SEAL ASSEMBLY FOR TURBINE COOLANT PASSAGEWAYS

• US 20130202433A1
• Filed: 02/07/2012
• Published: 08/08/2013
• Est. Priority Date: 02/07/2012
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Hafner, Matthew Troy
• Application Number:
  US13/367,486
• Publication Number:
  US 20130202433A1
• Time in Patent Office: Days
• US Class Current: 415/230
• CPC Class Codes: F01D 11/008 by spacer elements between the blades, e.g. independent interblade platforms
• CPC Class Codes: F01D 5/3015 with side plates
• CPC Class Codes: F05D 2240/55 Seals
• CPC Class Codes: Y10T 29/49297 Seal or packing making

Abstract

A seal assembly for use with a turbine having a rotor and at least one turbine blade facilitates the use of a wire seal with seal plate segments. The seal assembly includes a plurality of seal plate segments and a plurality of retainers disposed on a rotor flange on the rotor. A seal member is disposed between the retainers and the seal plate segments. The seal assembly includes at least one attachment member disposed through the rotor flange that limits radial displacement of the seal plate segments.

Claims

1. A seal assembly for use with a turbine having a rotor and at least one turbine blade, comprising

at least one seal plate segment;

at least one inner diameter retainer disposed on a rotor flange on the rotor;

a first seal member disposed between the inner diameter retainer and the seal plate segment; and

at least one attachment member disposed through the rotor flange that limits radial displacement of the seal plate segment.

2. The seal assembly of claim 1 further comprising at least one outer diameter retainer disposed adjacent to a blade flange on the turbine blade.

3. The seal assembly of claim 1 wherein the seal plate segment comprises a seal arm and a beveled end portion.

4. The seal assembly of claim 1 wherein the seal plate segment includes a recessed portion for supporting the first seal member.

5. The seal assembly of claim 2 wherein the rotor flange and the blade flange define an opening having a dimension that can accommodate the insertion of the seal plate segment.

6. The seal assembly of claim 2 wherein the rotor flange and blade flange define a retaining chamber having a dimension that provides sufficient play to accommodate the insertion of the outer diameter retainer.

7. The seal assembly of claim 1 wherein the seal member is a wire seal member.

8. The seal assembly of claim 7 wherein the inner diameter retainer includes a recessed portion to accommodate the wire seal member.

9. The seal assembly of claim 8 wherein the wire seal member comprises a wire seal rope.

10. A method for providing a seal for a turbine having a rotor with at least one rotor flange and at least one turbine blade with a blade flange, the method comprising:

positioning an inner diameter subassembly in a chamber formed by the rotor flange and the blade flange;

displacing the inner diameter subassembly in a radial direction within the chamber; and

securing the inner diameter subassembly within the chamber.

11. The method of claim 10 wherein the inner diameter subassembly comprises:

an inner diameter retainer;

a first seal member; and

a seal plate segment.

12. The method of claim 11 further comprising positioning an outer diameter subassembly on the seal plate segment.

13. The method of claim 12 wherein the method element of positioning the inner diameter subassembly and outer diameter subassembly comprises inserting the inner diameter subassembly and the outer diameter subassembly through an opening defined by the rotor flange and the blade flange.

14. The method of claim 10 wherein the method element of securing the inner diameter subassembly to the rotor comprises inserting a pin through the rotor flange and adjacent to the seal assembly.

15. A turbine comprising:

a rotor having at least one rotor flange;

at least one turbine blades having a blade flange;

a chamber defined by the blade flange and the rotor flange;

at least one seal plate segment disposed in the chamber;

at least one inner diameter retainer disposed in the chamber and proximate to the rotor flange;

a first seal member disposed between the inner diameter retainer and the seal plate segment; and

at least one attachment member disposed through the rotor flange that limits radial displacement of the seal plate segment.

16. The turbine of claim 15 further comprising at least one outer diameter retainer disposed on the seal plate segment.

17. The turbine of claim 15 wherein the rotor flange and the blade flange define an opening having a dimension that can accommodate the insertion of the seal plate segment.

18. The turbine of claim 15 wherein the first seal member is a wire rope seal.

19. The turbine of claim 15 wherein the attachment member is a pin.

20. The turbine of claim 15 further comprising a second seal member disposed between the outer diameter retainer and the seal plate segment.