Currently there is no efficient method to detect and isolate the failure of actuators
which are an integral part of aero-engine control system.In this paper a novel technique was introduced
which allowed to formulate the difference about the actuators output through the controller's command output and the engine's actual output by means of interaction matrix.Therefore
the failure of multiple actuators could be detected and isolated successfully.The digital simulations demonstrate that this strategy has a high accuracy when it is applied in failures detection of the actuators of aero-engine control system.
Fault diagnosis for actuators of aero-engine fuel system based on NN-ELM
Fault diagnosis for actuator and its sensor of aero-engine fuel system
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Related Author
JIANG Jie
LI Qiu-hong
ZHANG Gao-qian
LI Ye-bo
JU Xin-xing
PENG Yunlong
WU Xiong
DING Ting
Related Institution
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics