The invention relates to a flapping rotor aircraft capable of autonomously taking off. According to the technical scheme, the front end of a fuselage middle part (11) of a flapping rotor aircraft is fixedly connected with a head part (9) through connecting plates (10) on the two sides, and the rear end of the fuselage middle part (11) is fixedly connected with a tail rod (12); a front undercarriage (2) is fixed to the lower portions of the connecting plates (10) on the two sides, a driving mechanism (3) is installed in the middle of the connecting plates (10) on the two sides, two wings (4) are symmetrically installed on the outer sides of the connecting plates (10) on the two sides, a rear undercarriage (5) is installed on the rear portion of the lower portion of the fuselage middle part (11), a ducted fan system (6) is installed at the rear end of the fuselage middle part (11), and an empennage (7) is installed at the tail end of the tail rod (12). And the driving mechanism (3) completes the flapping, twisting and folding motion of the wings (4). And the ducted fan system (6) realizes steering lifting of the aircraft and provides power. The flapping rotor aircraft has the characteristics that the number of driving driving links is small, flapping-folding-twisting three-coupling motion can be achieved, the flying speed is high, the lifting force is large, and autonomous takeoff can be achieved.

    本发明涉及一种能自主起飞的扑旋翼飞行器。其技术方案是:所述扑旋翼飞行器的机身中部(11)前端通过两侧连接板(10)与头部(9)固定连接,机身中部(11)的后端与尾杆(12)固定连接;前起落架(2)固定在两侧连接板(10)的下部,驱动机构(3)安装在两侧连接板(10)的中间位置处,两个机翼(4)对称地安装在两侧连接板(10)的外侧,后起落架(5)安装在机身中部(11)的下部靠后处,涵道风扇系统(6)安装在机身中部(11)的后端,尾翼(7)安装在尾杆(12)的末端。驱动机构(3)完成机翼(4)的扑动扭转折叠运动。涵道风扇系统(6)实现飞行器的转向升降并提供动力。本发明具有驱动原动件少、能实现扑动‑折叠‑扭转三耦合运动、飞行速度快、升降力大和能自主起飞的特点。


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    Titel :

    Flapping rotor aircraft capable of autonomously taking off


    Weitere Titelangaben:

    一种能自主起飞的扑旋翼飞行器


    Beteiligte:
    HOU YU (Autor:in) / JIANG HOUQING (Autor:in) / WANG QIANG (Autor:in) / JIANG YIWEI (Autor:in) / LI HAONAN (Autor:in) / JIN ZIHAN (Autor:in)

    Erscheinungsdatum :

    09.11.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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