ADAPTIVE FAIL-FIXED SYSTEM FOR FADEC CONTROLLED GAS TURBINE ENGINES
摘要
<p>A gas turbine engine control system includes a module operable to fail-fix the gas turbine engine to one of a multiple of pre-determined modes in response to failure of an automatic control.</p>
申请公布号
WO2010056241(A1)
申请公布日期
2010.05.20
申请号
WO2008US83330
申请日期
2008.11.13
申请人
SIKORSKY AIRCRAFT CORPORATION;SWEET, DAVID H.;SILDER, STEPHEN H.
