MATERIALS
Densification and formation of structure and properties of inconel 625 alloy during direct powder forging
This study investigates the compaction and deformation behavior of Inconel 625 powder using direct powder forging at temperatures of 950 °C and 1150 °C. Finite element modeling was conducted and validated with experimental data. The residual porosity after deformation was 6.5% at 950 °C and 2% at 1150 °C. Samples forged at 1150 °C demonstrated superior mechanical properties, including a bending strength of 1750 MPa and fracture toughness of 42 MPa·m¹ᐟ². In contrast, lower temperature deformation resulted in poorer grain boundary quality and reduced mechanical performance. Post-deformation annealing at 950 °C enhanced microstructural integrity through recrystallization, improving strength to 1540 MPa and toughness to 30.9 MPa·m¹ᐟ². Flow stress at 700 °C ranged from 450 to 650 MPa, confirming the material’s suitability for high-temperature aerospace applications. The findings indicate that 1150 °C is the optimal forging temperature for producing dense, high-strength components from Inconel 625 powder.