Effect of Microstructure Instability on Hot Plasticity During Thermomechanical Processing in PM Nickel-Based Superalloy
Ming ZHANG1,2, Guoquan LIU1,2(), Benfu HU1
1 School of Materials Science and Engineering, University of Science and Technology Beijing, Beijing 100083, China 2 Collaborative Innovation Center of Steel Technology, University of Science and Technology Beijing, Beijing 100083, China
Cite this article:
Ming ZHANG, Guoquan LIU, Benfu HU. Effect of Microstructure Instability on Hot Plasticity During Thermomechanical Processing in PM Nickel-Based Superalloy. Acta Metall Sin, 2017, 53(11): 1469-1477.
High alloying Ni-based powder metallurgy (PM) superalloys show excellent fatigue performance and damage tolerance properties, and good creep resistance at 750 ℃, and are used for advanced gas turbine disks and other hot components. The hot-working window of high alloying PM superalloy is narrow because of its poor workability. The formation of the γ+γ′ microduplex structure during the thermomechanical processing always results in a decrease in flow stress and a promotion of hot plasticity. However, the stability of the γ+γ′ microduplex structure has not been evaluated. The high temperature flow behavior of a Ni-based superalloy FGH98 prepared by hot isostatic pressing has been examined by means of uniaxial compression testing isothermally at 1060, 1105, 1138 and 1165 ℃ and at constant true strain rates between 0.01 and 10 s-1. The microstructural evolution and instabilities during plastic flow have been studied. Under all testing conditions, the as-hipped material exhibits flow hardening, flow softening and steady-state flow sequentially with the true strain increased. The dynamic recrystallization occurs and the γ+γ′ microduplex structures are generated when steady state flow or highest strains achieved at temperatures below the γ′ solvus. The formation of the γ+γ′ microduplex structures results in a remarkable decrease in grain size and a promotion of hot plasticity. The relationships between steady-state grain sizes and steady-state stresses during deformation and the formation mechanism of the γ+γ′ microduplex structure were analyzed. The possibility of the microstructure controlling during hot working was discussed.
Fund: Supported by National High Technology Research and Development Program of China (No.2015AA034201) and National Natural Science Foundation of China No.51371030
Fig.1 Quantities for sizing irregular planar grain
Fig.2 Microstructure of hot isostatic pressed FGH98 alloy at 1180 ℃, 130 MPa, 3 h (a) and morphology of γ′ phase (b)
Fig.3 True stress-true strain (σ-ε) curves of hot isostatic pressed FGH98 alloy at 1060 ℃ (a), 1105 ℃ (b), 1138 ℃ (c) and 1165 ℃ (d)
Fig.4 Microstructures of as-deformed FGH98 alloy at T=1105 ℃, =1 s-1 and ε =0.2 (a), 0.4 (b), 0.6 (c) (T—temperature, —strain rate)
Fig.5 Microstructures of as-deformed FGH98 alloy at ε =0.6, =1 s-1 and T=1060 ℃ (a), 1105 ℃ (b), 1138 ℃ (c) and 1165 ℃ (d)
Fig.6 Microstructures of as-deformed FGH98 alloy at ε =0.6, T=1105 ℃ and =0.01 s-1 (a), 0.1 s-1 (b), 1 s-1 (c) and 10 s-1 (d)
Fig.7 TEM image of γ+γ′ microduplex structure
Fig.8 Strain induced γ-γ′ interface migration led to dissolution (a) and re-precipitation (b) of γ′phase (D, E and F are the new microduplex structures formed in discontinuous dynamic recrystallization. The arrows indicate the migration of γ-γ′ interface)
Fig.9 Processing maps at ε =0.2 (a), 0.4 (b) and 0.6 (c)
Fig.10 Effect of true strain on grain size (λ), σ and efficiency of power dissipation (η) at T=1105 ℃, =1 s-1
Fig.11 Effect of temperature on grain size, steady-state stress and efficiency of power dissipation at ε =0.6, =1 s-1 (σs—steady state stress)
Fig.12 Relationships between steady-state stress and steady-state grain size at ε =0.6
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