首页> 外国专利> Pressure vessel or rocket motor has annular casing segments inside which annular rubber seals are mounted, one of which has slit dilated by pressurized gas to form pressure seal

Pressure vessel or rocket motor has annular casing segments inside which annular rubber seals are mounted, one of which has slit dilated by pressurized gas to form pressure seal

机译:压力容器或火箭发动机具有环形壳体段,环形壳体段内安装有环形橡胶密封件,其中之一具有被压缩气体扩张的狭缝以形成压力密封

摘要

The pressure vessel comprises annular casing segments (144, 146). Annular rubber seals (190, 200) are mounted on the inside of each segment. One seal (190) has a slit (192) which separates a flexible section, which fits against the second seal, from the remainder of the ring. The pressurized gas in the vessel dilates the slit and forms a pressure seal between the two rings. Reinforcing pockets (220) are embedded in the rubber of the two rings. An Independent claim is included for a rocket motor constructed as described above.
机译:压力容器包括环形壳体段(144、146)。环形橡胶密封圈(190、200)安装在每个段的内部。一个密封件(190)具有狭缝(192),该狭缝(192)将与第二密封件配合的柔性部分与环的其余部分分开。容器中的加压气体使缝隙膨胀并在两个环之间形成压力密封。加强袋(220)嵌入两个环的橡胶中。包括如上所述构造的火箭发动机的独立权利要求。

著录项

  • 公开/公告号FR2824612A1

    专利类型

  • 公开/公告日2002-11-15

    原文格式PDF

  • 申请/专利权人 ALLIANT TECHSYSTEMS INC;

    申请/专利号FR20020005229

  • 发明设计人 MCGUIRE JOHN R;

    申请日2002-04-25

  • 分类号F16J15/10;F02K9/32;F16J12/00;

  • 国家 FR

  • 入库时间 2022-08-21 23:38:03

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