Welding process
AssigneeGeneral Electric Company
InventorsGary Edward Trewiler, Daryl Peacock, William Henry Harrison
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AssigneeGeneral Electric Company
InventorsGary Edward Trewiler, Daryl Peacock, William Henry Harrison
Estimating the term…
A process for repairing a compressor rear frame of a gas turbine engine. The process entails removing a seal flange from the inner casing wall of the frame to define an annular face on the casing wall, and fabricating a replacement flange to have an annular face with a radial width greater than the radial width of the annular face of the casing wall. The faces of the flange and wall are mated to form a joint, a penetration-enhancing flux is deposited adjacent the joint, and a single-pass gas tungsten arc welding operation is performed to form a root weldment that extends completely through the joint. The flux is then removed and a gas tungsten arc welding operation is performed to deposit a filler on the root weldment and form a second weldment that completely overlays but does not penetrate through the root weldment.
A process for repairing a compressor rear frame of a gas turbine engine, the compressor rear frame comprising a cylindrically-shaped inner casing wall and a cylindrically-shaped outer casing wall that substantially circumscribes the inner casing wall, the inner casing wall having a flange adapted to carry a seal member, the process comprising the steps of:
A process for repairing a compressor rear frame of a gas turbine engine, the compressor rear frame comprising a cylindrically-shaped inner casing wall and a cylindrically-shaped outer casing wall that substantially circumscribes the inner casing wall, the inner casing wall having a seal flange that projects radially inward from one end of the inner casing wall so as to be substantially normal to a longitudinal axis of the inner casing wall, the seal flange being adapted to carry a seal member, the process comprising the steps of:
Dependencies are inferred from the claim text.