Turbine exhaust diffuser

Patent metadata

Field	Value
Publication number	US-11215085-B2
Application number	US-201816029708-A
Country	US
Kind code	B2
Filing date	Jul 9, 2018
Priority date	Aug 11, 2017
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

The present application provides an exhaust diffuser. The exhaust diffuser may include an outer diffuser section with a forward portion. An outer forward seal system may be positioned on the forward portion. The outer forward seal system may include a seal base removably positioned in a seal pocket.

First claim

The invention claimed is:

1. An exhaust diffuser, comprising:
an outer diffuser section, the outer diffuser section comprising a forward portion disposed about an exit end of a turbine, the forward portion including a flow side and a seal side and extending between a free end and a connected end, the forward portion defining a seal pocket between the free end and the connected end on the seal side, the seal pocket having a radially extending portion and an axially extending portion extending directly from the radially extending portion; and
an outer forward seal system positioned within the forward portion;
wherein the outer forward seal system comprises a seal base removably positioned in the seal pocket, the seal base comprising a body installed in the radially extending portion, a pair of flanges extending radially outward from the body, and a hook installed in the axially extending portion, wherein the body and the pair of flanges define a radial slot, and wherein the hook extends axially from the body and axially beyond the body.

2. The exhaust diffuser of claim 1 , wherein the seal base comprises a seal member positioned within the radial slot.

3. The exhaust diffuser of claim 2 , wherein the seal member extends towards a casing.

4. The exhaust diffuser of claim 2 , wherein the seal member comprises a flexible seal.

5. The exhaust diffuser of claim 1 , wherein the forward portion comprises a channel therein extending radially outward from the flow side and extending to the axially extending portion of the seal pocket.

6. The exhaust diffuser of claim 5 , wherein the forward portion comprises a dowel removably positioned within the channel and extending into the axially extending portion.

7. The exhaust diffuser of claim 1 , wherein the forward portion comprises a skin facing a flow of combustion gases.

8. The exhaust diffuser of claim 7 , wherein the seal base is positioned on the seal side of the forward portion opposite of the skin facing the flow of combustion gases such that the seal base forms no portion of the skin.

9. The exhaust diffuser of claim 1 , wherein the exhaust diffuser comprises a plurality of segments.

10. A method of operating an exhaust diffuser, the exhaust diffuser comprising a forward portion being disposed about an exit end of a turbine, the forward portion including a flow side and a seal side and extending between a free end and a connected end, the method comprising:
removably positioning a hook of a seal base in an axially extending portion of a seal pocket of the forward portion of the exhaust diffuser and a body of a seal base in a radially extending portion of the seal pocket, the seal pocket being defined in the forward portion between the free end and the connected end on the seal side, wherein the hook extends axially from the body and axially beyond the body, wherein the seal base comprises a pair of flanges defining a radial slot, the pair of flanges extending radially outward from the body of the seal base, and wherein the body of the seal base partially defines the radial slot;
locking the seal base into place by extending a dowel into a channel extending through the forward portion from the flow side thereof; and
flowing combustion gases past the forward portion on the flow side thereof.

11. An exhaust diffuser, comprising:
an outer diffuser section, the outer diffuser section comprising a forward portion disposed about an exit end of a turbine, the forward portion including a flow side and a seal side and extending between a free end and a connected end, the forward portion defining a seal pocket between the free end and the connected end on the seal side, the seal pocket having an axially extending portion; and
an outer forward seal system positioned on the forward portion, the outer forward seal system comprising:
a seal base with a seal member, the seal base having a hook, a pair of flanges, and a body, the hook extending axially from the body and axially beyond the body, the hook configured for installation in the axially extending portion of the seal pocket, the pair of flanges extending radially outward from the body, and the body and the pair of flanges defining a radial slot;
wherein the seal base forms no portion of the flow side, and wherein the seal base is removably positioned within the axially extending portion of the seal pocket and is secured via a dowel extending through the forward portion.

12. The exhaust diffuser of claim 11 , wherein the forward portion comprises a channel therein extending radially outward from the flow side and extending to the axially extending portion of the seal pocket; and wherein the dowel is removably positioned within the channel and extends from the flow side to the hook.

13. The exhaust diffuser of claim 12 , wherein the dowel terminates radially at the hook.

Assignees

• General Electric Comany
• Gen Electric

Inventors

• Jakubczak Przemyslaw Michal
• Leszczynski Karol
• Jamiolkowski Robert

Classifications

• F05D2240/55

  Seals · CPC title

• F05D2220/32

  in gas turbines · 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

• F01D25/30 Primary

  Exhaust heads, chambers, or the like · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title