Chloride- and SO3 induced hot corrosion of state-of-the-art and developmental coatings were studied in a program of laboratory hot corrosion testing correlated with metallographic examination of service hardware. Laboratory furnace tests showed that CoCrAlY coatings are highly susceptible to degradation by chloride-containing salt deposits; the mechanism of attack involves dealloying of aluminum via formation of an interconnected network of coarse and fine pores. Sputtered platinum overlayers are an effective means of retarding the onset of this type of degradation, especially at low temperatures where dissolution of the overlayer by interdiffusion is slow. In spite of this demonstrated potential for chloride-induced degradation, dissimilar microstructures of test specimens and service hardware (primarily the presence of a zone of internal attack in test specimens but not in engine-run parts) indicates that chloride alone cannot account for the severity of the marine environment. Emphasis on the program was then shifted to examination of SO3 effects. It was shown that the microstructural features of service hardware could be reproduced in furnace tests with Na2SO4 deposits and SO3 in the gas.

  • Corporate Authors:

    Pratt and Whitney Aircraft

    Materials Engineering and Research Lab, 400 Main Street
    East Hartford, CT  United States  06118
  • Authors:
    • Barkalow, R H
    • Pettit, F S
  • Publication Date: 1978-6-15

Media Info

  • Pagination: 121 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00185490
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: PWA-FR-10225 Final Rpt.
  • Contract Numbers: N00173-76-C-0146
  • Files: TRIS
  • Created Date: Dec 29 1979 12:00AM