2014
DOI: 10.1016/j.msea.2014.03.030
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The effect of ageing on microstructure and mechanical properties of powder Ti–5Al–5Mo–5V–1Cr–1Fe alloy

Abstract: E. (2014). The effect of ageing on microstructure and mechanical properties of powder Ti-5Al-5Mo-5V-1Cr-1Fe alloy. Materials Science and Engineering A, 605 (May), 89-97. The effect of ageing on microstructure and mechanical properties of powder Ti-5Al-5Mo-5V-1Cr-1Fe alloy

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Cited by 47 publications
(13 citation statements)
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“…[31] that deformation twinning and martensitic transformation together with their constant interactions are responsible for the continuous increase of work-hardening rate during stage II. On the other hand, only two stages of work-hardening rate are found for 500°C sample as described in the previous study [32]. These two stages are exponential decrease in workhardening rate followed by a slower, nearly plateauing decrease.…”
Section: Methodssupporting
confidence: 53%
“…[31] that deformation twinning and martensitic transformation together with their constant interactions are responsible for the continuous increase of work-hardening rate during stage II. On the other hand, only two stages of work-hardening rate are found for 500°C sample as described in the previous study [32]. These two stages are exponential decrease in workhardening rate followed by a slower, nearly plateauing decrease.…”
Section: Methodssupporting
confidence: 53%
“…(3), (7), (8) and (10), a fracture toughness model correlated with crack propagation path is shown in Eq. (11).…”
Section: Prediction Modelmentioning
confidence: 99%
“…Among various kinds of titanium alloys, Ti-5Al-5Mo-5V-1Cr-1Fe (wt%) alloy, a near b damage-tolerant titanium alloy, is especially suitable for making big critical aviation forgings due to its advantages such as low cost, high strength and toughness [7]. The excellent properties of Ti-55511 (Ti-5Al-5Mo-5V-1Cr-1Fe) alloy have attracted too much attention [8][9][10][11][12][13]. Liu et al [8] studied the deformation behavior in the isothermal compression of Ti-55511 alloy.…”
Section: Introductionmentioning
confidence: 99%
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“…Ahmed et al [32] studied the effect of aging time on the structure-property correlation of the thermo-mechanically processed powder Ti-5Al-5V-5Mo-1Cr-1Fe (TC18) alloy at 923 K. The influences of solution treatment on microstructure and mechanical properties of the Ti7333 and Ti6554 alloys have been investigated by Fan et al [33] and Li et al [34], respectively. As refined dispersions of secondary α phase precipitates play a critical role in the improvement of the mechanical properties of β titanium alloys, experiments on α phase nucleation sites and influence of ω phase on the refinement of the α phase precipitates have been conducted by Zheng et al [35], Ahmed et al [36], Coakley et al [37] and Nag et al [38].…”
Section: β Titanium Alloys For Aircraft Structural Applicationsmentioning
confidence: 99%