 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0636 , F17C2203/0646 , F17C2203/0663 , F17C2205/0107 , F17C2205/0142 , F17C2205/0305 , F17C2205/0332 , F17C2205/0361 , F17C2205/037 , F17C2205/0373 , F17C2209/224 , F17C2209/228 , F17C2221/012 , F17C2223/0123 , F17C2223/0161 , F17C2270/0178
Abstract: A set of fittings for a fuel tank including an elongated stem and a ferrule. The stem includes an elongated coupling body at one end configured to couple within a cavity defined by an end of a fuel tank liner. The ferrule includes a ferrule body having a first ferrule end and a second ferrule end; a lip defining a coupling orifice at the first ferrule end with the stem being operable to extend though the coupling orifice and engaging the lip, and a ferrule cavity defined by the ferrule body that extends between the first and second ferrule ends and opening to the coupling orifice at the first ferrule end and a ferrule opening at the second ferrule end, the ferrule cavity configured to surround the end of the fuel tank liner.
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公开(公告)号:US09708120B2
公开(公告)日:2017-07-18
申请号:US14923015
申请日:2015-10-26
Applicant: Altair Engineering, Inc.
Inventor: Regu Ramoo , Thomas Lamb
CPC classification number: B65D90/12 , B65D90/0066 , B65D90/08 , F17C3/00 , F17C2201/0152 , F17C2201/0166 , F17C2201/052 , F17C2203/012 , F17C2203/0646 , F17C2203/0648 , F17C2209/221 , F17C2221/033 , F17C2223/0161 , F17C2260/016 , F17C2270/0105
Abstract: A large volume natural gas storage tank comprises a plurality of rigid tubular walls having opposing ends and intermediate segments with closed cross-sections extending along longitudinal axes. Each wall is interconnected at each end with respective ends of two other walls such that interconnected interiors define an interior fluid storage chamber. Exterior surfaces of planarly successive interconnected walls define sides of the storage tank. The tank further comprises exterior support structures each extending between the exterior surfaces of the walls forming each side of the storage tank and reinforcing the storage tank against dynamic loading from fluid in the interior fluid storage chamber. The tank further comprises closure plates each extending at least partially across exterior surfaces of the exterior support structures. Interior surfaces of the closure plates, interior surfaces of the exterior support structures, and exterior surfaces of walls at least partially define an auxiliary fluid storage chamber.
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公开(公告)号:US20170184251A1
公开(公告)日:2017-06-29
申请号:US15384567
申请日:2016-12-20
Applicant: GE Oil & Gas, Inc.
Inventor: Christopher Joseph Collins , Emmanuel G. Galindo , Daisy Yuen Lau , Anindra Mazumdar , Garrick Gerald Mullen , Mae Alane Plummer
CPC classification number: F17C5/06 , B60P3/2245 , F17C7/00 , F17C13/02 , F17C13/04 , F17C2201/0166 , F17C2205/0323 , F17C2205/0338 , F17C2223/035 , F17C2223/036 , F17C2225/033 , F17C2227/00 , F17C2227/0309 , F17C2227/036 , F17C2250/043 , F17C2250/0439 , F17C2250/0443 , F17C2250/0626 , F17C2250/0631 , F17C2250/0636 , F17C2265/068 , F17C2270/0168
Abstract: A system that can offload compressed gas from a storage tank to a customer site. The system can have a fluid circuit that is configured to fit within a container structure, like a trailer, for mobility to remote locations. This fluid circuit can include a transfer unit to automatically switch between tanks. The transfer unit can couple with a heat exchanger. Downstream of the heat exchanger, the fluid circuit can reduce pressure of fluid from the tanks through multiple pressure reduction stages. Each of the pressure reduction stages can include a throttling device, for example, a pilot-type fluid regulator and a control valve assembly. The throttling device may be selected to maintain flow of fluid at least at, e.g., 35,000 scfh, in accordance with pressure drops in the incoming fluid from the tanks.
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公开(公告)号:US20170159883A1
公开(公告)日:2017-06-08
申请号:US15360928
申请日:2016-11-23
Applicant: The Boeing Company
Inventor: Nieves Lapeña Rey , Jose Antonio Blanco , Jose Luis Lemus , Enrique Emilio Serrot Hauke , Eduardo Gabriel Ferreyra
CPC classification number: F17C13/001 , F17C3/08 , F17C2201/0109 , F17C2201/0119 , F17C2201/0161 , F17C2201/0166 , F17C2201/0171 , F17C2201/035 , F17C2201/056 , F17C2203/0391 , F17C2203/0629 , F17C2203/0646 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2260/016 , F17C2260/033 , F17C2270/0168 , F17C2270/0186 , F17C2270/0189 , Y02E60/321
Abstract: Method and apparatus for storing cryogenic liquids. A cryogenic tank comprising an inner storage volume within a first wall and a plurality of chambers defined by a plurality of chamber walls within the inner storage volume. The chamber walls extending the length of the inner storage volume, and the chambers disposed along the first wall and that at least one of the chambers of the plurality of chambers is defined by a plurality of chamber walls and a portion of the first wall.
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公开(公告)号:US20170025691A1
公开(公告)日:2017-01-26
申请号:US15155273
申请日:2016-05-16
Applicant: Encite LLC
Inventor: Stephen Alan Marsh , Donald M. Parker , William J. Grande
IPC: H01M8/04082 , H01M8/04746 , B01J13/04 , C30B33/12 , F17C1/00 , C30B29/06 , H01M8/04992
CPC classification number: H01M8/04208 , B01J13/02 , B01J13/04 , C30B29/06 , C30B33/12 , F17C1/00 , F17C2201/0166 , F17C2221/011 , F17C2221/012 , F17C2223/0123 , F17C2223/036 , F17C2270/0131 , F17C2270/0168 , F17C2270/0184 , F17C2270/0763 , H01M8/04201 , H01M8/04216 , H01M8/04753 , H01M8/04992 , Y02E60/321 , Y02E60/324 , Y02E60/50
Abstract: Among other things, a gas storage system includes a group of capsules and an activation element coupled to the group. The group of capsules are formed within a substrate and contain gas stored at a relatively high pressure compared to atmospheric pressure. The activation element is configured to deliver energy in an amount sufficient to cause at least one of the capsules to release stored gas.
Abstract translation: 除其他之外,气体存储系统包括一组胶囊和联接到该组的激活元件。 胶囊组在衬底内形成并且含有与大气压相比以较高压力储存的气体。 激活元件被配置成以足以使至少一个胶囊释放储存气体的量传送能量。
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公开(公告)号:US20160356420A1
公开(公告)日:2016-12-08
申请号:US15239159
申请日:2016-08-17
Inventor: Dae Jun CHANG , Pal, G BERGAN
CPC classification number: F17C1/08 , F17C1/02 , F17C1/12 , F17C3/025 , F17C13/02 , F17C2201/0157 , F17C2201/0161 , F17C2201/0166 , F17C2201/0171 , F17C2201/052 , F17C2203/013 , F17C2203/0304 , F17C2203/0345 , F17C2203/0629 , F17C2209/221 , F17C2221/033 , F17C2223/0161 , F17C2223/033 , F17C2223/035 , F17C2250/04 , F17C2250/0452 , F17C2250/0491 , F17C2260/011 , F17C2260/016 , F17C2270/0105
Abstract: Provided is a pressure tank having a lattice structure, including: a tank body that has a high-pressure fluid accommodated therein and is manufactured to have a prismatic shape; and cell structures that are disposed in the prismatic tank body, are manufactured in a lattice form, arrive from one side wall of the tank body to the other side wall thereof facing it, and are orthogonally arranged regularly.
Abstract translation: 本发明提供一种具有格子状结构的压力罐,其特征在于,包括容纳在其中并具有棱柱形状的高压流体的罐体, 并且设置在棱柱形箱体中的单元结构以格子形式制造,从罐体的一个侧壁到达面向其的另一个侧壁,并且正规布置。
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公开(公告)号:US20160312956A1
公开(公告)日:2016-10-27
申请号:US15106063
申请日:2014-12-16
Inventor: Albin CHAISE , David BOUFFETIER , Cedric DUPUIS , Mariana DUPUIS-ROSCA , Manon ELIE , Olivier GILLIA , David VEMPAIRE
CPC classification number: F17C11/005 , F17C1/12 , F17C1/16 , F17C2201/0166 , F17C2203/0362 , F17C2203/037 , F17C2203/066 , F17C2205/0149 , F17C2209/2109 , F17C2209/22 , F17C2209/234 , F17C2221/012 , F17C2270/0168 , F28D7/103 , Y02E60/321 , Y02E60/327
Abstract: A tank for storing hydrogen by absorption in a hydrogen storage material, including: a chamber; a hydrogen supplier to supply hydrogen into the chamber and/or collect hydrogen in the chamber; an inner structure for storing hydrogen storage material, the inner structure including at least two cups, each cup including a base, a side wall, and a closing element forming a volume impermeable to the hydrogen storage material, at least part of each cup being permeable to hydrogen, and the inner structure including a passage provided at least between part of an outer face of the side wall of the cup and an inner face of the chamber.
Abstract translation: 一种用于通过吸收在储氢材料中储存氢的罐,包括:室; 氢气供应器,用于向室内供应氢气和/或在室中收集氢气; 用于存储储氢材料的内部结构,所述内部结构包括至少两个杯,每个杯包括底座,侧壁和闭合元件,其形成对所述储氢材料不可渗透的体积,每个杯子的至少一部分是可渗透的 并且内部结构包括至少设置在杯的侧壁的外表面的一部分与腔室的内表面之间的通道。
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公开(公告)号:US09440529B2
公开(公告)日:2016-09-13
申请号:US14909288
申请日:2014-08-02
Applicant: Alternative Fuel Containers, LLC
Inventor: Joong-Kyu Lee
CPC classification number: B60K15/03006 , B60K15/013 , B60K15/04 , B60K15/063 , B60K15/07 , B60K2015/03236 , B60K2015/03322 , B60K2015/03328 , B60K2015/0631 , B60K2015/0632 , B60K2015/0633 , B60K2015/0634 , B60K2015/0638 , F17C11/005 , F17C11/007 , F17C2201/0166 , F17C2270/0168
Abstract: A conformable fuel gas storage tank includes a housing that has exterior walls surrounding an interior. First and second base walls are spaced apart in a direction along a normal axis, side walls extend between the base walls and are spaced apart in a direction along a lateral axis, and end walls extend between the base walls and the side walls and are spaced apart in a direction along a longitudinal axis. Interior walls divide the interior and extend in a direction between the base walls and the end walls, and are spaced apart in a direction along the lateral axis. The interior walls establish elongate, laterally spaced, through channels extending longitudinally between the end walls. A gas storage material is located within the channels, and a gas permeable flow guide ex tends along at least one of the channels and through the gas storage material.
Abstract translation: 适合的燃料气体储存箱包括具有围绕内部的外壁的壳体。 第一和第二基壁在沿着法向轴线的方向上间隔开,侧壁在基壁之间延伸并且沿着横向轴线的方向间隔开,并且端壁在基壁和侧壁之间延伸并且间隔开 沿着纵向轴线的方向分开。 内墙分隔内部并沿底壁和端壁之间的方向延伸,并沿着横向轴线方向间隔开。 内壁在端壁之间纵向延伸形成横向间隔开的通道。 气体储存材料位于通道内,气体渗透流动导向件沿着至少一个通道并通过气体储存材料。
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