ICAMS / Interdisciplinary Centre for Advanced Materials Simulation


Rejuvenation of single-crystal Ni-base superalloy turbine blades: Unlimited service life?

B. Ruttert, O. Horst, I. Lopez-Galilea, D. Langenkämper, A. Kostka, C. Somsen, J. V. Görler, M. A. Ali, O. Shchyglo, I. Steinbach, G. Eggeler, W. Theisen.

Metallurgical and Materials Transactions A, 49, 4262–4273, (2018)

Schematic illustration of Creep-Rejuvenation-Creep(CRC) cycle and corresponding creep curves, where black and red curves show the strain accumulation on the heat treated and rejuvenated microstructure, respectively

Rejuvenation of the initially hot isostatic pressing (HIP) heat-treated single-crystal Ni-base superalloy (SX) ERBO/1 was examined experimentally and via phase field simulation to establish rejuvenation treatments as a cost-effective alternative for another interval of service life. Creep was performed at 950 °C and 350 MPa, and the specimens were crept to 0.6 pct (creep rate minimum) or 2 pct strain, respectively. A slight coarsening of the γ/γ′ microstructure was observed experimentally and via simulation at 0.6 pct and rafting at 2 pct strain. The damaged microstructures were rejuvenated in a novel hot isostatic press that provides fast quenching rates before the same specimens were recrept under the same initial creep conditions. High-resolution microscopy proves that the rejuvenation re-establishes the original γ/γ′ microstructure in the dendrite core of the precrept specimens (0.6 and 2 pct). However, the interdendritic areas of the 2 pct precrept and rejuvenated specimen still contain elongated γ′ particles enwrapped by interfacial dislocation networks that survived the applied rejuvenation. The subsequent experimental and simulated creep tests after rejuvenation demonstrated that the creep behavior is only reproducible by the proposed rejuvenation for specimens that had crept until the end of the primary creep regime.

DOI: 10.1007/s11661-018-4745-6
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