发明名称 Two-piece aft closure for a rocket motor case
摘要 An aft closure assembly manufactured from two separate and distinct pieces made from different materials is provided for a rocket motor case. The aft closure assembly includes at least a retaining ring piece made from a first material similar to or having a coefficient of thermal expansion similar to that of the motor case. The aft closure assembly includes a blast tube and closure piece that can be manufactured from a second material that does not need to be similar to nor have a coefficient of thermal expansion similar to the motor case and retaining ring piece. This is possible because the blast tube and closure piece includes a face seal that seals against a face of the retaining ring.
申请公布号 US7717280(B2) 申请公布日期 2010.05.18
申请号 US20070953717 申请日期 2007.12.10
申请人 AEROJET-GENERAL CORPORATION 发明人 WALLACE WILLIAM M.;GAGNE MICHAEL T.;COPPERTHITE CHESTER A.
分类号 B65D53/06;B65D51/16;F16J15/02 主分类号 B65D53/06
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