In the seeking control of multivariable aero-engine
general optimization algorithm may find the locally optimal solution.An improved algorithm based on particle swarm optimization (PSO) and support vector regression (SVR) was applied to aero-engine stability seeking control
setting the lower limits for surge margin to keep aero-engine working stably.The working point with minimum surge margin was searched globally.The simulation results show that the designed stability control algorithm could reduce the surge margin while keeping the thrust constant and reduce the turbine inlet temperature and specific fuel consumption effectively.
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
ptimum design of rotor structure layout and its mechanical properties
Related Author
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
QIU Lu
曹大录
白广忱
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics