The invention belongs to the field of aviation, and particularly relates to an unmanned manned aircraft lifesaving system which comprises a propeller chassis with multiple rotor wings and a cabin. Wherein the cabin is mounted on the propeller chassis through explosive bolts; the cabin is provided with an airborne control center, a lifesaving handle, a seat restraint system and a parachute shooting rocket; when the airborne control center judges that the aircraft is in an emergency state, the airborne control center sends out an electric starting signal; when a passenger opens the lifesaving handle, the lifesaving handle sends out a detonation signal and an electric signal, and the electric signal starts the airborne control center to directly send out an electric starting signal; after the parachute shooting rocket and the explosive bolt receive an electric starting signal or a detonation signal, the explosive bolt is detonated, the propeller chassis is separated from the cabin, and the parachute shooting rocket ejects the parachute, so that the cabin slowly lands.

    本申请属于航空领域,特别涉及一种无人驾驶载人飞行器救生系统,包括:具有多旋翼的螺旋桨底盘与座舱;其中,座舱通过爆炸螺栓安装在螺旋桨底盘上;座舱具有机载控制中心、救生手柄、座椅约束系统以及射伞火箭;当机载控制中心判断飞行器处于紧急状态时,机载控制中心发出电启动信号;当乘员开启救生手柄后,救生手柄发出爆轰信号与电信号,所述电信号启动机载控制中心直接发出电启动信号;射伞火箭、爆炸螺栓接收电启动信号或者爆轰信号后,爆炸螺栓起爆,将螺旋桨底盘与座舱分离,射伞火箭将降落伞射出,使座舱缓慢降落。


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    Titel :

    Unmanned manned aircraft lifesaving system


    Weitere Titelangaben:

    一种无人驾驶载人飞行器救生系统


    Beteiligte:
    CUI DONGYUE (Autor:in) / ZHU YONGFENG (Autor:in)

    Erscheinungsdatum :

    28.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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