Effect of Rejuvenation Heat Treatment on the Creep Property and Microstructural Evolution of a Ni-Base Superalloy

Abstract

Interrupted creep tests were performed on a polycrystalline Ni-base superalloy, and rejuvenation heat treatment (RHT) was carried out to restore the creep resistance. During creep deformation, the microstructural evolution can be characterized as coarsening and rafting of γ precipitates, formation of dislocation networks in matrix channels, γ shearing by dislocations and carbides transformation from MC to M 6 C type. In the sample with low precrept strain, the dislocation networks can be effectively removed after RHT and the size and morphology of γ particles were similar to that just after heat treatment. However, the microstructure in the sample with higher creep strain after RHT cannot be fully restored to the original state in terms of dislocations and distribution of γ particles. The subsequent creep results exhibit that creep property is also relevant to the precrept strain, which exhibits a good agreement with microstructure observations. In addition, RHT cannot reverse the carbide transformation from MC to M 6 C type but enhances this process, which can be evident by the change of the area fraction of these two types of carbides. The effect of carbides transformation on the creep resistance of K465 alloy is not pronounced.

Effect of Heat Treatment on Microstructure and Creep Behavior of Fe-40Ni-24Cr Alloy

“…They are generally used at a temperature above 540 • C [1][2][3][4][5] and some exceed 85% of their initial melting temperatures, such as gas turbines and steam generators [6][7][8]. These superalloys need to exhibit combinations of good high strength and high creep resistance, and the potential to work at high temperatures for long periods [9][10][11][12][13][14]. Generally, for application at very high temperatures, nickel-based alloys are used, followed by cobalt-based alloys and then lastly iron-nickel alloys.…”