Prediction of oxidation-assisted crack growth has been carried out for a nickel-based superalloy at elevated temperature based on finite element analyses of oxygen diffusion, coupled with viscoplastic deformation, near a fatigue crack tip. The material constitutive behaviour, implemented in the fini
Crack growth in a coated gas turbine superalloy under thermo-mechanical fatigue
โ Scribed by Arnd Jung; Alexander Schnell
- Publisher
- Elsevier Science
- Year
- 2008
- Tongue
- English
- Weight
- 505 KB
- Volume
- 30
- Category
- Article
- ISSN
- 0142-1123
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โฆ Synopsis
The out-of-phase thermo-mechanical fatigue (TMF) behaviour of the single crystal superalloy CMSX-4 was studied in the uncoated and in the low-pressure plasma sprayed (LPPS) coated condition. In addition, growth measurements of in-depth coating cracks were performed. Cyclic hardening of the substrate and superimposed multiple crack initiation/propagation within the coating leads to cyclic softening that consumes a significant portion of TMF lifetime. A three-step crack propagation mode of the coated material is described. Special attention is paid to the role of the inter-diffusion zone, since coating cracks are decelerated in the inter-diffusion zone before penetrating into the substrate.
๐ SIMILAR VOLUMES
This paper deals with the prediction of fatigue crack growth at high temperatures in the N18 nickel base superalloy, which is employed by Snecma for turbine disc applications. This material and other nickel base superalloys were widely studied in the past under isothermal conditions and constant amp