Expansion joint and methods of assembling the same

Patent metadata

Field	Value
Publication number	US-10830103-B2
Application number	US-201815994375-A
Country	US
Kind code	B2
Filing date	May 31, 2018
Priority date	Jul 5, 2017
Publication date	Nov 10, 2020
Grant date	Nov 10, 2020

Abstract

An expansion joint for use between a turbine duct and a diffuser duct includes a first flange coupled to the turbine duct, a second flange coupled to the diffuser duct, and a flexible element positioned between and coupled to the first flange of the turbine duct and the second flange of the diffuser duct. The flexible element defines a trough for receiving a liquid therein. The trough includes a drain pipe configured to channel the liquid away from the trough.

First claim

What is claimed is:

1. An expansion joint for use between a turbine duct and a diffuser duct, said expansion joint comprising:
a first flange coupled to the turbine duct;
a second flange coupled to the diffuser duct; and
a flexible element positioned between and coupled to said first flange of the turbine duct and said second flange of the diffuser duct, said flexible element defining a trough for receiving a liquid therein, said trough comprising a drain pipe configured to channel the liquid away from said trough;
wherein said flexible element comprises a plurality of flexible seals coupled to said first flange and said second flange; and
wherein each flexible seal of said plurality of flexible seals is formed from a single sheet component and comprises a curved profile shape comprising a radius configured to optimize a low cycle fatigue of the expansion joint.

2. The expansion joint in accordance with claim 1 , wherein said each flexible seal of said plurality of flexible seals comprises a plurality of apertures therein.

3. The expansion joint in accordance with claim 1 , wherein said plurality of flexible seals comprises a first layer of flexible seals forming a first complete circumferential array, and a second layer of flexible seals forming a second complete circumferential array; and wherein each flexible seal of said second layer of flexible seals overlaps a radial seam defined between adjacent flexible seals of said first layer of flexible seals.

4. The expansion joint in accordance with claim 3 , wherein said plurality of flexible seals further comprises a third layer of flexible seals forming a third complete circumferential array, wherein each flexible seal of said third layer of flexible seals overlaps a radial seam defined between adjacent flexible seals of said second layer of flexible seals.

5. The expansion joint in accordance with claim 3 , further comprising a gasket positioned between at least one flexible seal of said first layer of flexible seals and at least one flexible seal of said second layer of flexible seals.

6. The expansion joint in accordance with claim 1 , wherein said flexible element comprises at least one of a nickel based alloy and stainless steel.

7. A gas turbine engine comprising:
a turbine duct comprising a first flange coupled to a downstream portion of said turbine duct;
a diffuser duct comprising a second flange coupled to an upstream portion of said diffuser duct; and
an expansion joint extending between said turbine duct and said diffuser duct, said expansion joint comprising a plurality of flexible seals coupled to said first flange and said second flange, said expansion joint defining a trough for receiving a liquid therein, said trough comprising a drain pipe configured to channel the liquid away from said trough;
wherein each flexible seal of said plurality of flexible seals is fabricated from a single sheet component and comprises a curved profile shape comprising a radius configured to optimize a low cycle fatigue of the expansion joint.

8. The gas turbine engine in accordance with claim 7 , wherein said each flexible seal of said plurality of flexible seals comprises a plurality of apertures therein.

9. The gas turbine engine in accordance with claim 7 , wherein said expansion joint comprises a plurality of layers of said plurality of flexible seals.

10. The gas turbine engine in accordance with claim 9 , wherein said plurality of layers comprises three layers.

11. The gas turbine engine in accordance with claim 10 , wherein said plurality of flexible seals of each layer of said plurality of layers are circumferentially offset from said plurality of flexible seals of an adjacent layer.

12. The gas turbine engine in accordance with claim 9 , further comprising a gasket positioned between at least one flexible seal of a first layer of said plurality of layers and at least one flexible seal of a second layer of plurality of layers.

13. The gas turbine engine in accordance with claim 7 , wherein said plurality of flexible seals comprise at least one of a nickel based alloy and stainless steel.

14. A method of assembling an expansion joint for use between a turbine duct and a diffuser duct, said method comprising:
coupling a first flange to the turbine duct;
coupling a second flange to the diffuser duct;
coupling a flexible element to the first flange of the turbine duct and the second flange of the diffuser duct, wherein the flexible element defines a trough for receiving a liquid therein, wherein coupling the flexible element to the first flange of the turbine duct and the second flange of the diffuser duct comprises coupling a plurality of flexible seals to the first flange of the turbine duct and the second flange of the diffuser duct; and
coupling a drain pipe to the trough to channel the liquid away from the trough; and
wherein each flexible seal of the plurality of flexible seals is formed from a single sheet component and includes a curved profile having a radius configured to optimize a low cycle fatigue of the expansion joint.

15. The method in accordance with claim 14 , wherein coupling the plurality of flexible seals comprises:
coupling a first layer of the plurality of flexible seals to the first flange of the turbine duct and the second flange of the diffuser duct forming a first complete circumferential array; and
coupling a second layer of flexible seals to the first flange of the turbine duct and the second flange of the diffuser duct forming a second complete circumferential array, wherein each flexible seal of the second layer of flexible seals overlaps a radial seam defined between adjacent flexible seals of the first layer of flexible seals.

Assignees

• Gen Electric

Inventors

• Mohammed Javeed Iqbaluddin
• Karmakar Pallab
• Kippel Bradly Aaron

Classifications

• F05D2240/55

  Seals · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• F05D2250/75

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

• F01D25/005

  Selecting particular materials · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title