A dynamic probabilistic design method for blade-tip radial running clearance of aeroengine high-pressure turbine

作者：Fei, Cheng-Wei^*; Tang, Wen-Zhong; Bai, Guang-chen; Chen, Zhi-Ying

来源：Proceedings of the Institution of Mechanical Engineers - Part C: Journal of Mechanical Engineering Science , 2015, 229(10): 1861-1872.

DOI：10.1177/0954406214549267

• High-pressure turbine
• blade-tip radial running clearance
• dynamic probabilistic anlysis
• distributed collaborative extremum response surface method
• multi-object multi-disciplinary

Around the engineering background of the probabilistic design of high-pressure turbine (HPT) blade-tip radial running clearance (BTRRC) which conduces to the high-performance and high-reliability of aeroengine, a distributed collaborative extremum response surface method (DCERSM) was proposed for the dynamic probabilistic analysis of turbomachinery. On the basis of investigating extremum response surface method (ERSM), the mathematical model of DCERSM was established. The DCERSM was applied to the dynamic probabilistic analysis of BTRRC. The results show that the blade-tip radial static clearance =1.82mm is advisable synthetically considering the reliability and efficiency of gas turbine. As revealed by the comparison of three methods (DCERSM, ERSM, and Monte Carlo method), the DCERSM reshapes the possibility of the probabilistic analysis for turbomachinery and improves the computational efficiency while preserving computational accuracy. The DCERSM offers a useful insight for BTRRC dynamic probabilistic analysis and optimization. The present study enrichs mechanical reliability analysis and design theory.

• 出版日期2015-7
• 单位北京航空航天大学