发明名称 Lubricating system for thermal medium delivery parts in a gas turbine
摘要 Cooling steam delivery tubes extend axially along the outer rim of a gas turbine rotor for supplying cooling steam to and returning spent cooling steam from the turbine buckets. Because of the high friction forces at the interface of the tubes and supporting elements due to rotor rotation, a low coefficient of friction coating is provided at the interface of the tubes and support elements. On each surface, a first coating of a cobalt-based alloy is sprayed onto the surface at high temperature. A portion of the first coating is machined off to provide a smooth, hard surface. A second ceramic-based solid film lubricant is sprayed onto the first coating. By reducing the resistance to axial displacement of the tubes relative to the supporting elements due to thermal expansion, the service life of the tubes is substantially extended.
申请公布号 US6422818(B2) 申请公布日期 2002.07.23
申请号 US20010769749 申请日期 2001.01.26
申请人 GENERAL ELECTRIC COMPANY 发明人 MASHEY THOMAS CHARLES
分类号 C23C28/00;F01D5/08;F01D9/06;F01D25/18;F16L58/08;F16L58/14;(IPC1-7):F01D5/08 主分类号 C23C28/00
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