The design method of an aero-engine surge elimination control system and the forced surge tests were discussed
especially a digital simulation of the surge elimination controller in loop was developed in this paper.The test results in both engine rig test and flight test show that
the control parameters can be optimized through the control system digital simulation test
then a reliable aero-engine surge elimination control system can be developed.
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
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
Related Author
LIU Zhi-you
GUO Rong-wei
HOU Min-jie
TIAN Jin-hu
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
China Gas Turbine Establishment, Jiangyou
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics