Journal
MATERIALS SCIENCE AND TECHNOLOGY
Volume 27, Issue 12, Pages 1858-1862Publisher
TAYLOR & FRANCIS LTD
DOI: 10.1179/1743284711Y.0000000056
Keywords
IN625 alloy; Deformation behaviour; Lomer-Cottrell; Twinning
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Simple compression and microscopy techniques were employed to characterise the microstructural origin of the deformation behaviour of nickel base superalloy IN625 during large strain testing. The alloy exhibited a four-stage strain hardening response similar to that previously reported for low stacking fault energy face centred cubic alloys. At strains lower than about -0.06 (stage A), a falling regime of the hardening rate was observed. This stage was followed by a second stage (stage B) of slow increasing hardening rate, which was found to be coincident with the formation of Lomer-Cottrell locks. The second falling regime of strain hardening (stage C) was seen in the strain range of -0.25 to -0.65. The occurrence of this stage was attributed to the increasing ease of dislocation cross-slip with increasing strain and consequently to the decreasing Lomer-Cottrell lock efficiency in hindering dislocation movement. Beyond a strain of -0.65, a final slightly constant hardening regime (stage D) was developed. The initiation of this stage was concurrent with the onset of deformation twinning in the microstructure.
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