Apparatus and methods for repairing compressor airfoils in situ

• US 7,032,279 B2
• Filed: 10/18/2002
• Issued: 04/25/2006
• Est. Priority Date: 10/18/2002
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Rozier, Elena, Hatley, Kenneth J., Hatley, Richard M., McCarvill, John, Lawson, Ronald H. Jr., Bousquet, Michael
• Primary Examiner(s): AGRAWAL, CHRISTOPHER K
• Application Number:
  US10/273,345
• Publication Number:
  US 20040074093A1
• Time in Patent Office: 1,285 Days
• Field of Search: 294/021.9, 298/897, 298/897.2, 298/880.2, 298/880.21, 298/891, 297/05, 297/09, 297/14, 297/20, 297/21, 29/900.1, 29/810.2, 451/9, 451/296, 451/297, 451/299, 451/355, 451/3, 451/439, 451/441, 451/440
• US Class Current: 29/90.01
• CPC Class Codes: B23P 6/002 Repairing turbine components, e.g. moving or stationary blades, rotors, B23P6/045 takes precedence
• CPC Class Codes: B24B 19/14 for grinding turbine blades, propeller blades or the like using grinding belts B24B21/16
• CPC Class Codes: B24B 21/16 for grinding other surfaces of particular shape single purpose machines for grinding cams or camshafts B24B19/12
• CPC Class Codes: B24B 39/026 Impact burnishing
• CPC Class Codes: B24C 1/10 for compacting surfaces, e.g. shot-peening for deforming sheet metal, tubes or profiles B21D31/06; as a metallurgical treatment C21D7/00, C22F1/00
• CPC Class Codes: B24C 5/02 Blast guns, e.g. for generating high velocity abrasive fluid jets for cutting materials perforating by fluid jet B26F1/26
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: Y10T 29/4511 Interior surface
• CPC Class Codes: Y10T 29/47 Burnishing
• CPC Class Codes: Y10T 29/49238 Repairing, converting, servicing or salvaging
• CPC Class Codes: Y10T 29/49318 Repairing or disassembling
• CPC Class Codes: Y10T 29/49336 Blade making
• CPC Class Codes: Y10T 29/49748 by shaping, e.g., bending, extruding, turning, etc.
• CPC Class Codes: Y10T 29/53039 with control means energized in response to activator stimulated by condition sensor
• CPC Class Codes: Y10T 29/53061 Responsive to work or work-related machine element

Abstract

The apparatus includes a track mounted in the inlet of a compressor. A manipulator is mounted for movement about the track and carries three modules, the last of which mounts a tool head for movement in a Cartesian coordinate system and about the track. A measuring head measures the location of the airfoil surface. An abrading tool mounted on the third module removes surface material from the airfoil. Subsequently, a shot-peening device, either a flapper with embedded shot or free shot is impacted against the abraded surface to strengthen the surface. Final inspection is performed by a light and camera head mounted on the third module.

Claims

1. Apparatus for in situ repair of airfoils of a compressor, comprising:

a manipulator for mounting to an inlet of the compressor and for movement in a generally circumferential direction about an axis;

a tool carried by said manipulator for movement therewith and relative thereto about three orthogonally related axes, said tool being movable into the inlet of the compressor to a position in contact with a selected airfoil;

a drive system for driving said tool into contact with the selected airfoil; and

a system for controlling the drive system to position the tool in contact with the selected airfoil for repairing the selected airfoil;

said drive system including a servo-motor coupled to a lead screw for driving said tool into contact with the selected airfoil.

2. Apparatus according to claim 1 including a system for measuring and recording the position of the tool relative to the selected airfoil, said control system being responsive to the measuring and recording system to position the tool in contact with the selected airfoil.

3. Apparatus according to claim 1 wherein said tool includes an abrasive carried by said manipulator for movement into contact with the selected airfoil.

4. Apparatus according to claim 3 wherein said abrasive is carried by a finger pivotally carried by said manipulator.

5. Apparatus for in situ repair of airfoils of a compressor, comprising:

a manipulator for mounting to an inlet of the compressor and for movement in a generally circumferential direction about an axis;

a tool carried by said manipulator for movement therewith and relative thereto about three orthogonally related axes, said tool being movable into the inlet of the compressor to a position in contact with a selected airfoil;

a drive system for driving said tool into contact with the selected airfoil; and

a system for controlling the drive system to position the tool in contact with the selected airfoil for repairing the selected airfoil;

said tool including a section carrying an abrasive and pivotally carried by said manipulator, and a spring for biasing said section to maintain the abrasive engaged against the airfoil with a substantial constant force.

6. Apparatus according to claim 5 wherein said tool includes an endless abrasive belt and a drive motor for driving the belt.

7. Apparatus according to claim 6 wherein said tool includes a fixed section, said pivoted section being pivoted to said fixed section, said abrasive belt being carried by said fixed section and said pivoted section with the pivoted section being pivoted about an axis intermediate a longitudinal extent of the belt.

8. Apparatus according to claim 7 including a motor carried by said fixed section for rotating the pivoted section about the intermediate axis.

9. Apparatus according to claim 7 wherein said fixed section includes a drive wheel engaging said belt, said pivoted section including a pair of idler wheels spaced from one another, one of said idler wheels being carried by said pivoted section adjacent an end thereof remote from said fixed section and a second idler wheel adjacent an opposite end of said pivoted section in coincidence with said pivot axis.

10. Apparatus for in situ repair of airfoils of a compressor, comprising:

a manipulator for mounting to an inlet of the compressor and for movement in a generally circumferential direction about an axis;

a tool carried by said manipulator for movement therewith and relative thereto about three orthogonally related axes, said tool being movable into the inlet of the compressor to a position in contact with a selected airfoil;

a drive system for driving said tool into contact with the selected airfoil; and

a system for controlling the drive system to position the tool in contact with the selected airfoil for repairing the selected airfoil;

said tool including a device for shot peening the surface of the selected airfoil.

11. Apparatus according to claim 10 wherein said shot peening device includes a flapper carrying shot within a flexible matrix and a drive carried by said manipulator for rotating the flapper about an axis to shot peen the surface of the selected airfoil.

12. Apparatus according to claim 10 wherein said shot peening device includes a gun barrel for propelling free steel shot for impact against the surface of the selected airfoil to strengthen the surface.

13. Apparatus according to claim 12 wherein the gun barrel includes a nozzle through which the steel shot passes for impact against the airfoil surface and an enclosure about the nozzle and at least a portion of the airfoil for collecting the steel shot after impact on the airfoil surface.

14. Apparatus according to claim 13 including a vacuum system coupled to said enclosure for removing the steel shot from the enclosure.

15. Apparatus according to claim 12 wherein the gun barrel includes a nozzle through which the steel shot passes for impact against the airfoil surface, said nozzle carrying a deflector for deflecting steel shot passing through the nozzle onto a surface of the airfoil.

16. Apparatus according to claim 10 wherein said tool includes a grinding tool and a guide for engagement with the airfoil to enable the grinding tool to remove material from the blade to only a limited depth.

17. Apparatus for in situ repair of airfoils of a compressor, comprising:

an arcuate track for mounting to an inlet of the compressor;

a manipulator mounted on said track for movement in a generally circumferential direction about an axis and along said track;

a support system for a tool including a first module carried by said manipulator for movement therewith and relative thereto in a generally tangential direction;

a second module carried by said first module for movement relative to said first module in a direction normal to said tangential direction and generally in a plane normal to an axis of the compressor;

a third module carried by said second module for movement relative to said second module in a direction generally parallel to said axis, said tool being carried by said third module for movement therewith;

a drive system for driving said modules in the respective directions;

a system for measuring and recording the position of the tool relative to a selected airfoil; and

a system responsive to the measuring and recording system for controlling the drive system to position the tool relative to the selected airfoil for repairing the selected airfoil.

18. Apparatus according to claim 17 wherein the drive system includes a servo-motor coupled to a lead screw for driving at least one of said modules.

19. Apparatus according to claim 17 wherein the drive system includes a servo-motor and a lead screw for driving each of the respective modules.

20. Apparatus according to claim 17 wherein said tool includes an abrasive carried by said third module for movement relative to said third module.

21. Apparatus according to claim 17 wherein said tool includes a finger carrying an abrasive and pivotally carried by said third module.

22. Apparatus according to claim 21 wherein said finger is pivotally carried for movement by said third module about an axis extending generally parallel to the direction of movement of said second module relative to said first module.

23. Apparatus according to claim 17 wherein said tool includes a section carrying an abrasive and pivotally carried by said third module, and a spring for biasing said abrasive to maintain the abrasive engaged against the airfoil with a substantial constant force.

24. Apparatus according to claim 17 wherein said tool includes an endless abrasive belt and a drive motor for driving the belt.

25. Apparatus according to claim 24 wherein said tool includes a fixed section and a second section pivoted to said fixed section, said abrasive belt being carried by said fixed section and said pivoted section with the pivoted section being pivoted about an axis intermediate a longitudinal extent of the belt.

26. Apparatus according to claim 25 including a motor carried by said fixed section for rotating the pivoted section about the intermediate axis.

27. Apparatus according to claim 25 wherein said fixed section includes a drive wheel engaging said belt, said pivoted section including a pair of idler wheels spaced from one another, one of said idler wheels being carried by said pivotal section adjacent an end thereof remote from said fixed section and a second idler wheel adjacent an opposite end of said pivoted section in coincidence with said pivot axis.

28. Apparatus according to claim 17 wherein said tool includes a device for shot peening the surface of the selected airfoil.

29. Apparatus according to claim 28 wherein said shot peening device includes a flapper carrying captive shot within a flexible matrix and a drive carried by said module for rotating the flapper about an axis to shot peen the surface of the selected airfoil.

30. Apparatus according to claim 28 wherein said shot peening device includes a gun barrel for propelling free steel shot for impact against the surface of the selected airfoil to strengthen the surface.

31. Apparatus according to claim 30 wherein the gun barrel includes a nozzle through which the steel shot passes for impact against the airfoil surface and an enclosure about the nozzle and at least a portion of the airfoil for collecting the steel shot after impact on the airfoil surface.

32. Apparatus according to claim 31 including a vacuum system coupled to said enclosure for removing the steel shot from the enclosure.

33. Apparatus according to claim 30 wherein the gun barrel includes a nozzle through which the steel shot passes for impact against the airfoil surface, said nozzle carrying a deflector for deflecting steel shot passing through the nozzle onto a surface of the airfoil.