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Microstructure and creep properties of a cast intermetallic Ti–46Al–2W–0.5Si alloy for gas turbine applications

✍ Scribed by J Lapin; M Nazmy


Publisher
Elsevier Science
Year
2004
Tongue
English
Weight
601 KB
Volume
380
Category
Article
ISSN
0921-5093

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✦ Synopsis


The microstructure and creep properties including minimum creep rate, time to 1% creep deformation and creep fracture time of a cast TiAl-based alloy with nominal chemical composition Ti-46Al-2W-0.5Si (at.%) were investigated. The creep specimens were prepared from investment-cast plate and two large turbine blades. Constant load creep tests were performed in air at applied stresses ranging from 150 to 400 MPa in the temperature range 973-1073 K. The microstructure of the specimens is characterised by optical, scanning and transmission electron microscopy before and after creep deformation. The minimum creep rate is found to depend strongly on the applied stress and temperature. The power law stress exponent of minimum creep rate is n = 7.3 and the apparent activation energy for creep is Q a = 427 ± 14 kJ/mol. The initial microstructure of the creep specimen is unstable. The ␣ 2 (Ti 3 Al)-phase transforms to ␥(TiAl)-phase and needle-like B2-precipitates during long-term creep testing at all testing temperatures. At lower applied stresses, the creep specimens fail by the growth and coalescence of cavities and small cracks formed along the ␥/␣ 2 interfaces. At the highest applied stresses, the specimens fail by nucleation and propagation of cracks.