Abstract

Growth of corner cracks at temperatures up to 700°C under cyclic (0.25 Hz), 300 s dwell at peak load, both at R = 0.1, and constant load conditions has been studied in the nickel base turbine disc alloy Waspaloy. No significant effect of dwell on fatigue crack growth rate (d a/d N) is found at 550°C, where transgranular fatigue cracking predominated. At 600 and 650°C, under dwell cycling a transition to entirely intergranular cracking is accompanied by a severe increase in cyclic crack growth rate. Contrary to the trend for 600–650°C, dwell and constant load data at 700°C shows lower crack growth rates than for 650°C, indicating that a time dependent microstructural change occurs during prolonged exposure at 700°C generating an increased resistance to intergranular cracking. Using the stress intensity range (†K) as a correlating parameter, fatigue crack growth rates are successfully predicted by linear summation of pure fatigue and time dependent data.

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