CHEN Zhi-ying, WANG Chao, ZHOU Ping.Robust Optimization Method for Turbine Blade under Fatigue-Creep Interaction[J].航空发动机,2017,43(4):11-16
Robust Optimization Method for Turbine Blade under Fatigue-Creep Interaction
DOI:
Key Words:turbine blade  fatigue-creep  life prediction  robust optimization design  time-life fraction method  aeroengine
Author NameAffiliationE-mail
CHEN Zhi-ying, WANG Chao, ZHOU Ping School of Energy and Power Engineering, Beihang University, Beijing 100191, China chenzhiying@buaa.edu.cn 
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Abstract:In order to reflect fatigue-creep interaction of turbine blade clearly, raise the accuracy and reliability of life prediction result and improve sensitivity of fatigue life to random variables at the same time. low cycle fatigue life and creep life of turbine blade were calculated by Manson-Coffin formula and Larson-Miller equation, fatigue-creep damage was obtained by modified time-life fraction method. Robust optimization design of turbine blade fatigue life was developed by combining RSM 渊Response Surface Methodology冤and FFOA 渊Fruit Fly Optimization Algorithm冤, considering the uncertainty of loads, material parameters and the degree of fatigue-creep interaction. The results show that probability interval of fatigue-creep life for turbine is decreased by 8.48%, which verify the feasibility of this optimization method.
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