Radially stacked fuel injection module for a segmented annular combustion system

Berry, Jonathan Dwight; Hughes, Michael John

Title: Radially stacked fuel injection module for a segmented annular combustion system

Abstract

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 formed between the side walls of an integrated combustor nozzle, an aft end of which defines a turbine nozzle. In another instance, the bundled tube fuel nozzle may be provided as a radially inner fuel nozzle and a radially outer fuel nozzle, each with a respective bundled tube fuel plenum.

Inventors:: Berry, Jonathan Dwight; Hughes, Michael John

Issue Date:: 2019-12-31

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

Sponsoring Org.:: USDOE

OSTI Identifier:: 1600446

Patent Number(s):: 10520194

Application Number:: 15/464,411

Assignee:: General Electric Company (Schenectady, NY)

Patent Classifications (CPCs):: F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23D - BURNERS

F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS

Show more

F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23D - BURNERS
F23D14/62 - Mixing devices
F23D14/64 - with injectors

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
F23R3/28 - characterised by the fuel supply
F23R3/286 - {having fuel-air premixing devices
F23R3/34 - Feeding into different combustion zones
F23R3/346 - {for staged combustion}
F23R3/42 - characterised by the arrangement or form of the flame tubes or combustion chambers
F23R3/46 - Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings

Show less

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, and Hughes, Michael John. Radially stacked fuel injection module for a segmented annular combustion system.  United States: N. p., 2019. 
        Web.

Copy to clipboard


                    Berry, Jonathan Dwight, & Hughes, Michael John. Radially stacked fuel injection module for a segmented annular combustion system.  United States.

Copy to clipboard


                    Berry, Jonathan Dwight, and Hughes, Michael John. Tue .  
        "Radially stacked fuel injection module for a segmented annular combustion system".  United States.  https://www.osti.gov/servlets/purl/1600446.

Copy to clipboard


                    
@article{osti_1600446,

  title        = {Radially stacked fuel injection module for a segmented annular combustion system},

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

  abstractNote = {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 formed between the side walls of an integrated combustor nozzle, an aft end of which defines a turbine nozzle. In another instance, the bundled tube fuel nozzle may be provided as a radially inner fuel nozzle and a radially outer fuel nozzle, each with a respective bundled tube fuel plenum.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {2019},

  month        = {12}

}

Copy to clipboard

Patent:

Save / Share:

Export Metadata

Save to My Library

Works referenced in this record:

Modular combustor dome
patent, October 2001

Glynn, Christopher Charles; Halila, Ely E.; Bibler, John David
US Patent Document 6,298,667
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6298667

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

Steber, Charles E.
US Patent Document 4,422,288
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4422288

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

Cromer, Robert Harold; Bechtel, II, William Theodore; Sutcu, Maz
US Patent Document 6,412,268
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6412268

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

Powis, Andrew Charles; Clarke, Jonathan Philip; Tressler, Judd Dodge
US Patent Document RE40,658
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/RE40658

Gas turbine and operating method thereof
patent, February 2016

Mizukami, Satoshi; Ishiguro, Tatsuo; Masada, Junichiro
US Patent Document 9,255,490
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9255490

Transition duct with enhanced profile optimization
patent, November 2003

Jorgensen, Stephen W.; Resos, John C.; Xiao, Zhenhua
US Patent Document 6,644,032
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6644032

Annular combustor with outer transition liner cooling
patent, August 1993

Harris, Mark M.; Marsh, David
US Patent Document 5,237,813
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5237813

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

Mizukami, Satoshi; Ishiguro, Tatsuo; Masada, Junichiro
US Patent Document 9,512,781
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9512781

Spiral cooled fuel nozzle
patent, September 2012

Fox, Timothy A.; Schilp, Reinhard
US Patent Document 8,272,218
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8272218

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

Buelow, Philip E. O.; Williams, Brandon P.; Bretz, David H.
US Patent Application 11/399634; 20060248898
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20060248898

Secondary fuel delivery system
patent, February 2010

Parker, David M.; Cai, Weidong; Garan, Daniel W.
US Patent Document 7,665,309
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7665309

System for supporting a bundled tube fuel injector within a combustor
patent-application, January 2015

LeBegue, Jeffrey Scott; Melton, Patrick Benedict; Westmoreland, III, James Harold
US Patent Application 13/932301; 20150000286
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150000286

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

Butt, Graham P.
US Patent Document 4,903,477
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4903477

Gas turbine combustor transition
patent, May 1999

Coslow, Billy Joe; Whidden, Graydon Lane
US Patent Document 5,906,093
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5906093

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

Stokes, Mitchell O.
US Patent Document 6,082,111
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6082111

Segmented annular combustor
patent, June 1979

Reider, Samuel B.
US Patent Document 4,158,949
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4158949

Combustor assembly in a gas turbine engine
patent, February 2013

Wiebe, David J.; Fox, Timothy A.
US Patent Document 8,375,726
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8375726

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

Mandai, Shigemi; Suenaga, Kiyoshi; Tanaka, Katsunori
US Patent Document 6,463,742
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6463742

Cooled gas turbine transition duct
patent, December 2007

Marcum, Steven R.; Gill, David Alan; Slentz, Kenneth
US Patent Document 7,310,938
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7310938

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

Rullaud, Matthieu Francois; Carrere, Bernard Joseph, Jean-Pierre; Verdier, Hurbert Pascal
US Patent Application 14/352946; 20140260257
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140260257

Combustor assembly in a gas turbine engine
patent, April 2015

Wiebe, David J.; Fox, Timothy A.
US Patent Document 9,016,066
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9016066

Static Seal Structure
patent, August 1973

Adelizzi, Richard S.; Laurelli, James A.
US Patent Document 3,750,398
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3750398

System for supporting bundled tube segments within a combustor
patent-application, February 2015

Melton, Patrick Benedict
US Patent Application 13/959830; 20150040579
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150040579

Combustor liner cooling system
patent, August 2013

Lacy, Benjamin Paul; Berkman, Mert Enis
US Patent Document 8,499,566
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8499566

One-piece combustor cowl
patent, July 1999

Fortuna, Douglas Marti; Napoli, Phillip D.; Duke, Richard Allan
US Patent Document 5,924,288
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5924288

Combustion Apparatus
patent, April 1972

Huguson, Birger O.
US Patent Document 3,657,882
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3657882

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

Patel, Nayan Vinodbhai; Benjamin, Michael Anthony; Thomsen, Duane Douglas
US Patent Application 12/971597; 20120151930
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20120151930

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

Wilson, Jody W.; Nordlund, Raymond S.; Weaver, Adam J.
US Patent Document 8,015,818
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8015818

Thermal spreading combustion liner
patent, October 1999

Abuaf, Nesim; Goebel, Steven G.
US Patent Document 5,960,632
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5960632

Combustion Chamber Clustering Structure
patent, April 1972

De Corso, Serafino M.
US Patent Document 3,657,883
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3657883

Cooled heat shield for gas turbine combustor
patent, August 2001

Putz, Heinrich
US Patent Document 6,276,142
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6276142

Multi-premixer fuel nozzle
patent-application, February 2012

McMahan, Kevin Weston; Venkataraman, Krishna Kumar; Berry, Jonathan Dwight
US Patent Application 13/263995; 20120031097
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20120031097

Dual fuel mixer for gas turbine combustor
patent, April 1996

Joshi, Narendra Digamber; Ekstedt, Edward E.
US Patent Document 5,511,375
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5511375

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

Patel, Nayan Vinodbhai; Benjamin, Michael Anthony; Thomsen, Duane Douglas
US Patent Application 12/971632; 20120151928
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20120151928

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

Farmer, Gilbert; Devane, Shaun M.; Vandike, John L.
US Patent Application 10/119649; 20030192320
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20030192320

Aerodynamically Enhanced Fuel Nozzle
patent-application, June 2012

Patel, Nayan Vinodbhai; Benjamin, Michael Anthony; Thomson, Duane Douglas
US Patent Application 12/971676; 20120151929
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20120151929

Combustor dome heat shield
patent, July 1989

Clark, Jim A.
US Patent Document 4,843,825
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4843825

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

Sato, Isao; Kato, Fumio; Uchiyama, Yoshihiro
US Patent Document 4,297,843
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4297843

Transition piece external frame support
patent, June 1998

Barnes, John Eugene; Anderson, Rodger O.; Steber, Charles E.
US Patent Document 5,761,898
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5761898

Transition duct cooling feed tubes
patent, April 2012

Jennings, Stephen; Stuttaford, Peter; Jorgensen, Stephen W.
US Patent Document 8,151,570
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8151570

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

Glezer, Boris; Greenwood, Stuart A.; Dutta, Partha
US Patent Document 6,098,397
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6098397

Combustor
patent, March 1994

DuBell, Thomas L.; Shadowen, James H.
US Patent Document 5,297,385
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5297385

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

Fox, Timothy A.; Schilp, Reinhard; Gambacorta, Domenico
US Patent Document 8,752,386
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8752386

System and method for tube level air flow conditioning
patent-application, November 2014

Melton, Patrick Benedict; Chila, Ronald James; Boardman, Gregory Allen
US Patent Application 13/798012; 20140338340
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140338340

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

Lauck, Lawrence J.
US Patent Document 4,016,718
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4016718

Repair method for a gas turbine
patent, April 2003

Sekihara, Masaru; Sakurai, Shigeo
US Patent Document 6,546,627
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6546627

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

Buelow, Philip E. O.; Williams, Brandon P.; Bretz, David H.
US Patent Application 12/804374; 20100287946
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100287946

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

Scheihing, Paul E.; Laurelli, James A.
US Patent Document 4,413,470
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4413470

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

Wiebe, David J.
US Patent Document 8,281,594
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8281594

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

Hasselqvist, Magnus; Rubensdorffer, Frank
US Patent Application 14/369687; 20140373548
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140373548

Steam cooled rich-burn combustor liner
patent, April 1989

Schultz, Donald F.
US Patent Document 4,819,438
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4819438

Integral aft seal for turbine applications
patent, September 2002

Munshi, Jonathan
US Patent Document 6,450,762
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6450762

Fuel Nozzles for Injecting Fuel in a Gas Turbine Combustor
patent-application, July 2013

Berry, Jonathan Dwight
US Patent Application 13/343417; 20130167539
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130167539

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

Chopra, Sanjay; Youngblood, Bradley T.; Dawson, Robert W.
US Patent Document 7,886,517
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7886517

Steam cooled gas turbine system
patent, August 2000

Sugishita, Hideaki
US Patent Document 6,109,019
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6109019

Segmented annular combustor
patent, January 2011

Rubio, Mark; Ritland, David M.
US Patent Document 7,874,138
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7874138

Modular Transvane Assembly
patent-application, April 2010

Wilson, Jody; Nordlund, Raymond; Charron, Richard
US Patent Application 12/420149; 20100077719
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100077719

Triple annular combustor for gas turbine engine
patent, June 1994

Ekstedt, Edward E.; Joshi, Narendra Digamber; Ablett, Adrian M.
US Patent Document 5,323,604
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5323604

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

Dupuy, Philippe; Guillot, Laurent; Moreau, Eric
US Patent Application 11/911324; 20080208513
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20080208513

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

Donovan, Jon Peter; McManus, Michael
US Patent Document 6,298,656
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6298656

Gas turbine plant with combustor cooling system
patent, September 2000

Tanimura, Satoshi; Mandai, Shigemi; Gora, Tetsuo
US Patent Document 6,116,018
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6116018

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

Toqan, Majed; Gregory, Brent Allen; Yamane, Ryan Sadao
09/01/2011, vp
US Patent Application 12/786882; 20110209482
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20110209482

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

Ziegner, Manfred
US Patent Document 6,374,593
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6374593

Effusion cooled transition duct
patent, May 2003

Jorgensen, Stephen W.; Leahy, Jr., James H.
US Patent Document 6,568,187
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6568187

Aerodynamically enhanced fuel nozzle
patent, March 2013

Patel, Nayan Vinodbhai; Benjamin, Michael Anthony; Thomsen, Duane Douglas
US Patent Document 8,387,391
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8387391

Fuel injection assembly for gas turbine engine combustor
patent, March 2002

Candy, Anthony J.; Glynn, Christopher Charles; Barrett, John
US Patent Document 6,357,237
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6357237

Bolted gas turbine combustor transition coupling
patent, September 2000

Möller, Michael
US Patent Document 6,116,013
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6116013

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

Little, David A.
US Patent Document 5,826,430
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5826430

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

Wey, Stewart; Hershey, Albert E.; Boyd, John R.
US Patent Document 2,595,999
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2595999

Side seal for combustor transitions
patent, February 2002

Coslow, Bill
US Patent Document 6,345,494
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6345494

Impingement cooled transition duct
patent, January 1988

Davis, Jr., Lewis Berkley; Goodwin, Walter W.; Steber, Charles E.
US Patent Document 4,719,748
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4719748

Hollow Structure with Flange
patent-application, July 2003

Shimizu, Hiroshi; Kondo, Mitsuru; Hakoda, Hironobu
US Patent Application 10/378602; 20030140633
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20030140633

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

Glessner, John Carl; Dahlke, Stefan; Nicosia, Robert O.
US Patent Document 7,334,960
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7334960

Combustion chamber construction
patent, September 1986

Sterman, Albert P.; Wakeman, Thomas G.; Williams, Jesse J.
US Patent Document 4,614,082
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4614082

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

Jorgensen, Stephen W.
US Patent Document 6,619,915
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6619915

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

Bintz, Miles; Dehmer, deceased, Raymond L.
US Patent Document 4,195,474
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4195474

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

Coppola, Alessandro
US Patent Application 10/311251; 20030167776
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20030167776

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

Huffman, Marcus Byron
US Patent Document 8,549,861
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8549861

Apparatus for injecting fuel into gas turbine engines
patent, March 2003

Halila, Ely E.; Anderson, Michael J.
US Patent Document 6,536,216
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6536216

Gas turbine aerofoil
patent, June 2006

Self, Kevin P.; Bennett, Paul N.
US Patent Document 7,056,093
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7056093

Combustor and method for supplying fuel to a combustor
patent-application, April 2013

Melton, Patrick Benedict; Ziminsky, Willy Steve; Boardman, Gregory Allen
US Patent Application 13/252279; 20130084534
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130084534

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

McCarthy, Denis; Smith, Alan Douglas French
US Patent Document 2,625,792
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2625792

Dilution pole combustor and method
patent, August 1993

Stickles, Richard W.; Dodds, Willard J.; Sabla, Paul E.
US Patent Document 5,239,818
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5239818

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

Takahashi, Syuichi; Nishimura, Yoshiaki; Fujita, Hiroyuki
US Patent Document 6,523,352
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6523352

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

Martin, Scott M.; Cai, Weidong; Harris, Jr., Arthur J.
US Patent Document 8,387,398
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8387398

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

Intile, John Charles; West, James Anthony; Byrne, William Lawrence
US Patent Document 7,010,921
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7010921

Duplex turbine shroud
patent, January 2012

Lee, Ching-Pang; Robinson, Geoffrey Douglas; Orlando, Robert Joseph
US Patent Document 8,104,292
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8104292

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

Benim, Ali Cemal; Joos, Franz
US Patent Document 6,085,514
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6085514

Gas turbine engine combustion chambers
patent, February 1983

Adkins, Richard C.
US Patent Document 4,373,327
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4373327

Sector airflow variable geometry combustor
patent, January 1988

Hudson, Dale; Hopkins, Kenneth
US Patent Document 4,720,970
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4720970

Transition Piece Outlet Structure Enabling to Reduce the Temperature, and a Transition Piece, a Combustor and a Gas Turbine Providing the Above Output Structure
patent-application, August 2002

Kondo, Mitsuru; Hada, Satoshi; Tanaka, Katsunori
US Patent Application 10/075461; 20020112483
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20020112483

Similar Records in DOE Patents and OSTI.GOV collections:

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
Full Text Available
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
Full Text Available
Segmented annular combustion system with dual fuel capability

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

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.
Full Text Available
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
Full Text Available
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
Full Text Available

Similar Records

Title: Radially stacked fuel injection module for a segmented annular combustion system

Abstract

Citation Formats

Modular combustor dome patent, October 2001

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

System for supporting a bundled tube fuel injector within a combustor patent-application, January 2015

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

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

System for supporting bundled tube segments within a combustor patent-application, February 2015

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

Multi-premixer fuel nozzle patent-application, February 2012

Dual fuel mixer for gas turbine combustor patent, April 1996

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

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

System and method for tube level air flow conditioning patent-application, November 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

Steam cooled rich-burn combustor liner patent, April 1989

Integral aft seal for turbine applications patent, September 2002

Fuel Nozzles for Injecting Fuel in a Gas Turbine Combustor patent-application, July 2013

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

Triple annular combustor for gas turbine engine patent, June 1994

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

Fuel injection assembly for gas turbine engine combustor patent, March 2002

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

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

Modular combustor dome
patent, October 2001

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

System for supporting a bundled tube fuel injector within a combustor
patent-application, January 2015

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

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

System for supporting bundled tube segments within a combustor
patent-application, February 2015

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

Multi-premixer fuel nozzle
patent-application, February 2012

Dual fuel mixer for gas turbine combustor
patent, April 1996

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

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

System and method for tube level air flow conditioning
patent-application, November 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

Steam cooled rich-burn combustor liner
patent, April 1989

Integral aft seal for turbine applications
patent, September 2002

Fuel Nozzles for Injecting Fuel in a Gas Turbine Combustor
patent-application, July 2013

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

Triple annular combustor for gas turbine engine
patent, June 1994

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

Fuel injection assembly for gas turbine engine combustor
patent, March 2002

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

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

Apparatus for injecting fuel into gas turbine engines
patent, March 2003

Gas turbine aerofoil
patent, June 2006