According to the technical scheme, the electric rotor configuration characteristic multifunctional test bench is characterized in that the electric rotor configuration characteristic multifunctional test bench comprises a rack base, a rack platform and a tilting mechanism, the rack platform is rotationally connected with the rack base, the tilting mechanism is arranged on the rack platform, a tilting rotor is further connected to the tilting mechanism, and the tilting rotor is arranged on the rack base. The rack base is used for controlling rotation and pitching rotation adjustment of the rack platform; and the tilting mechanism is used for controlling the tilting rotor to simulate tilting so as to adjust the angle of the tilting rotor, simulate the aerodynamic characteristics of the aircraft in a pitching state, static or dynamic flight and simulate the attitude of the aircraft in the flight process. And the real stress condition and other physical properties of the rotor wing under different flight attitudes can be fully simulated.

    本发明公开了一种电动旋翼构型特性多功能试验台,其技术方案要点是包括台架基座、台架平台和倾转机构,台架平台与所述台架基座转动连接,倾转机构设置于台架平台上,倾转机构上还连接有倾转旋翼,台架基座用于控制台架平台旋转和俯仰转动调节;倾转机构用于控制倾转旋翼模拟倾转,以调节倾转旋翼的角度,并模拟飞行器在俯仰状态、静态或动态飞行时的气动特性和模拟飞行器飞行过程的姿态。具有充分模拟旋翼在不同飞行姿态下的真实受力情况和其他的物理性能。


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    Title :

    Electric rotor configuration characteristic multifunctional test bench


    Additional title:

    电动旋翼构型特性多功能试验台


    Contributors:
    YANG CHAO (author) / LI YIHENG (author) / LIN BO (author) / ZHAO MENG (author) / SHIN JIN (author)

    Publication date :

    2024-11-29


    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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