After laser cladding, hot isostatic pressing (HIP) is commonly applied to eliminate internal porosity and enhance bonding quality. HIP increases fatigue strength and prevents crack initiation—especially important for high-temperature superalloys used in aerospace and aviation applications.
Heat treatment is used to refine grain structure, reduce residual stress, and activate precipitation hardening in alloys such as Inconel 718. This step enhances creep and fatigue resistance—vital for long-term durability under cyclic loading or extreme thermal conditions.
To restore dimensional accuracy, post-cladding finishing via superalloy CNC machining ensures correct tolerances and surface quality. Accurate machining is essential when repairing shafts, turbine components, or sealing interfaces that require assembly-ready conditions.
Final validation through material testing and analysis, including X-ray, SEM, fatigue testing, and dimensional inspection, confirms that the repaired component meets operational standards. This ensures that the microstructural transformation achieved through cladding and post-processing is effective and reliable.
Components used in power generation and oil and gas sectors may require additional corrosion or thermal barrier coatings. Processes such as thermal barrier coating (TBC) further protect the laser-cladded layer and extend service life in harsh environments.