发明名称 Method and apparatus to secure a component in position for fabrication
摘要 A method for forming an opening in two different turbine components is provided. The method includes coupling a clamp to a base and coupling the clamp to a clamp bar, wherein the clamp bar is moveable with respect to the base. A first bushing plate is selected based on a first turbine component being drilled and is removably coupled to the base. A bushing is removably coupled to at least one aperture extending through the first bushing plate. An opening is formed in the first turbine component. A second bushing plate is selected based on a second turbine component being drilled. The second turbine component is different from the first turbine component. The second bushing plate is removably coupled to the base. An opening is formed in the second turbine component.
申请公布号 US7862264(B2) 申请公布日期 2011.01.04
申请号 US20070679505 申请日期 2007.02.27
申请人 GENERAL ELECTRIC COMPANY 发明人 SHERLOCK GRAHAM DAVID;GAGNE LYNN CHARLES;WENCIL LARRY PAUL
分类号 B23B35/00;B23B47/28 主分类号 B23B35/00
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