Segmented annular combustion system with dual fuel capability

Berry, Jonathan Dwight; Widener, Stanley Kevin; Hughes, Michael John; Flanagan, James Scott

Title: Segmented annular combustion system with dual fuel capability

Abstract

A segmented annular combustion system with dual fuel capability includes an alternating arrangement of fuel injection modules and integrated combustor nozzles. The fuel injection module includes a bundled tube fuel nozzle portion and fuel injection lances, which are fluidly coupled via conduits to respective fuel plenums. A liquid fuel cartridge is disposed within the bundled tube fuel nozzle portion, within one of the plurality of fuel injection lances, or within both the bundled tube fuel nozzle portion and one of the plurality of fuel injection lances. A gas turbine having the segmented annular combustion system is also provided.

Inventors:: Berry, Jonathan Dwight; Widener, Stanley Kevin; Hughes, Michael John; Flanagan, James Scott

Issue Date:: 2020-11-10

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

Sponsoring Org.:: USDOE

OSTI Identifier:: 1771607

Patent Number(s):: 10830442

Application Number:: 15/464,400

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
F23R3/286 - {having fuel-air premixing devices
F23R3/34 - Feeding into different combustion zones
F23R3/346 - {for staged combustion}
F23R3/36 - Supply of different fuels
F23R3/46 - Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings

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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

Citation Formats


                    Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, and Flanagan, James Scott. Segmented annular combustion system with dual fuel capability.  United States: N. p., 2020. 
        Web.

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                    Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, & Flanagan, James Scott. Segmented annular combustion system with dual fuel capability.  United States.

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                    Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, and Flanagan, James Scott. Tue .  
        "Segmented annular combustion system with dual fuel capability".  United States.  https://www.osti.gov/servlets/purl/1771607.

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@article{osti_1771607,

  title        = {Segmented annular combustion system with dual fuel capability},

  author       = {Berry, Jonathan Dwight and Widener, Stanley Kevin and Hughes, Michael John and Flanagan, James Scott},

  abstractNote = {A segmented annular combustion system with dual fuel capability includes an alternating arrangement of fuel injection modules and integrated combustor nozzles. The fuel injection module includes a bundled tube fuel nozzle portion and fuel injection lances, which are fluidly coupled via conduits to respective fuel plenums. A liquid fuel cartridge is disposed within the bundled tube fuel nozzle portion, within one of the plurality of fuel injection lances, or within both the bundled tube fuel nozzle portion and one of the plurality of fuel injection lances. A gas turbine having the segmented annular combustion system is also provided.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {2020},

  month        = {11}

}

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Fuel injection module for segmented annular combustion system

Patent Berry, Jonathan Dwight; Hughes, Michael John; Flanagan, James Scott

The present disclosure is directed to a fuel injection module for a segmented annular combustion system. The fuel injection module includes a housing body, a fuel nozzle portion, and at least one fuel injection lance. The fuel nozzle portion is fluidly coupled to a fuel nozzle plenum within the housing body, and the at least one fuel injection lance is fluidly coupled to an injector fuel plenum within the housing body. In some cases, the fuel nozzle portion is a bundled tube fuel nozzle having one or more subsets of tubes. The fuel injection lances are positioned along a radialmore » « less
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Radially stacked fuel injection module for a segmented annular combustion system

Patent Berry, Jonathan Dwight; Hughes, Michael John

The present disclosure is directed to a radially stacked fuel injection module for a segmented annular combustion system. The fuel injection module includes a bundled tube fuel nozzle portion and a plurality of fuel injection lances. In one instance, a first set of fuel injection lances and a second set of fuel injection lances share a housing with the bundled tube fuel nozzle. The first and second sets of fuel injection lances are radially stacked, each set of lances being in communication with a respective injector fuel plenum. The fuel injection lances deliver fuel to a respective premixing channel formedmore » « less
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Segmented annular combustion system

Patent Berry, Jonathan Dwight; Hughes, Michael John

The present disclosure is directed to a segmented annular combustion system including a first panel fuel injector including a premix air plenum, a fuel plenum, and a plurality of first side premixing channels, where each first side premixing channel is in fluid communication with the premix air plenum, the fuel plenum, and a respective first side injection aperture of a plurality of first side injection apertures. A second panel fuel injector is circumferentially spaced from the first panel fuel injector and includes a premix air plenum, a fuel plenum, and a plurality of second side premixing channels where each secondmore » « less
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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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Title: Segmented annular combustion system with dual fuel capability

Abstract

Citation Formats

Secondary fuel delivery system patent, February 2010

System and Method Having Multi-tube Fuel Nozzle with Multiple Fuel Injectors patent-application, November 2014

Combustion chamber construction patent, September 1986

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

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

Modular Transvane Assembly patent-application, April 2010

Gas turbine combustor transition patent, May 1999

Hollow Structure with Flange patent-application, July 2003

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

Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine patent, May 2016

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

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

Transition duct with enhanced profile optimization patent, November 2003

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

Cooled gas turbine transition duct patent, December 2007

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

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

Gas turbine and operating method thereof patent, February 2016

Segmented annular combustor patent, June 1979

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

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

System and method having multi-tube fuel nozzle with multiple fuel injectors patent, September 2017

Gas turbine engine combustion chambers patent, February 1983

Steam cooled rich-burn combustor liner patent, April 1989

Catalytic combustor cooling tube vibration dampening device patent-application, March 2003

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

Spiral cooled fuel nozzle patent, September 2012

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

Aerodynamically Enhanced Fuel Nozzle patent-application, June 2012

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

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

Gas turbine plant with combustor cooling system patent, September 2000

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

Late Lean Injection Manifold Mixing System patent-application, June 2015

Side seal for combustor transitions patent, February 2002

Apparatus and method for controlling the secondary injection of fuel patent, March 2013

Impingement cooled transition duct patent, January 1988

Bolted gas turbine combustor transition coupling patent, September 2000

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

Method and apparatus for cooling combustor liner and transition piece of a gas turbine patent, March 2006

Dilution pole combustor and method patent, August 1993

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

Piping support of gas turbine steam cooled combustor patent, February 2003

Duplex turbine shroud patent, January 2012

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

Method of steam cooling thermally highly loaded units of a gas-turbine group patent, July 2000

Sector airflow variable geometry combustor patent, January 1988

Apparatus and method for improving combustion stability patent, September 2006

Effusion cooled transition duct patent, May 2003

Aerodynamically enhanced fuel nozzle patent, March 2013

Cooled heat shield for gas turbine combustor patent, August 2001

Integral aft seal for turbine applications patent, September 2002

Segmented annular combustor patent, January 2011

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

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

Removable diffusion stage for gas turbine engine fuel nozzle assemblages patent, April 2010

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

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

Repair method for a gas turbine patent, April 2003

Thermal spreading combustion liner patent, October 1999

Gas turbine aerofoil patent, June 2006

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

Pilot nozzle heat shield having connected tangs patent, February 2008

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

Combustor assembly in a gas turbine engine patent, February 2013

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

Combustor patent, March 1994

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

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

Steam cooled gas turbine system patent, August 2000

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

Combustor dome heat shield patent, July 1989

Support system for a pilot nozzle of a turbine engine patent, April 2007

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

Annular combustor with outer transition liner cooling patent, August 1993

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

Secondary fuel delivery system
patent, February 2010

System and Method Having Multi-tube Fuel Nozzle with Multiple Fuel Injectors
patent-application, November 2014

Combustion chamber construction
patent, September 1986

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

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

Modular Transvane Assembly
patent-application, April 2010

Gas turbine combustor transition
patent, May 1999

Hollow Structure with Flange
patent-application, July 2003

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

Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine
patent, May 2016

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

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

Transition duct with enhanced profile optimization
patent, November 2003

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

Cooled gas turbine transition duct
patent, December 2007

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

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

Gas turbine and operating method thereof
patent, February 2016

Segmented annular combustor
patent, June 1979

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

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

System and method having multi-tube fuel nozzle with multiple fuel injectors
patent, September 2017

Gas turbine engine combustion chambers
patent, February 1983

Steam cooled rich-burn combustor liner
patent, April 1989

Catalytic combustor cooling tube vibration dampening device
patent-application, March 2003

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

Spiral cooled fuel nozzle
patent, September 2012

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

Aerodynamically Enhanced Fuel Nozzle
patent-application, June 2012

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

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

Gas turbine plant with combustor cooling system
patent, September 2000

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

Late Lean Injection Manifold Mixing System
patent-application, June 2015

Side seal for combustor transitions
patent, February 2002

Apparatus and method for controlling the secondary injection of fuel
patent, March 2013

Impingement cooled transition duct
patent, January 1988

Bolted gas turbine combustor transition coupling
patent, September 2000

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

Method and apparatus for cooling combustor liner and transition piece of a gas turbine
patent, March 2006

Dilution pole combustor and method
patent, August 1993

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

Piping support of gas turbine steam cooled combustor
patent, February 2003

Duplex turbine shroud
patent, January 2012

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

Method of steam cooling thermally highly loaded units of a gas-turbine group
patent, July 2000

Sector airflow variable geometry combustor
patent, January 1988

Apparatus and method for improving combustion stability
patent, September 2006

Effusion cooled transition duct
patent, May 2003

Aerodynamically enhanced fuel nozzle
patent, March 2013

Cooled heat shield for gas turbine combustor
patent, August 2001

Integral aft seal for turbine applications
patent, September 2002

Segmented annular combustor
patent, January 2011

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

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

Removable diffusion stage for gas turbine engine fuel nozzle assemblages
patent, April 2010

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

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

Repair method for a gas turbine
patent, April 2003

Thermal spreading combustion liner
patent, October 1999

Gas turbine aerofoil
patent, June 2006

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

Pilot nozzle heat shield having connected tangs
patent, February 2008

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

Combustor assembly in a gas turbine engine
patent, February 2013

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

Combustor
patent, March 1994

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

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

Steam cooled gas turbine system
patent, August 2000

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

Combustor dome heat shield
patent, July 1989

Support system for a pilot nozzle of a turbine engine
patent, April 2007

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

Annular combustor with outer transition liner cooling
patent, August 1993

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

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

Combustion Chamber Clustering Structure
patent, April 1972

Transition piece external frame support
patent, June 1998