According to the SSPC power output-based redundancy undercarriage control method, a first electromechanical management system and a second electromechanical management system which are mutually redundant are included, and the first electromechanical management system is connected with a first retracting power control module and a first releasing power control module; the second electromechanical management system is connected with a second retracting power control module and a second releasing power control module, and the first retracting power control module and the second retracting power control module are used for retracting the airborne auxiliary system. The priority of the airborne auxiliary system controlled by the first retracting power control module is higher than that of the airborne auxiliary system controlled by the second retracting power control module, and the second releasing power control module and the second releasing power control module are respectively used for releasing the airborne auxiliary system. And the placement of the auxiliary system is determined according to the state information, so that the use safety of the airborne function is improved.

    本发明的基于SSPC功率输出的多余度起落架控制方法,包括互为余度的第一机电管理系统和第二机电管理系统,所述第一机电管理系统连接有第一收起功率控制模块和第一放落功率控制模块,所述第二机电管理系统连接有第二收起功率控制模块和第二放落功率控制模块,第一收起功率控制模块和第二收起功率控制模块分别用于机载辅助系统的收起,且第一收起功率控制模块控制机载辅助系统的优先级高于第二收起功率控制模块控制机载辅助系统,第二放落功率控制模块和第二放落功率控制模块分别用于机载辅助系统的放落。根据状态信息确定辅助系统的放落,提高机载功能使用的安全性。


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    Titel :

    Multi-redundancy undercarriage control method based on SSPC power output


    Weitere Titelangaben:

    基于SSPC功率输出的多余度起落架控制方法


    Beteiligte:
    ZHANG NAN (Autor:in) / GAO YINGJIE (Autor:in) / FAN YU (Autor:in)

    Erscheinungsdatum :

    03.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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