Method and apparatus to secure a component in position for fabrication
AssigneeGeneral Electric Company
InventorsGraham David Sherlock, Lynn Charles Gagne, Larry Paul Wencil
Life of this patent
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AssigneeGeneral Electric Company
InventorsGraham David Sherlock, Lynn Charles Gagne, Larry Paul Wencil
Estimating the term…
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.
A method for forming an opening in two different turbine components, said method comprising:
A drilling tool for use in fabricating a plurality of different turbine components, said drilling tool comprising:
A drilling assembly for forming an opening in a plurality of blades, said drilling assembly comprising:
Dependencies are inferred from the claim text.