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    Floating body type liquefied natural gas production, storage and shipping facilities
    182.
    发明专利
    Floating body type liquefied natural gas production, storage and shipping facilities 审中-公开
    浮动身体类型液化天然气生产，储存和运输设施

    公开(公告)号：JP2011219051A

    公开(公告)日：2011-11-04

    申请号：JP2010093068

    申请日：2010-04-14

    Applicant: Mitsubishi Heavy Ind Ltd ,  三菱重工業株式会社

    Inventor： KAWAKITA CHIHARU ,  FUJINO YOSHIKAZU ,  YAMANE SHIGEKI

    IPC: B63B25/16 ,  B63B29/00 ,  B63B29/02 ,  B63B29/20 ,  B63B35/44

    CPC classification number: B63B25/16 ,  B63B2025/087 ,  F17C13/082 ,  F17C2201/0128 ,  F17C2201/052 ,  F17C2205/013 ,  F17C2221/033 ,  F17C2223/0161 ,  F17C2270/0105

    Abstract: PROBLEM TO BE SOLVED: To improve ease of use of escape routes.SOLUTION: The floating body type liquefied natural gas production, storage and shipping facilities include a plant 3 for generating liquefied gas from mined natural gas; tanks 5-1 to 5-3 for storing the liquefied gas; a floating body 2 for supporting the plant 3 and the tanks 5-1 to 5-3; and the escape routes. The escape routes include a plant-side escape route 26-i close to the plant 3; and a tank-side escape route 27-i close to the tanks 5-1 to 5-3. Hereat, the plant-side escape route 26-i is disposed below an upper deck 21. The plant 3 is disposed on the upper deck 21. With the floating body type liquefied natural gas production, storage and shipping facilities 1, thanks to the upper deck 21, a crew more surely avoids fire and blast due to fire or explosion occurred in the plant 3 when the crew passes through an escape route 17-i close to the plant 3.

    Abstract translation: 要解决的问题：提高逃生路线的易用性。

    解决方案：浮体式液化天然气生产，储存和运输设施包括用于从天然气开采液化气的工厂3; 用于储存液化气的罐5-1至5-3; 用于支撑植物3和罐5-1至5-3的浮体2; 和逃生路线。 逃生路线包括靠近植物3的植物侧逃生路线26-i; 以及靠近坦克5-1至5-3的坦克侧逃生路线27-i。 在这里，植物侧逃生路线26-i设置在上甲板21的下方。植物3设置在上甲板21上。利用浮体型液化天然气生产，储存和运输设施1，由于上层 甲板21，机组人员通过靠近工厂3的逃生路线17时，机组人员更可靠地避免因工厂3发生火灾或爆炸而发生火灾和爆炸。（C）2012年，JPO＆INPIT

    Sealing structure of pressure vessel
    183.
    发明专利
    Sealing structure of pressure vessel 有权
    压力容器密封结构

    公开(公告)号：JP2011102614A

    公开(公告)日：2011-05-26

    申请号：JP2009257932

    申请日：2009-11-11

    Applicant: Yachiyo Industry Co Ltd ,  八千代工業株式会社

    Inventor： TANI TATSUSHI ,  WATANABE YOSHIHIRO ,  NAKAMURA TERUYUKI ,  SATO SHOJI

    IPC: F17C1/16 ,  F17C1/06 ,  F17C13/04

    CPC classification number: F17C1/16 ,  F17C2201/0109 ,  F17C2201/0128 ,  F17C2201/0147 ,  F17C2203/0619 ,  F17C2203/066 ,  F17C2203/0665 ,  F17C2203/0668 ,  F17C2203/067 ,  F17C2205/0305 ,  F17C2205/0382 ,  F17C2209/2127 ,  F17C2209/2154 ,  F17C2209/221 ,  F17C2209/227 ,  F17C2209/234 ,  F17C2221/033 ,  F17C2223/0123 ,  F17C2223/036 ,  F17C2260/011 ,  F17C2260/012 ,  F17C2270/0168

    Abstract: PROBLEM TO BE SOLVED: To provide a sealing structure of a pressure vessel preventing a reduction in a sealing function when a high pressure is loaded to the pressure vessel. SOLUTION: The sealing structure of the pressure vessel 1 comprises a resin liner 2 storing gas or a liquid, a fiber reinforced resin layer 3 reinforcing the outer surface of the resin liner 2, and a metal mouthpiece part 4 protruded on the outer surface of the fiber reinforced resin layer 3 to be a filling/discharging port. In the resin liner, a tubular filling/discharging part 22 with a through-hole 24, which is protruded outward from the inside of the pressure vessel, is formed. On the outer peripheral surface of the filling/discharging part, connection structures 23, 43 mutually connected with the inner peripheral surface of the mouthpiece part, are formed. In the through-hole 24 of the filling/discharging part, a tubular member 100 made by using a material with strength higher than that of the resin liner, is inserted and fitted. When a tubular valve 60 for filling/discharging the gas or liquid is inserted in a valve insertion hole 102 arranged in the tubular member through the mouthpiece part, a seal member 80 is interposed between the outer periphery 61 of the valve and the inner periphery of the valve insertion hole. COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：提供当高压被加载到压力容器时防止密封功能降低的压力容器的密封结构。 解决方案：压力容器1的密封结构包括储存气体或液体的树脂衬垫2，加强树脂衬垫2的外表面的纤维增强树脂层3和在外部突出的金属接口部分4 纤维增强树脂层3的表面成为填充/排出口。 在树脂衬套中，形成有从压力容器的内部向外突出的具有通孔24的管状填充/排出部22。 在填充/排出部分的外圆周表面上，形成与接口部分的内周表面相互连接的连接结构23,43。 在填充/排出部分的通孔24中，插入并装配由使用强度高于树脂衬垫的材料制成的管状构件100。 当用于填充/排出气体或液体的管状阀60通过接口部分插入到设置在管状构件中的阀插入孔102中时，密封构件80插入在阀的外周边61和阀的外周 阀插入孔。 版权所有（C）2011，JPO＆INPIT

    Tank for storing cryogenic fluid and storable liquid fuel
    185.
    发明专利
    Tank for storing cryogenic fluid and storable liquid fuel 有权
    储存低温液体和有毒液体燃料的油箱

    公开(公告)号：JP2009292466A

    公开(公告)日：2009-12-17

    申请号：JP2009133034

    申请日：2009-06-02

    Applicant: Astrium Gmbh ,  アストリウム ゲゼルシャフト ミット ベシュレンクテル ハフツング

    Inventor： BEHRUZI KEI PHILIPP ,  NETTER GASTON

    IPC: B64G1/40

    CPC classification number: F17C13/088 ,  B64G1/402 ,  F17C2201/0104 ,  F17C2201/0128 ,  F17C2201/0157 ,  F17C2205/0302 ,  F17C2205/0397 ,  F17C2221/011 ,  F17C2221/012 ,  F17C2221/08 ,  F17C2223/0161 ,  F17C2227/0192 ,  F17C2227/0302 ,  F17C2227/0379 ,  F17C2260/011 ,  F17C2260/012 ,  F17C2260/027 ,  F17C2270/0194 ,  F17C2270/0197 ,  Y02E60/321

    Abstract: PROBLEM TO BE SOLVED: To secure sure phase separation at various kinds of acceleration from a low acceleration in a ballistic flight phase to a high acceleration in a high acceleration phase as generated by a space navigation system, for a cryogenic fluid and for a non-cryogenic fluid in a tank.
    SOLUTION: A gas supply and extraction device 2 provided with a substantially cylindrical casing 25 is arranged directly on a tank shell 1 at an upper part region of a tank and directly connected with the tank shell 1. The casing 25 is provided with: a row of opening parts 3 arranged on the circumferential side of the upper part region of the casing 25 and expanding in a trumpet-like form; and at least another opening part 9 arranged in a lower part region of the casing 25 and expanding in a trumpet-like form. The casing 25 is provided with at least one take-out pipe 29 connected to at least a discharge part.
    COPYRIGHT: (C)2010,JPO&INPIT

    Abstract translation: 要解决的问题：确保各种加速度下的相分离从弹道飞行阶段的低加速度到由空间导航系统产生的高加速阶段的高加速度，对于低温流体和 罐中的非低温流体。

    解决方案：设置有大致圆筒形壳体25的气体供应和提取装置2直接布置在罐壳体1的罐体的上部区域处并与罐壳体1直接连接。壳体25设置有 一排开口部3，其设置在壳体25的上部区域的周向侧，并以喇叭状的形式扩张; 以及至少另一个开口部9，其布置在壳体25的下部区域中并且以喇叭状的形式扩展。 壳体25设置有至少一个连接到排出部分的取出管29。 版权所有（C）2010，JPO＆INPIT

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