Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
7973035 | Materials Science and Engineering: A | 2018 | 27 Pages |
Abstract
The effect of strain on the resultant microstructure of an experimental low stacking fault energy Nickel based superalloy containing 24â¯wt. pct. Co was investigated. Billets subjected to a preliminary heat treatment at 1110â¯Â°C were compressed to strain limits of 0.15 and 0.5 at strain rates ranging from 0.1/s to 0.01/s and temperatures at 1020â¯Â°C and 1060â¯Â°C. The as-deformed microstructures were assessed and characterized using electron backscatter diffraction, as were microstructures corresponding to a super-solvus anneal heat treatment at 1160â¯Â°C for one hour. This study sought to identify a critical strain limit at which conditions indicative of Strain induced boundary migration (SIBM) could be effectively triggered for the experimental Ni-based superalloy over a set range of thermal-mechanical parameters. Microstructures corresponding to SIBM were then compared to more extensively deformed billets which contained notable fractions of dynamically recrystallized grains to quantify differences in the length fraction and density of â3 twin boundaries of the respective microstructures. Though billet samples deformed to both 0.15 and 0.5 contained notable magnitudes of stored strain energy, microstructures deformed to 0.15 were noted as having maintained larger length fractions of â3 twins due to a predominant absence of dynamic recrystallization. Annealed samples originally deformed to 0.15 yielded annealing twin length fractions as high as 59% when compared a sample deformed to the 0.5 strain limit under equivalent thermal-mechanical conditions that resulted in a twin length fraction of 50%. Although samples deformed to the lower strain limit exhibited higher length fractions of annealing twins, samples deformed to the higher strain limit of 0.5 were noted to yield â3 densities as high as 0.65 μmâ1, whereas the annealed sample deformed under equivalent thermal-mechanical parameters to the 0.15 strain limit produced â3 densities as low as 0.32 μmâ1.
Related Topics
Physical Sciences and Engineering
Materials Science
Materials Science (General)
Authors
Joshua McCarley, Sammy Tin,