Competition between work-hardening effect and dynamic-softening behavior for processing as-cast GH4720Li superalloys with original dendrite microstructure during moderate-speed hot compression
“…The preferred properties of Ni-Fe-Cr-base superalloys are highly related to the hot forming processes [3,4]. During hot forming, the DRX behaviors of Ni-Fe-Cr-base superalloys are highly intricate owing to the multiple alloying compositions [5,6,7,8]. Meanwhile, the complex microstructure, large deformation resistance, and narrow forming temperature range make hot forming processes very complicate [ 9 , 10 ].…”
“…The preferred properties of Ni-Fe-Cr-base superalloys are highly related to the hot forming processes [3,4]. During hot forming, the DRX behaviors of Ni-Fe-Cr-base superalloys are highly intricate owing to the multiple alloying compositions [5,6,7,8]. Meanwhile, the complex microstructure, large deformation resistance, and narrow forming temperature range make hot forming processes very complicate [ 9 , 10 ].…”
“…As a consequence, creep-fatigue is the dominant damaging mode for a turbine disc, which is the life limiting damage to be considered in the design of a turbine disc [1][2][3]. GH720Li (in Chinese series, similar to Udimet 720Li in the series of U.S.A), a Ni based γ′ strengthened superalloy, is one of the most successful superalloys for turbine discs for a long-term employ at 650-750°C due to its excellent creep, fatigue, oxidation and corrosion resistance at high temperatures [4,5]. Therefore, the creep-fatigue behavior of turbine discs of superalloy GH720Li is the focus of this investigation by performing creep-fatigue experiments with different dwell times at the maximum load.…”
“…The bulging of initial grain boundaries is the main nucleation mechanism of dynamic recrystallization (DRX). Other studies have focused on the work-hardening behavior of nickel-based superalloys during hot deformation, and the constitutive model based on the stress–strain relationship [14,15,16,17,18,19,20,21,22,23,24,25]. The hot deformation behaviors of the Ni-based superalloy are investigated by tensile and compressional tests over a wide range of strain rates and deformation temperatures.…”
High-temperature compression and electron backscatter diffraction (EBSD) techniques were used in a systematic investigation of the dynamic recrystallization (DRX) behavior and texture evolution of the Inconel625 alloy. The true stress–true strain curves and the constitutive equation of Inconel625 were obtained at temperatures ranging from 900 to 1200 °C and strain rates of 10, 1, 0.1, and 0.01 s−1. The adiabatic heating effect was observed during the hot compression process. At a high strain rate, as the temperature increased, the grains initially refined and then grew, and the proportion of high-angle grain boundaries increased. The volume fraction of the dynamic recrystallization increased. Most of the grains were randomly distributed and the proportion of recrystallized texture components first increased and then decreased. Complete dynamic recrystallization occurred at 1100 °C, where the recrystallized volume fraction and the random distribution ratios of grains reached a maximum. This study indicated that the dynamic recrystallization mechanism of the Inconel625 alloy at a high strain rate included continuous dynamic recrystallization with subgrain merging and rotation, and discontinuous dynamic recrystallization with bulging grain boundary induced by twinning. The latter mechanism was less dominant.
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