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 language | English |
---|---|
Pages (from-to) | 4823-4840 |
Number of pages | 18 |
Journal | Philosophical Magazine |
Volume | 86 |
Issue number | 29-31 |
DOIs | |
State | Published - Oct 11 2006 |
Externally published | Yes |
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.
Funders | Funder number |
---|---|
Air Force Office of Scientific Research | FA9550-05-1-0135 |
Defense Advanced Research Projects Agency | F33615-00-C-5215 |