The invention relates to the field of static load detection, and discloses an aircraft landing gear static load detection device which comprises a detection platform, a fixing assembly and a loading assembly are arranged on the detection platform, the fixing assembly fixes a landing gear body, the loading assembly applies a load to the landing gear body, and the aircraft landing gear static load detection device further comprises a balance maintaining assembly arranged on the loading assembly. When the loading assembly applies a load to the undercarriage main body, the balance maintaining assembly is used for maintaining the loading assembly in a horizontal placement state; according to the aircraft landing gear static load detection device, through arrangement of the balance maintaining assembly, when the landing gear main body deforms, the deformed landing gear main body extrudes the loading assembly, and the loading assembly inclines and deflects, the balance maintaining assembly adjusts the loading assembly to recover to a horizontal placement state; therefore, the situation that the static load test data of the undercarriage main body is inaccurate due to the fact that the loading assembly is in an inclined state is avoided.

    本发明涉及静力载荷检测领域,公开了一种飞机起落架静力载荷检测装置,包括检测平台,检测平台上设置有固定组件与加载组件,固定组件固定起落架主体,加载组件向起落架主体施加载荷,还包括设置在加载组件上的平衡维持组件,当加载组件向起落架主体施加载荷时,平衡维持组件用于维持加载组件保持水平放置状态;该飞机起落架静力载荷检测装置,通过设置平衡维持组件,当起落架主体发生变形,变形的起落架主体挤压加载组件,导致加载组件出现倾斜偏转的情况时,平衡维持组件调整加载组件恢复成水平放置状态,从而避免了加载组件出现倾斜状态,导致起落架主体的静力载荷试验数据不准确的情况发生。


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear static load detection device


    Additional title:

    一种飞机起落架静力载荷检测装置


    Contributors:
    TAO WEI (author) / YAN CHUANSHENG (author) / WANG YAO (author) / WANG XIAOGANG (author)

    Publication date :

    2025-02-07


    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



    LOAD DETECTION IN AN AIRCRAFT LANDING GEAR

    BENNETT IAN | European Patent Office | 2015

    Free access

    LANDING LOAD MONITOR FOR AIRCRAFT LANDING GEAR

    YATES MICHAEL STUART / KEEN PHILLIP | European Patent Office | 2015

    Free access


    Aircraft landing gear aerodynamic load simulation loading device

    ZHENG JIANFEN / PENG MUPING / WU YONGQIANG et al. | European Patent Office | 2025

    Free access

    LANDING GEAR OF AIRCRAFT AND AIRCRAFT COMPRISING LANDING GEAR

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2018

    Free access