发明名称 Catalytic thermal barrier coatings
摘要 A catalyst element ( 30 ) for high temperature applications such as a gas turbine engine. The catalyst element includes a metal substrate such as a tube ( 32 ) having a layer of ceramic thermal barrier coating material ( 34 ) disposed on the substrate for thermally insulating the metal substrate from a high temperature fuel/air mixture. The ceramic thermal barrier coating material is formed of a crystal structure populated with base elements but with selected sites of the crystal structure being populated by substitute ions selected to allow the ceramic thermal barrier coating material to catalytically react the fuel-air mixture at a higher rate than would the base compound without the ionic substitutions. Precious metal crystallites may be disposed within the crystal structure to allow the ceramic thermal barrier coating material to catalytically react the fuel-air mixture at a lower light-off temperature than would the ceramic thermal barrier coating material without the precious metal crystallites.
申请公布号 US2006245984(A1) 申请公布日期 2006.11.02
申请号 US20050244739 申请日期 2005.10.06
申请人 发明人 KULKARNI ANAND A.;CAMPBELL CHRISTIAN X.;SUBRAMANIAN RAMESH
分类号 B01D50/00;F23C13/00;F23R3/40 主分类号 B01D50/00
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