The invention belongs to the technical field of vertical take-off and landing aircrafts, and particularly relates to a vertical take-off and landing electric aircraft test platform. The technical problem that an existing vertical take-off and landing aircraft is high in test, research and development cost in research and development is solved. The vertical take-off and landing electric aircraft test platform comprises a platform frame and a plurality of propeller motors, and is characterized in that the platform frame is provided with a mounting chamber for placing energy, equipment and a balancing weight, the plurality of propeller motors are located at the top of the platform frame, and the plurality of propeller motors are arranged around the mounting chamber; an adjusting device capable of adjusting the distance between the propeller motor and the mounting chamber is arranged between the propeller motor and the platform frame, and a cushioning structure capable of cushioning the falling platform frame is arranged at the bottom of the platform frame. The test research and development cost of the vertical take-off and landing aircraft in research and development is reduced.

    本发明属于垂直起降飞机技术领域,具体涉及一种垂直起降电动飞机测试平台。它解决了现有垂直起降飞机在研发中测试研发成本高的等技术问题。本垂直起降电动飞机测试平台包括平台框架和若干个螺旋桨电机,其特征在于,所述平台框架上具有用于放置能源、设备及配重块的安装室,所述若干个螺旋桨电机位于平台框架的顶部,且若干个螺旋桨电机围绕安装室设置,所述螺旋桨电机与平台框架之间设有能够调节螺旋桨电机相对于安装室之间距离的调节装置,所述平台框架底部设有能够对下落的平台框架进行缓震的缓震结构。本发明降低了垂直起降飞机在研发中的测试研发成本。


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    Title :

    Vertical take-off and landing electric aircraft test platform


    Additional title:

    垂直起降电动飞机测试平台


    Contributors:
    PEI JIANXUN (author)

    Publication date :

    2021-04-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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