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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|