发明名称 Valve system for a gas turbine engine
摘要 A valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary airflow into the primary gas flow path and control airflow injected from a higher pressure plenum into a lower pressure flowpath.
申请公布号 US8402744(B2) 申请公布日期 2013.03.26
申请号 US20080053591 申请日期 2008.03.22
申请人 SCHIRTZINGER GARY A.;PRATT & WHITNEY ROCKETDYNE, INC. 发明人 SCHIRTZINGER GARY A.
分类号 F02K1/00;B63H25/46 主分类号 F02K1/00
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