| CPC F01D 5/288 (2013.01) [B05D 1/005 (2013.01); B05D 1/04 (2013.01); B05D 1/36 (2013.01); C01F 7/02 (2013.01); C09D 1/00 (2013.01); C09D 5/18 (2013.01); C09D 201/00 (2013.01); C23C 4/02 (2013.01); C23C 4/10 (2013.01); C23C 4/11 (2016.01); C23C 4/18 (2013.01); C23C 28/3215 (2013.01); C23C 28/345 (2013.01); C23C 28/3455 (2013.01); C23C 28/347 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F01D 25/005 (2013.01); F02C 7/24 (2013.01); B05B 5/00 (2013.01); B05B 7/20 (2013.01); B05B 7/22 (2013.01); F05D 2220/32 (2013.01); F05D 2230/90 (2013.01); F05D 2260/231 (2013.01); F05D 2300/611 (2013.01)] | 17 Claims |

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1. A gas turbine engine component, comprising:
a superalloy substrate;
a bond coat on the substrate;
a thermal barrier material on the bond coat; and
a coating containing polynuclear aluminum oxide/hydroxide clusters on the thermal barrier material; wherein the polynuclear aluminum oxide/hydroxide clusters are Al13 Keggin clusters having the formula [AlO4Al12(OH)24(H2O)12]7+, or are salts of the Al13 Keggin clusters called Al13 Keggin complexes.
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