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Contact analysis and optimization design of blade and disc assembly based on mesh deformation

  • Wang, Baizhi (Department of Engineering Mechanics, Northwestern Polytechnical University) ;
  • Yu, Qingmin (Department of Engineering Mechanics, Northwestern Polytechnical University) ;
  • Hou, Naixian (Department of Engineering Mechanics, Northwestern Polytechnical University) ;
  • Yue, Zhufeng (Department of Engineering Mechanics, Northwestern Polytechnical University)
  • 투고 : 2008.12.17
  • 심사 : 2009.08.13
  • 발행 : 2009.12.20

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참고문헌

  1. Applied Manual of Engineering Materials, Vol. 5. Edited by Committee to Edit Applied Manual of Engineering Materials [M]. China standard Publishing Company, 29-43
  2. Chinese Aviation Material Manual, Vol. 2. Edited by Committee to Edit Chinese Aviation Material Manua [M]. China standard Publishing Company, 792-806
  3. Ding, Z.P., Liu, Y.L., Yin, Z.Y., Yang, Z.G. and Cheng, X.M. (2004), "Three dimensional nonlinear cyclic stress - strain analysis of gas turbine rotor disk - blade system", J. Mach. Des., 21(8), 38-40
  4. Meguid, S.A., Refaat, M.H. and Papanikos, P. (1996), "Theoretical and experimental studies of structural integrity of dovetail joints in aeroengine discs", J. Mater. Proc. Technol., 56, 668-677 https://doi.org/10.1016/0924-0136(95)01880-8
  5. Song, Wenbin, Keane, Andy, Rees, Janet, Bhaskar, Atul and Bagnall, Steven (2002), "Turbine blade fir-tree root designoptimisation using intelligent CAD and finite element analysis", Comput. Struct., 80, 1853-1867 https://doi.org/10.1016/S0045-7949(02)00225-0
  6. Zhao, Hai (2005), Research on Design Method of Turbine Tenon/Mortise. Master's degree dissertation of Nanjing University of Aeronautics and Astronautics