期刊文献+

钛合金干涉螺栓应力波安装质量模拟研究 被引量:3

Installation quality assessment of interference fit titanium bolt in stress-wave driving process by simulations
下载PDF
导出
摘要 提高干涉螺栓安装质量是提高螺接接头连接效率的有效途径.为了提高钛合金干涉螺栓安装质量,建立钛合金干涉螺栓有限元动态安装模型,研究干涉量、摩擦因数和安装次数对接头安装质量的影响,并结合试验对安装模型进行验证.结果表明:应力波安装阻力小于强迫安装;1.0%干涉量下安装孔壁挤压不充分,2.0%干涉量时会引起孔壁划伤,1.5%干涉量下安装孔壁表面质量最优;1.0%和1.5%干涉量下安装阻力对摩擦因数不敏感,但干涉量增加到2.0%时,安装阻力和最大凸瘤高度随摩擦因数增大而显著增加;二次安装导致安装阻力和最大凸瘤高度大幅上升,安装孔壁形成明显层叠累积.综上所述,工程实践中推荐使用1.5%干涉量,以保证安装孔壁表面质量.为了提高经济效益,摩擦因数选择0.1~0.15,多次安装应避免使用.干涉量大于1.5%时,应通过多次铰孔、改善螺栓表面润滑效果等方法尽可能降低摩擦因数,进而有效减小安装阻力和最大凸瘤高度. Improving the installation quality is vital for the design optimization of interference-fit bolted joints. The installation quality of interference-fit titanium bolt using stress-wave driving method was assessed by numerical simulations and tests. The results showed that installation resistance using stress-wave driving method was smaller than that using forced driving method. Small plastic deformation was observed on the mounting hole with interference-fit size of 1.0%, while damage occurred with interference-fit size of 2.0%. Moreover, the best quality was achieved with interference-fit size of 1.5%. The installation resistance for interference-fit sizes of 1.0% and 1.5% showed little sensitivity to friction coefficients, while the installation resistance and peek protuberance height increased significantly with friction coefficient for interference size fit of 2.0%. The twice driving method results in the greater installation resistance, higher protuberance, and lower surface quality. It can be concluded that, the interference fit size of 1.5% is suggested in service to achieve an excellent surface quality of the installation hole after installation, and friction coefficients ranging 0.1-0.15 are also suggested to reduce installation cost without using twice driving method. When interference fit size is larger than 1.5%, the decrease in the friction coefficient is beneficial for the improvement in the installation quality by reducing the installation resistance and peek protuberance height.
出处 《材料科学与工艺》 EI CAS CSCD 北大核心 2018年第1期24-30,共7页 Materials Science and Technology
基金 航空基金(2015ZE53065) 陕西省科技统筹创新工程计划项目(2015KTCQ01-83)
关键词 电磁铆接 高锁螺栓 安装 干涉配合 安装质量 模拟 electromagnetic riveting hi-lock bolt installation interference fit installation quality simulation
  • 相关文献

参考文献6

二级参考文献73

  • 1徐梅香,胡建清,韩志忠.高锁螺栓、高锁螺母的国产化研制[J].直升机技术,2009(3):94-97. 被引量:10
  • 2张爽,王栋,郦正能,寇长河,章怡宁.复合材料层合板多钉连接结构累积损伤过程可视化仿真模拟[J].复合材料学报,2006,23(3):135-140. 被引量:16
  • 3曹增强,刘洪.电磁铆接技术[J].塑性工程学报,2007,14(1):120-123. 被引量:31
  • 4中国航空科学技术研究院编著.飞机结构抗疲劳-断裂强化工艺手册[M].北京:航空工业出版社,1993.
  • 5贾玉红,何景武.现代飞行器制造工艺学[M].北京:北京航空航天大学出版社,2010.
  • 6DOMENICO F, NIKOLAUS O, GEBHARD S. Finite element analysis for advanced repair solutions: A stress analysis study of fastened and bonded fuselage skin repairs [C]// 50th AIAA/ASME/ASCE/AHS/ ASC Structures , Structural Dynamics , and Materials Conference, May4-7, 2009, Palm Springs, California.
  • 7雅可维茨.飞机长寿命螺栓连接和铆接技术[M].张国梁译.北京:航空工业出版社,1991.
  • 8CHAKHERLOU T N, MIRZAJANZADEH M. An investigation about interference fit effect on improving fatigue life of a holed single plate in joints [J]. European JournalofMechanicsA/Solids, 2010(29): 675-682.
  • 9BRIAN G B. Cracking during the installation of interference fit fasteners and bucked rivets in 7050-T7XXX machined aluminum parts[C]//2006 ASME International Mechanical Engineering Congress and Exposition, November5-10, 2006, Chicago, Illinois.
  • 10ATRE Amarendra, JOHNSON W S. Analysis of the effects of interference and sealant on riveted lap joints[J]. Journal of Aircraft, 2007, 44(2): 353-364.

共引文献81

同被引文献21

引证文献3

二级引证文献31

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