发明名称 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
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.
申请公布号 FR2824612(A1) 申请公布日期 2002.11.15
申请号 FR20020005229 申请日期 2002.04.25
申请人 ALLIANT TECHSYSTEMS INC 发明人 MCGUIRE JOHN R
分类号 B64G1/00;F02K9/10;F02K9/32;F02K9/34;F16J12/00;F42B15/36;(IPC1-7):F16J15/10 主分类号 B64G1/00
代理机构 代理人
主权项
地址
您可能感兴趣的专利