Heat shield for signature suppression system

Patent metadata

Field	Value
Publication number	US-10974840-B2
Application number	US-201916668345-A
Country	US
Kind code	B2
Filing date	Oct 30, 2019
Priority date	Jul 27, 2017
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

Devices, systems, and methods of a casing for a heat suppression system of a gas turbine engine exhaust include a heat shield and an insulation layer for arrangement between the heat shield and an outer skin.

First claim

What is claimed is:

1. A casing system for a heat suppression system of a gas turbine engine, the casing system comprising:
an outer skin defining an inner cavity and having at least one mount,
a heat shield disposed within the inner cavity and secured with the outer skin, and
an insulation layer disposed between the outer skin and the heat shield,
wherein the heat shield is supported to float relative to the outer skin on the at least one mount, wherein the at least one mount defines slanted surfaces for engagement with the heat shield,
wherein the heat shield includes a forward sheet and an aft sheet, the forward sheet secured to a first surface of the slanted surfaces and the aft sheet secured to a second surface of the slanted surfaces, wherein the first and second slanted surfaces have different pitch.

2. The casing system of claim 1 , wherein the forward sheet and the aft sheet are arranged to overlap.

3. The casing system of claim 1 , wherein the forward sheet is arranged to overlap the aft sheet to cascade in an aftward direction.

4. The casing system of claim 1 , wherein the forward sheet and the aft sheet each have a forward end and an aft end, wherein at least one of the forward sheet and the aft sheet is linear extending between the respective forward and aft ends of the at least one of the forward sheet and the aft sheet.

5. The casing system of claim 1 , wherein at least one of the forward sheet and the aft sheet have curvature complementary with the outer skin.

6. The casing system of claim 1 , wherein a gap is defined between the outer skin and at least one of the forward sheet and the aft sheet.

7. The casing system of claim 1 , wherein gaps are defined between the outer skin and each of the forward sheet and the aft sheet.

8. The casing system of claim 1 , wherein the insulation layer is arranged as a damper configured to absorb relative movement between the outer skin and the heat shield.

9. The casing system of claim 8 , wherein the insulation layer has a spring rate in the range of 25 to 100 lb-force/in.

10. The casing system claim 1 , wherein the heat shield is secured with the outer skin with an attachment system including a fastener and a spacer, the fastener penetrating through the heat shield.

11. A method of forming a casing, the casing system comprising:
an outer skin defining an inner cavity and having at least one mount,
a heat shield disposed within the inner cavity and secured with the outer skin, and
an insulation layer disposed between the outer skin and the heat shield,
wherein the heat shield is supported to float relative to the outer skin on the at least one mount, wherein the at least one mount defines slanted surfaces for engagement with the heat shield,
wherein the heat shield includes a first sheet and a second sheet, the first sheet secured to a first surface of the slanted surfaces and the second sheet secured to a second surface of the slanted surfaces, wherein the first and second slanted surfaces have different pitch,
the method comprising mounting the first sheet to the first surface, mounting the second sheet to the second surface, and
arranging the insulation layer between the heat shield and the outer skin.

12. The method of claim 11 , wherein at least one of mounting the first sheet and mounting the second sheet includes compressing the insulation layer as a damper.

13. The method of claim 12 , wherein mounting the first sheet and mounting the second sheet includes compressing the insulation layer as the damper.

14. The method of claim 11 , wherein mounting the first sheet includes warping the first sheet to have a curvature corresponding to the outer skin and/or wherein mounting the second sheet includes warping the second sheet to have curvature corresponding to the outer skin.

15. The method of claim 14 , wherein mounting the first sheet includes warping the first sheet to have a curvature corresponding to the outer skin and wherein mounting the second sheet includes warping the second sheet to have curvature corresponding to the outer skin.

16. The method of claim 11 , wherein the first sheet and the second sheet each have a forward end and an aft end, where at least one of the first sheet and the second sheet is linear extending between the respective forward and aft ends of the at least one of the forward sheet and the aft sheet.

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Petty Sr Jack D
• Faucett Colin
• Pesyna Kenneth M
• Loebig James C

Classifications

• F02K1/825

  Infrared radiation suppressors · CPC title

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title

• B64D27/12 Primary

  within, or attached to, wings · CPC title

• F02C7/24

  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

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title