Woven fibrous structure for forming a casing preform

US11230798B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11230798-B2
Application numberUS-201816642767-A
CountryUS
Kind codeB2
Filing dateAug 29, 2018
Priority dateAug 30, 2017
Publication dateJan 25, 2022
Grant dateJan 25, 2022

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A fibrous structure having the form of a band extending in a longitudinal direction (X) over a given length between a proximal part and a distal part and in a lateral direction (Y) over a given width between a first side edge and a second side edge, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns or strands extending longitudinally and a plurality of layers of weft yarns or strands extending laterally, wherein a first portion of the fibrous structure present between the proximal part and an intermediate part of the fibrous structure includes carbon fiber weft yarns or strands and wherein a second portion of the fibrous structure present between the intermediate part and the distal part includes glass fiber weft yarns or strands.

First claim

Opening claim text (preview).

The invention claimed is: 1. A fibrous structure having the form of a band extending in a longitudinal direction over a given length between a proximal part and a distal part and in a lateral direction over a given width between a first side edge and a second side edge, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns or strands extending longitudinally and a plurality of layers of weft yarns or strands extending laterally, wherein a first rigid portion of the fibrous structure present between the proximal part and an intermediate part of the fibrous structure comprises carbon fiber weft yarns or strands and in that a second elastically deformable portion of the fibrous structure present between the intermediate part and the distal part comprises glass fiber weft yarns or strands. 2. The fibrous structure as claimed in claim 1 , wherein the glass fiber weft yarns or strands in the second portion are present on the side of an outer face of the structure. 3. The fibrous structure as claimed in claim 1 , wherein only a portion of the weft yarns or strands of the second portion are made of glass fibers, the other weft yarns or strands of the second portion being made of carbon fibers. 4. The fibrous structure as claimed in claim 1 , further comprising glass fiber warp yarns or strands present on the side of an outer face of the structure, the other warp yarns or strands of the fibrous structure being of carbon fibers. 5. The fibrous structure as claimed in claim 4 , wherein the glass fiber warp yarns or strands are present in a central zone laterally set back from the first and second side edges and which extends over a given width which is less than the width of said fibrous structure. 6. The fibrous structure as claimed in claim 1 , wherein the carbon fiber yarns or strands and the glass fiber yarns or strands present in the fibrous structure have a similar titer. 7. A fibrous preform for an aircraft casing comprising a winding over a plurality of turns of a fibrous structure as claimed in claim 1 , the first portion being located on the side of a radially inner face of the preform, and the second portion being located on the side of a radially outer face of the preform. 8. A gas turbine engine casing of a composite material, comprising a fibrous reinforcement consisting of a fibrous preform as claimed in claim 7 , and a matrix densifying the fibrous reinforcement. 9. The casing as claimed in claim 8 , wherein said casing is a gas turbine fan casing. 10. An aircraft gas turbine engine having a casing as claimed in claim 8 .

Assignees

Inventors

Classifications

  • Processes for the fixation or treatment of textile materials in three-dimensional [3D] forms · CPC title

  • Double or multi-ply fabrics not otherwise provided for · CPC title

  • D03D1/0052Primary

    Antiballistic fabrics · CPC title

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

  • D03D25/005Primary

    Three-dimensional woven fabrics · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11230798B2 cover?
A fibrous structure having the form of a band extending in a longitudinal direction (X) over a given length between a proximal part and a distal part and in a lateral direction (Y) over a given width between a first side edge and a second side edge, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns or strands extending longitudinall…
Who is the assignee on this patent?
Safran Aircraft Engines
What technology area does this patent fall under?
Primary CPC classification D03D1/0052. Mapped technology areas include Textiles & Paper.
When was this patent published?
Publication date Tue Jan 25 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).