IP Library Granted Patent US 7,781,698
Granted Patent B2
US 7,781,698 · App. 11/420,648 · Granted Aug 24, 2010

Process for manufacturing a coiled insert of coated filaments

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Quick Facts
Patent No.
US 7,781,698
App. No.
11/420,648
Granted
Aug 24, 2010
Kind
B2
Abstract

A process for manufacturing a coiled insert of coated filaments is disclosed. Each filament includes a ceramic fiber coated with a metal sheath. The process includes a step of winding a sheet of coated filaments around a piece. At the start of winding, a first metal shim is placed beneath the sheet and coiled. At the end of winding, a second metal shim is placed on the sheet and coiled. The process is applied to the manufacture of aeronautical turbomachine components.

Claims (20)

1. A process for manufacturing a coiled insert of coated filaments, each filament comprising a ceramic fiber coated with a metal sheath, the process comprising:

manufacturing a sheet of coated filaments by laser welding; and

winding a sheet of coated filaments around a piece,

wherein at the start of winding, a first metal shim is placed beneath the sheet and coiled such that the first metal shim provides an internal part of the coiled insert,

wherein at the end of winding, a second metal shim is placed on the sheet and coiled such that the second metal shim provides an external part of the coiled insert,

wherein a portion of an innermost layer of the coiled insert is sandwiched between a first end portion of the first metal shim and a second end portion of the first metal shim, and

wherein a portion of an outermost layer of the coiled insert is sandwiched between a first end portion of the second metal shim and a second end portion of the second metal shim.

2. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein the second end portion of the second metal shim covers the outermost layer of the coiled insert and is welded close to the first end portion of the second metal shim.

3. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein the first end portion of the first metal shim is flush in line with a first end portion of the sheet.

4. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein, at the end of the process, the coiled insert is removed from the piece onto which it has been coiled with the shims.

5. A coiled insert of coated filaments, formed by the process as claimed in claim 1 , comprising:

a coil of a sheet of coated filaments with a first metal shim which provides an internal part of the coiled insert and a second metal shim which provides an external part of the coiled insert.

6. A process for manufacturing a component with an insert made of a composite having a metal matrix, within which ceramic fibers extend, comprising:

placing a coiled insert of coated filaments obtained according to the method of claim 1 in an annular cavity of a metal container;

adding a metal lid to the container to form an assembly; and

compacting the assembly by hot isostatic pressing.

7. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein each filament includes a silicon carbide ceramic fiber coated with a titanium alloy.

8. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein the first metal shim and the second metal shim each include a titanium alloy.

9. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein a width of the first metal shim and a width of the second metal shim is the same as a width of the sheet of coated filaments.

10. The process for manufacturing a coiled insert of coated filaments as claimed in claim 1 , wherein the coiled insert includes a plurality of layers disposed between a first end of the sheet and a second end of the sheet.

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 Jul 5, 2006
From: FRANCHET, JEAN-MICHEL PATRICK MAURICE; KLEIN, GILLES CHARLES CASIMIR; SALVAT, LOUIS
To: SNECMA; FSP-ONE
Reel/Frame 018064/0515 →