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Title: Method and system to facilitate sealing in gas turbines

Patent ·
OSTI ID:1390171

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.

Research Organization:
General Electric Co., Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company
Patent Number(s):
9,759,081
Application Number:
14/049,020
OSTI ID:
1390171
Resource Relation:
Patent File Date: 2013 Oct 08
Country of Publication:
United States
Language:
English

References (24)

Turbomachine stator interstage seal patent December 1977
Slip joint assembly for a split ring seal patent May 1986
Gas-path leakage seal for a gas turbine patent August 1997
Gas-path leakage seal for a turbine patent August 1999
Interstage van seal apparatus patent June 2000
Removable inner turbine shell with bucket tip clearance control patent July 2000
Seal apparatus for rotary machines patent November 2001
Supplemental seal for the chordal hinge seal in a gas turbine patent August 2003
Supplemental seal for the chordal hinge seal in a gas turbine patent October 2003
Cloth seal for an inner compressor discharge case and methods of locating the seal in situ patent November 2003
Seal element for sealing a gap and combustion turbine having a seal element patent January 2004
Turbine installation patent March 2004
System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor patent August 2006
Turboshaft engine comprising two elements connected to each other with the interposition of a seal patent November 2006
Gas turbine having a sealing structure patent June 2009
Seal assembly 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

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