The invention relates to the field of testing, in particular to a wing static load strength testing method which comprises the steps of providing a wing static load strength testing frame and placing the wing static load strength testing frame at the position of an aircraft wing to test the static load strength of the wing. The wing static load strength testing method provided by the invention is good in safety, high in integration level and small in occupied space, the loading mode is simple to operate, and the testing efficiency is improved.

    本发明涉及测试领域,尤其涉及一种机翼静载荷强度测试方法,所述方法包括提供一种机翼静载荷强度测试架以及将所述机翼静载荷强度测试架放置于飞行器机翼的位置,用于测试机翼的静载荷强度。本发明所提供的机翼静载荷强度测试方法,安全性好,集成度高,占用空间少,加载方式操作简单,提高测试效率。


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    Title :

    Wing static load strength testing method


    Additional title:

    机翼静载荷强度测试方法


    Contributors:
    TIAN YU (author) / DAI CHUNXU (author)

    Publication date :

    2023-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / 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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