Superalloy components manufactured via superalloy 3D printing—such as SLM or DMLS—exhibit different microstructural characteristics compared to cast or forged parts. Layer-by-layer solidification introduces high cooling rates and uneven thermal gradients, leading to residual stresses, anisotropic grain structures, and potential microcracking. Therefore, post-processing is not optional—it is mandatory to achieve aerospace and energy-grade mechanical properties.
Unlike conventional vacuum investment casting, 3D-printed parts often require stress relief heat treatment, HIP densification, and precise machining to meet dimensional tolerance and performance standards.
Internal porosity and microvoids naturally occur during powder fusion. Hot isostatic pressing (HIP) is widely used to collapse these defects, improving density and fatigue resistance. Subsequent heat treatment restores phase balance and enhances precipitation hardening. This is particularly important for nickel-based grades like Inconel 718 or cobalt-based alloys such as Stellite 21, where mechanical stability under cyclic loading relies on microstructural uniformity.
Residual stresses generated during rapid cooling must be relieved before any machining to prevent deformation or crack initiation during final finishing.
As-printed surfaces are typically rough and may contain partially melted powder particles. For precision-critical applications in aerospace and aviation and power generation, superalloy CNC machining is typically required to achieve dimensional tolerance and surface accuracy. In certain designs, finishing techniques such as deep hole drilling and EDM machining enable fabrication of internal channels and intricate geometries that can’t be conventionally machined.
Functional coatings like thermal barrier coating (TBC) may be applied to enhance oxidation and heat resistance, especially for combustion hardware and turbine blades.
Since additive manufacturing creates unique microstructures, rigorous material testing and analysis is essential. CT scanning, X-ray inspection, hardness testing, fatigue evaluation, and phase verification ensure the part complies with performance standards. Only after testing can the part be approved for use in high-stress environments like oil and gas or military and defense applications.