The invention provides an air entraining control system of an aircraft, a control method of the air entraining control system and the aircraft. The system comprises an air entraining subsystem and control equipment, the air entraining subsystem comprises a pressure sensing device, a temperature sensing device and a regulating valve which are arranged on an air circulation pipeline; the pressure sensing equipment is used for sensing the air entraining pressure in the air circulation pipeline; the temperature sensing equipment is used for sensing the air entraining temperature in the air circulation pipeline; the control equipment comprises a first control module and a second control module which are used for respectively acquiring temperature information of the temperature sensing equipment and pressure information of the pressure sensing equipment; the first control module controls the adjusting valve to rotate according to at least one of the pressure information and the temperature information so as to achieve air entraining temperature or air entraining pressure adjustment in the air circulation pipeline. The probability that the two control modules fail at the same time due to a common mode factor can be greatly reduced, and the safety performance of the system is further improved.
本申请提出一种飞行器的引气控制系统、其控制方法以及飞行器,系统包括引气子系统以及控制设备;引气子系统包括设置在气体流通管路上的压力感测设备、温度感测设备以及调节活门;压力感测设备用于感测气体流通管路内的引气压力;温度感测设备用于感测气体流通管路内的引气温度;控制设备包括第一控制模块与第二控制模块,用于分别获取温度感测设备的温度信息和压力感测设备的压力信息;第一控制模块根据压力信息和温度信息至少之一控制调节活门转动,以实现气体流通管路内的引气温度或引气压力调节。本申请能够极大地降低了共模因素导致的两个控制模块同时失效事件发生的概率,进一步提升了系统的安全性能。
Air entraining control system of aircraft, control method of air entraining control system and aircraft
一种飞行器的引气控制系统、其控制方法以及飞行器
2024-10-15
Patent
Electronic Resource
Chinese
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