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LOW-CYCLE FATIGUE OF NICKEL-BASED SUPERALLOY HASTELLOY X AT ELEVATED TEMPERATURES

机译:镍基超合金Hastelloy X的低循环疲劳在升高的温度下

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The fully-reversed total strain-controlled low-cycle fatigue tests with and without hold times, as well as stress-relaxation tests, were conducted at 816°C and 927°C in laboratory air on a nickel-based superalloy, HASTELLOY X. The influence of temperatures and hold times on low-cycle fatigue behavior of the alloy was investigated. At both temperatures of 816°C and 927°C, the alloy exhibited initial cyclic hardening, followed by a saturated cyclic stress response or cyclic softening under low-cycle fatigue without hold times. For low-cycle fatigue tests with hold times, however, the alloy showed either cyclic hardening or cyclic stability, which is closely related to the test temperature and the duration of the hold time. It was also observed that the low-cycle fatigue life of the alloy considerably decreased due to the introduction of strain hold times. Generally, a longer hold time would result in a greater reduction in the fatigue life. However, for the tests without hold times, the test temperature seems to have little influence on the fatigue life of the alloy at the test temperatures used in this investigation. The stress relaxation tests show that at the beginning of swain hold, the stress drops very quickly and then decreases very slowly with prolonging time. In addition, the fracture surfaces of the fatigued specimens were observed using scanning electron microscopy to determine the crack initiation and propagation modes. The fatigue life was predicted by the frequency modified tensile hysteresis energy method. The predicted lives were found to be in good agreement with the experiment results.
机译:在816°C和927°C上,在镍的超合金,Hastelloy X上的实验室空气中,在816°C和927°C下进行全反转的总应变控制的低循环疲劳试验以及应激缓解试验。研究了温度和保持时间对合金的低循环疲劳行为的影响。在816°C和927℃的两个温度下,合金表现出初始环状硬化,然后在低周期疲劳下饱和循环应力响应或循环软化而没有保持时间。然而,对于保持时间的低循环疲劳试验,合金显示循环硬化或循环稳定性,其与测试温度和保持时间的持续时间密切相关。还观察到,由于引入应变持续时间,合金的低循环疲劳寿命显着降低。通常,更长的保持时间会导致疲劳寿命更大。然而,对于没有保持时间的测试,测试温度似乎对该研究中使用的测试温度的对合金的疲劳寿命几乎没有影响。压力松弛测试表明,在Swain Hold的开始时,压力很快掉落,然后随着延长时间慢慢降低。另外,使用扫描电子显微镜观察疲劳标本的断裂表面,以确定裂纹引发和传播模式。通过频率改性拉伸滞后能量方法预测疲劳寿命。预测的生命被发现与实验结果一致。

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