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榫连结构的高应力梯度及破坏分析

魏大盛 王延荣

魏大盛, 王延荣. 榫连结构的高应力梯度及破坏分析[J]. 北京航空航天大学学报, 2010, 36(10): 1184-1188.
引用本文: 魏大盛, 王延荣. 榫连结构的高应力梯度及破坏分析[J]. 北京航空航天大学学报, 2010, 36(10): 1184-1188.
Wei Dasheng, Wang Yanrong. On the high stress gradient and failure analysis of dovetail attachments[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(10): 1184-1188. (in Chinese)
Citation: Wei Dasheng, Wang Yanrong. On the high stress gradient and failure analysis of dovetail attachments[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(10): 1184-1188. (in Chinese)

榫连结构的高应力梯度及破坏分析

基金项目: 凡舟青年科研基金资助项目(20080403)
详细信息
    作者简介:

    魏大盛(1978-),男,黑龙江宁安人,讲师,dasheng.w@163.com.

  • 中图分类号: V 231.91; V 232.3

On the high stress gradient and failure analysis of dovetail attachments

  • 摘要: 某燕尾形榫连结构的分析表明叶盘榫齿/榫槽接触区边缘存在较高的应力梯度,接触应力的有限元解同网格疏密程度密切相关.通过建立一系列不同密度网格的模型,对此问题展开有限元建模分析,以改善接触应力的求解精度,同时深入讨论材料弹塑性对接触应力的影响.在弹塑性接触应力分析的基础上,采用断裂力学方法建立了榫连结构高应力梯度位置的破坏分析模型,判断裂纹的萌生及扩展方向,以进行结构的强度及寿命分析.

     

  • [1] 何明鉴.机械构件的微动疲劳[M].北京:国防工业出版社,1994 He Mingjian.Fretting fatigue of component[M].Beijing:National Defense Industry Press,1994(in Chinese) [2] 温卫东,高德平.榫头/榫槽接触问题边界元分析[J].航空动力学报,1992,7(2):117-120 Wen Weidong,Gao Deping.Analysis of tenon and mortise contact problems by boundary element methods[J].Journal of Aerospace Power,1992,7(2):117-120(in Chinese) [3] 郑旭东,蔚夺魁,王兆丰,等.某型航空发动机涡轮叶片和轮盘榫齿裂纹故障力学分析[J].航空发动机,2005,31(3):35-38 Zheng Xudong,Yu Duokui,Wang Zhaofeng,et al.Mechanical analysis of crack failures in turbine blade and disk serration of an aeroengine[J].Aeroengine,2005,31(3):35-38(in Chinese) [4] Sinclair G B,Cormier N G,Griffin J H,et al.Contact stresses in dovetail attachments:finite element modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124:182-189 [5] Sinclair G B,Cormier N G.Contact stresses in dovetail attachments:physical modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124:325-331 [6] Sinclair G B,Cormier N G.Contact stresses in dovetail attachments:alleviation via precision crowning[J].Journal of Engineering for Gas Turbines and Power,2003,125:1033-1041 [7] 古远兴.高低周复合载荷下燕尾榫结构微动疲劳寿命研究 .南京:南京航空航天大学能源与动力学院,2007 Gu Yuanxing.Research on fretting fatigue life of dovetail joint under HCF-LCF load .Nanjing:School of Power and Energy,Nanjing University of Aeronautics and Astronautics,2007(in Chinese) [8] 刘道新,刘军,刘元镛.微动疲劳裂纹萌生位置及形成方式研究[J].工程力学,2007,24(3):42-47 Liu Daoxin,Liu Jun,Liu Yuanyong.Study on nucleating location and formation of fretting fatigue cracks[J].Engineering Mechanics,2007,24(3):42-47(in Chinese) [9] 魏大盛,王延荣.榫连结构接触面几何构形对接触区应力分布的影响[J].航空动力学报,2010,25(2):407-411 Wei Dasheng,Wang Yanrong.Effects of the profile of contact surfaces on the stress distribution for tenon jointing in bladed-disk assemblies[J].Journal of Aerospace Power,2010,25(2):407-411(in Chinese) [10] Golden P J,Calcaterra J R.A fracture mechanics life prediction methodology applied to dovetail fretting[J].Tribology International,2006,39:1172-1180
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出版历程
  • 收稿日期:  2009-08-07
  • 网络出版日期:  2010-10-31

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