The 22nd Advanced Aerospace Materials and Processes (AeroMat) Conference and Exposition (May 23-25, 2011) of ASM

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Monday, May 23, 2011 - 10:30 AM
MDE1.5

A New Constitutive Model for Anisotropic Creep Behavior of Ni-Base Single Crystal Superalloys In the Low Temperature, High Stress Regime

Y. S. Choi, T. A. Parthasarathy, UES, Inc., Dayton, OH; C. Woodward, D. M. Dimiduk, M. D. Uchic, Air Force Research Laboratory, AFRL/RXLM, Wright-Patterson AFB, OH

A new crystallographic constitutive model was developed in order to capture orientation sensitive primary and secondary creep behaviors within about 20 degrees from the [0 0 1] in single crystal superalloys at the low temperature and high stress regime.  The crystal plasticity based constitutive formulations incorporate experimentally observed dislocation micro-mechanisms.  This parameterization numerically delineates the nucleation, propagation and hardening of a<1 1 2> dislocations (ribbons) that shear gamma-prime precipitates by creating stacking faults.  Detailed numerical descriptions involve slip system kinematics from a/2<1 1 0> dislocations shearing the gamma-phase matrix, a<1 1 2> stacking fault dislocation ribbons shearing the gamma-prime-phase precipitate, and interactions between the two cases.  The new constitutive model was implemented in the FEM framework, and used to predict primary and secondary creep of a single crystal superalloy CMSX-4 in three selected orientations near the [0 0 1] at 750 oC and 750 MPa.  Simulation results showed a reasonable agreement with the experimental data. Modeling results also indicated that a/2<1 1 0> matrix dislocations are important in limiting the propagation of a<1 1 2> SF dislocation ribbons, which leads to the transition to secondary creep.