Air with integral spring for a gas turbine engine exhaust drive

Patent metadata

Field	Value
Publication number	US-9915228-B2
Application number	US-201414305606-A
Country	US
Kind code	B2
Filing date	Jun 16, 2014
Priority date	Aug 16, 2013
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

A seal assembly for an exhaust duct section of a gas turbine engine includes a multiple of springs that axially extend from a split hoop opposite a seal surface.

First claim

What is claimed is:

1. An exhaust duct section for a gas turbine engine, the exhaust duct section comprising:
a first exhaust duct;
a second exhaust duct adjacent to said first exhaust duct; and
a seal assembly between said first exhaust duct and said second exhaust duct, wherein said seal assembly includes a split hoop with a seal surface that interfaces with said first exhaust duct and a multiple of springs that extend from said split hoop, and wherein said multiple of springs interface with said second exhaust duct;
wherein each of said multiple of springs includes a respective distal and unsupported end that is disposed an axial distance away from said split hoop, and each of said multiple of springs is fixed to said split hoop and projects out from said split hoop to said respective distal and unsupported end;
wherein said multiple of springs include a first spring and a second spring; and
wherein said first spring and said second spring project out from said split hoop in opposite circumferential directions.

2. The exhaust duct section as recited in claim 1 , wherein said seal assembly is radially outboard of an exhaust duct liner.

3. The exhaust duct section as recited in claim 1 , wherein said seal assembly accommodates axial displacement between said first exhaust duct and said second exhaust duct.

4. The exhaust duct section as recited in claim 3 , wherein said seal assembly accommodates rotation of said first exhaust duct relative to said second exhaust duct.

5. The exhaust duct section as recited in claim 1 , wherein said split hoop is U-shaped in cross-section.

6. The exhaust duct section as recited in claim 1 , wherein said split hoop is L-shaped in cross-section.

7. The exhaust duct section as recited in claim 1 , wherein said split hoop is radially outboard of a seal carrier.

8. The exhaust duct section as recited in claim 7 , wherein said seal carrier is mounted to an annular bulkhead of said second exhaust duct.

9. The exhaust duct section as recited in claim 8 , wherein said multiple of springs is radially inboard of a seal retainer.

10. The exhaust duct section as recited in claim 9 , wherein said seal retainer is mounted to said annular bulkhead of said second exhaust duct.

11. The exhaust duct section as recited in claim 1 , wherein said seal surface interfaces with said first exhaust duct at a back plate.

12. The exhaust duct section as recited in claim 11 , wherein said seal surface interfaces with said first exhaust duct at a bearing plane to accommodate rotation of said first exhaust duct relative to said second exhaust duct.

13. The exhaust duct section as recited in claim 12 , wherein said seal assembly accommodates axial displacement between said first exhaust duct and said second exhaust duct, and said multiple of springs maintains said seal surface interface with said back plate.

14. The assembly of claim 1 , wherein said multiple of springs and said split hoop are formed integrally together as a single monolithic body.

15. A seal assembly for an exhaust duct section of a gas turbine engine, the assembly comprising:
a split hoop that defines a seal surface; and
a multiple of springs that axially extend from said split hoop opposite said seal surface, and include a first spring and a second spring;
wherein said first spring is cantilevered from and fixed to said split hoop;
wherein said second spring is cantilevered from and fixed to said split hoop; and
wherein said first spring and said second spring project out from said split hoop in different circumferential directions.

16. The assembly as recited in claim 15 , wherein said split hoop is U-shaped in cross-section.

17. The assembly as recited in claim 15 , wherein said split hoop is L-shaped in cross-section.

18. The assembly as recited in claim 15 , wherein said multiple of springs and said split hoop are formed integrally together as a single monolithic body.

19. The assembly as recited in claim 15 , wherein each of said multiple of springs is a discrete body and welded to said split hoop.

20. The assembly as recited in claim 15 , wherein each of said multiple of springs is a discrete body and fastened to said split hoop.

Assignees

• United Technologies Corp

Inventors

• Peters Christopher J
• Bowers Daniel R

Classifications

• F02K1/80 Primary

  Couplings or connections · CPC title

• F02K1/004

  by using one or more swivable nozzles rotating about their own axis · CPC title

• F05D2220/90

  in vehicles adapted for vertical or short take off and landing (v/stol vehicles) · CPC title