The accuracy of aero-engine model-based fault diagnosis is directly influenced by the matching accuracy between the self tuning model and real engine.The parameter selection of support vector regression by adaptive genetic algorithms was proposed and applied to the real-time on-board self tuning model
thus effectively improving the matching accuracy.After analyzing the influences of parameter selection of support vector regression(SVR) on the performances of the SVR model
optimal parameters in the given region were selected in the search area by genetic algorithms.Different methods such as back propagation neural network(BP-NN)
SVR
adaptive genetic algorithms-least square support veitor regression(AGA-LSSVR) were compared in the compensation of aero-engine model error;the results indicate that the proposed AGA-LSSVR is most feasible.
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