The invention discloses a pneumatic track catapult aircraft launching mechanism, and particularly relates to the field of aircraft launching mechanisms, the pneumatic track catapult aircraft launching mechanism comprises a sliding rail, a connecting frame is fixedly mounted on the rear side of the lower end of the sliding rail, the lower end of the connecting frame is movably connected with a rear adjustable support, and the lower portion of the front end of the sliding rail is movably connected with a front adjustable support; an energy storage device is fixedly connected to the rear adjustable support, braking systems are arranged on the left side and the right side of the front end of the sliding rail, a sliding device is arranged on the sliding rail in a sliding mode, an aircraft fixing device is fixedly installed on the sliding device, a traction rope is connected to the lower end of the sliding device, and an electric capstan is arranged on the connecting frame. The end, away from the sliding device, of the traction rope is wound around the electric capstan. According to the pneumatic orbit catapult aircraft launching mechanism, an aircraft is launched in a pneumatic catapult mode, launching is easy to operate, safety and reliability are achieved, the power adjustable range is large, and the pneumatic orbit catapult aircraft launching mechanism has the advantages of being wide in application range and high in environmental adaptability.

    本发明公开了气动轨道弹射飞行器发射机构,具体涉及飞行器发射机构领域,包括滑轨,所述滑轨下端后侧固定安装有连接架,所述连接架下端活动连接有后可调支架,所述滑轨前端下部活动连接有前可调支架,所述后可调支架上固定连接有蓄能装置,所述滑轨前端左右两侧均设置有制动系统,所述滑轨上滑动设置有滑动装置,所述滑动装置上固定安装有飞行器固定装置,所述滑动装置下端连接有牵引绳,所述连接架上设置有电动绞盘,所述牵引绳远离滑动装置的一端缠绕在电动绞盘上。本发明所述的气动轨道弹射飞行器发射机构,采用气动弹射的方式发射飞行器,发射易操作且安全可靠、动力可调范围大,具有适用范围广、环境适应性高的特点。


    Access

    Download


    Export, share and cite



    Title :

    Launching mechanism of pneumatic track catapult aircraft


    Additional title:

    气动轨道弹射飞行器发射机构


    Contributors:
    YU DONGMAN (author) / YANG QINGYUAN (author) / LI XIAOJING (author) / ZHANG NAIWEN (author) / YUE PENGFEI (author)

    Publication date :

    2023-02-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    Launching by catapult

    Wackett, L.J. | Engineering Index Backfile | 1931


    Catapult for launching aeroplanes

    Engineering Index Backfile | 1932


    Catapult ramp for launching UAVs

    PENTTI LIPPONEN | European Patent Office | 2018

    Free access

    PNEUMATIC HYDRAULIC CATAPULT

    MIGALIN KONSTANTIN VALENTINOVICH / SIDENKO KIRILL ALEKSEEVICH / SIDENKO ALEKSEJ ILICH et al. | European Patent Office | 2020

    Free access

    Vacuum-energy-storage-type launching catapult for fixed-wing aircraft

    WANG ZHENCHUAN | European Patent Office | 2016

    Free access