Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure

Patent metadata

Field	Value
Publication number	US-9719422-B2
Application number	US-201213527100-A
Country	US
Kind code	B2
Filing date	Jun 19, 2012
Priority date	Jun 20, 2011
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A process for the production of an acoustic treatment panel that includes an acoustically resistive layer ( 24 ), at least one alveolar structure ( 26 ), and a reflective layer ( 28 ), as well as at least one channel that is bordered at least in part by a wall ( 32 ) that is secant with at least one wall of a cell of the alveolar structure ( 26 ), includes elevating the temperature of the wall ( 32 ) and the ends of the cells of the alveolar structure ( 26 ) and injecting a pressurized gas into the channel ( 30 ) so as to expand the wall ( 32 ) of the channel so as to flatten it against the ends of the cells of the alveolar structure ( 26 ) in such a way as to produce a weld by continuous diffusion between the ends of the walls of the cells of the alveolar structure ( 26 ) and the wall ( 32 ) of the channel ( 30 ).

First claim

The invention claimed is:

1. A process for the production of an acoustic treatment panel having an acoustically resistive first layer, at least one multi-celled alveolar structure, and a reflective second layer, comprising the steps of:
providing a layer of material and shaping the layer of material so as to produce, at one surface of the layer of material, hollow shapes that form furrows in the layer of material;
flattening the layer of material with the furrows so as to make the layer of material integral with an inside surface of the acoustically resistive first layer so that the furrows and the inside surface of the acoustically resistive first layer form channels;
removing a portion of the layer of material, where the portion runs between each of the channels in a thickness direction;
cutting out at least one surface of the alveolar structure to yield at least one cut-out in the alveolar structure having an undercut shape configured to accommodate at least one of the channels;
providing the alveolar structure over the layer of material such that the at least one of the channels is received within the at least one cut-out of the alveolar structure;
providing the reflective second layer over the alveolar structure;
elevating a temperature of a wall of the at least one of the channels and ends of cells of the alveolar structure to achieve diffusion welding of the wall and the ends of the cells, the wall of the at least one of the channels being secant with at least one wall of a cell of the alveolar structure; and
injecting a pressurized gas into the at least one of the channels so as to expand the wall of the at least one of the channels that is secant with the at least one wall of a cell of the alveolar structure, and thereby flatten the wall of the at least one of the channels that is secant with the at least one wall of the cell of the alveolar structure against ends of walls of the cells of the alveolar structure so that a continuous weld by continuous diffusion is produced between the ends of the walls of the cells of the alveolar structure and the wall of the channel that is secant with the at least one wall of the cell of the alveolar structure.

2. The process according to claim 1 , further comprising:
causing the wall of the at least one of the channels that is secant with the at least one wall of the cell of the alveolar structure to undergo superplastic hot-shaping.

3. The process according to claim 2 , wherein the layer of material forming the channels is made of a titanium alloy.

4. The process according to claim 1 , wherein, the removing of the portion of the layer of the layer of material forming the channels forms, for each channel, two lugs extending opposite one another on either side of the channel, the lugs resting on the inside surface of the acoustically resistive first layer and extending in a direction that is essentially parallel to the acoustically resistive first layer.

5. The process according to claim 4 , wherein each of the lugs have a length of between 2 and 10 mm.

6. The process according to claim 1 , wherein the portion of the layer of material is removed between the channels by water jet.

7. The process according to claim 1 , wherein an entirety of the layer of material running between each of the channels in the thickness direction is removed.

8. A process for the production of an acoustic treatment panel, comprising the steps of:
providing an acoustically resistive first layer formed from a porous layer and a structural layer;
providing a layer of material, and shaping the layer of material so as to produce at one surface of the layer of material hollow shapes that form furrows on the one surface of the layer of material;
flattening the layer of material with the furrows so as to be made integral with an inside surface of the acoustically resistive first layer so that the furrows and the inside surface of the acoustically resistive first layer form channels;
removing a portion of the layer of material running between the channels in the thickness direction;
providing, over the inside surface of the acoustically resistive first layer, a multi-celled alveolar structure formed from a plurality of pipes;
providing a reflective second layer over the alveolar structure;
cutting out at least one surface of the alveolar structure to yield a cut-out having an undercut shape configured to accommodate at least one of the channels;
diffusion welding by elevating a temperature of the wall of the at least one of the channels and ends of cells of the alveolar structure; and
injecting a pressurized gas into the at least one of the channels so as to expand a wall of the at least one of the channels, the pressurized gas flattening the wall of the at least one channel against the ends of the cells of the alveolar structure in such a way as to produce a continuous weld by continuous diffusion between the ends of second walls of the cells of the alveolar structure and the wall of the at least one of the channels, the wall of the at least one of the channels being secant with at least one wall of a cell of the alveolar structure.

9. The process according to claim 8 , further comprising:
causing the wall of the at least one of the channels to undergo superplastic hot-shaping.

10. The process according to claim 8 , wherein layer of material forming the channels is made of a titanium alloy.

11. The process according to claim 7 , wherein a portion of the acoustically resistive first layer between the channels in the thickness direction is removed.

Assignees

• Porte Alain
• Chelin Frederic
• Airbus Operations Sas

Inventors

• Porte Alain
• Chelin Frederic

Classifications

• B21D47/00

  Making rigid structural elements or units, e.g. honeycomb structures · CPC title

• F05D2250/283

  honeycomb · CPC title

• B64D2033/0206

  comprising noise reduction means, e.g. acoustic liners · CPC title

• F02C7/045 Primary

  having provisions for noise suppression · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic