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HIGH CYCLE FATIGUE OF TI-6AL-4V ALLOY IN SIMULATED STEAM ENVIRONMENT

机译:模拟蒸汽环境中TI-6AL-4V合金的高循环疲劳

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Fatigue life and reliability are the critical problems for long blades design due to complicated stress state, wet steam and aggressive environment. In this report, the effects of stress ratio, surface properties, steam, and sodium-chloride (NaCl) aqueous environments on the fatigue strength and fracture mechanisms of Ti-6Al-4V alloy have been investigated. Results indicate that residual compressive stress decreases and vanishes finally with increasing stress ratio. Compared to fatigue crack originating from surface for annealed specimens, the fatigue crack initiation sites are located in the interior of the specimen due to the effect of residual stress when low stress ratios are present. Fatigue experiments have been performed in saturated steam with low oxygen content at 100°C and NaCl aqueous at 80 °C. Results indicate that, for 0.1 stress ratio loading conditions, steam environment demonstrates the most serious effect on the endurance limit with 12.3% reduction of fatigue strength. NaCl aqueous leads to the 9.6% drop in fatigue strength corresponding to 10~7 cycles of design life. For all corrosion environments, cracks originated from the surface and no corrosion pits were observed.
机译:由于复杂的应力状态,湿蒸汽和侵蚀性环境,疲劳寿命和可靠性是长叶片设计的关键问题。在这份报告中,研究了应力比,表面性能,蒸汽和氯化钠(NaCl)水性环境对Ti-6Al-4V合金的疲劳强度和断裂机理的影响。结果表明,残余压缩应力随着应力比的增加而减小并最终消失。与源自退火样品表面的疲劳裂纹相比,由于存在低应力比,由于残余应力的影响,疲劳裂纹萌生点位于样品内部。疲劳实验是在100°C的低氧含量的饱和蒸汽和80°C的NaCl水溶液中进行的。结果表明,在0.1应力比的加载条件下,蒸汽环境显示出对耐力极限的最严重影响,疲劳强度降低了12.3%。氯化钠水溶液导致疲劳强度下降9.6%,相当于设计寿命的10〜7个循环。对于所有腐蚀环境,裂纹均源自表面,没有观察到腐蚀坑。

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