发明名称 AIRCRAFT CRUISE SPEED CONTROL
摘要 The present invention provides an alternative to the auto-throttle integrated in an aircraft autopilot by restricting the conditions in which the system operates. The proposed system removes the auto-throttle function from the autopilot system and gives it directly to the Full Authority Digital Engine Control (FADEC). A cruise control mode is available to the pilot only under stable flight conditions.
申请公布号 US2009326745(A1) 申请公布日期 2009.12.31
申请号 US20090550878 申请日期 2009.08.31
申请人 EMBRAER-EMPRESA BRASILEIRA DE AERONAUTICA S.A.;PRATT & WHITNEY CANADA CORP. 发明人 RAMOS DOMINGOS CAANDIDO WONG;DA SILVA ALEX SANDER FERREIRA;CASAGRANDE CELSO VALERIO BASTOS;CALANDRA SALVATORE;MORGAN KEITH
分类号 G06F7/00 主分类号 G06F7/00
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