2017
DOI: 10.1016/j.matdes.2017.02.043
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Correlation between alpha phase morphology and tensile properties of a new beta titanium alloy

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Cited by 122 publications
(45 citation statements)
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“…%) alloy known as TB17, which has a MoE value of 5.3 [67]; the near-beta Ti-4Al-7Mo-3Cr-3V (wt. %) alloy, which has a MoE value of 9.8 [68]; and the metastable Ti-3.5Al-5Mo-6V-3Cr-2Sn-0.5Fe (wt. %) alloy, which has a MoE value of 11.1 [69,70].…”
Section: Aircraft Structuresmentioning
confidence: 99%
See 1 more Smart Citation
“…%) alloy known as TB17, which has a MoE value of 5.3 [67]; the near-beta Ti-4Al-7Mo-3Cr-3V (wt. %) alloy, which has a MoE value of 9.8 [68]; and the metastable Ti-3.5Al-5Mo-6V-3Cr-2Sn-0.5Fe (wt. %) alloy, which has a MoE value of 11.1 [69,70].…”
Section: Aircraft Structuresmentioning
confidence: 99%
“…%) alloy has decreasing tensile strengths with increasing aging temperature between approximately 490 °C (914 °F) and 600 °C (1112 °F), Figure 12. Since the mechanical properties of beta Ti alloys can be optimized for an application by aging, numerous studies of the structure-property relationships are present in the existing literature [68,70,127,129,130]. These studies typically focus on microstructural evolution of the secondary α-phase precipitates and concomitant changes in tensile or hardness properties.…”
Section: Agingmentioning
confidence: 99%
“…After double-aging heat treatment, a lot of α precipitations with different morphologies: fine particle α, acicular α and discontinued grain boundary α, were precipitated from the β titanium matrix, this contributed to both of the strength and ductility, because fine particles and/or acicular structure were harder than β phase and harder to be deformed; α/β interfaces pinned the movement of dislocations, increasing the strength; 9,10 and grain boundary α could be deformed by slipping and shearing mechanisms so that the dislocations could be activated and accumulated within them, improving the ductility. 11,12 Due to the finer microstructures and α precipitations formed in the as-extruded Ti-5553 alloy than that of the ingot Ti-5553 alloy, the strength of the studied Ti-5553 alloy was much more higher than that of the ingot metallurgy Ti-5553 alloy. 13 The oxygen contents for both of hot-pressed and extruded Ti-5553 alloy were 0.39wt.%, which were about 0.06wt.% increase comparing to the starting powder mixture (0.33wt.%).…”
Section: Microstructure and Properties Of Ti-5553 Alloymentioning
confidence: 99%
“…Titanium alloys have been widely used in various industries due to their high strength, low density and strong corrosion resistance. Among them, high-strength titanium alloys play an important role in the manufacture of aerospace structural parts [1,2]. TC21 titanium alloy is a high strength and high toughness titanium alloy developed on the basis of Ti-62222 alloy in the United States.…”
Section: Introductionmentioning
confidence: 99%