The invention discloses a saucer-shaped aircraft which comprises an aircraft support which is a supporting and bearing part of the whole aircraft, and an aircraft shell is arranged on the aircraft support and supported by the aircraft support; the double-rotor differential motor is a power part of the aircraft and is fixedly arranged on the inner side of the aircraft support, and a rotor wing is fixedly arranged at the output end of the double-rotor differential motor; the control wing structures are fixedly arranged on the periphery of the aircraft support and used for controlling the aircraft to ascend, descend, advance and retreat. According to the invention, a dual-rotor brushless motor driven by a coaxial differential bearing is used as a main power transmission mode, and the lifting control wing and the front and rear control wings control the aircraft to lift and advance and retreat; the space occupied by the transmission structure can be effectively reduced, and the weight of the transmission structure is reduced, so that the load can be effectively increased.

    本发明公开了一种碟形飞行器,包括:飞行器支架,所述飞行器支架为整个飞行器的支撑承载部分,飞行器外壳设置于飞行器支架上,并通过飞行器支架支撑;双转子差速电机,所述双转子差速电机为飞行器的动力部分,其固定设置于飞行器支架的内侧,且双转子差速电机的输出端上固定设置有旋翼;控制翼结构,所述控制翼结构固定设置于飞行器支架的四周,用于控制飞行器的升降及进退。本发明采用由同轴差速轴承传动的双转子无刷电机作为主动力传动方式,由升降控制翼及前后控制翼控制飞行器升降及进退;可有效的减少传动结构所占空间,并降低传动结构的重量,以达到可有效增加载荷。


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    Titel :

    Saucer-shaped aircraft


    Weitere Titelangaben:

    一种碟形飞行器


    Beteiligte:
    ZHOU JUNHE (Autor:in) / ZHOU LIYANG (Autor:in)

    Erscheinungsdatum :

    2023-07-28


    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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