期刊文献+

榫连结构接触面几何构形对接触区应力分布的影响 被引量:20

Effects of profile of contact surfaces on the stress distribution for tenon jointing in blade disk assemblies
原文传递
导出
摘要 为研究并降低传统榫连结构接触区边缘的高应力梯度,对几种典型接触形式展开了有限元分析,计算结果表明不同接触形式将导致不同的接触应力分布;针对某单齿燕尾形榫连结构,建立了一系列不同网格密度的有限元模型计算分析接触区的应力集中程度,并以此提高接触应力的求解精度;并进一步改进了接触面的几何形式,分析表明二维条件下圆弧/直线的接触形式改善了传统平面/平面接触的应力集中,圆弧/圆弧的接触形式将使接触应力进一步降低. To investigate and improve the high stress gradient near the edges of contact zone in conventional tenon jointing, several typical profiles of contact surface were analyzed by means of finite element method (FEM), indicating that different contact profiles would lead to different stress distributions. Then, a set of finite element models with different grids for dovetail attachment were established to analyze stress concentration effects, and improve the solving accuracy of contact stress. Different profiles of contact surface were chosen. The numerical solutions show that arc/line contact profile for two-dimensional (2-D) will remove the high stress concentration, and arc/arc one will further depress the contact stress.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2010年第2期407-411,共5页 Journal of Aerospace Power
基金 凡舟青年科研基金(20080403)
关键词 榫连结构 接触应力 接触面构形 高应力梯度 tenon jointing contact stress profile of contact surface high stress gradient
  • 相关文献

参考文献10

  • 1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. 被引量:9
  • 2郑旭东,蔚夺魁,王兆丰,董红联.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. 被引量:13
  • 3古远兴..高低周复合载荷下燕尾榫结构微动疲劳寿命研究[D].南京航空航天大学,2007:
  • 4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. 被引量:13
  • 5Sinclair 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. 被引量:1
  • 6Sinclair 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. 被引量:1
  • 7Sinclair 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. 被引量:1
  • 8GladwellGML.经典弹性理论中的接触问题[M].北京:北京理工大学出版社,1991.. 被引量:13
  • 9JOHSONKL.接触力学[M].北京:高等教育出版社,1991.. 被引量:3
  • 10魏大盛.凡舟青年基金研究报告-粉末冶金涡轮盘/叶接触部位压保载条件下强度及寿命分析[R].北京:北京航空航天大学,2008. 被引量:1

二级参考文献13

  • 1刘军,刘道新,刘元镛,唐长斌.微动接触应力的有限元分析[J].机械强度,2005,27(4):504-509. 被引量:24
  • 2高德平,1990年 被引量:1
  • 3陆山,航空学报,1985年,6卷,6期,548页 被引量:1
  • 4孙鹏 被引量:1
  • 5Hutson A L,Neslen C,Nicholas T.Characterization of fretting fatigue crack initiation processes in CRTi6Al4V[J].Tribology International,2003,36(1):252~263. 被引量:1
  • 6Kuno M,Waterhouse R B,Nowell D.Initiation and growth of fretting cracks in the partial slip regime[J].Fatigue Fract Engng Mater Struct,1989,12:387~398. 被引量:1
  • 7Tsai C T,Shankar Mall.Elasto-plastic finiteelement analysis of fretting stresses in pre-stressed strip in contact with cylindrical pad[J].Finite Element Analysis and Design,2000,36:171~187. 被引量:1
  • 8Mutoh Yosgiharu,Xu Jin-quan.Fracture mechanics approach to fretting fatigue and problems to be solved[J].Tribology International,2003,36:99~107. 被引量:1
  • 9Kozo Nakazawa,Norio Maruyama.Effect of contact pressure on fretting fatigue of austenitic stain lesssteel[J].Tribology International,2003,36:79~85. 被引量:1
  • 10JBarber M Ciavarella.Contact mechanics[J].International Journal of Solids and Structures,2000,37:29~43. 被引量:1

共引文献39

同被引文献136

引证文献20

二级引证文献35

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部