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Effects of shot peening on short crack growth rate and resulting low cycle fatigue behaviour in low pressure turbine blade material

机译:喷丸处理对低压涡轮叶片材料中短裂纹扩展速率和由此产生的低周疲劳行为的影响

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摘要

The effect of shot peening on subsequent low cycle fatigue behaviour of a representative low pressure steam turbine blade material has been investigated in bend test samples. An analysis of the short fatigue crack growth behaviour has been conducted. For samples with no stress concentration feature, shot peening was found to have a more evident beneficial effect at lower strain levels than at higher strain levels, whereas for samples with a stress concentration feature, the beneficial effect was retained even at higher strain levels. Preexisting cracks were observed on the shot peened surface, which started to grow at 10-25% of fatigue life in the low cycle fatigue regime. The crack propagation rate was slower than that observed in the ground sample, suggesting that the shot peening process delayed crack propagation. This improvement in fatigue life has been attributed to the significant slowing of small cracks while growing through surface regions of significant compressive residual stresses and local workhardening developed by the shot peening process. Once cracks in the notch root have penetrated this region in the depth direction, faster crack growth rates, similar to those observed in the ground case, were seen.
机译:已经在弯曲测试样品中研究了喷丸处理对代表性低压蒸汽涡轮叶片材料随后的低周疲劳行为的影响。已经对短疲劳裂纹扩展行为进行了分析。对于没有应力集中特征的样品,发现喷丸强化在较低的应变水平下具有比在较高的应变水平下更明显的有益效果,而对于具有应力集中特征的样品,即使在较高的应变水平下也保留了有益效果。在喷丸处理的表面上观察到预先存在的裂纹,在低循环疲劳状态下,该裂纹在疲劳寿命的10%至25%时开始增长。裂纹扩展速度比在地面样品中观察到的慢,这表明喷丸处理延迟了裂纹扩展。疲劳寿命的这种改善归因于小裂纹的显着减慢,而小裂纹在通过显着压缩残余应力的表面区域中生长时,以及喷丸处理过程中产生的局部加工硬化而增长。一旦切口根部的裂纹沿深度方向穿透该区域,就会发现裂纹扩展速度更快,类似于在地面情况下观察到的。

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