Turbine interstage seal system

Patent metadata

Field	Value
Publication number	US-9540940-B2
Application number	US-201213418281-A
Country	US
Kind code	B2
Filing date	Mar 12, 2012
Priority date	Mar 12, 2012
Publication date	Jan 10, 2017
Grant date	Jan 10, 2017

Abstract

A system includes a multi-stage turbine. The multi-stage turbine has an interstage seal extending axially between a first turbine stage and a second turbine stage. The interstage seal has an upper body that extends from an upstream seating arm to a downstream seating arm. The upstream and downstream seating arms are designed to constrain movement of the interstage seal along a radial direction of the multi-stage turbine. The interstage seal also has a lower body that extends from a seating end to a hook end. The seating end is designed to constrain movement of the interstage seal along the radial direction. The hook end has a protrusion that extends crosswise relative to a base of the lower body. The hook end is designed to constrain movement of the interstage seal along the radial direction and an axial direction of the multi-stage turbine.

First claim

The invention claimed is:

1. A system, comprising:
a multi-stage turbine, comprising:
an interstage seal extending in an axial direction relative to a rotational axis of the multi-stage turbine between a first turbine stage and a second turbine stage, wherein the interstage seal comprises:
an upper body extending from an upstream seating arm to a downstream seating arm, wherein the upstream and downstream seating arms are configured to constrain movement of the interstage seal along a radial direction relative to the rotational axis of the multi-stage turbine; and
a lower body extending from a seating end to a hook end, wherein the seating end is configured to constrain movement of the interstage seal along the radial direction, and the hook end comprises an integral protrusion extending crosswise relative to a base of the lower body, wherein the hook end is configured to constrain movement of the interstage seal along the radial direction and the axial direction, the integral protrusion is axially constrained in an upstream direction and a downstream direction by a groove adjacent a lower support of a second rotor wheel of the second turbine stage, and the lower body comprises a hollow region that is axially and radially enclosed relative to the rotational axis of the multi-stage turbine.

2. The system of claim 1 , wherein the upstream seating arm is radially constrained by an upper support extending axially from a first bucket of the first turbine stage and the seating end is radially constrained by a second lower support extending axially from a first rotor wheel of the first turbine stage.

3. The system of claim 1 , wherein the downstream seating arm is radially constrained by an upper support extending axially from a second bucket of the second turbine stage and the hook end is radially constrained by the lower support extending axially from the second rotor wheel of the second turbine stage.

4. The system of claim 1 , wherein the upper body comprises a substantially linear sealing portion that extends from the upstream and downstream seating arms.

5. The system of claim 4 , wherein the substantially linear sealing portion comprises a plurality of sealing teeth on a side of the sealing portion opposite the lower body.

6. The system of claim 1 , wherein the interstage seal is entirely radially supported by rotor wheels of the first and second turbine stages.

Assignees

• Liotta Gary Charles
• Potter Brian Denver
• Gen Electric

Inventors

• Liotta Gary Charles
• Potter Brian Denver

Classifications

• F01D11/001 Primary

  for sealing space between stator blade and rotor · CPC title

• F01D11/02

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title