Pressure actuated film riding seals for turbo machinery

• US 9,115,810 B2
• Filed: 10/03/2013
• Issued: 08/25/2015
• Est. Priority Date: 10/31/2012
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Bidkar, Rahul Anil, Thatte, Azam Mihir, Gibson, Nathan Evan McCurdy, Giametta, Andrew Paul
• Primary Examiner(s): Fulton, Kristina
• Assistant Examiner(s): Byrd, Eugene G
• Application Number:
  US14/045,083
• Publication Number:
  US 20140117624A1
• Time in Patent Office: 691 Days
• Field of Search: 277/411, 277/412, 277/413, 277/416, 277/500, 277/543, 277/545, 277/546, 277/578, 415/115
• US Class Current: 1/1
• CPC Class Codes: F16J 15/442 segmented
• CPC Class Codes: F16J 15/447 Labyrinth packings
• CPC Class Codes: Y10T 29/49826 Assembling or joining

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 sealing device segments includes a stator interface element, a shoe plate having an extended portion having one or more labyrinth teeth facing the rotor and a load bearing portion, wherein the shoe plate is configured to generate an aerodynamic force between the shoe plate and the rotor. The sealing device segment further includes a secondary seal configured to be in contact with the stator interface element at a radially outer end and configured to be in contact with an elevated nose section of the extended portion of the shoe plate on a radially inner end; and multiple flexible elements attached to the shoe plate and to the stator interface element.

Claims

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 plurality of sealing device segments comprises;

a stator interface element;

a shoe plate comprising an extended portion having one or more labyrinth teeth facing the rotor and a load bearing portion, wherein the shoe plate is configured to allow a high pressure fluid to an upstream portion of forwardmost labyrinth tooth and a low pressure fluid to a downstream portion of the aftmost labyrinth tooth and further configured to generate an aerodynamic force by varying film thickness in a tangential direction based on at least one of a curvature mismatch between the shoe plate and the rotor, steps on the shoe and grooves on the rotor,

a secondary seal configured to be in contact with the stator interface element at a radially outer end and configured to be in contact with an elevated nose section of the extended portion of the shoe plate on a radially inner end, wherein the secondary seal comprises an outer layer section and an inner layer section such that each of the outer layer section of the secondary seal having an overhanging portion overlaps a sealing device segment gap formed between inner layer section of adjacent secondary seal segments; and

a plurality of flexible elements attached to the shoe plate and to the stator interface element.

2. The seal assembly of claim 1, wherein the extended portion of the shoe plate comprises the one or more labyrinth teeth located on a protuded portion towards a front end of the shoe plate for separating, a high pressure side from a low pressure side.

3. The seal assembly of claim 1, wherein the rotor comprises a stepped section towards a high pressure side of the rotary machine for reducing an axial momentum of flow of fluid across the one or more labyrinth teeth of the shoe plate, wherein the stepped section comprises a rotor portion with a locally increased radius with a first length of the one or more labyrinth teeth facing the rotor portion with the locally increased radius for reducing an axial momentum of flow of fluid from a high pressure side to a low pressure side, and a locally decreased radius with a second length of the one or more labyrinth teeth facing the rotor portion with the locally decreased radius for reducing an axial momentum of flow of fluid from a high pressure side to a low pressure side.

4. The seal assembly of claim 1, wherein the extended portion of the shoe plate comprises one or more grooves or slots for allowing disposal of one or more spline seal shims for reducing leakage between neighboring sealing device segments.

5. The seal assembly of claim 1, wherein the shoe plate comprises the one or more labyrinth teeth located towards a backward end of the shoe plate for separating a high pressure side from a low pressure side.

6. The seal assembly of claim 5, wherein the rotor comprises a stepped section towards the low pressure side of the rotary machine for reducing, an axial momentum of flow of fluid across the one or more labyrinth teeth of the shoe plate.

7. The seal assembly of claim 5, wherein the shoe plate comprises one or more ports upstream of the labyrinth teeth for allowing flow of high pressure fluid to an upstream portion of frontmost labyrinth tooth from a front cavity formed by the plurality of flexible elements, the stator interface element and the shoe plate, thereby causing pressurization on the shoe plate to achieve an aerostatic force balance rendering the shoe plate towards the rotor during operation of the rotary machine.

8. 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 plurality of sealing device segments comprises;

a stator interface element;

a shoe plate comprising one or more labyrinth teeth facing the rotor and a load bearing surface region, wherein the shoe plate is configured to allow a high pressure fluid to an upstream portion of forwardmost labyrinth tooth and a low pressure fluid to a downstream portion of the aftmost labyrinth tooth and further configured to generate an aerodynamic force by varying film thickness in a tangential direction based on at least one of a curvature mismatch between the shoe plate and the rotor, steps on the shoe and grooves on the rotor,

a secondary seal configured to be in contact with the stator interface element at a radially outer end and configured to be in contact with an elevated nose of the shoe plate on a radially inner end, wherein the secondary seal comprises an outer layer section and an inner layer section such that each of the outer layer section of the secondary seal having an overhanging portion overlaps a sealing device segment gap formed between inner layer section of adjacent secondary seal segments; and

a plurality of flexible elements attached to the shoe plate and to the stator interface element; and

the rotor comprising a stepped section towards a high pressure side of the rotary machine for reducing an axial momentum of flow of fluid across the one or more labyrinth teeth of the shoe plate.

9. The seal assembly of claim 8, wherein the stepped section comprises a rotor portion with locally decreased radius with a first length of the one or more labyrinth teeth facing the rotor portion with locally decreased radius for reducing an axial momentum of flow of fluid from a high pressure side to a low pressure side.

10. The seal assembly of claim 8, wherein the stepped section comprises a rotor portion with locally increased radius with a second length of the one or more labyrinth teeth facing the rotor portion with locally increased radius for reducing an axial momentum of flow of fluid from a high pressure side to a low pressure side.

11. 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 plurality of sealing device segments comprises;

a stator interface element;

a shoe plate comprising an extended portion having one or more labyrinth teeth facing the rotor and a load bearing portion, wherein the shoe plate is configured to allow a high pressure fluid to an upstream portion of forwardmost labyrinth tooth and a low pressure fluid to a downstream portion of the aftmost labyrinth tooth and further configured to generate an aerodynamic force by varying film thickness in the tangential direction based on a curvature mismatch between the shoe plate and the rotor, and the extended portion of the shoe plate comprises one or more ports downstream of the labyrinth teeth for allowing flow of low pressure fluid to a downstream portion of aftmost labyrinth tooth from a rear cavity formed by the plurality of flexible elements, the stator interface element and the shoe plate, thereby causing pressurization on the shoe plate to achieve a force balance rendering the shoe plate towards the rotor during operation of the rotary machine;

a secondary seal configured to be in contact with the stator interface element at a radially outer end and configured to be in contact with an elevated nose section of the extended portion of the shoe plate on a radially inner end, wherein the secondary seal comprises an outer layer section and an inner layer section such that each of the outer layer section of the secondary seal having an overhanging portion overlaps a sealing device segment gap formed between inner layer section of adjacent secondary seal segments; and

a plurality of flexible elements attached to the shoe plate and to the stator interface element, wherein the plurality of flexible elements comprise one of bellows springs, leaf springs and coil springs, configured to support the shoe plate with radial, tangential and axial stiffness, and guide the motion of the shoe plate relative to the stator interface element.