CN104613498B - 燃气轮机燃烧器 - Google Patents

燃气轮机燃烧器 Download PDF

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Publication number
CN104613498B
CN104613498B CN201410608240.XA CN201410608240A CN104613498B CN 104613498 B CN104613498 B CN 104613498B CN 201410608240 A CN201410608240 A CN 201410608240A CN 104613498 B CN104613498 B CN 104613498B
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CN
China
Prior art keywords
gas turbine
mentioned
ring
burner
liner
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.)
Active
Application number
CN201410608240.XA
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English (en)
Chinese (zh)
Other versions
CN104613498A (zh
Inventor
横田修
日高政隆
沼田祥平
辰巳哲马
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.)
Mitsubishi Power Ltd
Original Assignee
Mitsubishi Hitachi Power Systems Ltd
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
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Publication of CN104613498A publication Critical patent/CN104613498A/zh
Application granted granted Critical
Publication of CN104613498B publication Critical patent/CN104613498B/zh
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041—Effusion cooled combustion chamber walls or domes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03042—Film cooled combustion chamber walls or domes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03043—Convection cooled combustion chamber walls with means for guiding the cooling air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03045—Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201410608240.XA 2013-11-05 2014-11-03 燃气轮机燃烧器 Active CN104613498B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2013229514A JP6246562B2 (ja) 2013-11-05 2013-11-05 ガスタービン燃焼器
JP2013-229514 2013-11-05

Publications (2)

Publication Number Publication Date
CN104613498A CN104613498A (zh) 2015-05-13
CN104613498B true CN104613498B (zh) 2017-05-10

Family

ID=51842438

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410608240.XA Active CN104613498B (zh) 2013-11-05 2014-11-03 燃气轮机燃烧器

Country Status (4)

Country Link
US (1) US10184662B2 (https=)
EP (1) EP2868971B1 (https=)
JP (1) JP6246562B2 (https=)
CN (1) CN104613498B (https=)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10337736B2 (en) * 2015-07-24 2019-07-02 Pratt & Whitney Canada Corp. Gas turbine engine combustor and method of forming same
US10378444B2 (en) * 2015-08-19 2019-08-13 General Electric Company Engine component for a gas turbine engine
US10260751B2 (en) 2015-09-28 2019-04-16 Pratt & Whitney Canada Corp. Single skin combustor with heat transfer enhancement
US20180180289A1 (en) * 2016-12-23 2018-06-28 General Electric Company Turbine engine assembly including a rotating detonation combustor
US10823414B2 (en) * 2018-03-19 2020-11-03 Raytheon Technologies Corporation Hooded entrance to effusion holes
JP7132096B2 (ja) * 2018-11-14 2022-09-06 三菱重工業株式会社 ガスタービン燃焼器
JP7550694B2 (ja) 2021-03-26 2024-09-13 本田技研工業株式会社 ガスタービン用燃焼器

Citations (6)

* Cited by examiner, † Cited by third party
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US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
CN1878987A (zh) * 2003-12-16 2006-12-13 株式会社日立制作所 燃气轮机用燃烧器
EP2107314A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Combustor for a gas turbine
CN102563699A (zh) * 2010-10-05 2012-07-11 株式会社日立制作所 燃气轮机燃烧器
CN102901125A (zh) * 2011-07-27 2013-01-30 株式会社日立制作所 燃烧器、燃烧嘴及燃气轮机

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US4242871A (en) * 1979-09-18 1981-01-06 United Technologies Corporation Louver burner liner
US4380906A (en) 1981-01-22 1983-04-26 United Technologies Corporation Combustion liner cooling scheme
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert
US4916906A (en) * 1988-03-25 1990-04-17 General Electric Company Breach-cooled structure
US5361828A (en) * 1993-02-17 1994-11-08 General Electric Company Scaled heat transfer surface with protruding ramp surface turbulators
JPH08254316A (ja) * 1995-03-16 1996-10-01 Toshiba Corp ガスタービン燃焼器用ライナおよびその製造方法
JP4134513B2 (ja) 1997-09-12 2008-08-20 株式会社日立製作所 ガスタービン燃焼器とそのライチ構造
US6145319A (en) * 1998-07-16 2000-11-14 General Electric Company Transitional multihole combustion liner
JP3967521B2 (ja) * 2000-03-30 2007-08-29 株式会社日立製作所 伝熱装置及びその製造方法並びに伝熱装置を備えたガスタービン燃焼器
US6568079B2 (en) * 2001-06-11 2003-05-27 General Electric Company Methods for replacing combustor liner panels
US6735949B1 (en) * 2002-06-11 2004-05-18 General Electric Company Gas turbine engine combustor can with trapped vortex cavity
US7007481B2 (en) * 2003-09-10 2006-03-07 General Electric Company Thick coated combustor liner
DE102006026969A1 (de) * 2006-06-09 2007-12-13 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammerwand für eine mager-brennende Gasturbinenbrennkammer
US20120047895A1 (en) * 2010-08-26 2012-03-01 General Electric Company Systems and apparatus relating to combustor cooling and operation in gas turbine engines
US8365534B2 (en) * 2011-03-15 2013-02-05 General Electric Company Gas turbine combustor having a fuel nozzle for flame anchoring
US8931280B2 (en) * 2011-04-26 2015-01-13 General Electric Company Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
GB201114745D0 (en) * 2011-08-26 2011-10-12 Rolls Royce Plc Wall elements for gas turbine engines
US20130074507A1 (en) * 2011-09-28 2013-03-28 Karthick Kaleeswaran Combustion liner for a turbine engine
JP6066065B2 (ja) 2013-02-20 2017-01-25 三菱日立パワーシステムズ株式会社 伝熱装置を備えたガスタービン燃焼器

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
CN1878987A (zh) * 2003-12-16 2006-12-13 株式会社日立制作所 燃气轮机用燃烧器
EP2107314A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Combustor for a gas turbine
CN102563699A (zh) * 2010-10-05 2012-07-11 株式会社日立制作所 燃气轮机燃烧器
CN102901125A (zh) * 2011-07-27 2013-01-30 株式会社日立制作所 燃烧器、燃烧嘴及燃气轮机

Also Published As

Publication number Publication date
JP2015090229A (ja) 2015-05-11
EP2868971A1 (en) 2015-05-06
CN104613498A (zh) 2015-05-13
US20150121885A1 (en) 2015-05-07
JP6246562B2 (ja) 2017-12-13
US10184662B2 (en) 2019-01-22
EP2868971B1 (en) 2021-01-06

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Address after: Kanagawa Prefecture, Japan

Patentee after: Mitsubishi Power Co., Ltd

Address before: Kanagawa Prefecture, Japan

Patentee before: MITSUBISHI HITACHI POWER SYSTEMS, Ltd.

CP01 Change in the name or title of a patent holder