IP Library Granted Patent US 9,193,101
Granted Patent B2
US 9,193,101 · App. 13/703,487 · Granted Nov 24, 2015

Method for manufacturing an article made of composite material

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Quick Facts
Patent No.
US 9,193,101
App. No.
13/703,487
Granted
Nov 24, 2015
Kind
B2
Abstract

A method for manufacturing an article made of a composite material including a polymer matrix reinforced by a fibrous structure, the method including: placing the fibrous structure on a substrate; forming a molding surface, covering the structure with a mating mold; and compacting the structure by moving the surface of the mating mold toward the surface of the substrate. The substrate includes a cylindrical portion and a wall positioned radially relative to the cylindrical portion, and the mating mold includes two portions that are mobile relative to one another and that are moved toward the axis of the cylindrical portion and towards the radial wall of the substrate, respectively. The method can be used for example for manufacturing a fan casing of a turbojet engine.

Claims (10)

1. A method for manufacturing an article made of composite material formed with a polymer matrix reinforced by a fibrous structure, comprising:

positioning the fibrous structure on a support forming a molding surface, the support including a cylindrical portion and a radially extending wall;

placing a first counter mold element on top of the fibrous structure, the first counter mold element having a first wall which is disposed opposite to the radially extending wall of the support, a second wall disposed opposite to the cylindrical portion of the support and adjacent to the radially extending wall of the support, and a third wall connecting the first and second walls of the first counter mold element;

covering the fibrous structure and the first counter mold element with a second counter mold element, the second counter mold element including a central part facing the cylindrical portion of the support and an angular surface;

compacting the fibrous structure through bringing the second counter mold element towards the support such that the angular surface of the second counter mold element abuts the third wall of the first counter mold element such that the first wall of the first counter mold element applies an axial stress to a portion of the fibrous structure abutting the radially extending wall of the support; and

injecting the polymer matrix in the fibrous structure, the first and second counter mold elements move relative to each other during the compacting, the second counter mold element moving towards an axis of the cylindrical portion, and the angular surface of the second counter mold element being arranged with the third wall of the first counter mold element so that when the second counter mold element moves towards the axis of the cylindrical portion, the first counter mold element moves towards the radially extending wall of the support.

2. A method according to claim 1 , wherein the first counter mold element includes a rounded section between the first and second walls.

3. A method according to claim 1 , wherein the article is a turbo-machine casing.

4. A method according to claim 1 , wherein the second wall of the first counter mold element is cylindrical and perpendicular to the first wall, and the third wall of the first counter mold element is frustoconical.

5. A method according to claim 1 , wherein the central part of the second counter mold element presents a shape complementary to the cylindrical portion of the support, and the angular surface of the second counter mold element presents a shape complementary with the third wall of the first counter mold element.

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 Dec 17, 2012
From: GUMMEL, MICAH; MARCHAL, YANN; PHELIPPEAU, ANTOINE
To: SNECMA
Reel/Frame 029480/0454 →