Supplemental seal for the chordal hinge seal in a gas turbine

• US 6,599,089 B2
• Filed: 12/28/2001
• Issued: 07/29/2003
• Est. Priority Date: 12/28/2001
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Kellock, Iain Robertson, Aksit, Mahmut Faruk, Safi, Ahmad, Mohammed-Fakir, Abdul-Azeez
• Primary Examiner(s): Nguyen, Ninh H.
• Application Number:
  US10/029,227
• Publication Number:
  US 20030123982A1
• Time in Patent Office: 578 Days
• Field of Search: 415/191, 415/209.2, 415/209.3, 415/231, 277/628, 277/630, 277/637, 277/641, 277/644, 277/647
• US Class Current: 415/191
• CPC Class Codes: F01D 11/005 Sealing means between non relatively rotating elements
• CPC Class Codes: F02C 7/28 Arrangement of seals
• CPC Class Codes: F16J 15/0812 with a braided or knitted body

Abstract

In a gas turbine having a chordal hinge seal between an inner rail of each nozzle segment and an annular axially facing sealing surface of a nozzle support ring, a supplemental seal is disposed between the support ring and inner rail of the nozzle segment on a high pressure side of the chordal hinge seal. The supplemental seal includes a pair of sheet metal shims overlaid by a woven metallic cloth supported by a bracket secured to a back side surface of the inner rail. The radially inner end of the cloth seal bears against the annular sealing surface of the nozzle support ring. The shims of the legs of the supplemental seal are slit along their distal margin and staggered in a chord-wise direction relative to one another to provide flexibility and effective sealing engagement with the nozzle support ring.

Claims

1. A turbine comprising:

a turbine nozzle support ring having a generally axially facing first surface;

a turbine nozzle segment having at least one stator vane and a radially inwardly extending inner rail having a second surface in axial opposition to said first surface;

a seal depending from a side surface of said inner rail remote from said second surface and extending radially inwardly of said inner rail for sealing engagement against said first surface to form a seal therebetween;

said seal including a seal segment having at least a first plate, an overlay of a woven metallic cloth and a distal margin covered by said cloth and engaging said first surface; and

a support bracket extending along at least a portion of one side of said seal body to support said seal segment on a side thereof remote from said inner rail, said margin of said seal segment being flexible and preloaded to seal against said first surface.

2. A turbine according to claim 1 wherein said seal segment includes a second plate, said plates lying back-to-back with one another, said cloth extending as an overlay along opposite sides of said first and second plates.

3. A turbine according to claim 2 wherein said seal extends linearly in a chord-wise direction along said inner rail, said plates having slits extending from edges thereof and along said margin to provide flexibility to said seal.

4. A turbine according to claim 3 wherein the slits along a margin of said first plate and the slits along a margin of said second plate are staggered relative to one another in a chordal direction about the rotor axis.

5. A turbine according to claim 1 wherein said inner rail has a projection extending axially from said inner rail for sealing engagement against said first surface and forming a second seal therewith.

6. A turbine according to claim 5 wherein said projection extends linearly along said inner rail.

7. A turbine according to claim 6 wherein said sealing engagement between said projection and said first surface lies on a low pressure side of the first-mentioned seal.

8. A turbine according to claim 7 wherein the first seal extends linearly in a chord-wise direction about the axis of the turbine.

9. A turbine according to claim 8 wherein said seal is welded to said side surface of said inner rail and along opposite end edges of said seal to opposite ends of said inner rail.

10. A turbine comprising:

a turbine nozzle support ring having a generally axially facing first surface;

a plurality of turbine nozzle segments each having at least one stator vane and a radially inwardly extending inner rail having a second surface in axial opposition to said first surface;

a seal comprised of a plurality of seal segments each depending from a side surface of said inner rail remote from said second surface and extending radially inwardly of said inner rail for sealing engagement against said first surface to form a seal therewith;

each said seal segment including a first plate, an overlay of a woven metallic cloth and a distal margin covered by said cloth and engaging said first surface; and

a plurality of support brackets extending along one side of said seal segments to support said seal bodies on a high pressure side thereof, said margins of said seal bodies being flexible and preloaded to seal against said first surface.

11. A turbine according to claim 10 wherein each said seal segment includes a second plate, said first and second plates of each said seal body lying back-to-back with one another, said cloth extending as an overlay along opposite sides of said first and second plates.

12. A turbine according to claim 10 wherein each of said seal segments extends in a chord-wise direction and has a chord-wise extent corresponding to the chord-wise extent of each inner rail.

13. A turbine according to claim 10 wherein each said seal segment includes a second plate, said first and second plates of each said seal body lying back-to-back with one another, said cloth extending as an overlay along opposite sides of said first and second plates, each said seal extending linearly about an axis of the turbine, said plates having slits extending from edges thereof and along said margin to provide flexibility to said seal.

14. A turbine according to claim 13 wherein the slits along a margin of said first plate and the slits along a margin of said second plate in each seal segment are staggered relative to one another in a chord-wise direction along the inner rail.

15. A turbine according to claim 10 wherein said inner rail has a projection extending axially therefrom for sealing engagement against said first surface and forming a second seal therewith.

16. A turbine according to claim 15 wherein said projections extend linearly along said inner rails.

17. A turbine according to claim 16 wherein said sealing engagement between said projections and said first surface lies on a low pressure side of the first-mentioned seal.

18. A turbine according to claim 16 wherein the first seal extends linearly in a chord-wise direction relative to the axis of the turbine.