A objective-oriented method for module workscope decision-making was proposed to supply support for the aero-engine module workscope and achieve automatic and intelligent decision-making after analyzing the objectives of aero-engine shop visit.Module workscope was made through two steps from five aspects of life limited parts
airworthiness directive/service bulletin
hardware damage
soft time and exhaust gas temperature margin.To solve the problem of distribution of module performance restoration value in decision-making process
an optimization model based on minimum shop visit cost was put forward and solved by using dynamic programming and heuristic algorithm
respectively.By comparing the results
an applicable environment of the two algorithms was given.Finally
the proposed decision-making method was applied to a prototype system.The test result in an airline shows that the proposed decision-making method is effective and capable of satisfying the requirements of airline companies.
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