The invention relates to an aircraft component test supporting end load measuring structure and a measuring method, the measuring structure comprises an end plate, a mounting plate and a supporting frame, an aircraft component is fixed on the end plate, the mounting plate is fixed on the supporting frame, the end plate and the mounting plate are connected through a plurality of load sensors, and the load sensors are connected with the supporting frame. Loads are transmitted to the mounting plates through the end plates, the load sensors measure the loads of the supporting ends of the aircraft parts, the course total load Fx, the vertical total load Fy and the lateral total load Fz of the test supporting ends of the aircraft parts are obtained, the loads measured by the load sensors in all directions are multiplied by the coordinates of the corresponding load sensors and then summed, and the total load Fx, the total load Fy and the total load Fz are calculated. And obtaining the course total distance Mx, the vertical total distance My and the lateral total distance Mz of the aircraft component test support end.

    一种飞机部件试验支持端载荷测量结构及测量方法,该测量结构含有端板、安装板和支撑架,所述的飞机部件固定在端板上,所述的安装板固定在支撑架上,在端板和安装板之间通过多个载荷传感器连接,飞机部件经过端板将载荷传递各安装板,载荷传感器测量飞机部件支持端的载荷,得到飞机部件试验支持端的航向总载Fx、垂向总载Fy和侧向总载Fz,将载荷传感器所测的各向载荷与对应载荷传感器的坐标相乘后求和,得到飞机部件试验支持端的航向总距Mx、垂向总距My和侧向总距Mz。


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    Title :

    Aircraft component test support end load measurement structure and measurement method


    Additional title:

    一种飞机部件试验支持端载荷测量结构及测量方法


    Contributors:
    WANG QIANG (author) / LI ZHEN (author) / HUO WENHUI (author) / WANG CHUANGQI (author) / WANG LEISHUO (author)

    Publication date :

    2024-09-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE / 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 / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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