Transmission loss panel for aircraft cabin noise and thermal treatment

Patent metadata

Field	Value
Publication number	US-2024262488-A1
Application number	US-202418416094-A
Country	US
Kind code	A1
Filing date	Jan 18, 2024
Priority date	Feb 8, 2023
Publication date	Aug 8, 2024
Grant date	—

Abstract

A vehicle panel includes two sidewalls and a resonator disposed between them on one of the cell walls. The resonator includes a network of cells, each cell defines an internal space to absorb and dissipate noise and vibrations within a specific frequency range. Certain cells or subsets of cells may be interconnected to define a larger internal cell space. An airgap between the resonator and one of the sidewalls may be partially or completely filled with dampening material to absorb high frequency noise. The dampening material may also provide thermal insulation.

First claim

What is claimed is:

1 . A panel resonator comprising:
a plurality of regularly spaced cells, each cell defining an internal space, the plurality of regularly spaced cells configured to at least partially define an airgap between a first sidewall of a panel and the resonator, wherein the regularly spaced cells are configured to be disposed on an internal surface of a second sidewall of the panel.

2 . The panel resonator of claim 1 , wherein at least one of the regularly spaced cells defines an opening to allow air movement from the internal space.

3 . The panel resonator of claim 2 , wherein:
the opening comprises a hole having a first diameter; at least one of the regularly spaced cells defines a hole having a second diameter different from the first diameter; and the first diameter and the second diameter are tuned for specific, different frequency ranges.

4 . The panel resonator of claim 1 , wherein at least two of the regularly spaced cells are in fluid communication with each other.

5 . The panel resonator of claim 4 , wherein one of the at least two regularly spaced cells defines an opening to allow air movement from the internal space.

6 . The panel resonator of claim 1 , further comprising a membrane layer configured to surround top portion of each of the regularly spaced cells to define a second internal space.

7 . An aircraft panel comprising:
a first sidewall; a second sidewall; and a resonator disposed between the first sidewall and second sidewall, the resonator comprising a plurality of regularly spaced cells, each cell defining an internal space, wherein:
the resonator is disposed on the second sidewall and at least partially define an airgap between the first sidewall and the resonator.

8 . The aircraft panel of claim 7 , wherein at least one of the regularly spaced cells defines an opening to allow air movement from the internal space.

9 . The aircraft panel of claim 8 , wherein:
the opening comprises a hole having a first diameter; at least one of the regularly spaced cells defines a hole having a second diameter different from the first diameter; and the first diameter and the second diameter are tuned for specific, different frequency ranges.

10 . The aircraft panel of claim 7 , wherein at least two of the regularly spaced cells are in fluid communication with each other.

11 . The aircraft panel of claim 7 , further comprising a filler material at least partially filling the airgap.

12 . The aircraft panel of claim 11 , wherein the filler material is configured to a frequency range of vibrations.

13 . The aircraft panel of claim 7 , wherein the filler material is configured as a thermal insulator.

14 . A mobile platform comprising:
a plurality of panels, each comprising:
a first sidewall;
a second sidewall; and
a resonator disposed between the first sidewall and second sidewall, the resonator comprising a plurality of regularly spaced cells, each cell defining an internal space,
wherein:
the resonator is disposed on the second sidewall and at least partially defines an airgap between the first sidewall and the resonator.

15 . The mobile platform of claim 14 , wherein at least one of the regularly spaced cells defines an opening to allow air movement from the internal space.

16 . The mobile platform of claim 15 , wherein:
the opening comprises a hole having a first diameter; at least one of the regularly spaced cells defines a hole having a second diameter different from the first diameter; and the first diameter and the second diameter are tuned for specific, different frequency ranges.

17 . The mobile platform of claim 14 , wherein at least two of the regularly spaced cells are in fluid communication with each other.

18 . The mobile platform of claim 14 , further comprising a filler material at least partially filling the airgap, configured to a frequency range of vibrations.

19 . The mobile platform of claim 18 , wherein the filler material is configured as a thermal insulator.

20 . The mobile platform of claim 14 , wherein the first sidewall, second sidewall, and resonator are curved to conform to a portion of the mobile platform.

Assignees

• Be Aerospace Inc

Inventors

• Winkler Julian
• St Rock Brian E
• Dempah Maxime
• Martz Thomas
• Pearson Matthew R

Classifications

• B64C1/066

  Interior liners · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B2307/304

  Insulating · CPC title

• B32B2307/102

  Insulating · CPC title