The invention belongs to the technical field of aircraft oxygen/life support system design, and relates to an aircraft life support system pilot operation control system which comprises an interface unit, a power distribution unit and a control unit. When an airplane is in the air, a pilot can directly send a request command to the control unit in the operation process, the control unit starts different functional modules after receiving the specific request command and sends different control instructions to the interface unit, and the interface unit calls different power distribution lines from the power distribution unit according to the specific control instructions. And supplying power to corresponding components of the life support system so as to complete a corresponding control instruction. A pilot only needs to complete all control instructions on the aircraft operating platform, operation is convenient, integration of operation and control functions of the aircraft life support system is achieved, the system active and weight is reduced, and the man-machine effect of pilot operation and control is improved.
本申请属于飞机氧气/生命保障系统设计技术领域,为一种飞机生命保障系统飞行员操作控制系统,包括接口单元、配电单元和控制单元;当飞机处于空中时,飞行员在操作过程中,可以直接向控制单元发出请求命令,控制单元在接收到具体的请求命令启用不同的功能模块,并向接口单元发出不同的控制指令,接口单元根据具体的控制指令向配电单元调用不同的配电线路,向相应的生命保障系统的元器件进行供电,从而完成相应的控制指令。飞行员只需要在飞机操作台上即可完成所有的控制指令,操作方便,实现了飞机生命保障系统操作与控制功能的集成,降低系统积极和重量,提升飞行员操作和控制的人机功效。
Pilot operation control system of aircraft life support system
一种飞机生命保障系统飞行员操作控制系统
2022-12-06
Patent
Electronic Resource
Chinese
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