Gas turbine engine and seal assembly therefore

Patent metadata

Field	Value
Publication number	US-10066496-B2
Application number	US-201514593979-A
Country	US
Kind code	B2
Filing date	Jan 9, 2015
Priority date	Mar 27, 2014
Publication date	Sep 4, 2018
Grant date	Sep 4, 2018

Abstract

The present disclosure relates generally to a hydrostatic advanced low leakage seal having a shoe supported by at least one beam. An anti-vibration seal is disposed in contact with beam and operative to mitigate an externally induced vibratory response of the beam.

First claim

What is claimed:

1. A seal assembly disposed between a stator and a rotor, the seal assembly comprising:
a hydrostatic advanced low leakage seal including:
a base;
at least one shoe;
a u-shaped plate defining an interior cavity, the u-shaped plate being disposed between the base and the stator;
at least one beam operatively coupling the at least one shoe to the at least one base, wherein the base and the at least one beam are disposed within the interior cavity;
wherein the base is operatively coupled to one of the stator and the rotor;
a first anti-vibration seal disposed in contact with at least one of the at least one beam that mitigates an externally induced vibratory response of the at least one of the at least one beam;
a spacer operatively disposed between the first anti-vibration seal and the u-shaped plate, wherein the spacer maintains the first anti-vibration seal in contact with at least one of the at least one beam; and
a second anti-vibration seal that is in contact with the at least one shoe, wherein the second anti-vibration seal mitigates an externally induced vibratory response of the at least one shoe, wherein the second anti-vibration seal is operatively disposed between the spacer and the u-shaped plate.

2. The seal assembly of claim 1 , wherein the base is operatively coupled to the stator.

3. The seal assembly of claim 1 , wherein the first anti-vibration seal comprises a brush seal.

4. The seal assembly of claim 1 , wherein the first anti-vibration seal extends circumferentially around a longitudinal axis of the stator and the rotor and contains a gap therein.

5. The seal assembly of claim 1 , wherein the spacer is in contact with at least a portion of the base.

6. The seal assembly of claim 1 , wherein the second anti-vibration seal comprises a brush seal.

7. The seal assembly of claim 1 , wherein the at least one beam comprises two beams.

8. A gas turbine engine comprising:
a compressor section, a combustor section and a turbine section in serial flow communication, at least one of the compressor section and turbine section including a stator, a rotor, and
a seal assembly, the seal assembly comprising:
a hydrostatic advanced low leakage seal including:
a base;
at least one shoe;
a u-shaped plate defining an interior cavity, the u-shaped plate disposed between the base and the stator;
at least one beam operatively coupling the at least one shoe to the at least one base, wherein the base and the at least one beam are disposed within the cavity;
wherein the base is operatively coupled to one of the stator and the rotor;
a first anti-vibration seal disposed in contact with at least one of the at least one beam that mitigates an externally induced vibratory response of the at least one of the at least one beam;
a spacer operatively disposed between the first anti-vibration seal and the u-shaped plate, wherein the spacer maintains the first anti-vibration seal in contact with at least one of the at least one beam; and
a second anti-vibration seal that is in contact with the at least one shoe, wherein the second anti-vibration seal mitigates an externally induced vibratory response of the at least one shoe, wherein the second anti-vibration seal is operatively disposed between the spacer and the u-shaped plate.

9. The gas turbine engine of claim 8 , wherein the base is operatively coupled to the stator.

10. The gas turbine engine of claim 8 , wherein the first anti-vibration seal comprises a brush seal.

11. The gas turbine engine of claim 8 , wherein the first anti-vibration seal extends circumferentially around a longitudinal axis of the stator and the rotor and contains a gap therein.

12. The gas turbine engine of claim 8 , wherein the spacer is in contact with at least a portion of the base.

13. The gas turbine engine of claim 8 , wherein the second anti-vibration seal comprises a brush seal.

14. The gas turbine engine of claim 8 , wherein the at least one beam comprises two beams.

Assignees

• United Technologies Corp

Inventors

• Schmitz John T

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

• F05D2240/56

  Brush seals · CPC title

• F05D2250/75

  given by its similarity to a letter, e.g. T-shaped · CPC title

• F01D1/04

  traversed by the working-fluid substantially axially · CPC title