公开(公告)号：US09882229B2

公开(公告)日：2018-01-30

申请号：US14428985

申请日：2013-09-17

Applicant: C. EN LTD.

Inventor： Moshe Stern

IPC: H01M8/04 ,  C03B23/207 ,  F17C1/00 ,  H01M8/04082

CPC classification number: H01M8/04216 ,  C03B23/20 ,  C03B23/207 ,  F17C1/00 ,  F17C2201/0104 ,  F17C2201/0157 ,  F17C2201/0161 ,  F17C2201/058 ,  F17C2203/0617 ,  F17C2203/0658 ,  F17C2203/0692 ,  F17C2205/0111 ,  F17C2205/0142 ,  F17C2205/0146 ,  F17C2205/0311 ,  F17C2205/0335 ,  F17C2209/227 ,  F17C2221/012 ,  F17C2223/0123 ,  F17C2223/035 ,  F17C2260/013 ,  F17C2270/0763 ,  H01M8/04201 ,  H01M8/04208 ,  Y02E60/321 ,  Y02E60/324

Abstract: A device for the storage of compressed hydrogen gas comprises a plurality of glass capillary tubes each having a sealed extremity and an open extremity, wherein said plurality of glass capillary tubes is sheathed in an external tubular cover, and wherein the open end of a bundle of said tubular covers is housed in an adaptor, and wherein said adaptor is suitable to allow compressed hydrogen gas to be added to, and to prevent said hydrogen gas from escaping from, said glass capillary tubes.

公开(公告)号：US20150014323A1

公开(公告)日：2015-01-15

申请号：US14326458

申请日：2014-07-08

Applicant: Adam R. Loukus ,  Josh E. Loukus

Inventor： Adam R. Loukus ,  Josh E. Loukus

IPC: B32B3/26 ,  F41H5/04 ,  B29C39/02 ,  B60P3/22 ,  B65D25/04

CPC classification number: F41H5/04 ,  B29C39/025 ,  B32B1/02 ,  B32B3/266 ,  B32B15/04 ,  B32B27/06 ,  B32B2305/02 ,  B32B2307/558 ,  B32B2439/00 ,  B32B2571/02 ,  B60P3/22 ,  F17C1/00 ,  F17C2201/0157 ,  F17C2201/0161 ,  F17C2201/0166 ,  F17C2201/0171 ,  F17C2201/054 ,  F17C2201/056 ,  F17C2203/0617 ,  F17C2203/0636 ,  F17C2203/0663 ,  F17C2209/21 ,  F17C2209/2109 ,  F17C2209/232 ,  F17C2221/033 ,  F17C2223/0123 ,  F17C2223/013 ,  F17C2223/035 ,  F17C2223/036 ,  F17C2260/01 ,  F17C2260/011 ,  F17C2260/012 ,  F17C2260/017 ,  F17C2260/018 ,  F17C2270/0171 ,  F41H7/044 ,  F42D5/045 ,  Y10T428/13 ,  Y10T428/249953

Abstract: A structural component with at least two side members has a support structure that includes a partition with multiple curved portions forming cells. The partition connects to the side members and extends between the side members at least partially along straight lines. The partition may extend along one or more straight lines from one side member to the other. One structural component is a container with a wall about the internal support structure. The container cells may be formed with a core structure. The core can include a permeable storage material and may be retained after formation, or may be removed. In some cases the container wall has generally planar surfaces, which may include surface undulations. Core structures are also provided for forming structural components. Formation can include casting a material about a core structure within a mold to form a partition extending between two or more sides.

Abstract translation: 具有至少两个侧部构件的结构部件具有支撑结构，该支撑结构包括具有形成电池的多个弯曲部分的隔板。 分隔件连接到侧构件并且至少部分地沿着直线在侧构件之间延伸。 分隔件可以沿着一个或多个直线从一个侧部件延伸到另一个。 一个结构部件是围绕内部支撑结构具有壁的容器。 容器单元可以形成有芯结构。 芯可以包括可渗透的储存材料，并且可以在形成之后保留，或者可以被去除。 在一些情况下，容器壁具有大致平坦的表面，其可包括表面起伏。 还提供用于形成结构部件的芯结构。 形成可以包括在模具内围绕芯结构铸造材料以形成在两个或更多个侧面之间延伸的隔板。

公开(公告)号：US08917809B2

公开(公告)日：2014-12-23

申请号：US13407196

申请日：2012-02-28

Applicant: Tsukasa Nozawa

Inventor： Tsukasa Nozawa

IPC: G21F5/008

CPC classification number: B29D99/0089 ,  B29C70/342 ,  B29C70/345 ,  B29C70/347 ,  B29L2031/608 ,  B32B3/12 ,  F17C1/00 ,  F17C2201/0109 ,  F17C2201/0161 ,  F17C2201/056 ,  F17C2203/0329 ,  F17C2203/0629 ,  F17C2203/0646 ,  F17C2203/066 ,  F17C2203/0663 ,  F17C2205/013 ,  F17C2221/012 ,  F17C2223/0123 ,  F17C2223/0153 ,  F17C2223/035 ,  F17C2223/036 ,  F17C2270/0168 ,  F17C2270/0171 ,  Y02E60/321 ,  Y10T428/1352 ,  Y10T428/24157 ,  Y10T428/24165

Abstract: The present invention is directed to a new manufacturing process for a FRP honeycomb structure where the honeycomb core assembly is arranged parallel to the surface. The honeycomb core is made from FRP prepreg with double structural walls and is manufactured by stiffening using heat and pressure. In a honeycomb core assembly set tank, a plurality of internal tanks are gathered in honeycomb core assembly. An internal tank FRP wall maintains the pressure of the internal tank, while an external FRP wall, heat foamed plastic resin and rigid FRP hull of set tank endure the external shock loading. A honeycomb core structure of six-corner cell can be infinitely arranged, and its structural position is unique. A set tank in which a plurality of internal tanks are gathered into a honeycomb core assembly can be arranged in infinite combinations, such that the total capacity can be extremely large.

Abstract translation: 本发明涉及一种用于FRP蜂窝结构的新的制造方法，其中蜂窝芯组件平行于表面布置。 蜂窝芯由具有双重结构壁的FRP预浸料制成，并通过加热和加压硬化制成。 在蜂窝芯组合箱中，多个内箱聚集在蜂窝芯组件中。 内箱FRP墙保持内箱的压力，而外部FRP墙，热发泡塑料树脂和固定罐的刚性FRP船体承受外部冲击载荷。 六角电池的蜂窝芯结构可无限排列，其结构位置独特。 将多个内部容器收集到蜂窝芯组件中的集合罐可以以无限组合布置，使得总容量可以非常大。

公开(公告)号：US20040089440A1

公开(公告)日：2004-05-13

申请号：US10294825

申请日：2002-11-13

Inventor： Stan A. Sanders

IPC: F28F007/00 ,  F28D007/10 ,  F28D007/02 ,  B21D053/02

CPC classification number: F17C1/00 ,  B29C47/00 ,  B29C47/0014 ,  B29C47/0023 ,  B29C47/0026 ,  B29C47/0028 ,  B29C47/003 ,  B29C47/0052 ,  B29C47/065 ,  B29C47/30 ,  B29C47/882 ,  B29C47/8895 ,  B29C53/66 ,  B29C53/8075 ,  B29C63/10 ,  B29C65/00 ,  B29C65/02 ,  B29C65/04 ,  B29C65/08 ,  B29C65/562 ,  B29C65/564 ,  B29C65/78 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/1222 ,  B29C66/1224 ,  B29C66/124 ,  B29C66/131 ,  B29C66/221 ,  B29C66/5344 ,  B29C66/54 ,  B29C66/542 ,  B29C66/5432 ,  B29C66/8221 ,  B29C66/8242 ,  B29C66/8322 ,  B29C66/83411 ,  B29C66/836 ,  B29C70/32 ,  B29C70/86 ,  B29C2793/0027 ,  B29D23/00 ,  B29L2023/00 ,  B29L2023/005 ,  B29L2031/18 ,  B29L2031/602 ,  B29L2031/7156 ,  B29L2031/772 ,  F17C2201/0138 ,  F17C2201/0142 ,  F17C2201/0147 ,  F17C2201/0157 ,  F17C2201/0161 ,  F17C2201/0166 ,  F17C2201/0176 ,  F17C2201/035 ,  F17C2201/056 ,  F17C2203/011 ,  F17C2203/012 ,  F17C2203/0629 ,  F17C2203/0658 ,  F17C2203/0663 ,  F17C2203/0665 ,  F17C2203/067 ,  F17C2203/0685 ,  F17C2203/069 ,  F17C2205/0314 ,  F17C2205/0323 ,  F17C2209/2154 ,  F17C2209/22 ,  F17C2209/221 ,  F17C2209/227 ,  F17C2209/228 ,  F17C2209/23 ,  F17C2223/0123 ,  F17C2223/035 ,  F17C2260/012 ,  F17C2260/021 ,  F17C2260/042 ,  F17C2265/031 ,  F17C2270/01 ,  Y10T29/4935

Abstract: A cellular reservoir flexible pressure vessel is formed as a series of closely packed tubes fitted into a pair of opposing end caps. The end caps have individual receptacles sized and shaped to receive the tube ends that are secured with adhesive or radio frequency welding. At least one end cap has a passageway for connection of the vessel. The vessel may be formed in a variety of useful shapes and the tubes may have various internal and external cross-sections. The end caps may be filled with sintactic foam with canals leading to the passageway. Microtubes through the syntactic foam may connect the tubes to the passageway. The vessel is further strengthened by overwrapping with high-strength braiding material, hoop winding or by overlayment with high-strength fabric. The vessel is further strengthened by coating with plastic resin. Apparatus and methods for forming the cellular reservoir flexible vessels are described.

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

IPC: F17C13/00 ,  F17C3/08

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.

公开(公告)号：US20160356420A1

公开(公告)日：2016-12-08

申请号：US15239159

申请日：2016-08-17

Applicant: KOREA ADVANCED INSTITUTE OF SCIENCE AND TECHNOLOGY

Inventor： Dae Jun CHANG ,  Pal, G BERGAN

IPC: F17C1/08 ,  F17C1/12 ,  F17C13/02

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。

公开(公告)号：US20130224410A1

公开(公告)日：2013-08-29

申请号：US13407196

申请日：2012-02-28

Applicant: Tsukasa NOZAWA

Inventor： Tsukasa NOZAWA

IPC: B32B1/02 ,  B32B3/12 ,  B65H81/06

CPC classification number: B29D99/0089 ,  B29C70/342 ,  B29C70/345 ,  B29C70/347 ,  B29L2031/608 ,  B32B3/12 ,  F17C1/00 ,  F17C2201/0109 ,  F17C2201/0161 ,  F17C2201/056 ,  F17C2203/0329 ,  F17C2203/0629 ,  F17C2203/0646 ,  F17C2203/066 ,  F17C2203/0663 ,  F17C2205/013 ,  F17C2221/012 ,  F17C2223/0123 ,  F17C2223/0153 ,  F17C2223/035 ,  F17C2223/036 ,  F17C2270/0168 ,  F17C2270/0171 ,  Y02E60/321 ,  Y10T428/1352 ,  Y10T428/24157 ,  Y10T428/24165

Abstract: The present invention is directed to a new manufacturing process for a FRP honeycomb structure where the honeycomb core assembly is arranged parallel to the surface. The honeycomb core is made from FRP prepreg with double structural walls and is manufactured by stiffening using heat and pressure. In a honeycomb core assembly set tank, a plurality of internal tanks are gathered in honeycomb core assembly. An internal tank FRP wall maintains the pressure of the internal tank, while an external FRP wall, heat foamed plastic resin and rigid FRP hull of set tank endure the external shock loading. A honeycomb core structure of six-corner cell can be infinitely arranged, and its structural position is unique. A set tank in which a plurality of internal tanks are gathered into a honeycomb core assembly can be arranged in infinite combinations, such that the total capacity can be extremely large.

Abstract translation: 本发明涉及一种用于FRP蜂窝结构的新的制造方法，其中蜂窝芯组件平行于表面布置。 蜂窝芯由具有双重结构壁的FRP预浸料制成，并通过加热和加压硬化制成。 在蜂窝芯组合箱中，多个内箱聚集在蜂窝芯组件中。 内箱FRP墙保持内箱的压力，而外部FRP墙，热发泡塑料树脂和固定罐的刚性FRP船体承受外部冲击载荷。 六角电池的蜂窝芯结构可无限排列，其结构位置独特。 将多个内部容器收集到蜂窝芯组件中的集合罐可以以无限组合布置，使得总容量可以非常大。

公开(公告)号：US20020179610A1

公开(公告)日：2002-12-05

申请号：US09872208

申请日：2001-06-04

Applicant: Lockheed Martin Corporation

Inventor： Walter Fraklin III ,  David A. Hooke

IPC: F17C001/00 ,  F17C003/00

CPC classification number: F17C1/02 ,  B64G1/402 ,  F17C1/04 ,  F17C1/16 ,  F17C2201/0142 ,  F17C2201/0161 ,  F17C2201/054 ,  F17C2201/056 ,  F17C2203/012 ,  F17C2203/0379 ,  F17C2203/0629 ,  F17C2209/232 ,  F17C2221/011 ,  F17C2221/012 ,  F17C2223/0161 ,  F17C2223/033 ,  F17C2260/036 ,  F17C2260/042 ,  F17C2270/0194 ,  Y02E60/321

Abstract: A wall of a cryogenic propellant tank includes inner and outer skins supported parallel to, and at a distance from, one another to define between them a zone into which pressurized gas is introduced. The zone houses a reinforcing structure, such as honeycomb or corrugated material, to create a sandwich structure. The gas is introduced into the zone using conduits in the reinforcing structure. The gas preferably is an inert gas, most preferably helium.

Abstract translation: 低温推进剂罐的壁包括彼此平行并且彼此间隔一定距离地支撑的内表皮和外表皮，以在它们之间限定加压气体被引入的区域。 该区域容纳加强结构，例如蜂窝或波纹材料，以形成夹层结构。 使用加强结构中的导管将气体引入该区域。 气体优选为惰性气体，最优选为氦气。

公开(公告)号：EP3176490A1

公开(公告)日：2017-06-07

申请号：EP15382600.3

申请日：2015-12-02

Applicant: The Boeing Company

Inventor： SERROT HAUKE, Enrique Emilio ,  FERREYRA, Eduardo Gabriel ,  LEMUS, Jose Luis ,  BLANCO, Jose Antonio ,  LAPEÑA-REY, Nieves

IPC: F17C1/12 ,  F17C1/14 ,  F17C13/00

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: This disclosure relates to a cryogenic tank which has an inner storage volume (102) within a first wall (104). The cryogenic tank (100) comprises additionally a plurality of chambers (108) within the inner storage volume (102), these chambers (108) placed longitudinally along the first wall (104), such that at least one of the chambers (108) is defined by a portion of the first wall (104).
Additionally, this disclosure relates to a method of storing cryogenic liquids, said method comprising storing the cryogenic liquids inside a cryogenic tank (100) comprising a plurality of chambers (108).

Abstract translation: 本公开涉及一种在第一壁（104）内具有内部存储容积（102）的低温罐。 低温储箱（100）还包括在内部储存空间（102）内的多个室（108），这些室（108）沿着第一壁（104）纵向放置，使得至少一个室（108） 由第一壁（104）的一部分限定。 另外，本公开涉及一种存储低温液体的方法，所述方法包括将低温液体存储在包括多个腔室（108）的低温罐（100）内。

公开(公告)号：EP2702310A2

公开(公告)日：2014-03-05

申请号：EP12777631.8

申请日：2012-04-25

Applicant: Korea Advanced Institute Of Science And Technology

Inventor： CHANG, Dae Jun ,  BERGAN, Pal, G

IPC: F17C1/08 ,  F17C1/02

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.