The invention relates to the technical field of aircraft assembly, in particular to a calibration auxiliary method for installation of aircraft avionics equipment, and the method comprises the steps: calculating the simulated pose coordinates of an adjustment point through avionics equipment simulated pose coordinate calculation based on a pitch angle and a roll angle; solving an optimal gasket specification type selection scheme of the adjustment points through pose adjustment optimization; and finally, adjusting the gasket according to the optimal scheme. Through the method, the problems of low efficiency, high labor intensity and large personal error can be effectively solved.

    本发明涉及飞机装配技术领域,特别是涉及一种飞机航电设备安装的校准辅助方法,通过基于俯仰角和横滚角的航电设备模拟位姿坐标解算,计算调整点的模拟位姿坐标;通过位姿调整优化,求解调整点的垫圈规格选型最优方案;最终按最优方案实施垫圈调整。通过本方法,能有效解决效率低、劳动强度大和人为误差大的问题。


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    Titel :

    Calibration auxiliary method for installation of aircraft avionics equipment


    Weitere Titelangaben:

    一种飞机航电设备安装的校准辅助方法


    Beteiligte:
    ZHENG BO (Autor:in) / YU YANG (Autor:in) / XIE YUN (Autor:in) / LIU KEFEI (Autor:in) / ZHU XUSHENG (Autor:in) / FENG HUI (Autor:in) / TANG WEICHEN (Autor:in) / NI CHENG (Autor:in) / MIAO XINGBO (Autor:in)

    Erscheinungsdatum :

    2021-06-04


    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 / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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