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ZTC4合金高周疲劳断裂机理
High-cycle Fatigue Fracture Mechanism for ZTC4 Alloy
【摘要】 对ZTC4合金室温高周疲劳断裂机理进行研究。结果表明:疲劳裂纹主要沿垂直和平行于α/β片层的方向扩展;裂纹萌生于试样表面、内部晶界以及α/β相界面;源区为类解理断裂,疲劳裂纹扩展区除有大量疲劳条带外,还出现扩展台阶和二次裂纹;断口形貌受晶体学取向和显微组织影响。
【Abstract】 The fracture mechanism of high cycle fatigue on ZTC4 alloy was studied.The results show that the fatigue cracks are mainly vertical and paralleled to the direction of α/β lamellar.The fatigue cracks initiate at the surface of the sample,the internal grain boundaries and α/β phase boundaries.Lots of fatigue striations together with the fatigue sidesteps and secondary cracks generate in the crack propagation regions.The fracture morphologies are deeply affected by crystal orientation and microstructure.
【关键词】 ZTC4合金;
热等静压;
组织;
疲劳裂纹萌生;
扩展;
【Key words】 ZTC4 alloy; hot isostatic pressing; microstructure; fatigue crack initiation; propagation;
【Key words】 ZTC4 alloy; hot isostatic pressing; microstructure; fatigue crack initiation; propagation;
- 【文献出处】 热加工工艺 ,Hot Working Technology , 编辑部邮箱 ,2013年10期
- 【分类号】TG292
- 【被引频次】5
- 【下载频次】189