发明名称 GAS TURBINE BRAKING APPARATUS AND METHOD
摘要 A device is provided which can serve one or more of the multiple functions of impeding rotation of a shaft de-coupled turbine rotor, selectively impeding rotation of a first spool of the engine, for example to permit a second spool to generate power for use in ground operation, and facilitating reduced aircraft ground speed.
申请公布号 EP1787010(A4) 申请公布日期 2011.03.09
申请号 EP20050777152 申请日期 2005.08.18
申请人 PRATT & WHITNEY CANADA CORP. 发明人 TRUMPER, RONALD;ANDERSON, STEPHEN ARTHUR;DOOLEY, KEVIN A.;BRAND, JOSEPH H.
分类号 F01D21/00;F01D21/04;F02C7/00;F02C7/36;F16D59/00 主分类号 F01D21/00
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