Take the air inlet window of blade tenon as detail-structure optimization object
the relationship model between maximum cast residual stress and structure parameters and temperature were established by the simulation of cast residual stress field of single crystal turbine blade based on the recrystallization critical stress of DD6 single crystal superalloy. The detail-structure optimization of air inlet window of blade tenon was studied under the conditions of geometric and dynamic constraints. Finally
through the analysis and comparison with the actual air window of blade tenon
this method was effectively verified. The results show that the maximum cast residual stress of optimized air inlet window of blade tenon is completely reduced by over 20%
and the recrystallization is effectively eliminated.
Crystallographic-orientation-related performance of single crystal turbine blade and optimization design of three-dimensional orientations
Creep-fatigue life prediction of single crystal turbine blade with the influence of stress relaxation
基于自适应MOMEDA滚动轴承故障特征提取方法
组合式弹性金属密封泄漏特性实验研究与结构优化
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
Related Author
GAO Jing-yun
FANG Lei
ZHANG Cheng-cheng
REN Yuan
LI Ying
GAO Jing-yun
ZHANG Cheng-cheng
HOU Nai-xian
Related Institution
Shanghai Engineering Research Center for Commercial Aircraft Engine, Commercial Aircraft Engine Compary Limited, Aviation Industry Corporation of China
Shanghai Engineering Research Center of Commercial Aircraft Engine, Commercial Aircraft Engine Company Limited, Aviation Industry Corporation of China
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University