2014
DOI: 10.1134/s0031918x14010098
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Effect of aging on structure and properties of quenched alloy based on orthorhombic titanium aluminide Ti2AlNb

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Cited by 26 publications
(7 citation statements)
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“…When secondary alpha-two goes into solution, lower tensile and creep strength should be expected. In this work the effect of surface finish on bonding behaviour agrees with earlier works [19,20].…”
Section: Above the β Transus (∼ 1060supporting
confidence: 91%
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“…When secondary alpha-two goes into solution, lower tensile and creep strength should be expected. In this work the effect of surface finish on bonding behaviour agrees with earlier works [19,20].…”
Section: Above the β Transus (∼ 1060supporting
confidence: 91%
“…• C but at this temperature, this phase does not go into solution unlike secondary α 2 and during slow cooling, β phase does not transform to secondary α 2 completely which is diffusion controlled process requiring time to complete transformation [18,19]. Atomic flux through α 2 /β interface appears to be not enough to complete β transformation to secondary α 2 , which is merely related to operating temperature and solubility effects [17].…”
Section: Above the β Transus (∼ 1060mentioning
confidence: 99%
See 1 more Smart Citation
“…A mechanism of formation of an O-phase from a B2-phase suggested in [5 -8] involves the appearance of an intermediate metastable orthorhombic phase ordered with respect to two elements and having a structure of type B19 (Pmma, AuCd). The stages of the transformation of structure in an alloy based on an O-phase in the course of the a 2 ® O transformation are studied in [9,10].…”
Section: Introductionmentioning
confidence: 99%
“…The Ti 2 AlNb-based alloy (Banerjee et al, 1988;Khadzhieva et al, 2014) combines low density, an improved oxidation resistance, and higher fracture toughness compared with the traditional TiAl and NiAl intermetallics (Feng et al, 2002;Yang et al, 2004;Lin et al, 2012). Therefore, Ti 2 AlNb intermetallics have been regarded as promising structural metals to be applied to aircraft engine components (Banerjee, 1997;Germann et al, 2005).…”
Section: Introductionmentioning
confidence: 99%