Acoustic attenuation structure made of composite material and method for manufacturing same

Patent metadata

Field	Value
Publication number	US-11959440-B2
Application number	US-202017631281-A
Country	US
Kind code	B2
Filing date	Aug 12, 2020
Priority date	Aug 22, 2019
Publication date	Apr 16, 2024
Grant date	Apr 16, 2024

Abstract

An annular or semi-annular acoustic attenuation structure includes an inner skin and an outer skin, defining between them an annular or semi-annular volume, and a plurality of partitions extending in the space in a radial direction perpendicular to the inner and outer skins and in a circumferential direction. The inner and outer skins and the partitions are made of composite material including a fibrous reinforcement densified by a matrix. The fibrous reinforcement of each partition includes yarns or fibers extending into the fibrous reinforcement of at least one of the inner or outer skins.

First claim

The invention claimed is:

1. Annular or semi-annular acoustic attenuation structure comprising an inner skin and an outer skin, defining between them an annular or semi-annular volume, and a plurality of partitions extending in a space in a radial direction perpendicular to the inner and outer skins and in a circumferential direction of the annular or semi-annular acoustic attenuation structure to define a plurality of adjacent chambers that extends along the circumferential direction, the inner and outer skins and the plurality of partitions being made of composite material comprising a fibrous reinforcement densified by a matrix, the fibrous reinforcement of the inner skin or the outer skin includes at least one fibrous layer extending over a length of the annular or semi-annular acoustic attenuation structure, wherein the fibrous reinforcement of each partition is formed with a first portion of one or several fibrous layers extending in the radial direction and in the circumferential direction, a second and remaining portion of said one or several fibrous layers of each partition extending in an axial direction from said first portion to substantially a first portion of another one or several fibrous layers of another partition that is adjacent said partition, wherein three adjacent partitions of the plurality of partitions extending in the radial direction and that define two adjacent chambers of the plurality of adjacent chambers are formed with, respectively, the first portions of three different ones of the one or several fibrous layers such that each partition of the three adjacent partitions is separately formed, wherein, for each partition, the second and remaining portion of said one or several fibrous layers extending in the axial direction is layered on said at least one fibrous layer of the fibrous reinforcement of only one of the inner skin and the outer skin,
wherein the second and remaining portions of two adjacent partitions of the plurality of partitions extend in said axial direction without being woven to each other,
wherein the first portions of said three different one or several fibrous layers extend in the radial direction without being woven to each other.

2. The annular or semi-annular acoustic attenuation structure according to claim 1 , wherein the outer skin includes a plurality of perforations.

3. Jet cone of an aero-engine comprising an annular or semi-annular acoustic attenuation structure according to claim 2 .

4. Gas-turbine aero-engine comprising a jet cone according to claim 3 .

5. Aircraft comprising at least one gas-turbine aero-engine according to claim 4 .

6. The annular or semi-annular acoustic attenuation structure according to claim 1 , wherein the inner skin includes a plurality of perforations.

7. Jet nozzle of an aero-engine comprising an annular or semi-annular acoustic attenuation structure according to claim 6 .

8. Gas-turbine aero-engine comprising a jet nozzle according to claim 7 .

9. Aircraft comprising at least one gas-turbine aero-engine according to claim 8 .

10. Method for producing an annular or semi-annular acoustic attenuation structure made of composite material, according to claim 1 , comprising:
producing an acoustic attenuation structure fibrous preform comprising a first part intended to form the inner skin, a second part intended to form the outer skin and a third part intended to form the partitions, and
densifying the fibrous preform by the matrix,
wherein the first part or the second part of the acoustic attenuation structure fibrous preform includes the at least one fibrous layer extending over the length of the acoustic attenuation structure and wherein the third part of the acoustic attenuation structure fibrous preform is formed with the first portion of said one or several fibrous layers extending in the radial direction, the second portion of said one or several fibrous layers extending in the axial direction layered on said first part or second part of the acoustic attenuation structure.

11. The method according to claim 10 , wherein the acoustic attenuation structure fibrous preform is at least partially produced by placing of fibers.

12. The method according to claim 10 , wherein the third part of the acoustic attenuation structure fibrous preform comprises one or more laminations of unidirectional or two-dimensional fabric, each lamination extending at least partially into the first part or the second part of the acoustic attenuation structure fibrous preform.

Assignees

• Safran Ceram

Inventors

• Bouillon Eric
• Conete Eric

Classifications

• F02K1/827 Primary

  Sound absorbing structures or liners · CPC title

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2230/21

  by casting · CPC title

• F05D2240/128

  Nozzles · CPC title