The invention provides a helicopter emergency floating system which comprises an emergency floating switch board 10, a floating control box 20, a gas cylinder system 30, an electromechanical management computer 40, a speed/height detector 50, a positive collective distance rod buoy inflation switch 60, an auxiliary collective distance rod buoy inflation switch 70 and a water immersion sensor 80. Wherein the emergency floating switch plate 10, the positive collective distance rod buoy inflation switch 60 and the auxiliary collective distance rod buoy inflation switch 70 are all connected with the floating control box 20; the floating control box 20 is respectively connected with the gas cylinder system 30, the electromechanical management computer 40, the speed/height detector 50 and the water immersion sensor 80; the electromechanical management computer 40 is respectively connected with the emergency lifesaving positioning system 401, the key part self-destruction system 402, the rotor braking system 403, the engine 404, the weapon control panel 405 and the engine fire extinguishing system 406; and the weapon control panel 405 is respectively connected with the weapon hanging rack 4051 and the inert gunpowder burning and explosion system 4052.
本申请提供一种直升机应急漂浮系统,直升机应急漂浮系统包括应急漂浮开关板10、漂浮控制盒20、气瓶系统30、机电管理计算机40、速度/高度检测器50、正总距杆浮筒充气开关60、副总距杆浮筒充气开关70和浸水传感器80,其中:应急漂浮开关板10、正总距杆浮筒充气开关60、副总距杆浮筒充气开关70均与漂浮控制盒20连接;漂浮控制盒20分别与气瓶系统30、机电管理计算机40、速度/高度检测器50、和浸水传感器80连接;机电管理计算机40分别与应急救生定位系统401、关键部位自毁系统402、旋翼刹车系统403、发动机404、武器控制板405和发动机灭火系统406连接;武器控制板405分别与控制着武器挂架4051和惰性火药燃爆系统4052连接。
Helicopter emergency floating system
一种直升机应急漂浮系统
2023-04-04
Patent
Elektronische Ressource
Chinesisch
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