发明名称 LINK BETWEEN A COMBUSTION CHAMBER END WALL AND THE BOOSTER MOTOR NOZZLE
摘要 The invention concerns a link between a combustion chamber end wall (14) and the booster motor nozzle (50) mechanically linking the nozzle to the end wall at least axially, and a thermal barrier (43), and at least one gasket (32, 34) arranged in the interface (30) defined by the opposite adjacent surfaces of the end wall and the nozzle. The thermal barrier (40) includes at least one refractory fiber texture fanning a cord (42) wound in the interface around the longitudinal axis (A) of the chamber and the cord(s) is/are produced so as to provide circumferential continuity of the heat barrier (40).
申请公布号 UA81643(C2) 申请公布日期 2008.01.25
申请号 UA20050005240 申请日期 2003.12.01
申请人 SNECMA PROPULSION SOLIDE 发明人 RENOUST GILLES
分类号 F02K9/34;F02K9/08;F16J15/06;F16J15/08 主分类号 F02K9/34
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