Composite material reinforcing part of pi-shaped section, in particular a platform for a turbine engine fan, and its method of fabrication

Patent metadata

Field	Value
Publication number	US-9657583-B2
Application number	US-201314371280-A
Country	US
Kind code	B2
Filing date	Jan 7, 2013
Priority date	Jan 9, 2012
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A reinforcing part of π-shaped section made out of composite material, and a method of making the part, the method including: making a first set of layers of interlinked yarns by three-dimensional weaving to form a first fiber blank portion to form a base preform; making a second set of layers of interlinked yarns by three-dimensional weaving to form a second fiber blank portion to form a stiffener preform, yarns of the second set being interlinked with yarns of the first set by weaving over a central interlinked strip that flares towards side edges of the first fiber blank portion in a zone corresponding to the step of the base; shaping the two fiber blank portions to obtain a single-piece fiber preform having a portion forming a base preform and a portion forming a stiffener preform; and depositing a resin in the fiber preform to form a matrix.

First claim

The invention claimed is:

1. A method of fabricating a reinforcing part of π-shaped section out of composite material, the part including a first portion forming a base that presents a step at at least one of its longitudinal ends, and a second portion forming a stiffener including two legs that extend from a face of the base over at least a fraction of the length thereof, the method comprising:
making a first set of a plurality of layers of yarns that are interlinked by three-dimensional weaving to form a first fiber blank portion that is to form a base preform;
making a second set of a plurality of layers of yarns that are interlinked by three-dimensional weaving to form a second fiber blank portion that is to form a stiffener preform, yarns of the second set of layers of yarns being interlinked by weaving with the yarns of the first set of layers of yarns in a central interlinked strip extending longitudinally between the two longitudinal ends of the first fiber blank portion and flaring towards side edges thereof in a zone corresponding to a step of the base;
shaping the two fiber blank portions to obtain a single-piece fiber preform having a portion forming a base preform and a portion forming a stiffener preform; and
depositing a resin in the fiber preform to form a matrix to obtain a composite material reinforcing part comprising fiber reinforcement constituted by the preform that is densified by the matrix.

2. A method according to claim 1 , wherein the interlinking of the yarns of the second set of layers of yarns and the yarns of the first set of layers of yarns by weaving is obtained by crossing said yarns respectively along the interlinked strip.

3. A method according to claim 1 , wherein when the base of the reinforcing part presents a step at both of its longitudinal ends, the interlinked strip between the yarns of the first and second sets of layers of yarns flares toward the side edges of the first fiber blank portion in each of the zones corresponding to the steps of the base.

4. A method according to claim 3 , wherein, upstream from the zone corresponding to the upstream step of the base and downstream from the zone corresponding to the downstream step of the base, the interlinked strip between the yarns of the first and second sets of layers of yarns extends transversely over an entire width of the first fiber blank portion.

5. A method according to claim 1 , wherein the shaping comprises forming at least one step by folding the two fiber blank portions along a common, substantially-transverse fold line.

6. A method according to claim 1 , wherein the shaping of the second fiber blank portion comprises folding the non-interlinked portions of the second fiber blank portion in a direction that is substantially perpendicular to the first fiber blank portion to form two leg preforms.

7. A reinforcing part of π-shaped section made of composite material, comprising:
a base-forming first portion that presents a step at at least one of its longitudinal ends; and
a stiffener-forming second portion including two legs that extend from a face of the base over at least a fraction of a length thereof,
wherein the first and second portions are interlinked along a central interlinked strip that extends longitudinally between the two longitudinal ends of the first portion and that flares towards side edges thereof in a zone corresponding to the step of the base.

8. A reinforcing part according to claim 7 , made of organic matrix composite material.

9. A reinforcing part according to claim 7 , wherein the first and second portions are interlinked by respective crossings of the yarns that constitute them in the interlinked strip.

10. A reinforcing part according to claim 7 , wherein downstream from the zone of the first portion corresponding to the step of the base, the interlinked strip between the first and second portions extends transversely over an entire width of said first portion.

11. A reinforcing part according to claim 7 , wherein the first portion includes a step at each of its longitudinal ends.

12. A reinforcing part according to claim 7 , constituting a fan platform of a turbine engine.

13. A turbine engine comprising at least one fan platform according to claim 12 .

Assignees

• Snecma

Inventors

• Marchal Yann
• Mahieu Jean-Noel

Classifications

• B29B11/16

  comprising fillers or reinforcement {(non-woven fabrics per se D04H1/00, D04H3/00)} · CPC title

• B29C70/24 Primary

  oriented in at least three directions forming a three-dimensional [3D] structure · CPC title

• B29C70/682

  Preformed parts characterised by their structure, e.g. form · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title

• F05D2300/44

  Resins · CPC title