发明名称 Method for the control of aero gas turbine engines
摘要 The exchange, removal or addition, as applicable, of media and/or power is provided between the individual shafts of an engine, between individual engines and between the engines and the aircraft. Thus, additional degrees of freedom are provided, enabling engine parameters to be addressed in terms of a reduction or avoidance of negative resonances or beats. It also provides an ability to alter thrust from engines of a multi-engined aircraft to reduce rudder trim.
申请公布号 US6712314(B2) 申请公布日期 2004.03.30
申请号 US20010012376 申请日期 2001.12.12
申请人 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 STEPHAN VOLKER
分类号 B64C11/50;B64D31/12;F02C9/42;(IPC1-7):B64D31/00;F02D9/00 主分类号 B64C11/50
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