The invention relates to test equipment and in particular to unmanned aerial vehicle airflow influence testing equipment, which comprises a machine body mechanism, a speed regulating mechanism, a linkage mechanism, an air volume regulating mechanism and a fan mechanism, wherein the equipment can provide air flow, wind power with different intensities, change the magnitude of the air flow and cleanthe equipment itself; the machine body mechanism is connected with the speed regulating mechanism; the machine body mechanism is connected with the linkage mechanism; the air volume regulating mechanism is connected with the machine body mechanism; the fan mechanism is connected with the machine body mechanism; and the fan mechanism is connected with the speed regulating mechanism.

    本发明涉及一种测试设备,更具体的说是一种无人机气流影响测试设备,包括机身机构、调速机构、联动机构、风量调节机构、风扇机构,设备能够提供气流,设备能够提供不同强度的风力,设备能够更改气流大小,设备能够清理自身,所述的机身机构与调速机构相连,机身机构与联动机构相连,风量调节机构与机身机构相连,风扇机构与机身机构相连,风扇机构与调速机构相连。


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    Titel :

    Unmanned aerial vehicle airflow influence testing equipment


    Weitere Titelangaben:

    一种无人机气流影响测试设备


    Beteiligte:
    WU TIELONG (Autor:in)

    Erscheinungsdatum :

    2020-04-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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