The invention relates to an aircraft nose landing gear taxiing and shimmy simulation test bed. The test bed comprises a test device main body structure, a power execution control mechanism, a vibration excitation mechanism and a vibration detection system. The method solves the problems of determination, contrast evaluation and detection analysis of the shimmy influence factors of the nose landing gear of the aircraft. The torsion steering engine is added, so that the turning condition of a ground plane can be simulated. The height-adjustable supporting cross beam can adapt to undercarriages of different sizes only by replacing the undercarriage clamp instead of replacing the whole frame, so that the use cost is greatly reduced. And more accurate data are provided for the design of the nose landing gear of the aircraft.

    本发明涉及一种飞机前起落架模拟滑跑摆振试验台,包括试验装置主体结构、动力执行控制机构、振动激励机构、振动检测系统。本发明解决飞机前起落架摆振影响因素的确定、对照评估,检测分析。增加了扭转舵机,可以模拟地面飞机转弯的情况。可调节高度的支撑横梁,只需替换起落架夹具,不用替换整个框架,能适应不同尺寸的起落架,大大降低使用成本。为飞机前起落架的设计提供更加准确的数据。


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    Title :

    Aircraft nose landing gear taxiing and shimmy simulation test bed


    Additional title:

    一种飞机前起落架模拟滑跑摆振试验台


    Contributors:
    ZHAO YANYING (author) / XIAO XIANGZHI (author) / WU HAO (author) / ZHU GUISHENG (author) / LIU YI'AN (author)

    Publication date :

    2025-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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