The invention discloses a gravity air-drop method suitable for an air-drop system of a chariot. A main parachute system and a central guide rail are reserved, a traction parachute system is omitted, a mechanical lock is replaced with an electronic lock, and a guide parachute system is additionally arranged on each chariot; the guide parachute system comprises a guide rope, a guide parachute pack and a guide parachute, one end of the guide rope is slidably hung on an original parachute opening steel rope in the cabin without falling off, the other end of the guide rope is connected with the guide parachute pack, a parachute canopy of the guide parachute is contained in the guide parachute pack, and a connecting rope is connected with the main parachute system; at the beginning, lock shafts of the electronic locks are inserted into the central guide rails to be limited, after the aircraft reaches a preset air-drop area, the aircraft flies at an elevation angle, the cabin door is opened, all the electronic locks are synchronously unlocked, the chariot slides out of the cabin under the action of gravity, after the chariot leaves the cabin, the guide rope opens the guide parachute pack to expose the guide parachute, and the main parachute system is opened after the guide parachute is opened. According to the method, gravity air-drop of the chariot can be achieved only by slightly improving an existing chariot air-drop system, landing points are concentrated, improvement is convenient, and cost is low.

    本发明公开了一种适用于战车空投系统的重力空投方法,保留主伞系统和中央导轨,取消牵引伞系统,将机械锁更换为电子锁,在每个战车上增加引导伞系统;引导伞系统包括引导绳、引导伞包和引导伞,引导绳的一端不脱出地滑动挂在机舱内原有的开伞钢索上、另一端连接引导伞包,引导伞的伞衣容纳在引导伞包内、连接绳连接主伞系统;初始时,电子锁的锁轴插入中央导轨内限位,到达预定空投区域后,飞机仰角飞行,打开舱门,同步解锁所有电子锁,战车在重力作用下滑行出舱,战车出舱后,引导绳打开引导伞包露出引导伞,引导伞张开后打开主伞系统。该方法只需对现有的战车空投系统进行少许改进就能实现战车的重力空投,落点较为集中,改进方便、成本低。


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    Titel :

    Gravity air-drop method suitable for chariot air-drop system


    Weitere Titelangaben:

    适用于战车空投系统的重力空投方法


    Beteiligte:
    CHEN YONG (Autor:in) / QIN YANG (Autor:in) / LI JINHONG (Autor:in) / XU RONGHUA (Autor:in) / CAO CHONG (Autor:in) / XU GUANGQING (Autor:in) / WU BIN (Autor:in)

    Erscheinungsdatum :

    2023-03-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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