期刊文献+

圆弧齿榫接结构应力的数值计算与分析 被引量:8

Numerical calculation and analysis of arc tooth tenon joint
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摘要 对两圆柱体接触问题和平面接触问题进行分析,探讨了接触区应力的收敛性.对某枞树形圆弧齿榫接结构的接触区应力进行了数值计算和分析.利用有限元软件ANSYS进行了接触分析,对比了梯形齿和圆弧齿榫接结构的应力结果,并采用光弹实验进行了验证.研究结果认为,与梯形齿榫接结构相比,圆弧齿榫接结构使接触应力、第三主应力和等效应力等降低.在此基础上,对圆弧齿榫接结构进行了优化分析,通过优化进一步降低了榫接结构的应力水平. Two cylinders contact problem and plan contact problem were analyzed, and feature of convergence was discussed. Some numerical calculations of an arc tooth tenon joint with three teeth were done. Then, the contact stress with ANSYS was analyzed, and the results of trapezoid tooth and arc tooth tenon joint were compared to find that the latter decreased the contact stress, the third principle stress and von Mises stress. Based on this, some optimizations about the arc tooth tenon joint were done, and the stress was decreased again by optimization.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2012年第3期610-616,共7页 Journal of Aerospace Power
关键词 榫接结构 接触分析 梯形齿 圆弧齿 优化 tenon joint contact analysis trapezoid tooth arc tooth optimization
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参考文献13

  • 1宋兆泓.航空燃气涡轮发动机强度设计[M].北京:北京航空航天大学出版社,2008.
  • 2Kosing O E,Scharl R,Shchmuhl H J.Design Improve-ments of the EJ200HP compressor[R].ASME-2001-GT-0283,2001.
  • 3Meguid S A,Kanth P S,Czekanski A.Finite element anal-ysis of fir-tree region in turbine discs[J].Finite Elementsin Analysis and Design,2000,35(4):305-317.
  • 4SONG Wenbin,Keane A J.An efficient evolutionary op-timisation framework applied to turbine blade firtree rootlocal profiles[J].Structural Multidisciplinary Optimiza-tion,2005,29(5):382-390.
  • 5Sinclair G B,Cormier N G,Griffin J H,et al.Contact stres-ses in dovetail attachments:finite element modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124(1):182-189.
  • 6Johnson K L.接触力学[M].徐秉业,罗学富,刘信声,等,译,北京:高等教育出版社,1992.
  • 7孙锡环,秦晓桐,钱浩生,刘耀乙,董勤喜.烟气轮机盘榫槽部位的实验应力分析[J].北京理工大学学报,1996,16(4):361-366. 被引量:1
  • 8张如一.实验应力分析[M].北京:机械工业出版社,1982..
  • 9陈开军,马枚.航空发动机叶片榫头优化设计研究[J].航空动力学报,1995,10(2):190-192. 被引量:14
  • 10Song W,Keane A.Turbine blade fir-tree root design op-timisation using intelligent CAD and finite element analysis[J].Computers and Structures,2002,80(24):1853-1867.

二级参考文献24

  • 1陈火红,何君毅,曹凤兰,邓剑波.涡轮叶片与涡轮盘热弹塑性蠕变接触分析[J].航空动力学报,1995,10(1):9-12. 被引量:3
  • 2陈开军,马枚.航空发动机叶片榫头优化设计研究[J].航空动力学报,1995,10(2):190-192. 被引量:14
  • 3邢誉峰,诸德超.航空发动机涡轮盘榫槽的形状优化设计[J].航空学报,1995,16(4):488-491. 被引量:17
  • 4Chan S K,Tuba I S. A finite element method for contact problems of solid bodies Part II : application to turbine blade fastenings[J].Int. J. Mech. Sci. , 1971,13 (7) : 627-639.
  • 5Zboinski G. Physical and geometrical non-linearities in contact problems of elastic turbine blade attachments[J]. Mechanics Engineering Science, 1995,209(4) :273-286.
  • 6Zboinski G. Finite element computer program for incremental analysis of large three dimensional frictional contact problems of linear elasticity[J].Computer Structure, 1993,46(4):679-687.
  • 7Uchino K, Kamiyama T, Inamura T, et al. Three-dimensional photoelastic analysis of aeroengine rotary parts [C]// Proceedings International Symposiumon Photoelastieity. New York: Springer, 1986 : 209-214.
  • 8Abdul-Aziz A. Structural evaluation of a space shuttle main engine (SSME) high pressure fuel turbopump turbine blade[R]. NASA CR-198428,1996.
  • 9Meguid S A,Kanth P S,Czekanski A. Finite element analysis of fir-tree region in turbine dises[J]. Finite Elementsin Analysis and Design, 2000,35 (4) : 305-317.
  • 10Song W, Keane A, Rees J, et al. Turbine blade fir tree root design optimisation using intelligent CAD and finite element analysis[J]. Computer and Structures, 2002,80 (24) : 1853-1867.

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