05355668 is referenced by 93 patents and cites 11 patents.

A catalyst-bearing component of a gas turbine engine is provided. Catalytic materials are provided on components defining the gas flow path of the engine, so that emissions of carbon monoxide and unburned hydrocarbons are reduced. The catalytic materials are selected from the group consisting of noble metals and transition metal oxides. The portions of the gas flow path where such materials are advantageously applied include the combustor, the turbine and the exhaust system. The catalytic coating is preferably applied in conjunction with a thermal barrier coating system interposed between a substrate component and the catalytic coating.

Title
Catalyst-bearing component of gas turbine engine
Application Number
8/10939
Publication Number
5355668
Application Date
January 29, 1993
Publication Date
October 18, 1994
Inventor
Julia A Fields
Cincinnati
OH, US
Jon C Schaeffer
Milford
OH, US
Antoinette E Weil
Cincinnati
OH, US
Agent
Carmen Santa Maria
Jerome C Squillaro
Assignee
General Electric Company
OH, US
IPC
F02C 7/00
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