The invention belongs to the technical field of aviation ground tests, and discloses a helicopter blade root section static test device which comprises an internal force system frame assembly, a centrifugal force direction loading assembly, a flapping force direction loading assembly, a shimmy force actuator fixing assembly and a test piece fixing assembly. The test piece fixing assembly is arranged on the front section of the inner side of the internal force system frame assembly, the centrifugal force direction loading assembly is arranged on the rear section of the inner side of the internal force system frame assembly to apply simulated centrifugal force to a test piece, and the shimmy force actuator fixing assembly is arranged on the left side or the right side of the inner side of the internal force system frame assembly to apply simulated shimmy force to the test piece. The flapping force direction loading assembly is arranged at the top end of the inner side of the internal force system frame assembly and applies simulated flapping force to the test piece. According to the invention, loads in three directions of centrifugal force, flapping force and shimmy force can be applied to a test piece with a large structure size under the action of a large load, so that a static failure mode, a static strength dangerous part and a static strength characteristic of a blade root section can be obtained.

    发明属于航空地面试验技术领域,公开了一种直升机桨叶根段静力试验装置,包括内力系统框架组件、离心力方向加载组件、挥舞力方向加载组件、摆振力作动器固定组件和试验件固定组件;试验件固定组件设在内力系统框架组件的内侧前段,离心力方向加载组件设在内力系统框架组件的内侧后段对试验件施加模拟的离心力,摆振力作动器固定组件设在内力系统框架组件的内侧左边或者右边对试验件施加模拟的摆振力,挥舞力方向加载组件设在内力系统框架组件的内侧顶端对试验件施加模拟的挥舞力。本发明可以在大载荷作用下对结构尺寸大的试验件进行离心力、挥舞力、摆振力三个方向载荷施加,得出桨叶根部段的静力破坏模式和静强度危险部位以及静强度特性。


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    Title :

    Helicopter blade root section static test device


    Additional title:

    一种直升机桨叶根段静力试验装置


    Contributors:
    LIU SIYI (author) / CHEN QINGTONG (author) / ZHOU XIN (author) / ZHANG PINGFU (author)

    Publication date :

    2023-03-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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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