The invention belongs to the aviation lifesaving technology, and relates to an electronic parachute opening control device, a parachute opening control method and a parachute. The electronic parachuteopening control device comprises a satellite positioning module (1), a microprocessor (2) and a cutter (3), the satellite positioning module (1) is in communication with a satellite, acquires position information of the parachute in real time and is connected with the microprocessor, the microprocessor is used for signal processing and is connected with the cutter, and the cutter receives a parachute opening signal sent by the microprocessor and opens the parachute. According to the invention, the height information acquisition is stable, the influence of environmental meteorological factorsis little, the instantaneous fluctuation during cabin separation is avoided, the safety and reliability are realized, and the technical progress is greater compared with the traditional parachute opening mode.

    本发明属于航空救生技术,涉及一种电子式开伞控制装置及开伞控制方法和降落伞。所述电子式开伞控制装置包括卫星定位模块(1)、微处理器(2)、切割器(3),其中,所述卫星定位模块(1)与卫星通信,实时获取降落伞的位置信息,并与微处理器连接,所述微处理器用于信号处理,并与切割器连接,所述切割器接收微处理器发送的开伞信号,打开降落伞。本发明高度信息获取稳定,不易受到环境气象因素影响,也不存在脱舱时的瞬时波动,安全可靠,相对于传统开伞方式具有较大的技术进步。


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    Titel :

    Electronic parachute opening control device, parachute opening control method and parachute


    Weitere Titelangaben:

    电子式开伞控制装置及开伞控制方法和降落伞


    Beteiligte:
    DAI YUXIAO (Autor:in) / LIU HU (Autor:in) / CHEN MINGSEN (Autor:in) / HOU BIDAN (Autor:in)

    Erscheinungsdatum :

    2021-03-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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