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Oxidation and hot corrosion of coated and bare oxide dispersion strengthened superalloy MA-755E

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Abstract

Cyclic hot corrosion and oxidation testing of an experimental oxide dispersion strengthened (ODS) superalloy MA-755E were conducted in a hot gas stream at Mach 0.3. The response of the ODS alloy, bare or with protective coatings, was similar to that of a conventional cast alloy, IN-792, in hot corrosion at 900°C. However, during oxidation at 1100 and 1150°C the ODS alloy differed from the cast alloy by developing a greater amount of subsurface porosity. Compared with a diffused aluminide coating, an electron beam vapor deposited NiCrAlY coating offered superior oxidation protection and decreased porosity formation. In additional testing, the tendency to form porosity was associated with the large grains of recrystallized powder metallurgy alloys but was independent of the presence of an oxide dispersion.

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Authors and Affiliations

  1. Lewis Research Center, National Aeronautics and Space Administration, 44135, Cleveland, Ohio

    T. K. Glasgow & G. J. Santoro

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  1. T. K. Glasgow
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  2. G. J. Santoro
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Glasgow, T.K., Santoro, G.J. Oxidation and hot corrosion of coated and bare oxide dispersion strengthened superalloy MA-755E. Oxid Met 15, 251–276 (1981). https://doi.org/10.1007/BF01058828

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  • DOI: https://doi.org/10.1007/BF01058828

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