Research on low cycle fatigue reliability-based robust design optimization of turbine blade

被引:0
|
作者
Peng, Maolin [1 ]
Yang, Zichun [1 ]
Cao, Yueyun [1 ]
Chu, Zhuli [1 ]
机构
[1] College of Power Engineering, Naval University of Engineering, Wuhan 430033, Hubei Province, China
关键词
Aerodynamic efficiency - Design optimization - Deterministic equations - Response surface method - Robust designs - Sequential Quadratic Programming method - Stress and strain distribution - Turbine blade;
D O I
暂无
中图分类号
学科分类号
摘要
To solve the problem of low cycle fatigue reliability-based robust design optimization of turbine blade, a series of fatigue tests of the blade material under high temperature were completed. According to the tests data, the randomized approach of deterministic equation was introduced to obtain the probabilistic strain-life curves of the blade material. The Bezier curve was employed to establish the blade model line and the parameter models of the turbine blade and flow field. After, the thermal-aero-structure coupling finite element method was used to obtain the aerodynamic efficiency, stress and strain distribution of the blade. Then, the fatigue reliability-based robust design optimization model was established and the response surface method was used to simulate the output performance functions and the limit state functions of the blade. Finally, the design optimization result was calculated with the sequential quadratic programming method by taking the fatigue reliability as the basic constrain condition. The results prove that: the low cycle fatigue reliability and robustness of the blade are improved remarkably after design optimization; the model and the methods are correct and can be served as references for the low cycle fatigue reliability-based robust design optimization of turbine blade and other complex structures. © 2013 Chin. Soc. for Elec. Eng.
引用
收藏
页码:104 / 111
相关论文
共 50 条
  • [1] Reliability-based low-cycle fatigue damage analysis for turbine blade with thermo-structural interaction
    Gao, Haifeng
    Fei, Chengwei
    Bai, Guangchen
    Ding, Lan
    AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 49 : 289 - 300
  • [2] Reliability-based optimization for robust design
    Liaw, LD
    DeVries, RI
    INTERNATIONAL JOURNAL OF VEHICLE DESIGN, 2001, 25 (1-2) : 64 - 77
  • [3] Mesh parameterization in reliability-based design optimization for the life of turbine blade with film holes
    Lei J.
    Lyu Z.
    Jia B.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2022, 44 (02): : 55 - 63
  • [4] A unified fatigue reliability-based design optimization framework for aircraft turbine disk
    Song, Lu-Kai
    Bai, Guang-Chen
    Li, Xue-Qin
    Wen, Jie
    INTERNATIONAL JOURNAL OF FATIGUE, 2021, 152
  • [5] A mesh parameterization method and life reliability-based optimization for turbine blade
    Lei, Jingyu
    Lei, Qiannan
    Li, Hongbin
    Jia, Beixi
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2023, 49 (10): : 2651 - 2659
  • [6] Probability Analysis and Reliability Based Design Optimization Methods for Low Cycle Fatigue Life of Turbine Shaft
    Lu Y.-X.
    Lyu Z.-Z.
    Feng K.-X.
    He L.-L.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (02): : 8 - 20
  • [7] Reliability-based design optimization for fatigue damage analysis
    M. Haisam Ibrahim
    G. Kharmanda
    A. Charki
    The International Journal of Advanced Manufacturing Technology, 2015, 76 : 1021 - 1030
  • [8] Reliability-based design optimization for fatigue damage analysis
    Charki, A. (abderafi.charki@univ-angers.fr), 1600, Springer London (76): : 5 - 8
  • [9] Reliability-based design optimization for fatigue damage analysis
    Ibrahim, M. Haisam
    Kharmanda, G.
    Charki, A.
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2015, 76 (5-8): : 1021 - 1030
  • [10] Robust and Reliability-Based Design Optimization Framework for Wing Design
    Paiva, Ricardo M.
    Crawford, Curran
    Suleman, Afzal
    AIAA JOURNAL, 2014, 52 (04) : 711 - 724