摘要
综合了航空发动机控制和故障诊断方法,设计了基于模态切换的任务级和发动机级模式的容错控制系统.任务级模式在发动机部件故障时,通过切换控制策略和控制模式达到恢复或降低发动机性能的要求;发动机级模式在控制回路失效时,根据故障情况切换到容错控制回路,从而保证发动机继续正常工作.数字仿真结果表明:在稳态或加速过程中出现部件故障时,容错控制系统都能够100%恢复发动机的推力;在发动机中间、慢车和节流状态下,当压气机转速控制回路失效时,容错控制系统能够在3s内平稳切换到风扇转速控制回路.
By combining aero-engine control and fault diagnoses methods,the aero-engine fault-tolerant control system based on control mode switch was designed,including task-level mode and engine-level mode.In case of failure of the engine components,the tasklevel mode could change the control strategies and modes to recover or reduce the aero-engine performance.In case of failure of a control loop,the control strategies were switched to other fault-tolerant control loops according to fault conditions,so as to ensure that the aero-engine continues to work normally.Numerical simulation result shows,the designed fault-tolerant control system can recover the aero-engine performance in 100%in case of failure of the components in the process of steady state or accelerated.And the designed fault-tolerant control system can switch to the fan speed control loop smoothly in 3seconds in case of failure of the compressor speed control loop.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2014年第4期953-964,共12页
Journal of Aerospace Power
关键词
航空发动机
模态切换
容错控制
性能恢复
容错控制回路
aero-engine
mode switch
fault-tolerant control
performance recovery
fault-tolerant control loop