The invention belongs to the technical field of aircraft catapult-assisted take-off guarantee equipment, and particularly relates to a rotary friction energy absorption brake device, an aircraft catapult platform and a catapult method. Follow-up rope outlet, braking and reverse rope winding of the braking rope are achieved through the rotary friction energy absorption braking device. The aircraft catapulting platform carrying the rotary friction energy absorption braking device can simultaneously realize the functions of passive rope releasing during aircraft catapulting, active braking after aircraft catapulting and active resetting after aircraft catapulting.

    本发明属于飞机弹射起飞保障装备技术领域,具体涉及一种旋转式摩擦吸能制动装置、飞机弹射平台及弹射方法。本发明通过所述旋转式摩擦吸能制动装置实现制动绳的随动出绳、制动、反向收绳;搭载了该旋转式摩擦吸能制动装置的飞机弹射平台能够同时实现飞机弹射时被动放绳、飞机弹射后主动制动、飞机弹射后主动复位的功能。


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    Title :

    Rotary friction energy absorption braking device, aircraft ejection platform and ejection method


    Additional title:

    一种旋转式摩擦吸能制动装置、飞机弹射平台及弹射方法


    Contributors:
    XU JUN (author) / DAI YULIN (author) / LEI PEI (author) / WEI YABIN (author) / XIA FENGQIN (author) / ZHU AYUAN (author)

    Publication date :

    2023-11-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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