期刊文献+

石墨圆周密封热-结构耦合分析 被引量:10

Analysis on thermal-structure coupling for graphite circumferential seal
原文传递
导出
摘要 综合考虑作用于石墨圆周密封环机械载荷和温度载荷,利用软件ANSYS完成石墨圆周密封结构分析、稳态热分析和热-结构耦合分析。结果表明:石墨圆周密封环主密封面应力分布均匀,最大等效应力出现在接头搭接处,这是由于接头搭接处结构特点,使密封环在此处所受气体不平衡力较大引起的。辅助密封面受载荷力矩作用引起应力分布不均,导致不平行密封缝隙出现,影响密封性能。密封环温度场分布均匀,主密封面的温度高于辅助密封面,接头搭接处接触面积大,温度显著升高。热效应对石墨圆周密封性能影响不容忽视,考虑热效应作用时,密封环应力值产生了一个数量级的升高,并使最大应力区域自主密封面接头边缘处向中心附近移动。 The mechanical load and temperature load on the graphite circumferential seal ring were considered comprehensively,and the software ANSYS was utilized to complete the structure analysis,steady-thermal analysis and thermal-structure coupling analysis of graphite circumferential seal ring.Results showed that stress distribution was uniform on the main sealing surface of graphite circumferential seal ring,the maximum equivalent stress appeared in lapping area of joints,becasue the structural characteristics of joints made gas unbalanced force higher in the lapping area of joints.The stress distribution was nonuniform on the auxiliary sealing surface because of the action of the load torque,and affected the sealing performance.Temperature field distribution was uniform,and the main sealing surface temperature was higher than the temperature on auxiliary sealing surface,and temperature had a significant rise in the lapping area of joints due to large contact area.Thermal effect should not be ignored for the properties of graphite circumferential seal.The value of stress had a tenfold rise in consider-ation of the thermal effect,and made the largest stress area move from edge to the center.
作者 闫玉涛 张博 胡广阳 赵中强 YAN Yutao1, ZHANG Bo1 , HU Guangyang2 , ZHAO Zhongqiang1(1. School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China~ 2. Shenyang Engine Research Institute, Aero Engine (Group)Corporation of China, Shenyang 110015, China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2018年第2期273-281,共9页 Journal of Aerospace Power
基金 航空科学基金(20140450001)
关键词 圆周密封 结构分析 热-结构耦合分析 温度场 应力场 circumferential seal structure analysis thermal-structure coupling analysis temperature field stress field
  • 相关文献

参考文献8

二级参考文献70

  • 1高亮,梁涛.抗氧化碳-石墨密封材料的研制[J].机械工程材料,2004,28(7):35-36. 被引量:4
  • 2林基恕.航空涡轮喷气发动机传动润滑技术的发展动向[J].世界机械工业,1989(8):2-5. 被引量:2
  • 3孙晓萍,李卫东,刘晓远.刷式密封设计与试验研究[J].航空发动机,2005,31(2):17-19. 被引量:24
  • 4王峰,陈国定,余承涛.基于粗糙接触的指尖密封热分析[J].机械科学与技术,2007,26(7):893-896. 被引量:7
  • 5斯库巴切夫斯基.航空燃气涡轮发动机零件结构与计算[M].北京:国防工业出版社,1992..
  • 6李健.航空发动机轴承腔的热分析[M].西安:西北工业大学,1998..
  • 7工程材料实用手册编辑委员会.工程材料实用手册(第1卷-第8卷)[M].北京:中国标准出版社,1989..
  • 8Braun M J, Pierson H M, Deng D. Thermofluids considerations and the dynamic behavior of a finger seal assembly [J]. Tribology Transactions,2005,48:531-547.
  • 9Steinefz B M, Hendricks R C. Advanced seal technology in meeting next generation turbine engine goal[R]. NASA/ TM-1998-206961: 1-11.
  • 10Sirdhar M R,Yovanovich M M. Thermal contact conductance of tool steel and comparison with model[J]. Int. J. Heat Mass Transfer, 1995,39 (4) : 831-839.

共引文献174

同被引文献93

引证文献10

二级引证文献13

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