Microtwinning during intermediate temperature creep of polycrystalline Ni-based superalloys: Mechanisms and modelling

G. B. Viswanathan, S. Karthikeyan, P. M. Sarosi, R. R. Unocic, M. J. Mills

Research output: Contribution to journalArticlepeer-review

67 Scopus citations

Abstract

Deformation mechanisms, operative during intermediate temperature creep of Ni-based polycrystalline superalloys, are poorly understood. The creep deformation substructure has been characterized in Renè 88DT following rapid cooling from the super-solvus temperature, yielding a fine γ′-precipitate microstructure. After creep to modest strain levels (up to 0.5% strain) at 650°C and an applied tensile stress of 838 MPa, microtwinning is found to be the predominant deformation mode. This surprising result has been confirmed using diffraction contrast and high-resolution transmission electron microscopy. Microtwinning occurs via the sequential movement of identical 1/6[11-2] Shockley partials on successive (111) planes. This mechanism necessitates reordering within the γ′ precipitates in the wake of the twinning partials, so that the L1 2 structure can be restored. A quantitative model for creep rate has been derived on the basis that the reordering process is rate-limiting. The model is in reasonable agreement with experimental data. The results are also discussed in relation to previous studies under similar deformation conditions.

Original languageEnglish
Pages (from-to)4823-4840
Number of pages18
JournalPhilosophical Magazine
Volume86
Issue number29-31
DOIs
StatePublished - Oct 11 2006
Externally publishedYes

Funding

Support for this work has been provided by the DARPA Accelerated Insertion of Materials (AIM) Program under contract F33615-00-C-5215 and by the Air Force Office of Scientific Research, for model development, through the MEANS-2 theme grant # FA9550-05-1-0135.

FundersFunder number
Air Force Office of Scientific ResearchFA9550-05-1-0135
Defense Advanced Research Projects AgencyF33615-00-C-5215

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