发明名称 Cooling system for a convergent divergent nozzle
摘要 The engine has an annular flow straightening chamber (23) that is delimited at its downstream by a conical ring (16). A piercing (21) supplies cooling air to the chamber, and is formed in a leading wall (22) between the chamber and downstream end of an annular passage (6). A distribution compartment (30) is connected to and surrounds the chamber.
申请公布号 EP1522680(A1) 申请公布日期 2005.04.13
申请号 EP20040292285 申请日期 2004.09.23
申请人 SNECMA 发明人 CURTELIN, RAPHAEL;DOUSSINAULT, MARC;LAPERGUE, GUY;DURAND, DIDIER
分类号 F01D9/06;F02K1/12;F02K1/30;F02K1/80;F02K1/82;(IPC1-7):F01D9/06 主分类号 F01D9/06
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