The invention belongs to the field of aircraft static test load loading design, and particularly relates to an aircraft static test load loading method which comprises the following steps: applying aconcentrated load to an aircraft; applying a course balancing load to the aircraft, so that the course of the aircraft is balanced, and a vertical balancing load is applied, so that the bending momentof an examination part on the aircraft reaches a preset value. According to the method, the concentrated load is applied to the airplane, namely, the loaded state of the airplane for bearing the concentrated load is simulated, the static test of the airplane for bearing the concentrated load is carried out, the course balancing load is applied to the airplane, the course of the airplane is balanced, and the vertical balancing load is applied to the airplane, so that the bending moment of an examination part on the airplane reaches a preset value; effective application of the load of the assessment part on the airplane can be realized, and the assessment part on the airplane can be assessed.

    本申请属于飞机静力试验载荷加载设计领域,具体涉及一种飞机静力试验载荷加载方法,包括:在飞机上施加集中载荷;在飞机上施加航向配平载荷,使飞机航向平衡,以及,施加垂向配平载荷,使飞机上考核部位的弯矩达到预定值。上述方法中设计在飞机上施加集中载荷,即模拟飞机承受集中载荷的受载状态,进行飞机承受集中载荷下的静力试验,在飞机上施加航向配平载荷,使飞机航向平衡,以及,在飞机上施加垂向配平载荷,使飞机上考核部位的弯矩达到预定值,可实现对飞机上考核部位载荷的有效施加,对飞机上考核部位进行考核。


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    Titel :

    Aircraft static test load loading method


    Weitere Titelangaben:

    一种飞机静力试验载荷加载方法


    Beteiligte:
    SHANG JIN (Autor:in)

    Erscheinungsdatum :

    2021-04-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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