The invention discloses an aircraft takeoff thrust control method and device and a storage medium. The method comprises the steps that a takeoff thrust mode of an aircraft is activated, the running state of an engine is monitored, the takeoff thrust level is activated according to the running state of the engine, and an accelerator table and engine thrust are controlled according to a first thrust parameter corresponding to the takeoff thrust level; the real-time height of the aircraft and the thrust reduction height sent by the flight management system are monitored, and when the real-time height is larger than the thrust reduction height, a vertical-climbing mode is activated according to a vertical mode request of the flight management system; determining a target thrust mode and a target thrust level according to the running state of the engine and the vertical-climbing mode; and according to the second thrust parameter corresponding to the target thrust level, controlling the thrust of the accelerator table and the engine. According to the technical scheme provided by the invention, the technical problem that the thrust control of the aircraft cannot be automatically managed in the take-off stage of the aircraft in the prior art can be solved.
本发明公开了一种飞行器起飞推力控制方法、装置及存储介质,方法包括:激活飞行器的起飞推力模式并监测发动机的运行状态,根据发动机的运行状态激活起飞推力等级,根据起飞推力等级对应的第一推力参数控制油门台和发动机推力;监测飞行器的实时高度和飞行管理系统发送的减推力高度,当实时高度大于减推力高度时,根据飞行管理系统的垂直模式请求激活垂直‑爬升模式;根据发动机的运行状态和垂直‑爬升模式确定目标推力模式和目标推力等级;根据目标推力等级对应的第二推力参数控制油门台和发动机推力。本发明所提供的技术方案能够解决现有技术中在飞行器起飞阶段,不能自动管理飞机推力控制的技术问题。
Aircraft takeoff thrust control method and device and storage medium
飞行器起飞推力控制方法、装置及存储介质
2023-05-02
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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