Honeycomb acoustic liner

Patent metadata

Field	Value
Publication number	US-9567087-B1
Application number	US-201514971480-A
Country	US
Kind code	B1
Filing date	Dec 16, 2015
Priority date	Dec 16, 2015
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

Abstract

An acoustic liner for a duct of an air conditioning and temperature control system including a honeycomb structure having a thickness of about 0.375±0.006 inches (0.953±0.015 centimeters). The acoustic liner is configured to cover an outer surface of a cylinder having a length of about 30 inches (76 centimeters) and an outer diameter of about 8.30 inches (21.1 centimeters).

First claim

What is claimed is:

1. An aircraft cabin supply duct of an air conditioning and temperature control system, comprising:
a first tubular body having an inlet, an outlet, an inner surface, an outer surface, a longitudinal axis, an inner shell surface located between the inner surface and outer surface at distance of about 0.375±0.006 inches (0.953±0.015 centimeters) away from the inner surface, and an acoustic liner located between the inner surface and the inner shell surface of the first tubular body; and
a second tubular body having an inlet, an outlet, an inner surface, an outer surface, and a longitudinal axis, the inner surface of the second tubular body being fluidly connected to the inner surface of the first tubular body at the outlet of the second tubular body, the longitudinal axis of the first tubular body being perpendicular to the longitudinal axis of the second tubular body.

2. The aircraft cabin supply duct according to claim 1 , wherein:
the acoustic liner has a thickness of about 0.375±0.006 inches (0.953±0.015 centimeters).

3. The aircraft cabin supply duct according to claim 2 , wherein:
the acoustic liner is composed of a honeycomb structure.

4. The aircraft cabin supply duct according to claim 3 , wherein:
the acoustic liner is composed of at least one of a fibrous aramid material and a composite material.

5. The aircraft cabin supply duct according to claim 4 , wherein:
the acoustic liner is configured to cover an outer surface of a cylinder having a length of about 30 inches (76 centimeters) and an outer diameter of about 8.30 inches (21.1 centimeters).

6. The aircraft cabin supply duct according to claim 5 , wherein:
the acoustic liner contains at least one through hole configured to fit a cylinder with a diameter of about 8 inches (20 centimeters).

7. The aircraft cabin supply duct according to claim 6 , wherein:
the acoustic liner is composed of at least 2 separate pieces.

8. The aircraft cabin supply duct according to claim 7 , wherein:
the core density of the honeycomb structure is about 3.0 lb/ft 3 (0.048 g/cm 3 ).

9. The aircraft cabin supply duct according to claim 8 , wherein:
the honeycomb structure is composed of a plurality of over-expanded hexagonal cells.

10. The aircraft cabin supply duct according to claim 9 , wherein:
the hexagonal cells have a nominal size of about 3/16 inches (0.47625 centimeters).

11. The aircraft cabin supply duct according to claim 10 , wherein:
the inner surface of the first tubular body is composed of a stainless steel felt liner.

12. The aircraft cabin supply duct according to claim 11 , wherein:
the inner shell surface of the first tubular body is composed of aluminum.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Monacchio John D
• Smith Blair A
• Folsom Michael E
• Simpson Christopher
• Lokhandwalla Murtuza

Classifications

• B64F1/362

  Installations for supplying conditioned air to parked aircraft · CPC title

• B64D13/00 Primary

  Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space · CPC title

• F24F13/0263 Primary

  Insulation for air ducts · CPC title

• F24F13/24

  Means for preventing or suppressing noise · CPC title

• F24F2013/242

  Sound-absorbing material · CPC title