Film riding seals for rotary machines

Patent metadata

Field	Value
Publication number	US-9587746-B2
Application number	US-201213562705-A
Country	US
Kind code	B2
Filing date	Jul 31, 2012
Priority date	Jul 31, 2012
Publication date	Mar 7, 2017
Grant date	Mar 7, 2017

Abstract

A seal assembly for a rotary machine is provided. The seal assembly includes multiple sealing device segments disposed circumferentially intermediate to a stationary housing and a rotor. Each of the segments includes a shoe plate with a forward-shoe section and an aft-shoe section having one or more labyrinth teeth therebetween facing the rotor. The sealing device includes a stator interface element having a groove or slot for allowing disposal of a spline seal for preventing segment leakages. The sealing device segment also includes multiple bellow springs or flexures connected to the shoe plate and to the stator interface element. Further, the sealing device segments include a secondary seal integrated with the stator interface element at one end and positioned about the multiple bellow springs or flexures and the shoe plate at the other end.

First claim

The invention claimed is:

1. A seal assembly for a rotary machine, the seal assembly comprising:
a plurality of sealing device segments disposed circumferentially intermediate to a stationary housing and a rotor, wherein each of the segments comprises:
a shoe plate with a forward-shoe section and an aft-shoe section having one or more labyrinth teeth therebetween facing the rotor, wherein the shoe plate is configured to allow a high pressure fluid to a front portion of the one or more labyrinth teeth and a low pressure fluid behind the one or more labyrinth teeth and further configured to generate an aerodynamic force between the shoe plate and the rotor,
a stator interface element comprising a groove or slot for allowing disposal of a spline seal for reducing leakages;
a plurality of bellow springs or flexures connected to the shoe plate and to the stator interface element; wherein the plurality of bellow springs or flexures are configured to allow the high pressure fluid to occupy a forward cavity and the low pressure fluid to occupy an aft cavity; and
a secondary seal integrated with the stator interface element at one end and positioned about the plurality of bellow springs and the shoe plate at the other end.

2. The seal assembly of claim 1 , further comprising a plurality of shiplap shims located within the seal assembly and configured to overlap adjacent secondary seals in the seal assembly.

3. The seal assembly of claim 2 , wherein each of the shiplap shims comprises a first shim and a second shim angularly attached to each other.

4. The seal assembly of claim 3 , wherein for each of the shiplap shims, the first shim is attached to one of the secondary seal and the second shim is configured to freely slide on the adjacent secondary seal of the seal assembly.

5. The seal assembly of claim 1 , wherein the shoe plate is configured to generate the aerodynamic force due to radius of the shoe plate facing the rotor being larger than the radius of the rotor or due to presence of one or more Rayleigh steps on the shoe plate facing the rotor or due to the presence of grooves or slots angled in axial or tangential direction or in a herringbone pattern on the rotor.

6. The seal assembly of claim 1 , wherein the secondary seal is curved in a circumferential direction.

7. The seal assembly of claim 1 , wherein the secondary seal are curved in a circumferential direction.

8. The seal assembly of claim 1 , wherein the one end of the secondary seal comprises an angled end attached in a slot located in the stator interface element.

9. The seal assembly of claim 8 , wherein the secondary seal is integrated with the stator interface element via a supporting structure element.

10. The seal assembly of claim 9 , wherein the supporting structure element is an extension of the stator interface element.

11. The seal assembly of claim 10 , wherein the supporting structure element comprises a groove or slot for allowing disposal of a spline seal for reducing segment leakages.

12. The seal assembly of claim 10 , wherein the secondary seal is interfaced with the supporting structure element for allowing radially outward movement of the secondary seal.

13. The seal assembly of claim 10 , wherein the secondary seal is interfaced with the supporting structure element for preventing radially inward movement of the secondary seal.

14. The seal assembly of claim 1 , wherein the plurality of bellow springs or flexures comprises of holes for relieving pressure.

15. A rotary machine, comprising:
a rotor;
a stator housing; and
a plurality of sealing device segments disposed circumferentially intermediate to the stationary housing and the rotor, wherein each of the segments comprises:
a shoe plate with a forward-shoe section and an aft-shoe section having one or more labyrinth teeth therebetween facing the rotor, wherein the shoe plate is configured to allow a high pressure fluid to a front portion of the one or more labyrinth teeth and a low pressure fluid behind the one or more labyrinth teeth and further configured to generate an aerodynamic force between the shoe plate and the rotor,
a stator interface element comprising a groove or slot for allowing disposal of a spline seal for preventing leakages;
a plurality of bellow springs or flexures connected to the shoe plate and to the stator interface element; wherein the plurality of bellow springs or flexures are configured to allow the high pressure fluid to occupy a forward cavity and the low pressure fluid to occupy an aft cavity; and

a secondary seal integrated with the stator interface element at one end and positioned about the plurality of bellow springs and the shoe plate at the other end.

16. The rotary machine of claim 15 , further comprising a forward shoe feeding groove and an aft shoe feeding groove at sides of the shoe plate towards a high pressure side and a low pressure side of the rotary machine respectively.

17. The rotary machine of claim 15 ; wherein the secondary seal is attached to the stator interface element.

18. The rotary machine of claim 15 , wherein the one end of the secondary seal comprises an angled end attached in a slot located in the stator interface element.

19. The rotary machine of claim 15 , wherein the secondary seal is integrated with the stator interface element via a supporting structure element for allowing radially outward movement of the secondary seal and preventing radially inward movement of the secondary sea.

20. The rotary machine of claim 19 , wherein the supporting structure element comprises a groove or slot for allowing disposal of a spline seal for preventing leakages.

Assignees

• Bidkar Rahul Anil
• Sarawate Neelesh Nandkumar
• Wolfe Christopher Edward
• Ruggiero Eric John
• Raj Mohan Vivek Raja
• Gen Electric

Inventors

• Bidkar Rahul Anil
• Sarawate Neelesh Nandkumar
• Wolfe Christopher Edward
• Ruggiero Eric John
• Raj Mohan Vivek Raja

Classifications

• F01D11/14

  Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing (rotors with blades adjustable in operation F01D7/00) · CPC title

• F16J15/442

  segmented · CPC title

• F16J15/445

  with means for adjusting the clearance · CPC title

• F01D11/04

  using sealing fluid, e.g. steam · CPC title

• F01D11/025 Primary

  Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations · CPC title