IP Library Granted Patent US 7,511,248
Granted Patent B2
US 7,511,248 · App. 11/420,658 · Granted Mar 31, 2009

Process for manufacturing a bonded sheet composed of ceramic filaments with a metal matrix, device for implementing said process, bonded sheet obtained by said process

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Quick Facts
Patent No.
US 7,511,248
App. No.
11/420,658
Granted
Mar 31, 2009
Kind
B2
Abstract

A process for manufacturing a bonded sheet with a plurality of coated filaments, which include a ceramic fiber coated with a metal sheath, includes placing the filaments beside one another in one and the same plane, and welding the filaments together by laser spot welding.

Claims (20)

1. A process for manufacturing a bonded sheet comprising a plurality of coated filaments, wherein each filament comprises a ceramic fiber coated with a metal sheath so that said coated filaments include a plurality of ceramic fibers, said process comprising:

placing the filaments beside one another in one and a same plane such that the metal sheath of each filament contacts the metal sheath of an adjacent filament, and

welding the filaments together by laser spot welding by directing a laser beam perpendicularly to said plane in which said filaments are placed and toward contact points between two adjacent filaments so that said laser beam is perpendicular to said adjacent filaments at said contact points,

wherein said laser spot welding is performed by sequentially exposing contact points of different pairs of adjacent filaments to said laser beam thereby forming an interrupted weld across a transverse direction of said bonded sheet.

2. A process according to claim 1 , wherein said welding step is performed by running the filaments past a laser welding device so as to form spot welds aligned in segments perpendicular to a direction in which the filaments run.

3. A process according to claim 2 , wherein said welding step is performed while maintaining the filaments stationary during formation of a segment of spot welds.

4. A process according to claim 1 , wherein said welding step is performed by running the filaments past a laser welding device so as to form spot welds arranged in a zig-zag pattern on the bonded sheet.

5. A process according to claim 4 , wherein said welding step is performed by running the filaments continuously past the laser welding device.

6. A process according to claim 4 , wherein said welding step is performed while maintaining the filaments stationary during formation of a spot weld.

7. A process according to claim 2 , further comprising, prior to the filaments running past the laser welding device, running the filaments through a warping module.

8. A process according to claim 2 , further comprising driving the filaments by a rotating bobbin.

9. A process according to claim 2 , further comprising driving the filaments from a bobbin module, each bobbin of the module having a wound coated filament or a bundle of coated filaments.

10. A process according to claim 1 , further comprising adjusting the rigidity of said bonded sheet by adjusting a distance between successive weld spots.

11. A process according to claim 1 , wherein said process is free of any step of adding a binder throughout said manufacturing of said bonded sheet.

12. A process according to claim 1 , wherein said process is free of any step of removing a binder throughout said manufacturing of said bonded sheet.

13. A process according to claim 1 , further comprising a step of adjusting welding parameters of said laser spot welding such that weld pools at said contacts point do not flow out.

14. A process for manufacturing a tubular component according to claim 1 , wherein said laser spot welding is performed in an inert atmosphere.

15. A process for manufacturing a tubular component according to claim 14 , wherein said laser spot welding is performed in an argon atmosphere.

16. A process according to claim 1 , further comprising a step of winding the welded filaments, and wherein said process is free of a step of pressing said filaments with rollers between said welding step and said winding step.

17. A process according to claim 1 , wherein said laser spot welding is concentrated at said contact points such that said laser beam is not directed toward said ceramic fibers and such that said ceramic fibers are not affected by a local melting of the metal sheath caused by said laser beam at said contact points.

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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 28, 2006
From: FRANCHET, JEAN-MICHEL; KLEIN, GILLES
To: SNECMA
Reel/Frame 018525/0895 →