Analysis of component for presence, composition and/or thickness of coating

• US 20070296967A1
• Filed: 06/27/2006
• Published: 12/27/2007
• Est. Priority Date: 06/27/2006
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Das, Nripendra Nath, Gupta, Bhupendra Kumra, BENICEWICZ, PAMELA KING
• Application Number:
  US11/475,212
• Publication Number:
  US 20070296967A1
• Time in Patent Office: Days
• US Class Current: 356/318
• CPC Class Codes: G01J 3/2889 Rapid scan spectrometers; Time resolved spectrometry
• CPC Class Codes: G01J 3/443 Emission spectrometry
• CPC Class Codes: G01N 21/718 Laser microanalysis, i.e. with formation of sample plasma

Abstract

A method comprising the following steps: (a) providing a turbine component comprising a metal substrate having an external surface; and (b) analyzing the external surface by laser plasma spectroscopy to determine whether a metallic coating is present on or absent from the external surface. If a metallic coating is determined to be present on the external surface, the elemental composition, elemental concentration and/or thickness of the metallic coating present on the external surface may be determined (qualitatively and/or quantitatively) by laser plasma spectroscopy. Another method comprises the following steps: (a) providing a turbine component comprising a metal substrate having an external surface which has been subjected to treatment to remove a metallic coating applied to the external surface; and (b) analyzing the treated external surface by laser plasma spectroscopy to determine the degree of removal of the metallic coating from the treated external surface.

Claims

1. A method comprising the following steps:

(a) providing a turbine component comprising a metal substrate having an external surface; and

(b) analyzing the external surface by laser plasma spectroscopy to determine whether a metallic coating is present on or absent from the external surface.

2. The method of claim 1 wherein step (b) is carried out to determine whether a diffusion coating is present on or absent from the external surface.

3. The method of claim 2 wherein step (b) is carried out to determine whether a simple aluminide diffusion coating is present on or absent from the external surface.

4. The method of claim 1 wherein step (a) is carried out by providing a turbine blade.

5. The method of claim 4 wherein step (a) is carried out by providing a turbine blade with an internal surface having a simple aluminide diffusion coating thereon, and wherein the external surface may or may not have a simple aluminide diffusion coating thereon.

6. The method of claim 1 wherein step (b) is carried out with a portable laser plasma spectroscopy system.

7. The method of claim 1 wherein step (a) is carried out by providing a turbine component wherein the metal substrate comprises a superalloy based on nickel, cobalt and/or iron.

8. The method of claim 7 wherein step (b) is carried out to determine the presence or absence of a simple aluminide diffusion coating on the external surface.

9. The method of claim 1 wherein step (b) is carried out to determine the presence or absence of an overlay metal alloy coating on the external surface.

10. A method comprising the following steps:

(a) providing a turbine component comprising a metal substrate having an external surface;

(b) analyzing the external surface by laser plasma spectroscopy to determine whether a metallic coating is present on or absent from the external surface; and

(c) if a metallic coating is determined to be present on the external surface, determining by laser plasma spectroscopy the elemental composition, elemental concentration and/or thickness of the metallic coating present on the external surface.

11. The method of claim 10 wherein step (c) is carried out to qualitatively determine the elemental composition of the metallic coating present on the external surface.

12. The method of claim 10 wherein step (c) is carried out to determine the elemental concentration of the metallic coating present on the external surface.

13. The method of claim 12 wherein step (c) is carried out by monitoring a ratio of two marker elements present in the metallic coating, the metal substrate or both.

14. The method of claim 13 wherein the marker elements comprise Al and Cr.

15. The method of claim 10 wherein step (c) is carried out to determine the thickness of the metallic coating present on the external surface.

16. The method of claim 15 wherein the thickness of the metallic coating is determined in step (c) by using an ablation rate calibration curve.

17. The method of claim 16 wherein step (c) comprises:

(a) monitoring the change in ratio of two marker elements of the metallic coating measured by laser plasma spectroscopy;

(b) obtaining a total ablation time when the change in ratio of the marker elements indicates that the metallic coating has been completely penetrated; and

(c) comparing the total ablation time to the ablation rate calibration curve to determine the thickness of the metallic coating.

18. The method of claim 17 wherein the change in ratio of Al to Cr is monitored during step (c).

19. The method of claim 10 wherein step (a) is carried out by providing a turbine blade.

20. The method of claim 19 wherein step (a) is carried out by providing a turbine blade with an internal surface having a simple aluminide diffusion coating thereon, and wherein the external surface may or may not have a simple aluminide diffusion coating thereon.

21. The method of claim 10 wherein steps (b) and (c) are carried out with a portable laser plasma spectroscopy system.

22. The method of claim 10 wherein step (a) is carried out by providing a turbine component wherein the metal substrate comprises a superalloy based on nickel, cobalt and/or iron.

23. The method of claim 10 wherein the metallic coating detected during step (b) is a simple aluminide diffusion coating.

24. The method of claim 23 wherein step (c) is carried out to determine the thickness of the simple aluminide diffusion coating.

25. The method of claim 10 wherein step (c) comprises comparing a spectral profile obtained by laser plasma spectroscopy on the metallic coating to a known emission spectra to determine the elemental composition of the metallic coating.

26. The method of claim 10 wherein only selected emissions are collected during step (c).

27. The method of claim 26 wherein resolved spectra have been identified and correlated to differentiate the metallic coatings prior to carrying out step (c).

28. A method comprising the following steps:

(a) providing a turbine component comprising a metal substrate having an external surface which has been subjected to treatment to remove a metallic coating applied to the external surface; and

(b) analyzing the treated external surface by laser plasma spectroscopy to determine the degree of removal of the metallic coating from the treated external surface.

29. The method of claim 28 wherein the metallic coating of step (a) that is subjected to treatment for removal is a simple aluminide diffusion coating.

30. The method of claim 28 wherein the metallic coating of step (a) has been subjected to chemical stripping.

31. The method of claim 28 wherein if the metallic coating is detected during the carrying out of step (b), an additional step (c) is carried out to subject the detected metallic coating to further treatment to remove the detected metallic coating.

32. The method of claim 31 wherein an additional step (d) is carried out after step (c) by laser plasma spectroscopy to determine the degree of removal of the treated detected metallic coating.

33. The method of claim 32 wherein steps (c) and (d) are repeated one or more times.

34. The method of claim 32 wherein the degree of removal of the metallic coating is determined in step (c) by using an ablation rate calibration curve.