发明名称 Rotor blades controlling device for small sized revolving wing i.e. drone, of helicopter, has supports carrying portion of electronic controls of actuators and connecting actuators to controls
摘要 <p>The device has actuators i.e. rotative servomotor (23), connected to a non rotating plate to carry out controlled translation displacement of the rotating plate in parallel to a rotor mast (1) and angularly around axes perpendicular to the mast. The actuators are placed at a top of a swash plate (10) and supported by supports (30) i.e. printed circuit boards, extending on both sides of the swash plate. The supports carry a portion of electronic controls (52) of the actuators and connect the actuators to the controls.</p>
申请公布号 FR2945269(A1) 申请公布日期 2010.11.12
申请号 FR20090002273 申请日期 2009.05.11
申请人 UNIVERSITE DE TECHNOLOGIE DE COMPIEGNE 发明人 BONNET STEPHANE;DE MIRAS JEROME;VIDOLOV BORIS
分类号 B64C27/605;B64C39/02 主分类号 B64C27/605
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