共查询到19条相似文献,搜索用时 140 毫秒
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对断裂的气门弹簧断口部位进行化学成分,金相组织,硬度,断口扫描检验的结果表明,断裂是由于原材料的冶金缺陷造成弹簧表面局部区域出现疲劳裂纹,最终弹簧早期疲劳断裂。 相似文献
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对比研究了TB17钛合金3种典型组织形态(双态组织、网篮组织和片层组织)对其高周疲劳性能的影响,并分析了高周疲劳断口形貌。结果表明:双态组织特征的TB17钛合金具有最高的强塑性匹配水平,但其疲劳寿命与应力呈双线性关系,疲劳性能并不稳定;网篮组织的强塑性稍差,但具有最高的疲劳强度和疲劳比;片层组织的疲劳强度比网篮组织略低,但其疲劳比和拉伸塑性最差。高周疲劳加载应力处于低应力状态时,疲劳裂纹倾向于试样内部、单源萌生,而处于高应力状态时,疲劳裂纹倾向于试样表面、多源萌生。网篮组织存在更多的二次裂纹,且疲劳条带更为清晰密集,裂纹扩展路径更曲折,在扩展时消耗的能量更多。 相似文献
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汽车用弹簧(后簧)在试验过程中发生断裂。对断裂弹簧进行外观检查、金相组织和显微硬度检测,对弹簧断口进行宏微观检查、能谱分析,综合分析弹簧的断裂性质和原因。结果表明,弹簧的断裂性质为疲劳断裂。断裂过程及原因为:弹簧喷丸之前,由于磁粉探伤机故障产生电火花放电,引起弹簧局部接触高温而在表面形成一个烧伤区;该烧伤区破坏了弹簧的表面完整性,导致弹簧疲劳寿命大幅度降低,在试验载荷作用下,从烧伤区萌生疲劳裂纹并发生断裂。改进措施为加强关键设备、工艺的监控,以避免弹簧生产过程中受到异常损伤。 相似文献
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喷丸工艺通过改变试件的表面形貌、微观组织及残余应力等表面完整性可以影响裂纹的萌生和扩展;对于存在缺陷的试件,喷丸的作用机制和影响结果有所不同。采用白光干涉仪、SEM、XRD及显微硬度计等对单边带缺口的H13钢薄板试样喷丸前后的表面完整性进行了测定。并借助原位SEM开展了系列裂纹扩展试验,分析了喷丸对试样疲劳寿命、裂纹扩展速率以及疲劳断口特征的影响。研究结果表明,虽然残余压应力诱发裂纹闭合,但由于喷丸后表面粗糙度的大幅提高增强了缺口效应,表面加工硬化使得韧性有所降低,以及残余应力在加载过程中发生松弛等因素,喷丸后单边带缺口试样的裂纹萌生过程缩短,疲劳寿命降低,且裂纹扩展速率的变化较小。喷丸前后疲劳断口形貌均为准解理特征,喷丸后断口近表面处的撕裂棱特征消失。 相似文献
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The distributions of the extreme-value driving force(s) for surface vs. subsurface fatigue crack formation (nucleation and early growth) in high-cycle fatigue are evaluated for a microstructure variant of duplex Ti-6Al-4V. In polycrystalline metals, previous work has explored estimation of the driving force(s) for fatigue crack formation at the scale of the grains by computing non-local fatigue indicator parameters (FIPs) based on the cyclic plastic strain averaged over domains on the length scale of the grains. Instantiated statistical volume elements (SVEs), which sample the distributed microstructure attributes of interest for a given material system, can be simulated via the finite element method with embedded polycrystalline plasticity models to estimate the distributed plasticity and resulting FIPs. This strategy of simulating multiple SVEs is in contrast to the simulation of a single representative volume element which is typically untenably large for extreme-value distributions of microstructure attributes or response variables. In this work, multiple SVEs are instantiated with both traction-free (i.e. surface) boundary conditions and fully periodic (i.e. subsurface) boundary conditions. In addition to estimating the extreme-value distributions of the FIPs, newly introduced extreme-value marked correlation functions are applied to characterize the coupled crystallographic microstructure attributes (e.g. grain size, grain orientation, grain misorientation) that most influence the extreme-value distributions of the FIPs. It is shown that there is overlap in the distributions of the driving forces for surface vs. subsurface crack formation in the low to moderate range of failure probability based on FIPs; however, at higher failure probability levels, the driving forces are highest for surface crack formation. The overlap in the distributions of the driving forces for fatigue crack formation in the low to moderate probability range may assist in describing the competing surface vs. subsurface failure modes that are observed experimentally. 相似文献
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D.W. Gross K. Nygren G.J. Pataky J. Kacher H. Sehitoglu I.M. Robertson 《Acta Materialia》2013,61(15):5768-5778
The dislocation microstructure beneath surface slip traces produced by fatigue loading of Haynes 230 was revealed to be a function of distance from a crack tip. The microstructure beneath these traces evolves from planar slip bands with increasing dislocation density and decreasing interband spacing as the crack tip approaches one of refined subgrains and lamellar bands at and in the vicinity of the crack tip. Similarly, beneath fatigue striations the microstructure evolves from nanosized subgrains to a banded structure with increasing distance from the fracture surface. These structures are significantly different to those predicted to develop under fatigue loading of a planar slip material. The evolved structures are considered in terms of the microstructure generated by severe plastic deformation. 相似文献
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采用表面机械研磨工艺对工业纯锆进行处理,利用四点弯曲疲劳试验对试样的疲劳性能进行测试。通过对试样微观组织观察、显微硬度和残余应力表征,并结合有限元方法对四点弯曲试样应力分布的模拟,分析表面纳米化对工业纯锆四点弯曲疲劳性能的影响机理。研究表明,表面纳米化工业纯锆相对于原始试样疲劳极限提高约23%。这是由于原始工业纯锆在加载时最大拉应力位于试样表层,导致疲劳裂纹在表层萌生,而表面纳米化工业纯锆由于组织强化及残余压应力作用,使疲劳强度得到提高,并且使裂纹在次表层萌生,从而获得较好的疲劳性能。 相似文献