The invention belongs to the technical field of airplane wheel brake systems and discloses a six-wheel frame main undercarriage airplane electrical conduction braking control system and method. At a high speed section, braking of the back-row wheels is weakened and braking of front-row wheels is intensified to be adapted to airplane nose-down pitching moment, so that the ground normal force of theback-row wheels and the front-row wheels is distributed, that is, the normal force of the front-row wheels is larger than that of the back-row wheels, transitional slipping of the back-row wheels isreduced, and the purposes of improving the low airplane braking efficiency, shortening the running distance and reducing the tyre wear of the back-row wheels are realized.

    本发明属于飞机机轮刹车系统技术领域,公开了一种6轮车架主起落架飞机电传刹车控制系统及方法,在高速段,弱化后排轮刹车,强化前排轮刹车,以适应刹车低头力矩使前后排轮的地面法向力分配,即前排轮的法向力比后排轮的增大,从而减少后排轮的过渡打滑,达到提高飞机刹车效率低,缩短滑跑距离和减少后排轮的轮胎磨损的目的。


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    Title :

    Six-wheel frame main undercarriage airplane electrical conduction braking control system and method


    Additional title:

    一种6轮车架主起落架飞机电传刹车控制系统及方法


    Contributors:
    HE YONGLE (author) / GU MING (author) / MA XIAOJUN (author) / LIU WENLIANG (author) / HE WENJING (author)

    Publication date :

    2020-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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