본 발명은 랜딩기어 어셈블리의 액슬과 림 사이에 설치되어 휠에 제동력을 인가하는 휠 브레이크 조립체이다. 상기 휠 브레이크 조립체는 상기 회전하는 액슬에 대하여 고정설치된 캐리어 플레이트; 상기 캐리어 플레이트에 배치되어 제동 작동력을 발생하는 브레이크 액추에이터; 상기 브레이크 액추에이터에 의해 작동하여 휠을 정지시키는 복수의 디스크를 포함하는 디스크 팩; 및 상기 캐리어 플레이트와 연결되고 상기 림과 사이에서 상기 디스크 팩을 포위하는 토션 튜브; 를 포함한다.

    The present disclosure relates to a wheel brake assembly for an aircraft installed in a landing gear assembly between an axle and a tire mounted on a rim to apply a braking force to a wheel. The wheel brake assembly comprises a carrier plate fixedly mounted on the axle; a brake actuator disposed on the carrier plate to generate a braking force; a disc pack including a plurality of discs operated by the brake actuator to stop the rotating wheel against the ground; and a torsion tube connected to the carrier plate and surrounding the disc pack between the rim and the axle.


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    Title :

    WHEEL BRAKE ASSEMBLY FOR AIRCRAFT


    Additional title:

    항공기용 휠 브레이크 조립체


    Contributors:
    KANG DEUK SOO (author) / LEE BEOM JOO (author) / JU YOUNG CHAN (author) / LEE SE YOUNG (author)

    Publication date :

    2024-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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