Method of repairing turbine blades
AssigneeRefurbished Turbine Components Limited
InventorMichael J. Fraser
Life of this patent
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Abstract
A method of repairing a turbine blade of the type having one or more lacing wire holes comprising the steps of welding additional metal to the blade, subjecting the blade to a stress relieving heat treatment process before which the or each lacing wire hole is effectively eliminated by filling the hole or holes with material the same as or at least compatible with the material from which the blade is made. The turbine blade may be subjected to the application of mechanical forces to restore its form and machining to restore its shape can be gauged to ensure both its form and shape is correct.
Claims8
A method of repairing a solid turbine blade of the type having one or more lacing wire holes, the method comprising the steps of:
- (a) welding additional metal to a part of the blade requiring repair;
- (b) eliminating each lacing wire hole by completely filling the hole or holes with material the same as or at least compatible with the material from which the blade is made;
- (c) subjecting the blade to a stress relieving heat treatment process to relieve residual stress in the blade, said heat treatment step being performed after said lacing wire hole or holes are filled so that the build-up of residual stresses in the area of each lacing wire hole as a result of the heat treatment is minimized;
- (d) machining the repaired area of the blade to return it to its original shape.
A method of repairing a solid turbine blade of the type having one or more lacing wire holes, the method comprising the steps of:
- (a) welding additional metal to an eroded or damaged part of the blade;
- (b) filling each lacing wire hole completely with a metal the same as or compatible with the metal from which the turbine blade is made;
- (c) gauging the blade to ascertain if it is of the correct form;
- (d) applying mechanical forces to the blade to return it to its correct form if correction is necessary;
- (e) subjecting the blade to a heat treatment process to relieve residual stress, said heat treatment step being performed after said lacing wire hole or holes are filled so that the build up of residual stresses in the area of each lacing wire hole as a result of the heat treatment is minimized;
- (f) machining the blade to return it to its correct shape;
- (g) reforming the lacing wire hole or holes.
Dependencies are inferred from the claim text.