Development of alloyed and dispersion-strengthened MCrAlY coatings
作者： Thomas A. Taylor , David F. Bettridge
DOI: 10.1016/S0257-8972(96)02961-1
关键词: Dispersion (chemistry) 、 Corrosion 、 Metallurgy 、 Thermal expansion 、 Turbine blade 、 Oxide 、 Combustor 、 Creep 、 Materials science 、 Coating
摘要: Abstract An on-going research program has investigated the effects of separate and combined additions Ta, Pt an oxide dispersion to basic MCrAlY overlay coatings. The goals were improved oxidation hot corrosion resistance, greater diffusional stability, coating thermal expansion reduction in order be closer nickel base turbine blade alloys. It was found cyclic burner rig testing at 1050°C that each individual addition resistance baseline compositions. Oxide reduced expansion. Creep greatly increased by additions, which also strongly yield strength. Yield strength modestly low temperature significantly Ta moderate temperatures.
elsevier.com
sci-hub.se 参考文章(3)
G.W. Meetham, Use of protective coatings in aero gas turbine engines Materials Science and Technology. ,vol. 2, pp. 290- 294 ,(1986) , 10.1179/MST.1986.2.3.290
T. A. Taylor, M. P. Overs, B. J. Gill, R. C. Tucker, Experience with MCrAl and thermal barrier coatings produced via inert gas shrouded plasma deposition Journal of Vacuum Science and Technology. ,vol. 3, pp. 2526- 2531 ,(1985) , 10.1116/1.572828
G.B Prabhu, D.L Bourell, The hot hardness testing for superplasticity in nanocrystalline yttria stabilized tetragonal zirconia Scripta Metallurgica Et Materialia. ,vol. 33, pp. 761- 766 ,(1995) , 10.1016/0956-716X(95)00275-Z