IP Library › Granted Patent US 9,535,012
Granted Patent B2
US 9,535,012 · App. 14/323,183 · Granted Jan 3, 2017

Method for the non-destructive testing of workpiece surfaces

Inventors: Wilhelm Satzger (Munich, DE); Joachim Bamberg (Dachau, DE); Roland Hessert (Herrsching, DE); Robert Schuster (Munich, DE); Thomas Hess (Munich, DE)
Assignee: MTU AERO ENGINES AG
G01N21/91G01N21/33G01N21/6447
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Quick Facts
Patent No.
US 9,535,012
App. No.
14/323,183
Granted
Jan 3, 2017
Kind
B2
Abstract

Disclosed is a method for the non-destructive testing of workpiece surfaces of a workpiece by means of fluorescent penetrant testing or dye penetrant testing. The method comprises applying a penetrant to the region of the workpiece surface to be examined, thereby allowing the penetrant to penetrate into possible recesses in the workpiece surface, applying a developer to the region of the workpiece surface to be tested; bleaching the penetrant by a gaseous or liquid oxidant; and visually assessing the penetrant that has remained in the recesses present in the workpiece surface.

Claims (25)

1. A method for the non-destructive testing of a workpiece surface of a workpiece by fluorescent penetrant testing or dye penetrant testing, wherein the method comprises:

(a) cleaning a region of the workpiece surface which is to be examined;

(b) applying a liquid fluorescent penetrant or a liquid non-fluorescent dye penetrant to the region of the workpiece surface which is to be examined, thereby allowing the penetrant to penetrate into possible recesses in the workpiece surface;

(c) removing excess penetrant from the workpiece surface;

(d) applying a developer to the region of the workpiece surface which is to be examined and from which excess penetrant has been removed;

(e) bleaching the penetrant by a gaseous or liquid oxidant in a layer formed by applied developer on the workpiece surface; and

(f) visually assessing penetrant that has remained in the recesses present in the workpiece surface.

2. The method of claim 1 , wherein the oxidant comprises ozone.

3. The method of claim 2 , wherein in (e) the workpiece with the workpiece surface is introduced into a chamber or container filled with ozone.

4. The method of claim 2 , wherein in (e) the workpiece with the workpiece surface is exposed to an ozone stream at least in a region of the workpiece surface.

5. The method of claim 2 , wherein in (e) the workpiece with the workpiece surface is exposed to an oxygen stream and at the same time to UV radiation for forming the ozone at least in a region of the workpiece surface.

6. The method of claim 2 , wherein (b) to (f) are repeated after conclusion of (f).

7. The method of claim 1 , wherein in (e) the oxidant is heated.

8. The method of claim 1 , further comprising (d1) a first visual assessment of the workpiece surface prior to (e).

9. The method of claim 8 , wherein in (d1) the workpiece surface to be examined is irradiated with UV light.

10. The method of claim 1 , wherein in (f) the workpiece surface to be examined is irradiated with UV light.

11. The method of claim 1 , wherein a further operation for bleaching the fluorescent penetrant or the non-fluorescent dye penetrant in a developer layer by the gaseous or liquid oxidant is carried out after or during the visual assessment of (f).

12. The method of claim 1 , wherein (b) to (f) are repeated after conclusion of (f).

13. The method of claim 1 , wherein the workpiece surface is a surface of a turbomachine.

14. The method of claim 1 , wherein the workpiece surface is a surface of a component of a gas turbine.

15. The method of claim 1 , wherein the penetrant comprises a fluorescent dye penetrant.

16. The method of claim 1 , wherein the penetrant comprises a non-fluorescent dye penetrant.

17. A method for the production of a component of a turbomachine, wherein the method comprises carrying out the method of claim 1 .

18. The method of claim 1 , wherein the workpiece surface is a surface of a component of a gas turbine.

19. A method for the maintenance of a component of a turbomachine, wherein the method comprises carrying out the method of claim 1 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 24, 2014
From: SATZGER, WILHELM; BAMBERG, JOACHIM; HESSERT, ROLAND; SCHUSTER, ROBERT; HESS, THOMAS
To: MTU AERO ENGINES AG
Reel/Frame 033380/0437 →
Priority Claims (1)
DE 10 2013 213 369 · Jul 9, 2013 · national
Continuity (1)
Related Publication 20150017736A1 · Jan 15, 2015