The coarse and non-uniform grain structures arising from microstructural heredity in large rotors fabricated from 9Cr-3 W-3Co martensitic heat-resistant steel present a significant challenge to m
echanical property uniformity. This study investigates the influence of isothermal annealing pretreatment (single-step and stepwise) in conjunction with tempering temperature (700 ℃, 710 ℃, and 720 ℃) on microstructural homogeneity and mechanical properties. Both annealing routes, followed by normalizing, refined the prior austenite grains to ASTM No. 7.0 or finer. Notably, stepwise isothermal annealing substantially enhanced the spatial uniformity of the grain size and effectively mitigated the post-forging microstructural heredity. Following quenching and tempering, differences in strength and ductility between specimens subjected to the different isothermal annealing cycles were negligible (
<
5%). However, stepwise annealing significantly improved impact toughness and reduced data scatter. Tempering temperature was identified as the dominant factor controlling the strength-toughness balance: increasing the tempering temperature from 700 ℃ to 720 ℃, decreased the tensile strength from 852 MPa to 817 MPa, while concurrently increasing the impact absorbed energy from 22.3 J to 33.3 J. The optimal combination of properties (Rm
>
830 MPa, Rp
0.2
>
680 MPa, impact energy
>
24 J) was achieved through stepwise isothermal annealing followed by tempering at 710 ℃. This improvement is primarily attributed to the refinement and homogeneous distribution of carbides, as well as improved prior austenite grain uniformity. These findings provide a critical theoretical and experimental foundation for the engineering application of this material in 630 ℃ ultra-supercritical high-pressure turbine rotors.
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