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FATIGUE CRACKS INITIATION AND PROPAGATION BEHAVIOR IN WELDED JOINTS OF TITANIUM ALLOY

机译:钛合金焊接接头的疲劳裂纹萌生和扩展行为

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In this article, in-situ observation upon the dynamic extension of low cyclic fatigue cracks in weld fuse zone(FZ) and heat affected zone(HAZ) for TA15 titanium alloy were carried out. The results show that there are both two stages(stage I and stage II) during the process of fatigue crack propagation in FZ and HAZ. Slips at the tip of the cracks in FZ are very clear in the whole crack growth process and slip lines are much longer than those in HAZ which can only be found in fast expanded area. The fatigue cracks in HAZ are more deviated and bifurcate than those in FZ during the process of fatigue cracks propagation. And more secondary cracks are also found near the main crack at the surface of HAZ. Furthermore, the crack growth rates in FZ are larger than those in HAZ. It is concluded that the different fatigue crack growth behaviors between HZ and HAZ are related to different microstructures.
机译:本文对TA15钛合金的熔接区(FZ)和热影响区(HAZ)的低周疲劳裂纹的动态扩展进行了现场观察。结果表明,在FZ和HAZ疲劳裂纹扩展过程中,有两个阶段(第一阶段和第二阶段)。在整个裂纹扩展过程中,FZ裂纹尖端的滑移非常清晰,滑移线比热影响区中的滑移线长得多,后者只能在快速扩展的区域中找到。在疲劳裂纹扩展过程中,热影响区中的疲劳裂纹比FZ中的疲劳裂纹更加偏斜和分叉。在热影响区表面的主裂纹附近还发现了更多的次级裂纹。此外,FZ的裂纹扩展速率大于HAZ的裂纹扩展速率。结论:HZ和HAZ之间不同的疲劳裂纹扩展行为与不同的微观结构有关。

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