a corrected standardization model was proposed relating gas path parameter deviation based on third similarity theory
the multivariate nonlinear overdetermined equations were established using the historical data as learning sample
and the unknown parameters were solved using Gauss-Newton iterative method.The deviation was solved using the corrected standardization model proposed
and the result was compared with deviation solved by other models.the conclusion is drawn that the correction model proposed is closer to the original factory model with higher accuracy
and it is more innovative and has practical value.
Calculation method of aero-engine exhaust gas temperature margin ,and remaining life based on data
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
DU Fangzhou
SUN Youchao
GUO Yuanyuan
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
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