LOCALIZED REWORK USING DIRECTED ENERGY DEPOSITION

1 . A method, comprising:

receiving a stator stage including a plurality of stator vanes disposed between an outer diameter and an inner diameter;

analyzing the stator stage for defects, wherein the analysis identifies defects on a surface of the stator stage and below the surface of the stator stage, and uses a heat map to identify locations of the stator stage with a higher probability of having a defect relative to other locations of the stator stage;

determining based on the analysis that there is a first defect on an edge of a first stator vane of the plurality of stator vanes;

responsive to determining that there is the first defect on the edge, automatically removing a portion of the first stator vane including the first defect to form a first scallop on the edge of the first stator vane;

repairing the first stator vane including filling the first scallop to fill the first stator vane to its original size and shape creating a repaired portion; and

performing a blending process to the stator stage including the first stator vane and the repaired portion to smooth the plurality of stator vanes.

2 - 3 . (canceled)

4 . The method of claim 1 , wherein the edge is a leading edge of the first stator vane.

5 . The method of claim 1 , wherein the edge is a trailing edge of the first stator vane.

6 . The method of claim 1 , wherein the removing includes removing a standardized portion of the first stator vane so that the first scallop more closely conforms to a theoretical model plus tolerances.

7 . The method of claim 6 , wherein the repaired portion has a standardized size and shape.

8 . The method of claim 1 , wherein the repairing includes using an additive manufacturing process to rebuild the edge of the first stator vane.

9 . The method of claim 8 , wherein the additive manufacturing process is a directed energy deposition process.

10 . The method of claim 1 , wherein the blending process further includes shaping a leading edge and a trailing edge of the plurality of stator vanes.

11 . A method of repairing a stator stage for use with a turbine engine, comprising:

analyzing the stator stage for defects, wherein the analysis is conducted using at least one of x-ray, blue light scanner, or microwave;

determining, based on the analysis, that there is a first defect on an edge of a first stator vane of a plurality of stator vanes of the stator stage;

responsive to the determining that there is the first defect on the edge, automatically removing a portion of the edge of the first stator vane that includes the first defect to form a first scallop;

responsive to the removing the portion of the edge of the first stator vane, automatically repairing the edge of the first stator vane using an additive manufacturing process, including filling the first scallop to rebuild the edge of the first stator vane to form a repaired portion; and

responsive to the repairing the edge of the first stator vane, automatically performing a blending process on the stator stage to smooth and shape the plurality of stator vanes, including the first stator vane, wherein the blending process uses a material removal process, the material removal process including at least one of milling or computer numerical control (CNC) machining.

12 . The method of repairing the stator stage for use with the turbine engine of claim 11 , further comprising:

analyzing the stator stage to identify the first defect on the edge of the first stator vane.

13 . The method of repairing the stator stage for use with the turbine engine of claim 11 , wherein the edge is a leading edge of the first stator vane.

14 . The method of repairing the stator stage for use with the turbine engine of claim 11 , wherein the edge is a trailing edge of the first stator vane.

15 . The method of repairing the stator stage for use with the turbine engine of claim 11 , wherein the additive manufacturing process is a directed energy deposition process.

16 . The method of repairing the stator stage for use with the turbine engine of claim 11 , wherein the first scallop has a predefined standardized size and shape and the repaired portion has the predefined standardized size and shape.

17 . A method of repairing a stator stage for use with a turbine engine, comprising:

analyzing the stator stage for defects, wherein the analysis is conducted using at least one of x-ray, blue light scanner, microwave, or thermal examinations;

determining, based on the analysis, that there is a first defect on a first edge of a first stator vane of a plurality of stator vanes of the stator stage;

determining based on the analysis that there is a second defect on a second edge of the first stator vane of the plurality of stator vanes;

responsive to the determining that there is the first defect on the first edge and the second edge,

automatically removing a first portion of the first edge including the first defect to form a first scallop, and

automatically removing a second portion of the second edge including the second defect to form a second scallop, and

responsive to the removing the first portion of the first edge and the second portion of the second edge, automatically repairing the first stator vane including filling the first scallop and the second scallop using an additive manufacturing process.

18 . The method of repairing the stator stage for use with the turbine engine of claim 17 , wherein the first edge is a leading edge and the second edge is a trailing edge.

19 . The method of repairing the stator stage for use with the turbine engine of claim 17 , wherein the additive manufacturing process is a directed energy deposition process.

20 . The method of repairing the stator stage for use with the turbine engine of claim 17 , wherein the first scallop and the second scallop have the same size and shape.