The accurate simulation of aero-engine hydraulic mechanical controller was investigated by combining the computer technique and numerical simulation.A set of components library was founded
and then the whole control system of aero-engine was simulated accordingly.This simulation method was applied to the control system design of an aeroengine.Simulation results show that the requirement for controller is satisfied.
Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations
Model and Simulation of Aeroengine Load Spectrum Related to Operation
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
HUANG Kai-ming
YIN Ze-yong
HUANG Jing-quan
SONG Ying-dong
SUN Zhi-gang
PENG Yunlong
WU Xiong
DING Ting
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute
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