Flexible component providing sealing connection

Patent metadata

Field	Value
Publication number	US-9366444-B2
Application number	US-201314077594-A
Country	US
Kind code	B2
Filing date	Nov 12, 2013
Priority date	Nov 12, 2013
Publication date	Jun 14, 2016
Grant date	Jun 14, 2016

Abstract

A sealing component ( 61 ) for a turbine ( 15 ) positionable at an interface between a transition section ( 21 ) for carrying exhaust gas and a turbine inlet section ( 32 ). A U-shaped section ( 45 ) includes first and second legs ( 67, 69 ). When the sealing component is positioned at the interface, the legs extend about the turbine axis. A seal flange ( 75 ) connects to the U-shaped section. The positioned sealing component extends about the axis and in a direction away from the first leg. The seal flange faces the inner surface ( 76 ) of the flange. A flexible strip ( 79 ), positioned radially outward with respect to the seal flange, extends about the axis and extends along the axis between the U-shaped section and the flange. The flexible strip acts as a spring member pressing against the outer surface ( 96 ) of the flange.

First claim

The claimed invention is:

1. A transition seal assembly for a gas turbine engine, along which exhaust gas generated in a combustion chamber can flow toward a turbine of the gas turbine engine, the transition seal assembly comprising:
first and second opposing ends with a U-shape body member at the a first end and a seal flange extending along a second end, the transition seal assembly positionable between a transition section downstream of the combustion chamber and
an inlet flange attached to an inlet section of the turbine, wherein the inlet flange extends circumferentially about an axis of rotation of the turbine, the seal flange extending away from the first end and along an axial direction defined by the axis of rotation; and
a flexible member affixed to the transition seal assembly and extending along the seal flange so that, when the transition seal assembly is positioned between the transition section and the inlet flange of the inlet section, the flexible member is positioned radially outward from the seal flange with the flexible member comprising a bend making contact with the inlet flange of the turbine inlet section,
wherein the inlet flange has an inner surface and an outer surface opposite to the inner surface with the inner surface facing a flow path of the exhaust gas between the transition section and the inlet section and the outer surface faces away from the flow path, and wherein the flexible member is a spring seal including a first end attached to the transition seal assembly and a second end opposite to the first end, wherein the second end comprises the bend and wherein the bend comprises a bead configured to elastically press on the outer surface of the inlet flange such that sealing contact is maintained along a line of contact between the bead and the outer surface of the inlet flange.

2. The transition seal assembly of claim 1 wherein, with the transition seal assembly installed between the transition section and the inlet section, the U-shaped body member extends circumferentially about the axis of rotation, and the U-shape body member comprises a pair of parallel portions that fit about a rail surface of the transition section, wherein the rail surface extends radially outward with respect to a flow path of the exhaust gas between the transition section and the inlet section and extends circumferentially about the axis of rotation to effect connection between the transition seal assembly and the transition section.

3. The transition seal assembly of claim 1 wherein the spring seal comprises first and second finger seal plates positioned against one another to inhibit leakage when placed between high pressure and low pressure regions, the first and second finger seal plates forming a segment of an arc for positioning about the axis of rotation.

4. The transition seal assembly of claim 3 wherein each finger seal plate includes a series of partial cuts arranged so that, when the first and second finger seal plates are positioned against one another to inhibit leakage, the series of partial cuts on one of the first and second finger seal plates are staggered with respect to the series of partial cuts on the other of the first and second finger seal plates.

5. The transition seal assembly of claim 4 , wherein the first and second finger seal plates each comprise a series of metered holes, wherein the series of metered holes of the first and second finger seal plates are aligned to allow a controlled flow of air through the first and second finger seal plates.

6. The transition seal assembly of claim 4 wherein a backing ring segment is fastened to a radially inner edge of each of the first and second finger seal plates with a series of rivets.

7. The transition seal assembly of claim 1 wherein the first end includes a plurality of apertures and wherein a plurality of fasteners are passed through the plurality of apertures to secure the first end to the transition seal assembly.

8. The transition seal assembly of claim 1 wherein the U-shape body member includes an upstream leg member and a downstream leg member, wherein the upstream leg member and the downstream leg member form a slot to receive a rail surface of the transition section, and wherein the first end is attached to the downstream leg member.

9. The transition seal assembly of claim 8 wherein the first end is attached to a portion of the downstream leg member adjacent to a junction of the downstream leg member and the seal flange such that the first end comprises a bend opposite to the bend in the second end.

10. The transition seal assembly of claim 9 wherein the spring seal comprises a curve in a region between the bend at the first end and the bend at the second end.

11. The transition seal assembly of claim 8 wherein the first end is attached to a portion of the downstream leg member at a maximum distance away from the seal flange such that the first end comprises a bend opposite to the bend in the second end.

12. The transition seal assembly of claim 1 wherein the U-shape body member includes an upstream leg member and a downstream leg member, wherein the upstream leg member and the downstream leg member form a slot to receive a rail surface of the transition section, wherein the transition seal assembly further comprises an axial segment extending axially in a downstream direction from the downstream leg member to the seal flange, wherein the axial segment has a greater thickness than the seal flange, and wherein the flexible member is affixed to the axial segment.

13. A sealing connection component for an interface between a transition section and an inlet section of a turbine of a gas turbine engine, comprising:
a U-shaped section including first and second leg portions such that when the sealing connection component is positioned at the interface, each leg extends along a different side of a rail of the transition section;
a seal flange portion connected to the U-shaped section such that when the sealing connection component is positioned at the interface, the seal flange portion extends in an axial direction away from the first and second leg portions and a surface of the seal flange portion is in sliding contact with an inner surface of the inlet section of the turbine; and
a flexible strip positioned radially outward with respect to the seal flange portion such that the flexible strip comprises a bend that makes contact with an outer surface of the inlet section of the turbine opposite to the inner surface of the inlet section of the turbine.

14. The sealing connection component of claim 13 wherein the inner surface of the inlet section faces a flow path of exhaust gas across the interface, wherein the flexible strip is a spring seal including a first end attached to the sealing connection component and a second end opposite to the first end, wherein the second end comprises the bend.

15. The sealing connection component of claim 13 wherein the bend comprises a bead configured to elastically press on the outer surface of the inlet section such that sealing contact is maintained along a line of contact between the bead and the outer surface of the inlet flange.

16. The sealing connection component of claim 13 wherein the flexible strip is a spring seal comprising first and second finger seal plates positioned against one another to inhibit leakage when placed between high pressure and low pressure regions, wherein each finger seal plate includes a series of partial cuts arranged so that, when the first and second finger seal plates are positioned against one another to inhibit leakage, the series of par

Assignees

• Salunkhe Anil L
• Boudin Dustin C
• Siemens Energy Inc

Inventors

• Salunkhe Anil L
• Boudin Dustin C

Classifications

• F23R3/42 Primary

  characterised by the arrangement or form of the flame tubes or combustion chambers · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title

• F01D9/023 Primary

  Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings · CPC title

• F05D2240/57

  Leaf seals · CPC title

• F05D2240/55

  Seals · CPC title