Labyrinth seal

Patent metadata

Field	Value
Publication number	US-9650907-B2
Application number	US-201414202571-A
Country	US
Kind code	B2
Filing date	Mar 10, 2014
Priority date	Sep 12, 2011
Publication date	May 16, 2017
Grant date	May 16, 2017

Abstract

A labyrinth seal is provided for sealing the annular interspace between the rotor and the stator of a steam turbine or gas turbine. The labyrinth seal includes a multiplicity of sealing strips which are arranged in series in the axial direction and fastened on the stator and project into the interspace. The sealing strips interact, with sealing effect, with rotor-side sealing elements which are arranged in a staggered manner. An improved sealing effect is achieved by the sealing strips in the cold installed state being offset in relation to a symmetrical position, wherein the offset has the reverse direction and the same amount as the distance by which the sealing strip is displaced relative to adjacent rotor-side sealing elements as a result of thermal expansions of the stationary and rotating components and support structure when being heated from the cold installed state to a hot steady-state operating condition.

First claim

The invention claimed is:

1. A labyrinth seal for sealing an annular interspace
between a stationary part and a rotating part of a steam turbine or gas turbine,
comprising: a multiplicity of sealing strips which are arranged in series in an axial direction, are fastened on the stationary part and project into the interspace, which sealing strips interact, with sealing effect, with rotor-side sealing elements which are arranged in a staggered manner, wherein the sealing strips in a cold installed state are offset in relation to a symmetrical position, wherein the offset has a reverse direction in a same amount as a distance by which the sealing strip is displaced relative to adjacent rotor-side sealing elements as a result of thermal expansions of a stationary support structure and rotating components when being heated from a cold installed state to a hot steady-state operating condition, and wherein during the hot steady-state operating condition the sealing strips are in a symmetrical position, with an equal distance from one sealing strip to each adjacent rotor-side sealing element; wherein the rotor-side sealing elements are formed as annular formed projections of the rotating part; an wherein an intermediate contour is arranged between the annular formed projections, the intermediate contour comprising a and rotating components when being heated from a cold installed state to a hot steady state operating condition, and wherein during the hot steady-state operating condition the sealing strips are in a symmetrical position, with an equal distance from one sealing strip to each adjacent rotor-side sealing element; wherein the rotor-side sealing elements are formed as annular formed projections of the rotating part; and wherein an intermediate contour is arranged between the annular formed projections, the intermediate contour comprising 90 degree step and a conical contour on each side of the 90 degree step and wherein the intermediate contours are separated from each other by a diameter plateau, and wherein the interspace between each of the annular formed projections is configured to receive a single sealing strip, which during steady-state operation comes to lie opposite the intermediate contour after being displaced by a resulting shift from cold to hot conditions.

2. The labyrinth seal of claim 1 , wherein the cold installed state the
distance (b) from the rotor-side sealing elements to the nearest sealing strip of the stationary part is between 0.2 and 0.8 times the distance (a) to the farther sealing strip.

3. The labyrinth seal of claim 1 , wherein the formed
projections, between two adjacent rotor-side sealing elements in each case, have a rectangular cross section and extend in the radial direction into the interspace.

4. The labyrinth seal of claim 1 , wherein transitions
between the annular formed projections and the intermediate contour are rounded.

Assignees

• Alstom Technology Ltd
• Ansaldo Energia Ip Uk Ltd

Inventors

• Bricaud Cyrille
• Steiger Ulrich Robert
• Heidecke Axel
• Simon-Delgado Carlos

Classifications

• F05D2300/50212

  dissimilar · CPC title

• F16J15/445

  with means for adjusting the clearance · CPC title

• F01D11/025

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

• F16J15/4472

  with axial path · CPC title

• F01D11/02 Primary

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