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民航客机推力目标值计算方法

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推力管理是民航客机飞行管理系统的重要功能之一.在整个航线内,飞行管理系统根据不同飞行航段以及不同飞行状态,确定飞机对发动机的推力需求,并以此作为推力目标值形成发动机油门杆控制的指令,其中推力目标值的计算是推力管理的核心.针对民航客机各飞行航段的特点,采用飞行动力学方法对飞机爬升、巡航、下降三个航段中不同飞行方式下的推力目标值计算方法进行研究.以波音737-800实际飞行记录数据为算例,进行推力目标值计算方法仿真对比验证,结果表明:所计算的推力目标值变化趋势与飞行性能理论相符,典型航段推力目标值计算与实际飞行数据的对比误差不大于3%.所提出的推力目标值计算方法可为民航客机推力管理系统设计提供参考.
Calculation method of thrust target value for civil aircraft
Thrust management is one of the important functions of civil aircraft flight management system.In different flight phases and flight states of the whole route,the flight management system needs to calculate the aircraft thrust requirements for engine,and then use the required thrust as the target thrust to generate the command of engine throttle control.Of which,thrust target value calculation is the core of thrust management.According to different flight characteristics of each phase,the calculation method of aircraft thrust target value was studied by using flight dynamics.The calculation process of climb,cruise,descent phases at different flight modes were analyzed in detail.Taking Boeing 737-800 flight record data as an example,the thrust target value calculation method was simulated and verified.The results showed that the calculated thrust value was consistent with the flight performance theory,and the relative error between the calculated thrust and the actual flight record data in typical flight phases was less than 3%.The thrust target value calculation method can provide a reference for civil aircraft thrust management system design.

civil aircraftthrust managementthrust target value calculationflight performanceflight dynamics

李仪、苏三买、梁凯恒、朱天宇

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西北工业大学动力与能源学院,西安 710072

民航客机 推力管理 推力目标值计算 飞行性能 飞行动力学

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(7)