Abstract:Superalloys, as essential materials for high-temperature service, not only embody the frontier level of materials science and metallurgical processes, but also serve as a crucial indicator of a nation's capability in developing advanced aero-engines and gas turbines. The nickel-based superalloy GH4065A exhibits excellent high-temperature strength, microstructural stability, and processability through optimization of the γ' phase content and compositional design. This paper reviews and evaluates the development and current status of superalloys both domestically and internationally, focusing on the research progress of GH4065A in terms of microstructural control, fatigue behavior, and welding performance. Studies have shown that the microstructure and properties of GH4065A are influenced by multiple factors, including dendrite segregation, γ' phase evolution, and recrystallization behavior. The alloy de-monstrates outstanding oxidation resistance and thermal stability at 650~750 ℃, while its fatigue behavior is affected by grain size, inclusions, and unrecrystallized structures. Double-spot electron beam welding and inertia friction welding can produce high-quality joints, and post-weld heat treatment can improve microstructural uniformity and performance stability. Currently, research on GH4065A is still primarily at the laboratory scale, and its creep-fatigue coupling behavior under complex service conditions, as well as life prediction models, remain inadequate. Moreover, the coupled relationships among γ' phase dissolution, precipitation, and recrystallization lack quantitative description. Finally, future directions are proposed in the areas of multi-scale microstructural control, service mechanisms under complex environments, and engineering applications.