A vertical landing and take-off aircraft (VTOL) transitions from a vertical takeoff state to a cruise state where the vertical takeoff state uses propellers to generate lift and the cruise state useswings to generate lift. The aircraft has an M-wing configuration with propellers located on the wingtip nacelles, wing booms, and tail boom. The wing boom and/or the tail boom can include boom controleffectors. Hinged control surfaces on the wings, tail boom, and tail tilt during takeoff and landing to yaw the vehicle. The boom control effectors, cruise propellers, stacked propellers, and controlsurfaces can have different positions during different modes of operation in order to control aircraft movement and mitigate noise generated by the aircraft.

    垂直起降(VTOL)飞行器从垂直起飞状态过渡至巡航状态,其中垂直起飞状态使用螺旋桨来产生升力,且巡航状态使用机翼来产生升力。该飞行器具有M形机翼构型,其中螺旋桨位于翼梢吊舱、机翼吊杆和尾部吊杆上。机翼吊杆和/或尾部吊杆可以包括吊杆控制执行器。机翼、尾部吊杆和尾部上的铰接的控制表面在起飞和降落期间倾斜以使交通工具偏航。吊杆控制执行器、巡航螺旋桨、堆叠式螺旋桨和控制表面在不同的操作模式期间可以具有不同的位置,以控制飞行器的运动并减轻由飞行器产生的噪声。


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    Title :

    VTOL M-WING CONFIGURATION


    Additional title:

    垂直起降M形机翼构型


    Contributors:
    MOORE MARK (author) / BADALAMENTI JOHN (author) / VILLA IAN (author) / WARMOTH ADAM (author) / JOSEPHSON DAVID (author)

    Publication date :

    2020-07-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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