The invention discloses a cross double-rotor helicopter lift force testing device. The device comprises: a rack; a sensor which is arranged on the rack; a collector which is in communication connection with the sensor; a mounting plate which is arranged at the top of the sensor and is connected with the sensor; bases which are arranged on the mounting plate, wherein the mounting positions of the bases on the mounting plate can be changed, so that the distance between the different bases can be changed; a plurality of rotating bodies which are arranged on the base in a one-to-one correspondencemanner, wherein the arrangement angles of the rotating bodies on the bases can be changed, so that the included angles between power shafts connected to the rotating bodies and the mounting plate canbe changed. The cross double-rotor helicopter lift force testing device can be used for testing the lift force of the rotors of the crossed double-rotor helicopter.

    本申请公开了一种交叉双旋翼直升机升力测试装置,包括:台架;设置在所述台架上的传感器;与所述传感器通信连接的采集器;设置在所述传感器的顶部并与所述传感器连接的安装板;设置在所述安装板上的多个底座,所述底座在所述安装板上的安装位置能够发生改变,以使不同所述底座之间的间距能够改变;一对一的设置在所述底座上的多个旋转体,所述旋转体在所述底座上的设置角度能够发生改变,以使连接在所述旋转体上的动力轴与所述安装板之间的夹角能够改变。上述的交叉双旋翼直升机升力测试装置,能够实现交叉双旋翼直升机的旋翼升力的测试。


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    Titel :

    Cross double-rotor helicopter lift force testing device


    Weitere Titelangaben:

    一种交叉双旋翼直升机升力测试装置


    Beteiligte:
    LI JINGYANG (Autor:in) / WANG XIANYU (Autor:in) / YIN MINGWEI (Autor:in) / HAI RIHAN (Autor:in) / BAO CHANGCHUN (Autor:in)

    Erscheinungsdatum :

    2020-06-02


    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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