High temperature fatigue crack growth in Inconel 718

The nickel base superalloys are extensively used in high temperature applic ations, so it is important to know their behaviour under conditions of high -temperature fatigue. This paper studies the influence of DeltaK, loading f requency, stress ratio and temperature on the high temperature fatigue crac k growth rate of nickel base superalloys. This study is based on fatigue te sts carried out in corner crack specimens of Inconel 718 at 600 degreesC an d at room temperature. Three stress ratios (R = 0.05, 0.5 and 0.8) and load ing frequencies ranging from 0.0017 to 15 Hz were considered in the tests. For frequencies below 0.25 Hz, the load waveshape was trapezoidal with diff erent dwell times at maximum load. At relatively high frequencies the propa gation is cycle dependent, while for lower frequencies it is time dependent . At intermediate frequencies a mixed crack growth occurs. The transition f requencies from cycle dependent to mixed regime and from mixed to time depe ndent regime were obtained for each R. The increase of R increases the tran sition frequencies, i.e., extends the time dependent crack growth to higher frequencies. The increase of R also produces an increase of cyclic crack g rowth rate for all regimes of crack growth. In the time dependent regime, a higher variation is observed, that can be explained by an acceleration of oxidation damage promoted by the increase of maximum stress. An approach fo r modelling the high-temperature fatigue crack growth in nickel base supera lloys is presented. A good agreement was observed between time dependent fa tigue results and mathematical models based on static load results.