作者: Abdus Khan , Russell Albert Beers , Allan A. Noetzel
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摘要: The present invention relates to a metallic coating be deposited on gas turbine engine components. comprises up 18 wt % cobalt, 3.0 chromium, 5.0 15 aluminum, 0.1 1.0 yttrium, 0.6 hafnium, 0.3 silicon, 10 tantalum, 9.0 tungsten, 6.0 rhenium, molybdenum, and the balance nickel.