SOUND ATTENUATION PANEL FOR AIRCRAFT HAVING A COMBINATION OF ACOUSTIC ATTENUATION PROPERTIES

• US 20190309682A1
• Filed: 04/09/2019
• Published: 10/10/2019
• Est. Priority Date: 04/10/2018
• Status: Active Grant

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: PORTE, Alain, LALANE, Jacques, CARAZO MENDEZ, Arnulfo
• Granted Patent: US 11,459,950 B2
• Time in Patent Office: Days
• CPC Class Codes: B64D 2033/0206 comprising noise reduction means, e.g. acoustic liners
• CPC Class Codes: B64D 33/02 of combustion air intakes air intakes for gas-turbine plants or jet-propulsion plants per se F02C7/04; air intakes for combustion engines in general F02M35/00
• CPC Class Codes: F02C 7/045 having provisions for noise suppression
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise

Abstract

Sound attenuation panel for aircraft having a combination of acoustic attenuation properties. The acoustic panel includes an acoustic structure having a cellular structure and a resistive skin and a backing skin, the acoustic panel also including at least one auxiliary acoustic device with cavities that is configured to produce additional acoustic absorption, the auxiliary acoustic device with cavities being attached to the acoustic structure and including adjacent chambers or cavities separated by shared walls, each of the chambers or cavities having perforations and being adapted to produce acoustic absorption. The combination of the acoustic structure and the auxiliary acoustic device with cavities enables combination of the acoustic absorption properties of these two types of element and an increased range of frequencies of the noise that can be attenuated by the acoustic panel without increasing its overall size.

Claims

1. An acoustic panel for aircraft, the acoustic panel comprising an acoustic structure having a cellular structure and a resistive skin and a backing skin on respective opposite sides of the cellular structure, the acoustic panel comprising at least one auxiliary acoustic device with cavities configured to produce acoustic absorption, the auxiliary acoustic device with cavities being attached to the acoustic structure, the auxiliary acoustic device with cavities comprising a plurality of adjacent chambers separated by shared walls, each of the chambers having perforations and configured to produce acoustic absorption,

wherein the auxiliary acoustic device with cavities is on a peripheral edge of the acoustic structure where the acoustic panel comprises an edge part for fixing the acoustic panel and wherein the perforations are on a front face of the auxiliary acoustic device with cavities.

2. The acoustic panel of claim 1, wherein the acoustic structure and the auxiliary acoustic device with cavities form a one-piece part.

3. The acoustic panel of claim 2, wherein the auxiliary acoustic device with cavities has a first face that corresponds to an extension of the resistive skin, walls of at least some of the chambers forming part of the first face.

4. The acoustic panel of claim 2, wherein the auxiliary acoustic device with cavities has a second face that corresponds to an extension of the backing skin, the walls of at least some of the chambers forming part of the second face.

5. The acoustic panel of claim 1, wherein the auxiliary acoustic device is fixed to the acoustic structure.

6. The acoustic panel of claim 5, wherein the auxiliary acoustic device with cavities has a front face, the front face having at least a first part with perforations and a second part with no perforations, and wherein the resistive skin of the acoustic structure is fixed to the second part of the front face.

7. The acoustic panel of claim 5, wherein the auxiliary acoustic device with cavities has a rear face that is fixed to the backing skin of the acoustic structure in an aligned or non-aligned manner.

8. The acoustic panel of claim 1, wherein the at least one auxiliary acoustic device with cavities is at least on part of at least one peripheral edge of the acoustic structure.

9. The acoustic panel of claim 8, comprising at least two auxiliary acoustic devices on at least two peripheral edges of the acoustic structure or on at least two sections of a peripheral edge of the acoustic structure.

10. The acoustic panel of claim 1, wherein the auxiliary acoustic device has at least one perforated face with perforations and the perforated face is on a same side of the acoustic panel as the resistive skin.

11. The acoustic panel of claim 1, wherein the auxiliary acoustic device comprises chambers of identical volume.

12. The acoustic panel of claim 1, wherein the auxiliary acoustic device comprises chambers of different types.

13. The acoustic panel of claim 12, wherein, for each chamber of the auxiliary acoustic device, at least a volume of the chamber and an area of the perforations of the chamber are adapted to confer on the chamber preferential acoustic absorption in at least one given range of acoustic frequencies.

14. The acoustic panel of claim 1, wherein the perforations have surfaces of a shape included in a circle having a diameter between 0.1 and 1.2 millimeters inclusive.

15. A method of manufacturing an acoustic panel, comprising a plurality of steps including at least one curing step and comprising:

manufacturing an acoustic panel for aircraft, the acoustic panel comprising;

an acoustic structure having a cellular structure and a resistive skin and a backing skin on respective opposite sides of the cellular structure, the acoustic panel comprising at least one auxiliary acoustic device with cavities configured to produce acoustic absorption, the auxiliary acoustic device with cavities being attached to the acoustic structure, the auxiliary acoustic device with cavities comprising a plurality of adjacent chambers separated by shared walls, each of the chambers having perforations and configured to produce acoustic absorption,

wherein the auxiliary acoustic device with cavities is on a peripheral edge of the acoustic structure where the acoustic panel comprises an edge part for fixing the acoustic panel and wherein the perforations are on a front face of the auxiliary acoustic device with cavities.

16. The method of claim 15, wherein the plurality of steps comprises at least:

forming a one-piece assembly comprising the acoustic structure having the cellular structure and the resistive and backing skins and one or more auxiliary acoustic devices; and

curing the one-piece assembly to manufacture a one-piece part.

17. The method of claim 15, wherein the plurality of steps comprises at least:

manufacturing the acoustic structure having the cellular structure and the resistive and backing skins;

manufacturing one or more auxiliary acoustic devices, including curing; and

fixing the auxiliary acoustic device or devices to the acoustic structure.