Characterization of the Superalloy Inconel 718 After Double Aging Heat Treatment

The application of heat treatment, by solid solution and precipitation hardening, is very important to optimize the mechanical properties of superalloys. The main phases present in Inconel 718 are: gamma prime gamma' face ordered Ni-3(Al, Ti); gamma double prime gamma '' bct ordered Ni3Nb; eta. hexagonal ordered Ni3Ti; delta delta orthorhombic Ni3Nb intermetallic compounds and other topologically closed/packed structures such as mu and Laves phases. delta, mu and Laves phases have low ductility, which causes losses in mechanical and corrosion properties (Fu et al. in Mater Sci Eng A 499: 215-220, 2009 [1]). The heat treatment applied to Inconel 718, precipitation hardening, has two steps: solid solution and aging treatment. In first step the secondary (hardening) phases are dissolved along the matrix, as well as carbides. It is important to note that after 650 degrees C (Durand-Charre in The microstructure of superalloys. CRC Press, Boca Raton, 1997 [2]) and with long exposure times, gamma '' transforms in the stable phase d, which results in a loss of mechanical resistance. In this study we aim to characterize the microstructure and phases in superalloy Inconel 718 during the steps of heat treatment with double aging. The double aging treatment performed followed the steps of solid solution to 1095 degrees C/1 h and double aging at 955 degrees C/1 h to 720 degrees C/8 h + 620 degrees C/8 h. The characterizations were performed through the techniques of XRD and SEM/EDS. It was possible to obtain the microstructural and phases characterizations before and after heat treatment in all steps.