Aircraft emergency risk avoiding system

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Aircraft emergency risk avoiding system

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GUO ZHI / BA QI / ZHANG YUE

The invention discloses an aircraft emergency risk avoiding system which comprises a digital risk sensing module, a central control module and an execution module. Wherein the risk sensing module comprises a stall sensor and a self-checking sensor, and in the risk sensing module, the stall sensor is used for capturing a risk signal; the central control module comprises a controller, the module is electrically connected with the digital risk sensing module and the execution module, detection indexes are built in through the controller, the central control module is used for detecting equipment dysfunction, and different electric signals are transmitted through a relay. The stall sensor automatically identifies a risk signal through the digital risk sensing module and transmits an electric signal to the controller, the controller starts the alarm to work, and when the alarm is manually confirmed or the manual no-response sensor carries out double-loop self-inspection confirmation again, engine power can be automatically removed to remove power and eject a parachute, so that the safety of the parachute is ensured. And safe directional landing is completed.

本发明公开了一种飞行器紧急避险系统，包括数字风险感应模块，中央控制模块和执行模块；其中，风险感应模块包括失速传感器和自检感应器，在该模块中，失速传感器用以捕获风险信号；所述中央控制模块包括控制器，该模块分别与数字风险感模块和执行模块电性连接，通过控制器内置检测指标，用以设备功能障碍检测，并通过继电器传输不同的电信号。本发明通过数字风险感应模块失速传感器自动识别风险信号，向控制器传输电信号，控制器打开报警器工作，当报警器经人工确认或人工无应答感应器再次双回路自检确认后均可自动执行发动机动力解除去解除动力并弹射降落伞，完成安全定向降落。