INFLUENCE OF RESIDUAL STRESS AND SURFACE MORPHOLOGY ON FATIGUE PROPERTIES OF STEEL 60Mn

Influence of residual stress and surface morphology induced by shot-peening on fatigue behav-ior of a medium temperature tempered spring steel 60 Mn has been studied.The compressiveresidual stress induced in the near-surface region may improve fatigue limit from 930 to 1010MPa,and the very high tensile residual stress in the interior may reduce it from 1010 to 940MPa,whereas the severe surface damage may cause a drop-off of it from 1010 down to 800MPa.Fatigue cracks initiated in such position where the equivalent Mises stress,includingresidual stress,exceeded the local strength of the material.The compressive residual stress,induced by shot-peening,may intensify the effect of crack closure,so as to decrease the crackgrowth rate.     

表面处理对Ti-6-22-22合金高温疲劳寿命的影响

采用喷丸和离子注入对Ti-6-22-22合金机械加工样品进行表面处理,研究表面处理对Ti-6-22-22合金室温和高温疲劳寿命的影响.结果表明,喷丸和离子注入对材料疲劳S-N曲线的影响与实验温度有关.喷丸和离子注入对Ti-6-22-22合金的室温疲劳强度影响较小,400℃时的疲劳强度明显提高.SEM断口分析显示,400℃长寿命疲劳后的表面处理样品裂纹在亚表面萌生.     

基于SPH结合FEM的喷丸残余应力数值模拟

针对以往有限元模型中弹丸数量较少且为规则阵列排布的缺陷,采用光滑粒子流体动力学法(Smoothed particle hydrodynamics,SPH)与有限元法(Finite element method,FEM)相结合的方法,对喷丸过程进行数值模拟;使用MATLAB对弹丸空间位置坐标进行随机化处理,形成了大量丸粒冲击工件表面的随机喷丸仿真模型。通过分析确定了喷丸饱和时间,研究了喷射角度、弹丸流量对残余应力场的影响。结果表明:在喷丸参数一定的条件下,存在相应的饱和喷丸时间;研究喷丸参数对残余应力的影响时,应在喷丸达到饱和时间之后提取残余应力值;喷射角度增大,残余压应力增大;开始时弹丸流量增大,残余压应力会有所增大,但当其达到饱和值后,残余压应力不再变化。     

Fatigue performance of metastable β titanium alloys: Effects of microstructure and surface finish

This investigation examined the role of microstructure and surface finish on the high cycle fatigue (HCF) performance of TIMETAL LCB (Ti-6.8Mo-4.5Fe-1.5Al). The as-received microstructure of LCB consisted of elongated β grains with a semicontinuous grain boundary α layer. In contrast, a fine equiaxed β + spheroidized α LCB microstructure was achieved by hot swaging and solution (recrystallization) anneal. The latter modification of the prior β grain structure, together with the size, morphology, and distribution of the primary α phase, resulted in a significant enhancement in the tensile and HCF properties. Furthermore, prestraining (PS), as would be expected during the fabrication of an automotive coil spring, and prior to aging for 30 min at temperatures between 500 and 550 °C, led to additional increases in tensile strength. In contrast, the HCF performance was always reduced when PS prior to aging was included in the overall processing procedure. Finally, shot-peening and roller-burnishing both resulted in an increased fatigue life in the finite life regimen; however, significant reductions in the 10⁷ cycle fatigue strengths were observed when these procedures were used. These observations have been explained by including the effect of process-induced residual tensile stresses in the fatigue analysis, resulting in subsurface fatigue crack nucleation. This paper was presented at the Beta Titanium Alloys of the 00’s Symposium sponsored by the Titanium Committee of TMS, held during the 2005 TMS Annual Meeting & Exhibition, February 13–16, 2005 in San Francisco, CA.     

液体喷丸在汽轮机零件表面强化上的应用

介绍了液体喷丸技术中的参数选择及在汽轮机零件表面强化中的应用。     

The effect of hole drilling on fatigue and residual stress properties of shot-peened aluminum panels

The effect of hole drilling after shot peening on the fatigue life and residual stress state of selected aluminum alloys was investigated. Compared to the unpeened condition, the hole drilling after shot peening reduced the fatigue life of the 2024-T351 and 2324-T39 alloys to a small extent. On the other hand, the fatigue life of 7150-T7751 decreased considerably due to hole drilling after shot peening. A compressive residual stress was at the surface of the shot peened specimens. Hole drilling reduced the compressive residual stress by 60%. The excess dislocation density was mostly concentrated at the surface of the specimens.     

喷丸对DD6单晶高温合金拉伸性能的影响

采用扫描电子显微镜(SEM)、X射线(X-ray)和透射电子显微镜(TEM)等手段研究铸钢丸喷丸对第二代单晶高温合金DD6在500,600,650℃拉伸性能的影响。结果表明:500,600,650℃时,喷丸对DD6合金抗拉强度影响不大,略微提高屈服强度,显著降低伸长率和断面收缩率。喷丸DD6合金在流变应力上升到最高点后断裂,试样拉伸断裂后的横截面为圆形;未喷丸DD6合金拉伸曲线呈现双重阶段特征,试样拉伸断裂后的横截面为椭圆形。     

喷丸对DD6单晶合金高温疲劳性能的影响

用陶瓷丸CZ50对DD6单晶高温合金(简称DD6单晶)进行喷丸,研究喷丸后DD6单晶的表面形貌和650℃旋转弯曲疲劳应力-寿命曲线的变化。结果表明:喷丸消除了加工刀痕,缓和了表面应力集中;DD6单晶喷丸后疲劳极限达到486MPa,比未喷丸的原始试样提高了19.7%。喷丸后试样疲劳源呈现小刻面状的原因是由于喷丸强化层内较大的位错密度,裂纹扩展方向在距疲劳源30～50μm处出现变化,延长了单晶高温合金的扩展寿命。     

喷丸强化对H08Mn2Si堆焊层残余应力及组织结构的影响

利用气动式喷丸机对H08Mn2Si堆焊层表面进行强化处理。借助X射线衍射方法,研究了强化层中残余应力沿材料层深分布规律,采用金相显微镜、显微硬度仪、三维形貌仪分析了强化层的组织结构、显微硬度和表面粗糙度。结果表明:喷丸强化使H08Mn2Si堆焊层形成了约500μm的强化层,表层的显微硬度呈先增大后减小的趋势,金相分析表明铁素体组织未发生转化,表面粗糙度有不同程度的增大。     

提高水力机械抗磨蚀性能的喷丸工艺数值分析

针对流体机械磨蚀特点,对喷丸工艺引起的残余应力场进行数值模拟。运用有限单元法对弹丸撞击后钢板材料表面应力分布进行了数值计算。讨论了弹丸直径、喷射速度与残余应力的关系,选择几组典型参数比较,分析不同情况下喷丸对局部变形的影响,进而探讨了水力机械防磨蚀的喷丸强化工艺参数的选择。