CN104048323A - 包括带有燃料喷嘴外壳的多管燃料喷嘴的系统 - Google Patents

包括带有燃料喷嘴外壳的多管燃料喷嘴的系统 Download PDF

Info

Publication number
CN104048323A
CN104048323A CN201410093498.0A CN201410093498A CN104048323A CN 104048323 A CN104048323 A CN 104048323A CN 201410093498 A CN201410093498 A CN 201410093498A CN 104048323 A CN104048323 A CN 104048323A
Authority
CN
China
Prior art keywords
fuel nozzle
fuel
tube
wall
container
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201410093498.0A
Other languages
English (en)
Chinese (zh)
Inventor
J.T.斯图尔特
C.P.基纳
H.M.奥斯特比
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN104048323A publication Critical patent/CN104048323A/zh
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012Details of sealing devices
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Hydrogen, Water And Hydrids (AREA)
CN201410093498.0A 2013-03-15 2014-03-13 包括带有燃料喷嘴外壳的多管燃料喷嘴的系统 Pending CN104048323A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/838726 2013-03-15
US13/838,726 US9303873B2 (en) 2013-03-15 2013-03-15 System having a multi-tube fuel nozzle with a fuel nozzle housing

Publications (1)

Publication Number Publication Date
CN104048323A true CN104048323A (zh) 2014-09-17

Family

ID=51419083

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410093498.0A Pending CN104048323A (zh) 2013-03-15 2014-03-13 包括带有燃料喷嘴外壳的多管燃料喷嘴的系统

Country Status (5)

Country Link
US (1) US9303873B2 (enExample)
JP (1) JP6483957B2 (enExample)
CN (1) CN104048323A (enExample)
CH (1) CH707843A8 (enExample)
DE (1) DE102014103085B4 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111720820A (zh) * 2019-03-19 2020-09-29 奥隆技术有限公司 燃烧器和锅炉-燃烧器组件及在其中生成火焰的方法
CN113803744A (zh) * 2021-09-27 2021-12-17 中国联合重型燃气轮机技术有限公司 燃烧室入料装置及入料系统

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9534781B2 (en) 2012-05-10 2017-01-03 General Electric Company System and method having multi-tube fuel nozzle with differential flow
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9759425B2 (en) 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
US9291352B2 (en) 2013-03-15 2016-03-22 General Electric Company System having a multi-tube fuel nozzle with an inlet flow conditioner
US9546789B2 (en) 2013-03-15 2017-01-17 General Electric Company System having a multi-tube fuel nozzle
US9316397B2 (en) 2013-03-15 2016-04-19 General Electric Company System and method for sealing a fuel nozzle
US9784452B2 (en) 2013-03-15 2017-10-10 General Electric Company System having a multi-tube fuel nozzle with an aft plate assembly
US9423136B2 (en) * 2013-12-13 2016-08-23 General Electric Company Bundled tube fuel injector aft plate retention
US9664392B2 (en) * 2013-12-13 2017-05-30 General Electric Company Bundled tube fuel injector with outer shroud and outer band connection
EP3134682B1 (de) * 2014-11-03 2018-08-22 Siemens Aktiengesellschaft Brenneranordnung
US10024539B2 (en) * 2015-09-24 2018-07-17 General Electric Company Axially staged micromixer cap
US10429073B2 (en) * 2015-12-21 2019-10-01 General Electric Company Combustor cap module and retention system therefor
US10571126B2 (en) * 2017-02-08 2020-02-25 General Electric Company Method to provide a braze coating with wear property on micromixer tubes
US11226100B2 (en) * 2019-07-22 2022-01-18 Delavan Inc. Fuel manifolds
KR102433706B1 (ko) * 2021-01-07 2022-08-19 두산에너빌리티 주식회사 노즐 어셈블리, 연소기 및 이를 포함하는 가스터빈
KR102459999B1 (ko) 2021-01-13 2022-10-26 두산에너빌리티 주식회사 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈
US11725820B1 (en) * 2022-06-07 2023-08-15 Thomassen Energy B.V. Halo ring fuel injector for a gas turbine engine
EP4328487A1 (en) * 2022-08-26 2024-02-28 Sustainable Business & Engineering Solutions GmbH Multi-tube burner system for efficient mixing of fuel and air for combustion
CN115451431B (zh) * 2022-09-22 2024-04-16 中国联合重型燃气轮机技术有限公司 一种用于燃气轮机燃烧室的燃料喷嘴预混系统
CN115451432B (zh) * 2022-09-22 2024-03-12 中国联合重型燃气轮机技术有限公司 一种燃气轮机燃烧室燃料的微混喷嘴组件及系统
GB202305347D0 (en) * 2023-04-12 2023-05-24 Rolls Royce Plc Fuel injector
US12434362B2 (en) 2023-10-02 2025-10-07 Ge Infrastructure Technology Llc Aft inner cap plate removal method and tooling for a combustor with micromixer tubes

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0936406B1 (en) * 1998-02-10 2004-05-06 General Electric Company Burner with uniform fuel/air premixing for low emissions combustion
CN101532679A (zh) * 2008-03-12 2009-09-16 通用电气公司 贫燃料直接喷射燃烧系统
US7752850B2 (en) * 2005-07-01 2010-07-13 Siemens Energy, Inc. Controlled pilot oxidizer for a gas turbine combustor
CN102607062A (zh) * 2011-01-18 2012-07-25 通用电气公司 用于喷射燃料的系统及方法

Family Cites Families (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
US4845952A (en) 1987-10-23 1989-07-11 General Electric Company Multiple venturi tube gas fuel injector for catalytic combustor
US5263325A (en) * 1991-12-16 1993-11-23 United Technologies Corporation Low NOx combustion
US5274991A (en) * 1992-03-30 1994-01-04 General Electric Company Dry low NOx multi-nozzle combustion liner cap assembly
JP3364169B2 (ja) 1999-06-09 2003-01-08 三菱重工業株式会社 ガスタービン及びその燃焼器
US6446439B1 (en) * 1999-11-19 2002-09-10 Power Systems Mfg., Llc Pre-mix nozzle and full ring fuel distribution system for a gas turbine combustor
US6282904B1 (en) 1999-11-19 2001-09-04 Power Systems Mfg., Llc Full ring fuel distribution system for a gas turbine combustor
JP4709433B2 (ja) * 2001-06-29 2011-06-22 三菱重工業株式会社 ガスタービン燃焼器
US6672073B2 (en) 2002-05-22 2004-01-06 Siemens Westinghouse Power Corporation System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate
US7093438B2 (en) * 2005-01-17 2006-08-22 General Electric Company Multiple venture tube gas fuel injector for a combustor
US8122721B2 (en) 2006-01-04 2012-02-28 General Electric Company Combustion turbine engine and methods of assembly
US20070277530A1 (en) 2006-05-31 2007-12-06 Constantin Alexandru Dinu Inlet flow conditioner for gas turbine engine fuel nozzle
DE102006054910A1 (de) 2006-06-14 2007-12-20 Hübner GmbH Fluggastbrücke oder Fluggasttreppe
KR20090067152A (ko) 2006-09-06 2009-06-24 엔엑스피 비 브이 클러스터 커플러 유닛, 클러스터 동기화 방법 및 네트워크
US8438853B2 (en) 2008-01-29 2013-05-14 Alstom Technology Ltd. Combustor end cap assembly
US8147121B2 (en) 2008-07-09 2012-04-03 General Electric Company Pre-mixing apparatus for a turbine engine
US20100175380A1 (en) 2009-01-13 2010-07-15 General Electric Company Traversing fuel nozzles in cap-less combustor assembly
US8171737B2 (en) * 2009-01-16 2012-05-08 General Electric Company Combustor assembly and cap for a turbine engine
US9140454B2 (en) 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
US8424311B2 (en) * 2009-02-27 2013-04-23 General Electric Company Premixed direct injection disk
US8648336B2 (en) 2009-03-03 2014-02-11 The University Of Western Ontario Method for fabrication of layered heterojunction polymeric devices
US8234872B2 (en) 2009-05-01 2012-08-07 General Electric Company Turbine air flow conditioner
US8789372B2 (en) * 2009-07-08 2014-07-29 General Electric Company Injector with integrated resonator
US8438852B2 (en) 2010-04-06 2013-05-14 General Electric Company Annular ring-manifold quaternary fuel distributor
US8800289B2 (en) 2010-09-08 2014-08-12 General Electric Company Apparatus and method for mixing fuel in a gas turbine nozzle
US8312724B2 (en) 2011-01-26 2012-11-20 United Technologies Corporation Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone
US8397514B2 (en) * 2011-05-24 2013-03-19 General Electric Company System and method for flow control in gas turbine engine
US20130025285A1 (en) 2011-07-29 2013-01-31 General Electric Company System for conditioning air flow into a multi-nozzle assembly
US8904797B2 (en) 2011-07-29 2014-12-09 General Electric Company Sector nozzle mounting systems
US8950188B2 (en) 2011-09-09 2015-02-10 General Electric Company Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber
US8801428B2 (en) * 2011-10-04 2014-08-12 General Electric Company Combustor and method for supplying fuel to a combustor
US9243803B2 (en) 2011-10-06 2016-01-26 General Electric Company System for cooling a multi-tube fuel nozzle
US20130232979A1 (en) 2012-03-12 2013-09-12 General Electric Company System for enhancing mixing in a multi-tube fuel nozzle
US9534781B2 (en) 2012-05-10 2017-01-03 General Electric Company System and method having multi-tube fuel nozzle with differential flow
US8701419B2 (en) 2012-05-10 2014-04-22 General Electric Company Multi-tube fuel nozzle with mixing features
US8943833B2 (en) * 2012-07-06 2015-02-03 United Technologies Corporation Fuel flexible fuel injector
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US20140338340A1 (en) 2013-03-12 2014-11-20 General Electric Company System and method for tube level air flow conditioning
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
US9347668B2 (en) 2013-03-12 2016-05-24 General Electric Company End cover configuration and assembly
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9366439B2 (en) 2013-03-12 2016-06-14 General Electric Company Combustor end cover with fuel plenums
US9759425B2 (en) 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9650959B2 (en) 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9546789B2 (en) 2013-03-15 2017-01-17 General Electric Company System having a multi-tube fuel nozzle
US9784452B2 (en) 2013-03-15 2017-10-10 General Electric Company System having a multi-tube fuel nozzle with an aft plate assembly
US9316397B2 (en) 2013-03-15 2016-04-19 General Electric Company System and method for sealing a fuel nozzle
US9291352B2 (en) 2013-03-15 2016-03-22 General Electric Company System having a multi-tube fuel nozzle with an inlet flow conditioner

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0936406B1 (en) * 1998-02-10 2004-05-06 General Electric Company Burner with uniform fuel/air premixing for low emissions combustion
US7752850B2 (en) * 2005-07-01 2010-07-13 Siemens Energy, Inc. Controlled pilot oxidizer for a gas turbine combustor
CN101532679A (zh) * 2008-03-12 2009-09-16 通用电气公司 贫燃料直接喷射燃烧系统
US20090229269A1 (en) * 2008-03-12 2009-09-17 General Electric Company Lean direct injection combustion system
CN102607062A (zh) * 2011-01-18 2012-07-25 通用电气公司 用于喷射燃料的系统及方法

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111720820A (zh) * 2019-03-19 2020-09-29 奥隆技术有限公司 燃烧器和锅炉-燃烧器组件及在其中生成火焰的方法
CN113803744A (zh) * 2021-09-27 2021-12-17 中国联合重型燃气轮机技术有限公司 燃烧室入料装置及入料系统
CN113803744B (zh) * 2021-09-27 2023-03-10 中国联合重型燃气轮机技术有限公司 燃烧室入料装置及入料系统

Also Published As

Publication number Publication date
CH707843A2 (de) 2014-09-15
US9303873B2 (en) 2016-04-05
CH707843A8 (de) 2015-01-15
US20140338344A1 (en) 2014-11-20
DE102014103085A1 (de) 2014-09-18
JP6483957B2 (ja) 2019-03-13
JP2014181900A (ja) 2014-09-29
DE102014103085B4 (de) 2025-12-18

Similar Documents

Publication Publication Date Title
US9303873B2 (en) System having a multi-tube fuel nozzle with a fuel nozzle housing
US9546789B2 (en) System having a multi-tube fuel nozzle
US9784452B2 (en) System having a multi-tube fuel nozzle with an aft plate assembly
US9316397B2 (en) System and method for sealing a fuel nozzle
US9291352B2 (en) System having a multi-tube fuel nozzle with an inlet flow conditioner
EP3343108B1 (en) System for dissipating fuel egress in fuel supply conduit assemblies
JP6514432B2 (ja) 複数の燃料噴射器を持つ多管式燃料ノズルを有するシステム及び方法
EP3171088B1 (en) Bundled tube fuel nozzle assembly with liquid fuel capability
US10655858B2 (en) Cooling of liquid fuel cartridge in gas turbine combustor head end
US9371997B2 (en) System for supporting a bundled tube fuel injector within a combustor
EP3290805B1 (en) Fuel nozzle assembly with resonator
CN103562643B (zh) 用于燃气轮机燃烧室喷口盖组的结构框架
EP2664852A2 (en) Fuel Nozzle Cap
EP2664851A2 (en) Fuel nozzle cap
US12215867B2 (en) Gas turbine combustor with dynamics mitigation system
US20170343216A1 (en) Fuel Nozzle Assembly with Tube Damping
EP3309457B1 (en) Combustion dynamics mitigation system
US10677466B2 (en) Combustor inlet flow conditioner
EP4123224B1 (en) Cartridge tip for turbomachine combustor
JP2022070219A (ja) 統合型ヘッドエンドを有する一体型燃焼ノズル
EP3586061B1 (en) Endcover assembly for a combustor
WO2024148123A1 (en) Method of operating gas turbine combustor with multiple fuel stages

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140917

WD01 Invention patent application deemed withdrawn after publication