The invention relates to fluid experiment equipment, in particular to unmanned aerial vehicle fluid experiment equipment. The equipment comprises a speed regulation wind power mechanism, an air volumecontrol mechanism and a sundry feeding mechanism. The equipment can provide wind power, provide air flows with different sizes and change the air volume, and the equipment can automatically add somesundries to test an unmanned aerial vehicle. The speed regulation wind power mechanism is connected with the air volume control mechanism, and the air volume control mechanism is connected with the sundry feeding mechanism.

    本发明涉及一种流体实验设备,更具体的说是一种无人机流体实验设备,包括调速风力机构、风量控制机构、杂物给料机构,设备能够提供风力,设备能够提供大小不同的气流,设备能够改变风量,设备能够自动加一些杂物来测试无人机,所述的调速风力机构与风量控制机构相连,风量控制机构与杂物给料机构相连。


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    Title :

    Unmanned aerial vehicle fluid experiment equipment


    Additional title:

    一种无人机流体实验设备


    Contributors:
    WU TIELONG (author)

    Publication date :

    2020-04-10


    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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