发明名称 Sprayable noble metal coating for high temperature use directly on aircraft engine alloys
摘要 A method of applying a heat-rejection coating directly on a substrate of a metallic component is disclosed. The steps include supplying a metallic component, such as of a gas turbine engine, before applying a reflective-coating mixture onto the component, wherein the reflective-coating mixture comprises a metallic pigment and a reflective-coating-mixture carrier, and wherein the step of applying is accomplished by a method selected from the group consisting of air-assisted spraying, airless spraying, brushing, and decal transfer. The component having the reflective-coating mixture thereon is fired to form a reflective coating on the component.
申请公布号 US7250192(B2) 申请公布日期 2007.07.31
申请号 US20030726361 申请日期 2003.12.03
申请人 GENERAL ELECTRIC COMPANY 发明人 SKOOG ANDREW JAY;MURPHY JANE ANN;BOJANOWSKI BRYAN THOMAS
分类号 B05D3/02;B05D3/00;B05D5/00;B41M5/00;C23C4/02;C23C4/12;C23C4/18;C23C24/04;C23C24/08;C23C26/00;C23C28/00;C23C30/00;F01D5/28 主分类号 B05D3/02
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