Seal assembly to seal corner leaks in gas turbine

Patent metadata

Field	Value
Publication number	US-9869194-B2
Application number	US-201615087394-A
Country	US
Kind code	B2
Filing date	Mar 31, 2016
Priority date	Mar 31, 2016
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

Various embodiments include gas turbine seals and methods of forming such seals. In some cases, a turbine includes: a first arcuate component adjacent to a second arcuate component, each arcuate component including one or more slots located in an end face, each of the one or more slots having a plurality of axial surfaces and radially facing surfaces extending from opposite ends of the axial surfaces and a seal assembly disposed in the slot. The seal assembly including an intersegment seal including a plurality of seal segments defining one or more corner regions. The intersegment seal disposed in a slot defining a high-pressure slot side and a low-pressure slot side, wherein the slot includes a plurality of slot segments. Each of the plurality of seal segments including at least one extended portion to either seal the one or more corner regions on a low-pressure slot side, form a recess in the intersegment seal, or both.

First claim

What is claimed is:

1. A seal assembly to seal a gas turbine hot gas path flow in a gas turbine, the seal assembly comprising:
an intersegment seal including a plurality of seal segments, the plurality of seal segments defining one or more corner regions, the intersegment seal disposed in a slot defining a high-pressure slot side and a low-pressure slot side, wherein the slot includes a plurality of intersecting slot segments, the one or more corner regions spanning each of the intersecting slot segments, one or more of the plurality of seal segments including at least one extended portion to at least one of:
seal the one or more corner regions on a low-pressure slot side; and
form a recess in one or more of the plurality of seal segments.

2. The seal assembly of claim 1 , wherein the intersegment seal is an intersegment laminate seal with each of the plurality of seal segments comprised of a plurality of outer layers and one or more inner layers.

3. The seal assembly of claim 2 , wherein the at least one extended portion of at least one of the plurality of seal segments includes one or more first extended inner layer to seal the one or more corner regions on the low-pressure slot side.

4. The seal assembly of claim 3 , wherein the at least one extended portion of at least one of the plurality of seal segments further includes one or more additional extended inner layers to seal the one or more corner regions on a high-pressure slot side.

5. The seal assembly of claim 2 , wherein the at least one extended portion of at least one of the plurality of seal segments includes at least one extended outer layer to seal the one or more corner regions on a low-pressure slot side.

6. The seal assembly of claim 5 , wherein at least one of the plurality of seal segments includes an outer layer defining at least one recess to accommodate the extended outer layer of another of the plurality of seal segments.

7. The seal assembly of claim 1 , further comprising a shim seal disposed on a high-pressure slot side and supported by the extended portion to seal the one or more corner regions.

8. The seal assembly of claim 1 , wherein at least one of the plurality of seal segments includes an extended outer portion, an extended inner portion, and a shim seal disposed at least partially within a recess defined between the extended inner portion and the extended outer portion to seal the one or more corner regions.

9. The seal assembly of claim 1 , wherein at least one of the plurality of seal segments includes at least one extended outer portion to seal the one or more corner regions on a high-pressure slot side and further comprising a shim seal disposed on a low-pressure slot side to seal the one or more corner regions.

10. The seal assembly of claim 1 , wherein at least one of the plurality of seal segments includes at least one recess on a high-pressure slot side and further comprising an extended shim seal disposed on a low-pressure slot side, the extended shim seal including a gap formed therein, that in combination with the recess, seals the one or more corner regions.

11. A gas turbine comprising:
a first arcuate component adjacent to a second arcuate component, each arcuate component including one or more slots located in an end face, each of the one or more slots having a plurality of substantially axial surfaces and one or more radially facing surfaces extending from opposite ends of the substantially axial surfaces, defining a plurality of intersecting slot segments; and
a seal assembly disposed in the slot of the first arcuate component and the slot of the second arcuate component, the seal assembly comprising:
an intersegment seal including a plurality of seal segments, the plurality of seal segments defining one or more corner regions spanning between the axial surface and each of the radially facing surfaces of the one or more slots, the intersegment seal disposed in a slot defining a high-pressure slot side and a low-pressure slot side, wherein one or more of the plurality of seal segments including at least one extended portion to at least one of:
seal the one or more corner regions on a low-pressure slot side; and
form a recess in one or more of the plurality of seal segments.

12. The gas turbine of claim 11 , wherein the intersegment seal is an intersegment laminate seal with each of the plurality of seal segments comprised of a plurality of outer layers and one or more inner layers.

13. The gas turbine of claim 12 , wherein the at least one extended portion of at least one of the plurality of seal segments includes one or more first extended inner layer to seal the one or more corner regions on the low-pressure slot side.

14. The gas turbine of claim 12 , wherein the at least one extended portion of at least one of the plurality of seal segments further includes one or more additional extended inner layers to seal the one or more corner regions on a high-pressure slot side.

15. The gas turbine of claim 12 , wherein the at least one extended portion of at least one of the plurality of seal segments includes at least one extended outer layer to seal the one or more corner regions on a low-pressure slot side.

16. The gas turbine of claim 12 , wherein at least one of the plurality of seal segments includes an outer layer defining at least one recess to accommodate the extended outer layer of another of the plurality of seal segments.

17. The gas turbine of claim 11 , further comprising a shim seal disposed on one of a high-pressure slot side or a low-pressure slot side to seal the one or more corner regions.

18. The gas turbine of claim 11 , wherein at least one of the plurality of seal segments includes an extended outer portion, an extended inner portion, and a shim seal disposed at least partially within a recess defined between the extended inner portion and the extended outer portion to seal the one or more corner regions.

19. The seal assembly of claim 11 , wherein at least one of the plurality of seal segments includes at least one recess on a high-pressure slot side and further comprising an extended shim seal disposed on a low-pressure slot side, the extended shim seal including a gap formed therein, that in combination with the recess, seals the one or more corner regions.

20. A method of assembling a seal in a turbine, the method comprising:
forming a seal assembly, the forming including:
providing an intersegment seal including a plurality of seal segments, and including at least one extended portion to at least one of:
seal one or more corer regions on a low-pressure slot side; and
form a recess in one or more of the plurality of seal segments,

applying the intersegment seal in the turbine, the turbine having:
a first arcuate component adjacent to a second arcuate component, each arcuate component including one or more slots located in an end face, each of the one or more slots having a plurality of axial surfaces and radially facing surfaces extending from opposite ends of the axial surfaces, defining a plurality of intersecting slot segments;

the applying including inserting the seal assembly in a slot of the one or more slots such that the intersegment seal is disposed in the slot on each arcuate component and in contact with the axial surface of the slots and extending over the radially facing surfaces of the slots.

21. The method of claim 20 , wherein the intersegment seal is an intersegment laminate seal with each of the plurality of seal segments comprised of an outer layer

Assignees

• Gen Electric

Inventors

• Dev Bodhayan
• Meyer Robert Carl
• Sarawate Neelesh Nandkumar
• Albert Jason Edward
• Itzel Gary Michael

Classifications

• F05D2240/59

  Lamellar seals · CPC title

• F01D11/005 Primary

  Sealing means between non relatively rotating elements · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F16J15/442

  segmented · CPC title

• F05D2240/57

  Leaf seals · CPC title