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HIGH CYCLE FATIGUE OF AN ORTHORHOMBIC TI-22AL-25NB INTERMETALLIC ALLOY

机译:正骨间Ti-22AL-25NB金属间合金的高循环疲劳

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An evaluation of fatigue behavior of the orthorhombic Ti-22Al-25Nb intermetallic alloy with the duplex microstructure has been carried out with high cycle rotary bending fatigue testing at room temperature (RT), 650°C and 750°C with a test frequency of 50Hz. The testing results show that the fatigue strengths (σ{sub}(-1)) are up to 530MPa at RT, 600MPa at 650°C at or more than 1×10{sup}7 cycles, and 500MPa at 750°C at 8.34×10{sup}6 cycles. Damage mechanisms at crack initiation sites and crack propagation were investigated with the use of scanning electron microscopy. The fatigue failure mechanisms of the duplex microstructure of the present alloy are simply discussed.
机译:在室温(RT),650°C和750°C的高循环旋转弯曲疲劳试验中进行了对双工微结构的疲劳性能与双工微观结构的疲劳行为评价。测试频率为50Hz 。测试结果表明,疲劳强度(σ{sub}( - 1))在室温下高达530MPa,650℃以上或超过1×10 {sup} 7个循环,500mpa在750°C处8.34×10 {sup} 6周期。利用扫描电子显微镜研究了裂缝引发位点和​​裂纹繁殖的损伤机制。简单地讨论了本合金的双工微结构的疲劳失效机制。

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