The invention discloses a model parameter equivalent correction method for aircraft tire rigidity testing, and relates to the technical field of aircraft testing, and the method comprises the following steps: S1, test system construction; s2, carrying out a test experiment; and S3, data fitting. According to the invention, the rigidity test of the aircraft tire under the influence of various motion states can be realized, and the equivalent aircraft tire rotating speed and equivalent vibration frequency which can be completed under the laboratory condition can be obtained according to the real rotating speed and vibration frequency of the aircraft tire equivalently, and are finally imported into a shimmy analysis model. The precision of undercarriage shimmy analysis can be improved, and the precision of aircraft taxiing stability analysis can be improved.

    本发明公开了一种飞机轮胎刚度测试用模型参数等效修正方法,涉及飞机测试技术领域,包括以下步骤:S1、测试系统构建;S2、测试试验;S3、数据拟合。本发明能够实现飞机轮胎多种运动状态影响下的刚度测试,并根据飞机轮胎真实的转速以及振动频率等效得到能够在试验室条件下完成的等效飞机轮胎转速以及等效振动频率,最终导入到摆振分析模型中,能够提高对起落架摆振分析的精度,提高飞机滑跑稳定性分析精度。


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    Titel :

    Model parameter equivalent correction method for aircraft tire rigidity test


    Weitere Titelangaben:

    一种飞机轮胎刚度测试用模型参数等效修正方法


    Beteiligte:
    LIU CHONGCHONG (Autor:in) / WANG BINWEN (Autor:in) / ZHANG YU (Autor:in) / LIU SHENGLI (Autor:in) / LI WEIMING (Autor:in) / MA XIAOLI (Autor:in) / BAI CHUNYU (Autor:in) / WANG JIZHEN (Autor:in)

    Erscheinungsdatum :

    08.12.2023


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



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