The invention discloses a dual-mode dual-redundancy emergency ejection lifesaving electronic parachute opening device which comprises a sensor assembly, a dual-mode dual-redundancy control circuit assembly, an adapter plate assembly, a power supply circuit board assembly, a thermal battery assembly and a filtering input and output assembly. The sensor assembly, the dual-mode dual-redundancy control circuit assembly, the power supply circuit board assembly and the thermal battery assembly are all connected with an adapter plate, and the power supply circuit board assembly is connected with thefiltering input and output assembly. Ignition control signals are output through the dual-redundancy monitoring control technology, ignition electric energy is safely and reliably output to strike anelectric exploder when an aircraft is out of control due to faults and an ejection seat is emergently ejected off the aircraft, so that the escape parachute is safely ejected out, people and the seatare separated, and the life of a pilot is saved; and the safety is improved.
本发明公开了一种双模双余度应急弹射救生电子式开伞器,包括传感器组件、双模双余度控制电路组件、转接板组件、电源电路板组件、热电池组件和滤波输入输出组件,传感器组件、双模双余度控制电路组件、电源电路板组件和热电池组件均与转接板连接,电源电路板组件与滤波输入输出组件连接。本发明实现双余度监测控制技术输出点火控制信号,实现飞机故障失控等故障弹射座椅应急弹射离机时,安全可靠的输出点火电能,击发电起爆器,使救生伞安全射出,人‑椅分离,挽救飞行员的生命;提高安全性。
Dual-mode dual-redundancy emergency ejection lifesaving electronic parachute opening device
一种双模双余度应急弹射救生电子式开伞器
2021-01-12
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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