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Silicon-slurry/aluminide coatingA low cost coating protects metallic base system substrates from high temperatures, high gas velocity ovidation, thermal fatigue and hot corrosion and is particularly useful fo 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 substrates 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 and increased the resistance of certain superalloys to hot corrosion.
Document ID
19830023524
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
February 15, 1983
Subject Category
Metallic Materials
Report/Patent Number
Patent Number: US-PATENT-4,374,183
Patent Application Number: US-PATENT-APPL-SN-293418
Patent Number: NASA-CASE-LEW-13343
Accession Number
83N31795
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,374,183|NASA-CASE-LEW-13343
Patent Application
US-PATENT-APPL-SN-293418
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