首页> 外文会议>1st International Conference on Component Optimisation, 1st, Mar 29 - Apr 1, 1999, University of Wales, Swansea, United Kingdom >EFFECTS OF LOADING WAVEFORM ON FATIGUE CRACK GROWTH AT ELEVATED TEMPERATURE IN NICKEL BASE SUPERALLOYS
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EFFECTS OF LOADING WAVEFORM ON FATIGUE CRACK GROWTH AT ELEVATED TEMPERATURE IN NICKEL BASE SUPERALLOYS

机译:加载波形对镍基高温合金高温下疲劳裂纹扩展的影响

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The effects of loading waveform on fatigue crack growth in Alloy X at 650℃ have been examined. Fatigue crack growth behaviour was studied at frequencies from 0.001 to 2.5Hz using triangular and sawtooth waveforms. The fracture mode was found to be predominantly mixed trans/ intergranular. Further research was carried out under dwell waveforms with dwell at maximum load from 1 to 1000 s. Effects of dwell became significant with dwell times above 120 s. All tests were carried out under constant , load ratio and temperature conditions. Fatigue mechanism maps have been produced for Alloy X , showing the different modes of failure under various loading waveforms. The results have been compared with those of U720Li and Waspaloy and correlated with models by Gayda (2) and Tong & Byrne (1).
机译:研究了加载波形对650℃X合金疲劳裂纹扩展的影响。使用三角波和锯齿波在0.001至2.5Hz的频率下研究了疲劳裂纹扩展行为。发现骨折模式主要是反式/晶间混合。在驻留时间为1到1000 s的最大负载下的驻留波形下​​进行了进一步的研究。驻留时间超过120 s时,驻留效果变得显着。所有测试均在恒定,负载比和温度条件下进行。合金X的疲劳机理图已经绘制出来,显示了在各种载荷波形下的不同破坏模式。该结果已与U720Li和Waspaloy的结果进行了比较,并与Gayda(2)和Tong&Byrne(1)的模型相关。

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