The invention discloses a full-aircraft drop test method and a full-aircraft drop test device for a principle prototype of a large anti-back headstand angle aircraft, and particularly relates to a method and a test device for keeping the time of the principle prototype consistent with the time of a landing dynamic process of an original aircraft in a drop test. On the basis that lifting and releasing of a small-size principle prototype can be achieved, equivalent simulation of dynamic response in the time period from the main landing gear to the front landing gear in the landing process of the principle prototype can be achieved in cooperation with a shrinkage specific gravity acceleration loading method and an aerodynamic force applying method, and therefore a full-aircraft drop test can be conducted in a limited site. According to the technical scheme, the device comprises a lifting and releasing device, a shrinkage specific gravity acceleration applying device, an aerodynamic force applying device and a force measuring platform; according to the invention, the consistency of a small-size principle prototype in the time period from the main landing gear to the front landing gear to the original aircraft can be realized.

    本发明公开了一种大防后倒立角飞行器原理样机全机落震试验方法与装置,具体涉及一种实现原理样机在落震试验中与原飞行器保持着陆动态过程时间一致的方法与试验装置。在可实现小尺寸原理样机提升与释放的基础上,配合缩比重力加速度的加载方法和空气动力的施加方法,可实现原理样机着陆过程中主起落架触地到前起落架触地时间段的动态响应的等效模拟,以实现在有限场地下进行全机落震试验。本发明的技术方案为:包括提升与释放装置、缩比重力加速度施加装置、空气动力施加装置以及测力平台;本发明可实现小尺寸原理样机在主起落架触地到前起落架触地时间段与原飞行器保持时间上的一致性。


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    Title :

    Full-aircraft drop test method and device for principle prototype of large-anti-back headstand angle aircraft


    Additional title:

    一种大防后倒立角飞行器原理样机全机落震试验方法与装置


    Contributors:
    WEI XIAOHUI (author) / GAO TIANCHI (author) / FANG XINGBO (author) / LIU YICHAO (author) / NIE HONG (author)

    Publication date :

    2025-01-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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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