发明名称 Method and apparatus for balancing gas turbine engines
摘要 A method and apparatus is provided for field balancing an assembly including a power turbine. The method includes coupling the power turbine to a load, identifying a first balancing plane that is aft of the power turbine, and identifying a second balancing plane that is forward of the power turbine. A balancing correction is determined at each of the first and second balancing planes. A balance weight is mounted at the first balancing plane based on the balancing correction determined for the first balancing plane, and a balance weight is mounted at the second balancing plane based on the balancing correction determined for the second balancing plane, wherein each balance weight at the second balancing plane is coupled to a respective bolt head without removing the bolt.
申请公布号 US7234916(B2) 申请公布日期 2007.06.26
申请号 US20040942510 申请日期 2004.09.16
申请人 GENERAL ELECTRIC COMPANY 发明人 LEE MICHAEL J.;DIX BRIAN EDWARD;FREEDMAN MAX;ADELMANN WILLIAM JOSEPH
分类号 F01D25/04 主分类号 F01D25/04
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