期刊文献+

内螺纹低频振动冷挤压试验研究 被引量:10

Experimental Research on Internal Thread Formation by Cold Extrusion Based on Low Frequency Vibration
原文传递
导出
摘要 内螺纹低频振动冷挤压加工是通过挤压丝锥棱齿的振动挤压,将传统内螺纹冷挤压加工中的干摩擦状态转变为更有利的边界摩擦状态,从而改善传统内螺纹冷挤压加工过程中冷却润滑液不易进入挤压区的严重缺陷。通过试验可知:随着激振频率的不断增大,挤压扭矩呈不断增大趋势;随着激振力的不断增大,挤压扭矩呈现为先减小后增大的趋势;随着激振力臂长度的不断增大,挤压扭矩总体呈不断增大的趋势。在其他工艺参数相同条件下,低频振动冷挤压可以进一步提高传统内螺纹的牙高率和改善牙顶处凹陷的缺陷,从而提高冷挤压内螺纹的抗疲劳强度及获得更好的表面形貌。 Internal thread formation by cold extrusion based on low-frequency vibration can realize vibration extrusion by extruding tap.It can turn the process of dry friction into a more favorable state of boundary friction.Therefore it can overcome the defect of traditional cold extrusion that the coolant cannot easily enter the extrusion zone.The experimental study shows that: as the exciting frequency increases,so does the extrusion torque;as the exciting force increases,the extrusion torque decreases first,and then increases;as the exciting arm length increases,the extrusion torque also increases.Under the same conditions of the process parameters,the internal thread formation by cold extrusion based on low-frequency vibration exhibits a higher rate of thread teeth height and fewer defects of the teeth top than traditional methods,and the method can improve the fatigue strength and surface morphology of the thread so formed.
出处 《航空学报》 EI CAS CSCD 北大核心 2013年第2期442-450,共9页 Acta Aeronautica et Astronautica Sinica
基金 空装"十一五"预研项目~~
关键词 内螺纹 冷挤压 低频振动 挤压扭矩 摩擦 internal thread cold extrusion low-frequency vibration extrusion torque friction
  • 相关文献

参考文献16

二级参考文献35

  • 1左大为,陈秀敏,申光宪.轧机压下螺纹副承载特性测试研究[J].中国机械工程,2006,17(3):307-311. 被引量:15
  • 2隈部淳一郎.韩昆 薛万夫 孙祥根 等译.精密加工振动切削(基础与应用)[M].北京:机械工业出版社,1985..
  • 3Franco L A L, Loureneo N J, Graca M L A, et al. Aircraft fracture of a nose landing gear in a military" transport aircraft [J]. Eng Fail Anal 2006, 13:474 -9.
  • 4Deshpande V S, Needleman A, Van der G E. Discrete dislocation modelling of fatigue crack propagation[ J]. Acta Mater,2002, 50:831 -46.
  • 5Ozdemir A T, Edwards L. Relaxation of residual stresses at coldworked fastener holes due to fatigue loading [ J ]. Fatigue Fract Eng Mater Struct, 1997, 20(10) :1443 -51.
  • 6Faraahi G H, Lebrun J L, Couratin D. Effect of shot peening on residual stress and fatigue life of a spring steel[J]. Fatigue Fract Eng Mater Struct, 1995, 18(2) : 211 -20.
  • 7Zeller R. Influence of stress peening on residual stresses and fatigue limit[ C]. Proceedings of European Conference on Residual Stresses, Germany, 1992:907 -17.
  • 8Ossa E A. Failure analysis of a civil aircraft landing gear[ J]. Engineering Failure Analysis, 2006, 13 : 1177 - 1183.
  • 9Jien Jongchen, Yan Shinshih. A study of the helical effect on the thread connection by three dimensional finite element analysis[J]. Nuclear Engineering and Design, 1999, 191:109 -116.
  • 10Franco L A L, Loureneo N J,Graca M L A,et al. Fatigue Fracture of a Nose Landing Gear in a Military Transport Aircraft [J]. Engineering Failure Analysis, 2006,13 (3) : 474-479.

共引文献107

同被引文献105

引证文献10

二级引证文献37

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