Mounting of integrated combustor nozzles in a segmented annular combustion system

Berry, Jonathan Dwight; Hughes, Michael John; McMahan, Kevin Weston

Title: Mounting of integrated combustor nozzles in a segmented annular combustion system

Abstract

A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. An aft end portion of the fuel injection panel defines a turbine nozzle. One or more hook plates attached to the outer surfaces of the liner segments are used to mount the integrated combustor nozzle to an inner mounting ring or an outer mounting ring. A mounting strut or mounting tenon(s) attached to the liner segments may also be employed.

Inventors:: Berry, Jonathan Dwight; Hughes, Michael John; McMahan, Kevin Weston

Issue Date:: Tue Mar 10 00:00:00 EDT 2020

Research Org.:: General Electric Co., Schenectady, NY (United States)

Sponsoring Org.:: USDOE

OSTI Identifier:: 1637866

Patent Number(s):: 10584880

Application Number:: 15/464,443

Assignee:: General Electric Company (Schenectady, NY)

Patent Classifications (CPCs):: F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS

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F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
F23R2900/00001 - Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses
F23R3/002 - {Wall structures
F23R3/283 - {Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances}
F23R3/286 - {having fuel-air premixing devices
F23R3/34 - Feeding into different combustion zones
F23R3/346 - {for staged combustion}
F23R3/46 - Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings
F23R3/50 - Combustion chambers comprising an annular flame tube within an annular casing
F23R3/60 - Support structures

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DOE Contract Number:: FE0023965

Resource Type:: Patent

Resource Relation:: Patent File Date: 03/21/2017

Country of Publication:: United States

Language:: English

Subject:: 33 ADVANCED PROPULSION SYSTEMS

Citation Formats


                    Berry, Jonathan Dwight, Hughes, Michael John, and McMahan, Kevin Weston. Mounting of integrated combustor nozzles in a segmented annular combustion system.  United States: N. p., 2020. 
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                    Berry, Jonathan Dwight, Hughes, Michael John, & McMahan, Kevin Weston. Mounting of integrated combustor nozzles in a segmented annular combustion system.  United States.

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                    Berry, Jonathan Dwight, Hughes, Michael John, and McMahan, Kevin Weston. Tue .  
        "Mounting of integrated combustor nozzles in a segmented annular combustion system".  United States.  https://www.osti.gov/servlets/purl/1637866.

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@article{osti_1637866,

  title        = {Mounting of integrated combustor nozzles in a segmented annular combustion system},

  author       = {Berry, Jonathan Dwight and Hughes, Michael John and McMahan, Kevin Weston},

  abstractNote = {A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. An aft end portion of the fuel injection panel defines a turbine nozzle. One or more hook plates attached to the outer surfaces of the liner segments are used to mount the integrated combustor nozzle to an inner mounting ring or an outer mounting ring. A mounting strut or mounting tenon(s) attached to the liner segments may also be employed.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {Tue Mar 10 00:00:00 EDT 2020},

  month        = {Tue Mar 10 00:00:00 EDT 2020}

}

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Cooling of integrated combustor nozzle of segmented annular combustion system

Patent Berry, Jonathan Dwight; Widener, Stanley Kevin; Hughes, Michael John

A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. The fuel injection panel includes an aft end portion, a first side wall, a second side wall, premixing channels defined between the first side wall and the side wall, and injection outlets defined along at least one of the first side wall and the second side wall. The aft end portion defines a turbine nozzle portion. An interior portion between the first side wall and the second side wall includes wallsmore » « less
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Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system

Patent Berry, Jonathan Dwight; Hughes, Michael John

A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. The fuel injection panel includes an aft end portion, a first side wall, a second side wall, premixing channels defined between the first side wall and the side wall, and injection outlets defined along at least one of the first side wall and the second side wall. The aft end portion defines a turbine nozzle portion. An interior portion between the first side wall and the second side wall includes wallsmore » « less
Full Text Available
Integrated combustor nozzle for a segmented annular combustion system

Patent Berry, Jonathan Dwight; Widener, Stanley Kevin; Hughes, Michael John; ...

The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbinemore » nozzle. « less
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Integrated combustor nozzles with continuously curved liner segments

Patent Berry, Jonathan Dwight; Hughes, Michael John; DeForest, Russell Pierson; ...

An integrated combustor nozzle includes an inner liner segment; an outer liner segment; and a panel extending radially between the inner and outer liner segments. The panel includes a forward end, an aft end, and a side walls extending axially from the forward end to the aft end. The aft end defines a turbine nozzle having a trailing edge circumferentially offset from the forward end. The inner liner segment has a pair of sealing surfaces, each of which defines a first continuous curve in the circumferential direction. The outer liner segment has a pair of sealing surfaces, each of whichmore » « less
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Segmented annular combustion system with axial fuel staging

Patent Berry, Jonathan Dwight; Widener, Stanley Kevin; Hughes, Michael John; ...

A segmented annular combustion system includes an alternating arrangement of fuel nozzles and integrated combustor nozzles. The fuel nozzles deliver fuel to the primary combustion zones. The integrated combustor nozzles include an inner liner segment, an outer liner segment, and a fuel injection panel extending between the liner segments. The fuel injection panel includes injection outlets on one or both side walls to deliver a combustible mixture to the secondary combustion zones. Each fuel injection panel, which provides a boundary between adjacent primary and secondary combustion zones, includes an aft end that defines a turbine nozzle. The segmented annular combustionmore » system is part of a gas turbine. « less
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Title: Mounting of integrated combustor nozzles in a segmented annular combustion system

Abstract

Citation Formats

Gas turbine engine combustor patent, May 2016

Aft mounting system for combustion transition duct members patent, December 1983

Cooling air recycling for gas turbine transition duct end frame and related method patent, July 2002

Methods and apparatus for cooling gas turbine nozzles patent, March 2009

Gas turbine and operating method thereof patent, February 2016

Transition duct with enhanced profile optimization patent, November 2003

Annular combustor with outer transition liner cooling patent, August 1993

Cooling structure for recovery-type air-cooled gas turbine combustor patent, December 2016

Spiral cooled fuel nozzle patent, September 2012

Lean Direct Injection Atomizer for Gas Turbine Engines patent-application, November 2006

Secondary fuel delivery system patent, February 2010

Gas turbine combustor transition duct forced convection cooling patent, February 1990

Gas turbine combustor transition patent, May 1999

Annular premix section for dry low-NO.sub.x combustors patent, July 2000

Segmented annular combustor patent, June 1979

Precision counter-swirl combustor patent, November 2013

Combustor assembly in a gas turbine engine patent, February 2013

Gas turbine steam-cooled combustor with alternately counter-flowing steam passages patent, October 2002

Cooled gas turbine transition duct patent, December 2007

Annular Wall of a Combustion Chamber with Improved Cooling at the Level of Primary and/or Dilution Holes patent-application, September 2014

Combustor assembly in a gas turbine engine patent, April 2015

Static Seal Structure patent, August 1973

Combustor liner cooling system patent, August 2013

One-piece combustor cowl patent, July 1999

Combustion Apparatus patent, April 1972

Fuel Atomization Dual Orifice Fuel Nozzle patent-application, June 2012

Cooled transition duct for a gas turbine engine patent, September 2011

Thermal spreading combustion liner patent, October 1999

Combustion Chamber Clustering Structure patent, April 1972

Cooled heat shield for gas turbine combustor patent, August 2001

Cooling Flowpath Dirt Deflector in Fuel Nozzle patent-application, June 2012

Annular one-piece corrugated liner for combustor of a gas turbine engine patent-application, October 2003

Aerodynamically Enhanced Fuel Nozzle patent-application, June 2012

Combustor dome heat shield patent, July 1989

Combustor of gas turbine with features for vibration reduction and increased cooling patent, November 1981

Transition piece external frame support patent, June 1998

Mixing ducts for a gas-turbine annular combustion chamber patent, November 1998

Transition duct cooling feed tubes patent, April 2012

Combustor for a low-emissions gas turbine engine patent, August 2000

Combustor patent, March 1994

Air/fuel supply system for use in a gas turbine engine patent, June 2014

Gas turbine engine having an improved transition duct support patent, April 1977

Repair method for a gas turbine patent, April 2003

Lean Direct Injection Atomizer for Gas Turbine Engines patent-application, November 2010

Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element patent, November 1983

Fuel injector for use in a gas turbine engine patent, October 2012

Combustion Chamber of a Combustor for a Gas Turbine patent-application, December 2014

Segmented Annular Combustor patent-application, March 2010

Steam cooled rich-burn combustor liner patent, April 1989

Integral aft seal for turbine applications patent, September 2002

Impingement jets coupled to cooling channels for transition cooling patent, February 2011

Steam cooled gas turbine system patent, August 2000

Segmented annular combustor patent, January 2011

Modular Transvane Assembly patent-application, April 2010

Combustor For Gas Turbine Engine patent-application, April 2007

Protection of an Integrated Circuit and Method Thereof patent-application, August 2008

Compressed air steam generator for cooling combustion turbine transition section patent, October 2001

Gas turbine plant with combustor cooling system patent, September 2000

Tangential Combustor with Vaneless Turbine for Use on Gas Turbine Engines patent-application,

Burner and method for reducing combustion humming during operation patent, April 2002

Effusion cooled transition duct patent, May 2003

Aerodynamically enhanced fuel nozzle patent, March 2013

Bolted gas turbine combustor transition coupling patent, September 2000

Fuel heating system used in conjunction with steam cooled combustors and transitions patent, October 1998

Power Plant Combustion Apparatus Having Apertured Combustion Chamber Walls patent, May 1952

Side seal for combustor transitions patent, February 2002

Impingement cooled transition duct patent, January 1988

Hollow Structure with Flange patent-application, July 2003

Gas Turbine Combustion Apparatus {Text Available in USOCR Database] patent, March 1969

Attachment device for removable components in hot gas paths in a turbine engine patent, February 2008

Combustion chamber construction patent, September 1986

Thermally free aft frame for a transition duct patent, September 2003

Liquid-cooled transition member to turbine inlet patent, April 1980

Transition piece for non-annular gas turbine combustion chambers patent-application, September 2003

Method and apparatus to enhance transition duct cooling in a gas turbine engine patent, October 2013

Gas turbine aerofoil patent, June 2006

Combuster Liner patent-application, July 2016

Gas turbine engine combustor
patent, May 2016

Aft mounting system for combustion transition duct members
patent, December 1983

Cooling air recycling for gas turbine transition duct end frame and related method
patent, July 2002

Methods and apparatus for cooling gas turbine nozzles
patent, March 2009

Gas turbine and operating method thereof
patent, February 2016

Transition duct with enhanced profile optimization
patent, November 2003

Annular combustor with outer transition liner cooling
patent, August 1993

Cooling structure for recovery-type air-cooled gas turbine combustor
patent, December 2016

Spiral cooled fuel nozzle
patent, September 2012

Lean Direct Injection Atomizer for Gas Turbine Engines
patent-application, November 2006

Secondary fuel delivery system
patent, February 2010

Gas turbine combustor transition duct forced convection cooling
patent, February 1990

Gas turbine combustor transition
patent, May 1999

Annular premix section for dry low-NO.sub.x combustors
patent, July 2000

Segmented annular combustor
patent, June 1979

Precision counter-swirl combustor
patent, November 2013

Combustor assembly in a gas turbine engine
patent, February 2013

Gas turbine steam-cooled combustor with alternately counter-flowing steam passages
patent, October 2002

Cooled gas turbine transition duct
patent, December 2007

Annular Wall of a Combustion Chamber with Improved Cooling at the Level of Primary and/or Dilution Holes
patent-application, September 2014

Combustor assembly in a gas turbine engine
patent, April 2015

Static Seal Structure
patent, August 1973

Combustor liner cooling system
patent, August 2013

One-piece combustor cowl
patent, July 1999

Combustion Apparatus
patent, April 1972

Fuel Atomization Dual Orifice Fuel Nozzle
patent-application, June 2012

Cooled transition duct for a gas turbine engine
patent, September 2011

Thermal spreading combustion liner
patent, October 1999

Combustion Chamber Clustering Structure
patent, April 1972

Cooled heat shield for gas turbine combustor
patent, August 2001

Cooling Flowpath Dirt Deflector in Fuel Nozzle
patent-application, June 2012

Annular one-piece corrugated liner for combustor of a gas turbine engine
patent-application, October 2003

Aerodynamically Enhanced Fuel Nozzle
patent-application, June 2012

Combustor dome heat shield
patent, July 1989

Combustor of gas turbine with features for vibration reduction and increased cooling
patent, November 1981

Transition piece external frame support
patent, June 1998

Mixing ducts for a gas-turbine annular combustion chamber
patent, November 1998

Transition duct cooling feed tubes
patent, April 2012

Combustor for a low-emissions gas turbine engine
patent, August 2000

Combustor
patent, March 1994

Air/fuel supply system for use in a gas turbine engine
patent, June 2014

Gas turbine engine having an improved transition duct support
patent, April 1977

Repair method for a gas turbine
patent, April 2003

Lean Direct Injection Atomizer for Gas Turbine Engines
patent-application, November 2010

Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element
patent, November 1983

Fuel injector for use in a gas turbine engine
patent, October 2012

Combustion Chamber of a Combustor for a Gas Turbine
patent-application, December 2014

Segmented Annular Combustor
patent-application, March 2010

Steam cooled rich-burn combustor liner
patent, April 1989

Integral aft seal for turbine applications
patent, September 2002

Impingement jets coupled to cooling channels for transition cooling
patent, February 2011

Steam cooled gas turbine system
patent, August 2000

Segmented annular combustor
patent, January 2011

Modular Transvane Assembly
patent-application, April 2010

Combustor For Gas Turbine Engine
patent-application, April 2007

Protection of an Integrated Circuit and Method Thereof
patent-application, August 2008

Compressed air steam generator for cooling combustion turbine transition section
patent, October 2001

Gas turbine plant with combustor cooling system
patent, September 2000

Tangential Combustor with Vaneless Turbine for Use on Gas Turbine Engines
patent-application,

Burner and method for reducing combustion humming during operation
patent, April 2002

Effusion cooled transition duct
patent, May 2003

Aerodynamically enhanced fuel nozzle
patent, March 2013

Bolted gas turbine combustor transition coupling
patent, September 2000

Fuel heating system used in conjunction with steam cooled combustors and transitions
patent, October 1998

Power Plant Combustion Apparatus Having Apertured Combustion Chamber Walls
patent, May 1952

Side seal for combustor transitions
patent, February 2002

Impingement cooled transition duct
patent, January 1988

Hollow Structure with Flange
patent-application, July 2003

Gas Turbine Combustion Apparatus {Text Available in USOCR Database]
patent, March 1969

Attachment device for removable components in hot gas paths in a turbine engine
patent, February 2008

Combustion chamber construction
patent, September 1986

Thermally free aft frame for a transition duct
patent, September 2003

Liquid-cooled transition member to turbine inlet
patent, April 1980

Transition piece for non-annular gas turbine combustion chambers
patent-application, September 2003

Method and apparatus to enhance transition duct cooling in a gas turbine engine
patent, October 2013

Gas turbine aerofoil
patent, June 2006

Combuster Liner
patent-application, July 2016

Bled diffuser fed secondary combustion system for gas turbines
patent, February 2013

Flame Tube Having Telescoping Walls with Fluted Ends to Admit Air
patent, January 1953

Bled diffuser fed secondary combustion system for gas turbines
patent-application, July 2011