The invention relates to the field of aircrafts, in particular to an adjustable aircraft which comprises an aircraft body, at least four multi-direction adjusting mechanisms are arranged on the peripheral side of the aircraft body, the fixed ends of the multi-direction adjusting mechanisms are fixedly connected with the aircraft body, and the movable ends of the multi-direction adjusting mechanisms are fixedly connected with one ends of connecting arms. A propeller assembly is installed at the other end of the connecting arm, a controller is installed on the aircraft body, and the controller is electrically connected with the propeller assembly and the multi-direction adjusting mechanism. The propeller is adaptively adjusted at multiple angles, so that the aircraft can be operated and adjusted more flexibly.

    本发明设计飞行器领域,具体的涉及一种可调节飞行器,包括飞行器主体,所述飞行器主体周侧设有至少四个多向调节机构,所述多向调节机构的固定端与所述飞行器主体固定连接,所述多向调节机构的活动端固定连接有连接臂的一端,所述连接臂的另一端安装有螺旋桨总成,所述飞行器主体上安装有控制器,所述控制器与所述螺旋桨总成、多向调节机构电连接。本发明通过使螺旋桨在多个角度上进行适应性的调整,以使得飞行器可以更加灵活的进行操作调整。


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    Titel :

    Adjustable aircraft


    Weitere Titelangaben:

    一种可调节飞行器


    Beteiligte:
    HE JIAN (Autor:in)

    Erscheinungsdatum :

    06.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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