METHOD FOR AUTOMATED SUPERALLOY LASER CLADDING WITH 3D IMAGING WELD PATH CONTROL

• US 20150048058A1
• Filed: 07/08/2013
• Published: 02/19/2015
• Est. Priority Date: 09/12/2012
• Status: Active Grant

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Energy Incorporated (Siemens AG)
• Inventors: Bruck, Gerald J., Kamel, Ahmed
• Granted Patent: US 9,272,369 B2
• Time in Patent Office: Days
• US Class Current: 219/76.14
• CPC Class Codes: B23K 2101/001 Turbines
• CPC Class Codes: B23K 2103/26 Alloys of Nickel and Cobalt and Chromium
• CPC Class Codes: B23K 26/032 using optical means
• CPC Class Codes: B23K 26/0626 Energy control of the laser beam B23K26/0622 takes precedence
• CPC Class Codes: B23K 26/08 Devices involving relative movement between laser beam and workpiece
• CPC Class Codes: B23K 26/32 taking account of the properties of the material involved
• CPC Class Codes: B23K 26/34 Laser welding for purposes other than joining
• CPC Class Codes: B23K 26/342 Build-up welding
• CPC Class Codes: B23K 31/125 Weld quality monitoring
• CPC Class Codes: B23K 35/0244 Powders, particles or spheres; Preforms made therefrom
• CPC Class Codes: B23K 35/0255 for use in welding B23K35/0205 takes precedence
• CPC Class Codes: B23K 35/36 Selection of non-metallic compositions, e.g. coatings, fluxes B23K35/34 takes precedence; Selection of soldering or welding materials, conjoint with selection of non-metallic compositions, both selections being of interest selection of soldering or welding materials proper B23K35/24
• CPC Class Codes: F01D 5/005 Repairing methods or devices

Abstract

Superalloy components, such as service-degraded turbine blades and vanes, are clad by laser beam welding. The welding/cladding path, including cladding application profile, is determined by prior, preferably real time, non-contact 3D dimensional scanning of the component and comparison of the acquired dimensional scan data with specification dimensional data for the component. A welding path for cladding the scanned component to conform its dimensions to the specification dimensional data is determined The laser welding apparatus, preferably in cooperation with a cladding filler material distribution apparatus, executes the welding path to apply the desired cladding profile. In some embodiments a post-weld non-contact 3D dimensional scan of the welded component is performed and the post-weld scan dimensional data are compared with the specification dimensional data. Preferably the welding path and/or cladding profile application are modified in a feedback loop with the pre- and/or post-welding 3D dimensional scanning.

Claims

1. A method for welding turbine components, comprising:

providing a work table, laser profilometer and laser welding apparatus under common control by a control system, for providing controlled relative motion between the work table and either of the profilometer or welding apparatus;

coupling a turbine component having a substrate to the work table;

scanning a surface of the turbine component substrate in real time by operating the laser profilometer and work table apparatus under control of the control system and acquiring component dimensional data;

comparing component dimensional data with specification dimensional data in real time with the control system and determining a welding pattern for building up component substrate surface portions to conform welded component dimensions to the specification dimensional data; and

welding the component substrate surface in real time by operating the laser welding and work table apparatuses in conformity with the determined welding pattern under control of the control system.

2. The method of claim 1, further comprising:

subsequently scanning the welded component surface in real time with a laser profilometer to acquire post-weld component dimensional data; and

determining with the control system whether the post-weld data are in conformity with the specification dimensional data.

3. The method of claim 2, further comprising modifying the welding pattern with the control system in a feedback loop to conform the post-weld dimensional data to the specification dimensional data.

4. The method of claim 1, the welding step further comprising:

introducing filler material on the component substrate surface;

focusing a welding laser beam on the filler material and substrate;

transferring optical energy from the welding laser to the filler material and substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate; and

moving the substrate and welding laser beam relative to each other while maintaining uniform energy transfer;

wherein the provided laser welding apparatus has;

a welding laser generating a welding laser beam for transferring optical energy to the turbine component substrate and filler material on the substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate;

at least one movable mirror intercepting the welding laser beam, for orienting the laser beam on the substrate; and

at least one drive system coupled to each of the respective control system, at least one movable mirror and welding the laser, for causing relative motion between the welding laser beam and substrate.

5. The method of claim 4, the maintaining uniform energy transfer step comprising any one of:

varying optical energy transfer based on component surface topology;

varying relative movement rate of the substrate and welding laser beam;

varying welding laser power output;

rastering the welding laser beam and substrate relative to each other;

translating and oscillating the substrate and welding laser beam relative to each other along the welding pattern path modulating the welding laser power output;

varying filler material composition, introduction rate or dispersal pattern;

or monitoring energy transfer with the control system in a closed feedback loop and varying energy transfer rate based on the monitored energy transfer.

6. The method of claim 1, further comprising:

providing a. a fiber optic tube having a pair of separate optical paths that are optically coupled to the respective profilometer and welding lasers on an input end thereof; and

a variable focus lens for focusing laser beams generated by the respective lasers optically coupled to an output end of the fiber optic tube; and

selectively energizing one of the corresponding respective lasers when performing a scanning or welding operation and focusing the energized laser with the variable focus lens.

7. The method of claim 1, further comprising:

providing a common laser source for the laser profilometer and laser welding apparatus; and

operating the laser source in different modes for the profilometer and welding apparatus by varying one or more of laser power output, frequency or output modulation.

8. The method of claim 1 further comprising improving profilometer scanning sensitivity by:

selecting a profilometer laser frequency outside frequency range of reflected frequencies generated during laser welding; and

filtering from laser profilometer scanning sensors the frequency range of reflected frequencies generated during laser welding. .

9. A method for welding turbine components, comprising:

providing a work table, laser profilometer and laser welding apparatus under common control by a control system, for providing controlled relative motion between the work table and either of the profilometer or welding apparatus;

coupling a turbine component having a substrate to the work table;

scanning a surface of the turbine component substrate by operating the laser profilometer and work table apparatus under control of the control system and acquiring component dimensional data;

comparing component dimensional data with specification dimensional data with the control system and determining a welding pattern for building up component substrate surface portions to conform welded component dimensions to the specification dimensional data; and

welding the component substrate surface by operating the laser welding and work table apparatuses in conformity with the determined welding pattern under control of the control system.

10. The method of claim 9, further comprising:

subsequently scanning the welded component surface with a laser profilometer to acquire post-weld component dimensional data; and

determining with the control system whether the post-weld data are in conformance with the specification dimensional data.

11. The method of claim 10, further comprising modifying the welding pattern with the control system in a feedback loop to conform the post-weld dimensional data to the specification dimensional data.

12. The method of claim 9, the welding step further comprising:

introducing filler material on the component substrate surface;

focusing a welding laser beam on the filler material and substrate;

transferring optical energy from the welding laser to the filler material and substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate; and

moving the substrate and welding laser beam relative to each other while maintaining uniform energy transfer;

wherein the provided laser welding apparatus has;

a welding laser generating a welding laser beam for transferring optical energy to the turbine component substrate and filler material on the substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate;

at least one movable mirror intercepting the welding laser beam, for orienting the laser beam on the substrate; and

at least one drive system coupled to each of the respective control system, at least one movable mirror and welding the laser, for causing relative motion between the welding laser beam and substrate.

13. The method of claim 12, further comprising:

subsequently scanning the welded component surface with a laser profilometer to acquire post-weld component dimensional data; and

determining with the control system whether the post-weld data are in conformance with the specification dimensional data.

14. The method of claim 13, further comprising modifying the welding pattern with the control system in a feedback loop to conform the post-weld dimensional data to the specification dimensional data.

15. The method of claim 9 further comprising improving profilometer scanning sensitivity by:

selecting a profilometer laser frequency outside frequency range of reflected frequencies generated during laser welding; and

filtering from laser profilometer scanning sensors the frequency range of reflected frequencies generated during laser welding.

16. The method of claim 15 further comprising performing the scanning and welding steps dynamically and simultaneously in a real time continuous process.

17. A method for welding turbine components, comprising:

providing a work table, laser profilometer , welding powder filler dispenser, and galvanometer laser welding apparatus under common control by a control system, for providing controlled relative motion between the work table and either of the profilometer or welding apparatus, the galvanometer laser welding apparatus having;

a welding laser generating a welding laser beam for transferring optical energy to the turbine component substrate and filler material on the substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate,

at least one movable mirror intercepting the welding laser beam, for orienting the laser beam on the substrate, and

at least one drive system coupled to each of the respective control system, at least one movable mirror and welding the laser, for causing relative motion between the welding laser beam and substrate;

coupling a turbine component having a substrate to the work table;

scanning a surface of the turbine component substrate by operating the laser profilometer and work table apparatus under control of the control system and acquiring component dimensional data;

comparing component dimensional data with specification dimensional data with the control system and determining a welding pattern for building up component substrate surface portions to conform welded component dimensions to the specification dimensional data; and

welding the component substrate surface by;

introducing filler material on the component substrate surface with the welding powder filler dispenser at a selected feed rate and dispersal pattern determined by the control system;

focusing a welding laser beam on the filler material and substrate;

transferring optical energy from the welding laser to the filler material and substrate that fuses the filler material to the substrate as a filler layer without causing thermal degradation to the substrate; and

moving the substrate and welding laser beam relative to each other while maintaining uniform energy transfer by operating the laser welding and work table apparatuses in conformity with the determined welding pattern under control of the control system.

18. The method of claim 17, the maintaining uniform energy transfer step comprising any one of:

varying relative movement rate of the substrate and welding laser beam;

varying welding laser power output;

rastering the welding laser beam and substrate relative to each other;

translating and oscillating the substrate and welding laser beam relative to each other along the welding pattern path;

modulating the welding laser output;

varying filler material composition, introduction rate or dispersal pattern;

or monitoring energy transfer with the control system in a closed feedback loop and varying energy transfer rate based on the monitored energy transfer.

19. The method of claim 18, further comprising:

subsequently scanning the welded component surface with a laser profilometer to acquire post-weld component dimensional data;

determining with the control system whether the post-weld data are in conformance with the specification dimensional data; and

modifying the welding pattern with the control system in a feedback loop to conform the post-weld dimensional data to the specification dimensional data.

20. The method of claim 19 further comprising performing the scanning and welding steps dynamically and simultaneously in real time in a continuous process.