Enclosure for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10971127-B2
Application number	US-201815925921-A
Country	US
Kind code	B2
Filing date	Mar 20, 2018
Priority date	Mar 20, 2018
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

Abstract

An engine enclosure for containing a gas turbine engine is provided. An exemplary engine enclosure includes features that improve noise and thermal attenuation, reduce the weight of the enclosure, and provide for more accessible access points to the interior volume of the engine enclosure.

First claim

What is claimed is:

1. An enclosure for containing at least a portion of a gas turbine engine, the enclosure comprising:
at least one wall defining at least a portion of an interior volume of the enclosure, the wall of the enclosure comprising:
a first insulation panel;
a sound absorption member positioned outwardly of the first insulation panel with respect to the interior volume;
an acoustic barrier positioned adjacent to and outwardly of the sound absorption member with respect to the interior volume;
an outer shell positioned outwardly of the acoustic barrier with respect to the interior volume, wherein the outer shell is formed as a monolithic unitary composite component from a composite material, the outer shell coupling the at least one wall.

2. The enclosure of claim 1 , wherein the sound absorption member is a first sound absorption member and the acoustic barrier is a first acoustic barrier, and wherein the wall of the enclosure further comprises:
a second sound absorption member positioned outwardly of the first acoustic barrier with respect to the interior volume; and
a second acoustic barrier positioned adjacent to and outwardly of the second sound absorption member with respect to the interior volume.

3. The enclosure of claim 2 , wherein the wall of the enclosure further comprises:
a third sound absorption member positioned outwardly of the second acoustic barrier with respect to the interior volume; and
a third acoustic barrier positioned adjacent to and outwardly of the third sound absorption member with respect to the interior volume.

4. The enclosure of claim 3 , wherein the third acoustic barrier is positioned adjacent to and inwardly of the outer shell.

5. The enclosure of claim 1 , further comprising:
a second insulation panel positioned between the first insulation panel and the sound absorption member.

6. The enclosure of claim 5 , wherein the second insulation panel is positioned adjacent to the first insulation panel.

7. The enclosure of claim 1 , wherein the acoustic barrier is a vinyl mat.

8. The enclosure of claim 1 , further comprising:
a perforated sheet positioned adjacent to and inwardly of the first insulation panel.

9. The enclosure of claim 8 , wherein the perforated sheet is formed of a Polyethylene Terephthalate material.

10. The enclosure of claim 1 , wherein the sound absorption member is formed of mineral wool.

11. The enclosure of claim 1 , wherein the composite material of the outer shell is a carbon fiber reinforced phenolic composite material.

12. The enclosure of claim 1 , wherein the wall has a thickness that is less than or equal to about four (4) inches.

13. An enclosure for containing at least a portion of a gas turbine engine, the enclosure comprising:
a plurality of walls defining an interior volume, a monolithic outer shell coupling adjacent walls and forming at least a portion of each of the walls, the monolithic outer shell formed of a composite material, at least one of the walls comprising:
a first insulation panel;
a sound absorption member positioned outwardly of the first insulation panel with respect to the interior volume; and
an acoustic barrier positioned adjacent to and outwardly of the sound absorption member with respect to the interior volume;
wherein the outer shell is positioned outwardly of the acoustic barrier with respect to the interior volume.

14. The enclosure of claim 13 , wherein the enclosure further comprises:
a roof coupled with one or more of the plurality of walls by the monolithic outer shell, and wherein the outer shell forms at least a portion of the roof.

15. The enclosure of claim 13 , wherein the enclosure further comprises:
a floor coupled with one or more of the plurality of walls by the monolithic outer shell, and wherein the outer shell forms at least a portion of the floor.

16. The enclosure of claim 13 , further comprising:
an access point for selectively accessing the interior volume of the enclosure, the access point comprising:
a perforated sheet;
an insulation panel positioned outwardly of the perforated sheet with respect to the interior volume;
an epoxy layer positioned outwardly of the insulation panel along at least a part of the access point with respect to the interior volume;
at least one acoustic panel positioned outwardly of the epoxy layer with respect to the interior volume; and
an outer shell positioned outwardly of the acoustic panel with respect to the interior volume.

17. An enclosure for containing at least a portion of a gas turbine engine, the enclosure comprising:
at least one wall defining at least a portion of an interior volume of the enclosure, the wall of the enclosure comprising:
a first insulation panel;
an acoustic panel positioned outwardly of the first insulation panel with respect to the interior volume, the first acoustic panel comprising a sound absorption member and an acoustic barrier;
an outer shell formed of a composite material and positioned outwardly of the acoustic panel with respect to the interior volume; and
a hat stiffener, comprising:
a hat member defining a stiffener volume, the hat member comprising a first flange attached to the outer shell, a hat portion extending inwardly from the outer shell, and a second flange attached to the outer shell; and
a foam member disposed within the stiffener volume.

18. The enclosure of claim 17 , wherein the hat member further comprises:
an inner member;
an outer member positioned outwardly of the inner member with respect to the interior volume, the inner and outer members of the hat member positioned at an inner portion of the hat member, wherein the inner member and the outer member define an inner volume; and
a stiffening member disposed within the inner volume.

19. The enclosure of claim 17 , wherein the acoustic panel is a first acoustic panel and the sound absorption member is a first sound absorption member and the acoustic barrier is a first acoustic barrier, and wherein the first acoustic barrier is positioned outwardly of the first sound absorption member with respect to the interior volume, and wherein the wall of the enclosure further comprises:
a second acoustic panel positioned outwardly of the first acoustic panel with respect to the interior volume, the second acoustic panel comprising a second sound absorption member and a second acoustic barrier; and
a third acoustic panel positioned outwardly of the second acoustic panel with respect to the interior volume, the third acoustic panel comprising a third sound absorption member and a third acoustic barrier;
wherein the hat portion extends inwardly from the outer shell to an inner surface of the first sound absorption member.

20. The enclosure of claim 19 , wherein the first flange is disposed between the third acoustic barrier and the outer shell and the second flange is disposed between the third acoustic barrier and the outer shell.

Assignees

• Gen Electric

Inventors

• Johnson Randy Ray
• Linnemann Steven Robert
• Long Loren Lee
• Linnemann Brian Macdonald
• Rao Justin Sanjay
• Wunsch John Joseph
• Spirk Andrew William
• Young Adam Patrick

Classifications

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F05D2240/15

  Heat shield · CPC title

• F02C7/24 Primary

  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

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D25/145

  Thermally insulated casings · CPC title