IP Library Granted Patent US 7,837,139
Granted Patent B2
US 7,837,139 · App. 12/018,525 · Granted Nov 23, 2010

Tubular part that includes an insert made of a metal matrix composite

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Quick Facts
Patent No.
US 7,837,139
App. No.
12/018,525
Granted
Nov 23, 2010
Kind
B2
Abstract

The invention relates to a process for manufacturing a tubular part, which includes an insert made of a metal matrix composite and within which ceramic fibers extend. The process comprises the following steps: the filaments of a filament bundle are fixed close to one end of a support part, said filaments being separate from one another and each filament comprising a ceramic fiber coated with a metal sheath; and all the filaments of the bundle are wound around the support part along a helical path.

Claims (23)

1. A process for manufacturing a tubular part which includes an insert made of a metal matrix composite and within which ceramic fibers extend, the process comprising the steps of:

fixing filaments of a filament bundle close to one end of a support part, said filaments being separate from one another and each filament comprising a ceramic fiber coated with a metal sheath;

placing the support part through a cylindrical passage of a die; and

translating the die along an axis of the support part while the support part is rotated around the axis to wind all the filaments of the bundle around the support part along a helical path.

2. The process as claimed in claim 1 , wherein the die is driven rotationally about the axis of the support part.

3. The process as claimed in claim 1 , wherein a length of the cylindrical passage is 20% to 30% of a diameter of the support part.

4. The process as claimed in claim 1 , wherein the filaments are coated with a titanium alloy prior to being wound around the support part.

5. An installation for manufacturing a tubular part which includes an insert made of a metal matrix composite and within which ceramic fibers extend, the installation comprising:

a module for forming a bundle of coated filaments, the filaments being separate from one another, each filament comprising a ceramic fiber coated with a metal sheath;

means for fixing the filaments close to one end of a support part; and

winding means for winding all of the filaments of the bundle around the support part along a helical path, the winding means comprising a die placed around the support part and driven translationally along an axis of the support part, the installation driving the support part rotationally about the axis.

6. The installation as claimed in claim 5 , wherein the module for forming a bundle of coated filaments comprises two plates each drilled with a plurality of holes.

7. The installation as claimed in claim 6 , wherein each hole includes a sleeve for guiding the filaments, the sleeve protecting the filaments and tensioning the filaments.

8. The installation as claimed in claim 7 , wherein the sleeves are made of rubber.

9. The installation as claimed in claim 5 , wherein the die is rotationally driven about the axis of the support part.

10. The installation as claimed in claim 5 , wherein the die includes a cylindrical passage in a central part thereof, a length of the cylindrical passage being 20% to 30% of a diameter of the support part.

11. The installation as claimed in claim 5 , wherein a diameter of the die is equal to a diameter of the support part plus 2.1 to 2.5 times a diameter of a filament.

12. The installation as claimed in claim 5 , wherein the filaments are coated with a titanium alloy prior to being wound around the support part.

13. A process for manufacturing a tubular part including an insert made of a metal matrix composite and within which ceramic fibers extend, the process comprising the steps of:

fixing filaments of a filament bundle near a first end of a support part, said filaments being separate from one another and each filament comprising a ceramic fiber coated with a metal sheath;

placing the support part through a cylindrical passage of a die;

translating the die along an axis of the support part while the support part is rotated around the axis to wind all the filaments of the bundle helically around the support part,

wherein the die is driven rotationally about the axis of the support part.

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 Mar 25, 2008
From: FRANCHET, JEAN-MICHEL PATRICK MAURICE; KLEIN, GILLES CHARLES CASIMIR; SALVAT, LOUIS
To: SNECMA
Reel/Frame 020698/0273 →