Effect of Solution Treatment on the Microstructure and Mechanical Properties of IN718 Alloy

IN718 alloy exhibits excellent mechanical properties at high-temperature and good workability, which has been widely used in aircraft engine turbine disks, compressor disks, and power turbine shafts (i.e. rotating components). The mechanical properties of IN718 alloy, especially its creep and fatigue properties are a key factor determining the safety and reliability of engines. In this study, the effects of solution treatment at temperature ranging from 900 degrees C to 1050 degrees C on the microstructure and mechanical properties (including the tensile strength at room temperature and 650 degrees C, the stress-rupture behavior at 650 degrees C and 700 MPa, and the low-cycle fatigue behavior at 450 degrees C) were investigated by optical microscopy (OM), scanning electron microscopy (SEM) and electron backscatter diffraction (EBSD). The results show that in specimens subjected to solution treatment at temperature from 900 degrees C to 990 degrees C, the mass fraction of the 8-phase decreases with increasing temperature, whereas the grain size remains the same. However, in specimens treated at temperature ranging from 990 degrees C to 1050 degrees C, the delta-phase is dissolved and the grain size increases from 15 gm to 100 mu m. With proper adjustment of the microstructure of IN718 alloy, this material can satisfy the requirements for high-temperature, corrosion-resistance, and radiation-tolerance, such as the aviation, petrochemical, and nuclear power industries.