IP Library Granted Patent US 8,684,255
Granted Patent B2
US 8,684,255 · App. 13/637,593 · Granted Apr 1, 2014

Method of manufacturing an elongate insert made of a metal matrix composite

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,684,255
App. No.
13/637,593
Granted
Apr 1, 2014
Kind
B2
Abstract

A method of manufacturing an elongate insert configured to be integrated by CIC in a metal container, including coated yarns bonded together, the coated yarns being formed from metal-coated ceramic fibers. The method includes placing the coated yarns side by side in a bundle and pulling the fiber bundle through a shaping element so as to compact the fiber bundle transversely while forming the fiber bundle so as to have a defined cross section. A metal part incorporating a fibrous insert can be manufactured by the CIC technique.

Claims (17)

1. A method for manufacturing an insert of elongate shape configured to be incorporated by CIC into a metal container, including coated yarns bound together, the coated yarns being formed of metal-coated ceramic fibers, the method comprising:

placing the coated yarns side by side in a bundle including a plurality of layers of coated yarns;

placing a first metal sheet on a top of the bundle and a second metal sheet on a bottom of the bundle;

pulling the bundle and the first and second metal sheets through a shaping element to compact the bundle transversely while forming the bundle and the first and second metal sheets with a determined cross section by the shaping element; and

placing straps transversely clamping the bundle and the first and second metal sheets, downstream of the shaping element,

wherein the shaping element includes first and second rollers which press against the first and second metal sheets, respectively, and first and second lateral sliders which contact first and second lateral sides of the bundle, respectively, during the pulling of the bundle, the first and second lateral sliders are secured to a frame on which the first and second rollers are rotatably mounted, and

wherein the metal of the first and second metal sheets is the same as the metal of the metal container.

2. The method according to claim 1 , wherein the first and second rollers have parallel axes.

3. The method according to claim 1 , wherein a passageway cross section of the shaping element is polygonal with rectilinear or curved sides.

4. The method according to claim 1 , a passageway cross section of the shaping element being oval or circular.

5. The method according to claim 1 , wherein, before the coated yarns are grouped into the bundle, the coated yarns are placed in elementary bundles that are assembled together to form the bundle.

6. The method according to claim 1 , wherein the straps being placed along the insert downstream of the shaping element.

7. A method for manufacturing a metal part comprising:

incorporation of an insert formed according to claim 1 in a metal container; and

hot isostatic compaction of the assembly.

8. A part of elongate shape comprising at least one fibrous reinforcement in the longitudinal direction, obtained according to the method of claim 7 , wherein cross section of the reinforcement has a non-rectangular shape, or a trapezoidal or oval shape.

9. The method according to claim 1 , wherein the coated yarns of the bundle are free of transverse stress prior to the pulling of the bundle and the first and second metal sheets through the shaping element.

Assignments (4)
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 Dec 8, 2016
From: MESSIER-BUGATTI-DOWTY
To: SAFRAN LANDING SYSTEMS
Reel/Frame 040851/0908 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 1, 2012
From: FRANCHET, JEAN-MICHEL PATRICK MAURICE; KLEIN, GILLES CHARLES CASIMIR; MASSON, RICHARD; SALVAT, LOUIS
To: SNECMA; MESSIER-BUGATTI-DOWTY
Reel/Frame 029054/0938 →