The invention discloses a loading method and loading device for an aircraft engine frame fatigue test. The method comprises the steps of setting a plurality of lifting points on a truss structure of the loading device, and respectively simulating the connection between an aircraft engine and an engine frame; and arranging a heading loading support, a vertical loading support and a lateral loadingsupport on the truss structure of the loading device, and applying course load, vertical bending moment, vertical load, lateral bending moment, lateral load and course bending moment to the loading device. The loading device meets the real gravity center position of the engine, simulates the real connection relationship between the engine and the engine frame, more accurately simulates the loadingcondition of the engine frame in the flight process of an aircraft, and effectively improves the reliability and authenticity of a test result.

    一种飞机发动机架疲劳试验加载方法及加载装置,在加载装置的桁架结构上设有多个吊点,分别模拟飞机发动机与发动机架的连接;在加载装置的桁架结构上设有航向加载支座、垂向加载支座和侧向加载支座,向加载装置施加航向载荷和垂向弯矩、垂向载荷和侧向弯矩、侧向载荷和航向弯矩,该加载装置满足发动机真实的重心位置,模拟发动机与发动机架真实的连接关系,更加准确的模拟发动机架在飞机飞行过程中的受载情况,有效提高了试验结果的可靠性和真实性。


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    Titel :

    Loading method and loading device for aircraft engine frame fatigue test


    Weitere Titelangaben:

    一种飞机发动机架疲劳试验的加载方法及加载装置


    Beteiligte:
    HUO WENHUI (Autor:in) / FU YOUBO (Autor:in) / MENG YAOWEI (Autor:in)

    Erscheinungsdatum :

    13.10.2020


    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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