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Title: Leaf seal for transition duct in turbine system

Abstract

A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a leaf seal contacting the interface member to provide a seal between the interface member and the turbine section.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1084327
Patent Number(s):
8459041
Application Number:
13/292,366
Assignee:
General Electric Company (Schenectady, NY)
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
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Flanagan, James Scott, LeBegue, Jeffrey Scott, McMahan, Kevin Weston, Dillard, Daniel Jackson, and Pentecost, Ronnie Ray. Leaf seal for transition duct in turbine system. United States: N. p., 2013. Web.
Flanagan, James Scott, LeBegue, Jeffrey Scott, McMahan, Kevin Weston, Dillard, Daniel Jackson, & Pentecost, Ronnie Ray. Leaf seal for transition duct in turbine system. United States.
Flanagan, James Scott, LeBegue, Jeffrey Scott, McMahan, Kevin Weston, Dillard, Daniel Jackson, and Pentecost, Ronnie Ray. Tue . "Leaf seal for transition duct in turbine system". United States. https://www.osti.gov/servlets/purl/1084327.
@article{osti_1084327,
title = {Leaf seal for transition duct in turbine system},
author = {Flanagan, James Scott and LeBegue, Jeffrey Scott and McMahan, Kevin Weston and Dillard, Daniel Jackson and Pentecost, Ronnie Ray},
abstractNote = {A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a leaf seal contacting the interface member to provide a seal between the interface member and the turbine section.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jun 11 00:00:00 EDT 2013},
month = {Tue Jun 11 00:00:00 EDT 2013}
}

Works referenced in this record:

Transition with a linear flow path with exhaust mouths for use in a gas turbine engine
patent-application, February 2010


Supplemental seal for the chordal hinge seal in a gas turbine
patent, March 2003


Transition with a linear flow path for use in a gas turbine engine
patent-application, February 2010


Canted Outlet for Transition in a Gas Turbine Engine
patent-application, February 2010


Interstage van seal apparatus
patent, June 2000


Leaf seal for inner and outer casings of a turbine
patent, August 2002


Three degrees of freedom aft mounting system for gas turbine transition duct
patent, September 2002


Transition piece external frame support
patent, June 1998


Support system for transition ducts
patent, September 2009


Gas turbine diffuser
patent, January 1997


Segmented Annular Sealing Ring and Method of Its Manufacture
patent, November 1968


Transition duct mounting system
patent, December 2003


Tangentially aligned pre-mixing combustion chamber for a gas turbine
patent, March 2001


Combustor liner support and seal assembly
patent, February 2002


Mount Device for Transition Duct in Turbine System
patent-application, December 2012


Gas turbine vane assembly seal and support system
patent, September 1992


Combustor mounting for gas turbine engine
patent, September 2002


Turbine nozzle seal arrangement
patent, October 1993


Tangential Combustor
patent-application, October 2011


Seal assembly
patent, August 1994


Profile matched diffuser
patent, January 1992


Low strain shroud for a turbine technical field
patent, May 2000


Structural Attachment System for Transition Duct Outlet
patent-application, July 2010


Turbine nozzle
patent, November 1978


Transition duct assembly
patent, December 2012


Seal between static turbine parts
patent, August 2002


Methods and apparatuses for assembling a gas turbine engine
patent, December 2009


Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
patent, May 2005


Seal
patent, March 2001


Combustion transition duct providing stage 1 tangential turning for turbine engines
patent, May 2010


Leaf seals
patent, June 1992


Integrated Combustor and Stage 1 Nozzle in a Gas Turbine and Method
patent-application, May 2010


Load Member For Transition Duct In Turbine System
patent-application, December 2012


Rolling contact mounting arrangement for a ceramic combustor
patent, October 1995


Multi-axial pivoting combustor liner in gas turbine engine
patent, March 2006


Diffuser for gas turbine engine
patent, February 2007


Integrated duct diffuser
patent, October 2002


Gas-path leakage seal for a turbine
patent, August 1999