发明名称 Aircraft equipped with rotating piston engines and counter-rotating propellers
摘要 The aircraft rotating piston engines with counter-rotating propellers (3) are placed in a cradle around the airframe. either on each side of the fuselage or above each wing. The engines and propellers are mounted on a transverse shaft (4). The transverse shaft is displaced frontwards or rearwards on runners (5) integral with the fuselage by electro-mechanical or hydraulic actuators (6). Displacement of the weight of the engines and the propellers towards the front or rear re-establishes a correct centring for stability if required.
申请公布号 FR2735098(A1) 申请公布日期 1996.12.13
申请号 FR19950006805 申请日期 1995.06.09
申请人 DELMOTTE DIDIER PAUL JEAN 发明人
分类号 B64D27/02;(IPC1-7):B64D27/02;B64D29/06;B64D35/06;B64C17/00 主分类号 B64D27/02
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