发明名称 Coatings for gas turbine compressor components
摘要 A compressor coating is described which can reduce corrosion in the turbine system of a gas turbine engine. The coating is essentially not wet by droplets or aerosols of sea water or other corrodants. The coating reduces the build up of salt deposits on compressor components and their subsequent passage into the turbine section, thereby preventing severe localized corrosion which would otherwise occur.
申请公布号 EP0926261(B1) 申请公布日期 2007.07.04
申请号 EP19980310540 申请日期 1998.12.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BORNSTEIN, NORMAN;WESSON, JOHN P
分类号 C23C18/12;F02C7/05;F01D5/28;F02C7/30;F04D29/02 主分类号 C23C18/12
代理机构 代理人
主权项
地址