Method for the non-destructive testing of workpiece surfaces

US9535012B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9535012-B2
Application numberUS-201414323183-A
CountryUS
Kind codeB2
Filing dateJul 3, 2014
Priority dateJul 9, 2013
Publication dateJan 3, 2017
Grant dateJan 3, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

Opening claim text (preview).

What is claimed is: 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 .

Assignees

Inventors

Classifications

  • by visual observation · CPC title

  • using ultraviolet light (G01N21/39 takes precedence) · CPC title

  • G01N21/91Primary

    using penetration of dyes, e.g. fluorescent ink · CPC title

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Frequently asked questions

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What does patent US9535012B2 cover?
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 workpi…
Who is the assignee on this patent?
MTU Aero Engines AG
What technology area does this patent fall under?
Primary CPC classification G01N21/91. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jan 03 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).