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Method of protecting a surface with a silicon-slurry/aluminide coatingA low cost coating for protecting metallic base system substrates from high temperatures, high gas velocity oxidation, thermal fatigue and hot corrosion is described. The coating is particularly useful for protecting vanes and blades in aircraft and land based gas turbine engines. A lacquer slurry comprising cellulose nitrate containing high purity silicon powder is sprayed onto the superalloy substrates. The silicon layer is then aluminized to complete the coating. The Si-Al coating is less costly to produce than advanced aluminides and protects the substrate from oxidation and thermal fatigue for a much longer period of time than the conventional aluminide coatings. While more expensive Pt-Al coatings and physical vapor deposited MCrAlY coatings may last longer or provide equal protection on certain substrates, the Si-Al coating exceeded the performance of both types of coatings on certain superalloys in high gas velocity oxidation and thermal fatigue. Also, the Si-Al coating increased the resistance of certain superalloys to hot corrosion.
Document ID
19820020565
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Deadmore, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Young, S. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 12, 1982
Subject Category
Nonmetallic Materials
Report/Patent Number
Patent Number: US-PATENT-4,310,574
Patent Application Number: US-PATENT-APPL-SN-161254
Patent Number: NASA-CASE-LEW-13343-1
Accession Number
82N28441
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,310,574|NASA-CASE-LEW-13343-1
Patent Application
US-PATENT-APPL-SN-161254
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