Qiang Zhao, Zhiwei Qin, Xiaolong Hong, Jilong Wang, Fushuai Jin, Juncheng Xu, Bin Wang, Bingzhi Wang, Wu Liang, Chunbo Zhang, Yongxian Huang, Honggang Dong
Inertia friction welding (IFW) of dissimilar Ni-based superalloys offers great promise for manufacturing critical aero-engine components, yet the persistent strength-ductility trade-off in welded joints restricts their reliable service under extreme conditions. This work proposes an interfacial nanostructure-specific tailoring strategy via a double-stage aging treatment to precisely regulate the γ' strengthening phases, dislocation structures, and microtwins/stacking faults at the FGH4108/GH4065A IFWed interface. γ' strengthening phases in the as-welded joint underwent extensive dissolution and micro-precipitation at the interface, forming a fine-precipitate zone several nanometers in width, accompanied by high dislocation density and pronounced local strain concentration. After double-stage aging, the fine-precipitate zone was significantly narrowed, nanoscale γ' strengthening phases re-precipitated and grew to ∼15 nm, while abundant microtwins and stacking faults were introduced at the interface. The post-weld heat treated (PWHT) joint achieved an ultimate tensile strength of 1529.1 MPa with an elongation of 16.9% at room temperature, demonstrating simultaneous enhancement in strength and ductility. Mechanistically, the coherent strain field at the γ/γ' interface, together with the microtwins/stacking faults, elevated the energy barrier for dislocation motion and induced hetero-deformation hardening. 3D-APT analysis further confirmed that Al and Ti elements were preferentially enriched within the γ' precipitates, whereas Cr and Co tended to partition into the γ channels. Such elemental partitioning behaviors effectively reduced interfacial diffusivity and enhanced the coarsening resistance of the γ' precipitates. These findings lay a solid groundwork for the future development of integrated IFW-PWHT methodologies, offering a scalable route toward tailored microstructures in aerospace systems.