Failure Mechanisms in Thermo-Mechanical Fatigue of DS Superalloy Rene 80

Directionally solidified (DS) Rene 80 Superalloy was tested in thermo-mechanical fatigue (TMF) over the temperature range 500-900°C and plastic strain levels from 0.2 to 0.8% using a DSI Gleeble thermal simulator. Thermo-mechanical testing was carried out on the parent material in the conventional solution treated and aged condition (STA), as well as gas tungsten arc welded with an IN-738 filler, followed by solution treatment and ageing. Comparison of the base TMF unwelded alloy with that of the welded and heat treated alloy showed that varying crack initiation mechanisms, notably oxidation either by stress assisted grain boundary oxidation, or associated with grain boundary MC carbides fatigue crack propagation along grain boundaries and creep deformation were operating, leading to different "weakest link" failure initiation points.