2010
DOI: 10.1590/s1517-70762010000200038
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Deformation and fracture of an alpha/beta titanium alloy

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Cited by 12 publications
(7 citation statements)
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“…Today's high performance aircrafts, including engine power to weight ratios, airframe strength, aircraft speed and range, are largely attributable to the use of titanium alloys with high specific strength and fracture toughness (Ezugwu and Wang 1997;Andrade et al 2010). The use of titanium alloys in airframe application has recently been growing as the use of CFRP (carbon fiber reinforced polymer) increases (Inagaki et al 2014;Mrazova 2013).…”
Section: Introductionmentioning
confidence: 99%
“…Today's high performance aircrafts, including engine power to weight ratios, airframe strength, aircraft speed and range, are largely attributable to the use of titanium alloys with high specific strength and fracture toughness (Ezugwu and Wang 1997;Andrade et al 2010). The use of titanium alloys in airframe application has recently been growing as the use of CFRP (carbon fiber reinforced polymer) increases (Inagaki et al 2014;Mrazova 2013).…”
Section: Introductionmentioning
confidence: 99%
“…The general microstructure consists of a HCP alpha phase matrix with lamellar grains of BCC beta phase [58]. The chemical composition is shown in Table 2.…”
Section: Timetal 54mmentioning
confidence: 99%
“…Depending on required mechanical properties, the heat treatment can be applied to Ti-6Al-4V alloy, and it is as follows: partial annealing (from 600 to 650 °C), full annealing (from 700 to 850 °C / furnace cooling to 600 °C /air cooling) or solutionizing (from 880 to 950 °C / water quenching) and ageing (from 400 to 600 °C) [4][5][6][7][8][9].…”
Section: Introductionmentioning
confidence: 99%