发明名称 Valve system for a gas turbine engine
摘要 A valve system (30) intermediate a secondary flow path (C) and a primary flow path (E) to selectively communicate secondary airflow into the primary gas flow path (E) and control airflow injected from a higher pressure plenum into a lower pressure flowpath comprises a contoured frame (34) and a shaped door (32) pivotable relative to the frame (34).
申请公布号 EP2103784(B1) 申请公布日期 2014.08.27
申请号 EP20090250649 申请日期 2009.03.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SCHIRTZINGER, GARY A.
分类号 F01D17/10;F02K1/30;F02K1/38;F02K3/06;F02K3/075 主分类号 F01D17/10
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