A wing body fusion tilting rotorcraft comprises a wing body fusion fuselage, a tilting mechanism, an attitude control rotor combination, a power rotor combination, a flight controller, a battery and an electronic speed regulator. According to the invention, a fuselage structure with fused wing bodies is adopted, so that the air resistance in the flight process can be greatly reduced, and meanwhile, a relatively large lift force is obtained. The unmanned aerial vehicle further comprises a tilting mechanism, the direction of the power rotors can be adjusted by 90 degrees, upward pull force can be provided during take-off and landing, and thrust consistent with the flight direction can be provided before the rotors tilt during horizontal flight. The attitude control rotor wing combination isused for adjusting the flight attitude of the unmanned aerial vehicle, the flight control system controls the attitude of the vehicle body, and the flight attitude and the flight direction of the rotorcraft are adjusted.

    一种翼身融合倾转旋翼机,包括翼身融合机身、倾转机构、姿态控制旋翼组合、动力旋翼组合、飞行控制器、电池、电子调速器。该发明采用了翼身融合的机身结构,可以大幅减少飞行过程中的空气阻力,同时获得较大的升力。该发明还包括一个倾转机构,可将动力旋翼的方向进行90°的调节,在起降时可以提供向上的拉力,在水平飞行时则可以将旋翼倾转向前提供与飞行方向一致的推力;该发明同时使用姿态控制旋翼组合调节无人机飞行姿态,由飞控系统通过对其控制来实现对机身姿态的控制,调节旋翼机的飞行姿态和飞行方向。


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    Titel :

    Wing body fusion tilting rotorcraft


    Weitere Titelangaben:

    一种翼身融合倾转旋翼机


    Beteiligte:
    YU YIYANG (Autor:in)

    Erscheinungsdatum :

    02.06.2020


    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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