IP Library Granted Patent US 7,066,799
Granted Patent B2
US 7,066,799 · App. 10/997,863 · Granted Jun 27, 2006

Protection mask for surface treatment of turbomachine blades

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Quick Facts
Patent No.
US 7,066,799
App. No.
10/997,863
Granted
Jun 27, 2006
Kind
B2
Abstract

A protection mask used during surface treatment for a turbomachine blade, including for example a sand blasting step and/or a metal coating step, includes at least one part matching the shape of a portion of the blade. The mask is designed to resist surface treatment effects and to be placed on the surface to be protected, and can form a removable and reusable tool according to the invention.

Claims (27)

1. A protection mask for surface treatment of surfaces of a turbomachine blade comprising a root wherein said surfaces are located on the root of the blade, said protection mask comprising:

at least one part matching a shape of the root, and

openings having a same shape as a shape of said surfaces and wherein said surfaces to be treated can be seen through said openings when said at least one part is mounted on said root.

2. A mask according to claim 1 , wherein said at least one part comprises at least two half-shells.

3. A mask according to claim 1 , wherein said at least one part is made of a material resistant to thermal effects of a plasma deposition.

4. A mask according to claim 1 , wherein said at least one part is made of a material resistant to thermal effects of sand blasting.

5. A mask according to claim 1 , wherein said at least one part is made of stainless steel.

6. A mask according to claim 5 , wherein said at least one part is configured to be mounted on said root of said blade by force fitting.

7. A mask according to claim 1 , wherein said at least one part is made of a silicone.

8. A mask according to claim 2 , wherein said at least two half-shells are held together by at least one of bolts and clamps.

9. A mask according to claim 2 , wherein said at least two half-shells are made of stainless steel.

10. A mask according to claim 1 , wherein said at least one part is made of a polymer material.

11. A mask according to claim 1 , wherein said at least one part has a dovetail cross-section so as to fit over a root having a dovetail shape.

12. A mask according to claim 1 , wherein said openings are defined by walls that are perpendicular to said surfaces.

13. A mask according to claim 1 , wherein said at least one part defines a groove.

14. A mask according to claim 13 , wherein said groove is located on a wall covering a bottom of said root.

15. A mask according to claim 1 , wherein said at least one part is mounted on said root of said blade so that said openings expose said surfaces.

16. A mask according to claim 1 , wherein said at least one part is resistant to effects of said surface treatment.

17. A mask according to claim 16 , wherein said at least one part is removable from said blade after said surface treatment.

18. A mask according to claim 17 , wherein said at least one part is reusable for treating surfaces of another blade.

19. A protection mask for surface treatment of a surface of a tubromachine blade comprising a fin, wherein said surface is located at an end of the fin, said protection mask comprising:

two half shells matching a shape of the fin and assembled with each other by clamps.

20. A mask according to claim 19 , wherein said two half shells define a window that exposes said end of said fin when said two half shells are mounted on said turbomachine blade.

21. A mask according to claim 20 , wherein said window is defined by walls that are perpendicular to said surface.

22. A mask according to claim 19 , wherein said two half shells are resistant to effects of said surface treatment.

23. A mask according to claim 22 , wherein said two half shells are removable from said turbomachine blade after said surface treatment.

24. A mask according to claim 23 , wherein said two half shells are reusable for treating a surface of another turbomachine blade.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →