Nimonic 80A maintains excellent strength and resistance to creep deformation at temperatures exceeding 800 °C, making it ideal for turbine blades, exhaust components and thermal insulation structures. SLM’s rapid solidification refines the microstructure of Nimonic 80A, enhancing phase stability and supporting long-term performance in hot environments typical of aerospace and aviation systems.
Compared with other nickel-based alloys, Nimonic 80A offers good printability in SLM with limited susceptibility to hot cracking. Its manageable thermal shrinkage and composition make it well-suited for layer-by-layer melting, ensuring stable melt pools and reduced distortion during complex part fabrication.
After SLM printing, Nimonic 80A responds well to heat treatment and ageing procedures to optimize γ′ precipitation and improve high-temperature strength. When required, HIP can eliminate porosity and enhance fatigue resistance for critical rotating components.
The alloy’s thermal stability and mechanical durability make it ideal for combustion chambers, turbine stages and hot gas components used in power generation and oil and gas applications. Through SLM, near-net-shape parts can be produced with internal cooling channels and weight-optimized structures that traditional processes struggle to achieve.