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表面完整性对30CrMnSiNi2A钢疲劳极限的影响 被引量:17

Influence of surface integrality on fatigue limit for 30CrMnSiNi2A steel
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摘要 采用喷丸强化和振动冲击强化两种表面形变强化方法改变 30CrMnSiNi2A钢的表面完整性 ,用升降法测定了 10 7循环周次下光滑试样的疲劳极限。试验结果表明 ,振动强化使疲劳极限提高 11% ,喷丸强化使疲劳极限提高 16 %。 The changes of surface integrality caused by shot peening and vibration peening were investigated and its influence on fatigue limit of 30CrMnSiNi2A steel for 107 cycles was determined. Due to the local plastic deformation, residual stresses are developed and the surface topography is changed. Results on the influence of shot peening and vibration peening on 30CrMnSiNi2A steel are compared. The results indicate that the fatigue endurance limit of the shot-peened specimens is higher than the corresponding limit of the virgin specimens by about 16% and the fatigue limit of vibration-peened specimens is higher than that of virgin specimens by about 11%. The reason why fatigue limit is improved is that surface integrality is modified by mechanical surface treatment such as shot peening and vibration peening.
出处 《航空材料学报》 EI CAS CSCD 2002年第2期21-23,共3页 Journal of Aeronautical Materials
关键词 表面完整性 30CRMNSINI2A钢 疲劳极限 影响 喷丸强化 振动强化 Chromium Fatigue of materials Plastic deformation Residual stresses Shot peening Surface topography Surface treatment Vibrations (mechanical)
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  • 1高玉魁,硕士学位论文,2000年
  • 2赵振业,合金钢设计,1999年
  • 3王声平,博士学位论文,1994年
  • 4李金魁,博士学位论文,1989年
  • 5朱荆璞,金属表面强化技术,1989年
  • 6束德林,金属力学性能,1987年
  • 7刘锁,金属材料的疲劳性能与喷丸强化工艺,1977年

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