The invention relates to a tilting mechanism of an electric vertical take-off and landing aircraft, which comprises an upper fixed support arm, a lower fixed support arm and a motor seat, the upper fixed support arm and the lower fixed support arm are fixedly supported in a nacelle of the aircraft, a power mechanism is arranged on the lower fixed support arm, and the power mechanism is connected with the motor seat through a transmission mechanism. And the output of the control power mechanism drives the motor base to tilt. The aircraft with the tilting mechanism can take off and land conventionally in an area with an airport; under the condition that runway conditions are insufficient, vertical take-off and landing can be achieved.

    本发明涉及一种电动垂直起降飞行器的倾转机构,包括上固定支臂、下固定支臂、电机座,上固定支臂和下固定支臂固支于飞行器短舱内,下固定支臂上设置有动力机构,动力机构通过传动机构与电机座连接,控制动力机构的输出带动电机座倾转。具有该倾转机构的飞行器在有机场的地区,可以常规起降;在跑道条件不足的情况下,可以垂直起降。


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    Title :

    Tilting mechanism of electric vertical take-off and landing aircraft


    Additional title:

    一种电动垂直起降飞行器的倾转机构


    Contributors:
    ZHANG ZHIWEI (author) / YANG YOUXU (author) / WU YIFEI (author) / DUAN YIWEI (author)

    Publication date :

    2024-07-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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