The invention relates to an aircraft stall protection method. The method comprises the following steps: determining that an aircraft is under an icing meteorological condition; determining a working state of a wing anti-icing system of the aircraft, wherein the working state of the wing anti-icing system at least comprises one or more of the following items: opening or closing of an anti-icing switch, whether the wing anti-icing system fails or not, wing anti-icing temperature, the opening degree of an air entraining valve of the wing anti-icing system and air entraining pressure of the wing anti-icing system; reducing the stall attack angle protection value of the aircraft according to different working states of the wing anti-icing system; and providing stall protection for the aircraft according to the reduced stall angle of attack protection value.

    本公开涉及一种飞行器失速保护方法,包括:确定所述飞行器处于结冰气象条件下;确定所述飞行器的机翼防冰系统的工作状态,所述机翼防冰系统的工作状态至少包括以下各项中的一者或多者:防冰开关的开启或关闭、所述机翼防冰系统是否失效、机翼防冰温度、所述机翼防冰系统的引气活门的开度、所述机翼防冰系统的引气压力;取决于所述机翼防冰系统的不同工作状态,来降低所述飞行器的失速迎角保护值;以及根据经降低的失速迎角保护值来对所述飞行器提供失速保护。


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    Titel :

    Aircraft stall protection method and system


    Weitere Titelangaben:

    飞行器失速保护方法和系统


    Beteiligte:
    ZHAO JINGHUI (Autor:in) / GAO NAN (Autor:in) / ZHENG XIAOHUI (Autor:in) / FU LIN (Autor:in) / ZOU CANDONG (Autor:in) / WU NAN (Autor:in)

    Erscheinungsdatum :

    2021-09-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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