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Title: Method and system to facilitate sealing in gas turbines

Abstract

A method and system for sealing between components within a gas turbine is provided. A first recess defined in a first component receives a seal member. A second recess defined in a second component adjacent the first component also receives the seal member. The first and second recesses are located proximate a hot gas path defined through the gas turbine, and define circumferential paths about the turbine axis. The seal member includes a sealing face that extends in a direction substantially parallel to the turbine axis. The seal member also includes a plurality of seal layers, wherein at least one of the seal layers includes at least one stress relief region for facilitating flexing of the first seal member.

Inventors:
; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1390171
Patent Number(s):
9759081
Application Number:
14/049,020
Assignee:
General Electric Company
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2013 Oct 08
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Morgan, Victor John, Foster, Gregory Thomas, and Sarawate, Neelesh Nandkumar. Method and system to facilitate sealing in gas turbines. United States: N. p., 2017. Web.
Morgan, Victor John, Foster, Gregory Thomas, & Sarawate, Neelesh Nandkumar. Method and system to facilitate sealing in gas turbines. United States.
Morgan, Victor John, Foster, Gregory Thomas, and Sarawate, Neelesh Nandkumar. Tue . "Method and system to facilitate sealing in gas turbines". United States. https://www.osti.gov/servlets/purl/1390171.
@article{osti_1390171,
title = {Method and system to facilitate sealing in gas turbines},
author = {Morgan, Victor John and Foster, Gregory Thomas and Sarawate, Neelesh Nandkumar},
abstractNote = {A method and system for sealing between components within a gas turbine is provided. A first recess defined in a first component receives a seal member. A second recess defined in a second component adjacent the first component also receives the seal member. The first and second recesses are located proximate a hot gas path defined through the gas turbine, and define circumferential paths about the turbine axis. The seal member includes a sealing face that extends in a direction substantially parallel to the turbine axis. The seal member also includes a plurality of seal layers, wherein at least one of the seal layers includes at least one stress relief region for facilitating flexing of the first seal member.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {9}
}

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Gas-path leakage seal for a turbine
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Removable inner turbine shell with bucket tip clearance control
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Gas turbine having a sealing structure
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patent, March 2011


Gas turbine having a sealing structure
patent-application, October 2006


Gas turbine and sealing means for a gas turbine
patent-application, February 2007


Reducing Inter-Seal Gap In Gas Turbine
patent-application, September 2010


Transition Piece Sealing Assembly
patent-application, May 2012


Cloth Seal For Turbo-Machinery
patent-application, May 2012


Assembly And Method For Preventing Fluid Flow
patent-application, July 2012


Assembly For Preventing Fluid Flow
patent-application, July 2012


Sealing Device And Method For Providing A Seal In A Turbine System
patent-application, August 2012