细晶表面种植体钛合金的长寿命疲劳断裂特性

    Long Life Fatigue Fracture Characterics of Implant Titanium Alloys with Fine Grain Surface

    • 摘要: 借助超声冲击对植入物用Ti6Al4V(TC4)和Ti3Zr2Sn3Mo25Nb(TLM)两种钛合金进行细晶表面强化。采用透射电镜对表面细晶进行表征,在扫描电镜下对长寿命疲劳断面进行观察,分析两者的断裂特性。结果表明,位错滑移不仅是TC4和TLM表面细晶的主要形成机制,而且是长寿命内部裂纹的萌生机制。多滑移系的β相为TC4钛合金中α相变形提供了便利,其滑移汇聚的三叉晶界成为TLM钛合金中的微裂纹核心。通过TC4裂纹源区零散的滑移小平面及TLM裂纹源密集的滑移线近似划出Facet区后,根据村上公式计算得到的断裂应力强度因子略高于未处理试样。

       

      Abstract: The surface of two implant titanium alloys Ti6Al4V(TC4) and Ti3Zr2Sn3Mo25Nb(TLM)were modified into fine grains by ultrasonic impact. The surface fine grains were characterized by TEM. The fatigue fracture surface of long-life specimens were investigated with SEM. The fracture characterics were analyzed. The results show that the dislocation glide is not only the main formation mechanism of fine grains in the surface of TC4 and TLM, but also the initiation mechanism of long-life internal cracks. Multi slip system β phase is advantage to the deformation of α phase in TC4. The trigeminal grain boundary of the converged slip of β phase is usually the core of the micro cracks of TLM. The facet area can be approximately delineated by the scattered slip Facets in the crack initiation of TC4 and the dense slip lines of the TLM’s crack initiation.According to the Murakami formula, the calculated fracture stress intensity factor is slightly higher than which of the untreated specimen.

       

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