A turbofan engine and its main fuel control system with hydromechanical regulator are studied.The rotational speed control system and the acceleration control system are modelled according to the analysis of the engine control program.The temperature sensor
temperature amplifier and blade control system are also modeled.According to thse mathematical models
all systems are simulated with the SIMULINK in toolbox of MATLAB.This work has important value for further research and improvement in the engine main fuel control system.
Model and Simulation of Aeroengine Load Spectrum Related to Operation
Numerical simulation on the effect of misalignment on outlet flow field of double-swirler
Mission reliability simulation modeling of space TT&C system based on DSPN
Methods for test and state analysis of determinate simulation results
Safety margins analysis on turbocharging system in aircraft piston engine
Related Author
SONG Ying-dong
SUN Zhi-gang
JIANG Yao
HU Jian
HU Hao-sheng
YANG Xiao-song
WU Xiao-yue
FU Hui-min
Related Institution
Nanjing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute, Aviation Industry Corporation of China
College of Information System and Management, National University of Defense Technology
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics