Investigation on hot deformation behavior of P/M Ni-base superalloy FGH96 by using processing maps

The hot deformation behavior of a powder metallurgy (P/M) Ni-base superalloy FGH96 was investigated at the temperature (T) of 1050-1140 degrees C, strain rate (epsilon) of 0.002-1.0 s(-1), and the height reduction of 20-50% via isothermal hot compression experiment. The flow behavior and the microstructural mechanism of the synthesized superalloy were systematically studied. The processing map was constructed based on the experiment data to evaluate the efficiency of power dissipation and recognize the instability regimes for forging process determination. The processing map with the strain of 0.15 exhibits a smooth and small variation of eta and predicts a little instability regime confined at (T: 1050 degrees C, epsilon : 1.0 s(-1)), attributed to the previous particle boundary (PPB) cracks. The map obtained at the strain of 0.65 reveals a large domain with the efficiency above 40% and predicts two instability regimes at around (1050 degrees C, 1s(-1)) and located in the regime of (T: 1080-1140 degrees C, epsilon : 0.002 - 0.01 s(-1)), respectively. The optimum processing condition is identified as (T: 1140 degrees C, epsilon : 1.0 s(-1)), which presented the highest efficiency in hot working process, as well as the obtained fine microstructure after the hot processing. Via microstructure characterization and observation, it is concluded that the dynamic recrystallization (DRX) occurred at the PPBs in the P/M superalloy. The DRX and the strain rate sensitivity exponent m are both affected by true strain. The local DRX presents a relatively low m in a small strain compression. With an increase of strain, the fraction of the recrystallized grains increases with to. The global DRX. however, presents a relatively high m in a large strain compression. It is thus indicated that the superplasticity of FGH96 superalloy can be realized at a slow strain rate such as 0.001 s(-1) and the deformation temperature of 1110 degrees C, near to the gamma'-transus temperature, by using the uniformly fine-grained superalloys as well as the high temperature superplastic forming equipment. Crown Copyright (C) 2010 Published by Elsevier B.V. All rights reserved.