SLM-printed AlSi10Mg components require immediate stress relief annealing at 300-350°C to mitigate the significant residual stresses accumulated during the rapid thermal cycling of the printing process. This prevents distortion and potential cracking. For applications requiring optimized mechanical properties, a T6 heat treatment is typically applied, consisting of solution treatment at 500-540°C followed by rapid quenching and artificial aging. This treatment transforms the fine, cellular microstructure of as-printed AlSi10Mg into a more conventional microstructure with spheroidized silicon particles, significantly enhancing ductility and toughness while maintaining good strength characteristics.
While less common than with superalloys, Hot Isostatic Pressing (HIP) can be beneficial for AlSi10Mg components destined for high-integrity applications in the aerospace and automotive industries. HIP effectively eliminates internal porosity and gas-entrapped voids, improving fatigue resistance and fracture toughness. The process parameters for aluminum alloys are specifically tailored to avoid excessive grain growth or deterioration of mechanical properties while achieving near-full densification.
The removal of support structures is a critical first step in mechanical post-processing, typically performed using cutting tools or band saws. The as-built surface of SLM AlSi10Mg contains partially melted powder particles and high surface roughness that act as stress concentrators. Abrasive blasting with glass beads or aluminum oxide is commonly used to clean and smooth general surfaces. For components requiring superior surface quality, such as those for aerospace applications, vibratory finishing or flow polishing may be employed to achieve lower roughness values and reduce the risk of fatigue crack initiation.
Functional surfaces, mating interfaces, and threaded features require precision CNC machining to achieve dimensional accuracy and proper fit. This machining is optimally performed after heat treatment to ensure dimensional stability. Final validation includes material testing and analysis to verify mechanical properties, dimensional inspection, and for critical components, non-destructive testing such as dye penetrant inspection or X-ray computed tomography to detect internal defects.