CN115335638A - 燃气轮机的燃烧器以及燃气轮机 - Google Patents

燃气轮机的燃烧器以及燃气轮机 Download PDF

Info

Publication number
CN115335638A
CN115335638A CN202180024645.7A CN202180024645A CN115335638A CN 115335638 A CN115335638 A CN 115335638A CN 202180024645 A CN202180024645 A CN 202180024645A CN 115335638 A CN115335638 A CN 115335638A
Authority
CN
China
Prior art keywords
throttle
fuel
gas turbine
combustor
fuel nozzle
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
CN202180024645.7A
Other languages
English (en)
Chinese (zh)
Inventor
福场信一
泷口智志
木下泰希
谷口健太
中村聪介
松村嘉和
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of CN115335638A publication Critical patent/CN115335638A/zh
Pending legal-status Critical Current

Links

Images

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/08—Purpose of the control system to produce clean exhaust gases
    • F05D2270/082—Purpose of the control system to produce clean exhaust gases with as little NOx as possible
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/14—Purpose of the control system to control thermoacoustic behaviour in the combustion chambers
    • 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
    • F23R2900/00013—Reducing thermo-acoustic vibrations by active means
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CN202180024645.7A 2020-03-31 2021-03-31 燃气轮机的燃烧器以及燃气轮机 Pending CN115335638A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2020-063062 2020-03-31
JP2020063062 2020-03-31
PCT/JP2021/013809 WO2021201093A1 (ja) 2020-03-31 2021-03-31 ガスタービンの燃焼器、及び、ガスタービン

Publications (1)

Publication Number Publication Date
CN115335638A true CN115335638A (zh) 2022-11-11

Family

ID=77928561

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202180024645.7A Pending CN115335638A (zh) 2020-03-31 2021-03-31 燃气轮机的燃烧器以及燃气轮机

Country Status (6)

Country Link
US (1) US20240027069A1 (https=)
JP (1) JP7386325B2 (https=)
KR (1) KR102693689B1 (https=)
CN (1) CN115335638A (https=)
DE (1) DE112021002128T5 (https=)
WO (1) WO2021201093A1 (https=)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12460817B2 (en) 2022-03-11 2025-11-04 Mitsubishi Heavy Industries, Ltd. Assembly, method for manufacturing assembly, burner, and method for manufacturing burner
WO2023176570A1 (ja) * 2022-03-14 2023-09-21 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4490156A (en) * 1981-06-10 1984-12-25 Texaco Inc. Partial oxidation system
JPH11166707A (ja) * 1997-12-04 1999-06-22 Sanyo Electric Co Ltd ロータリーバーナ
JP2001041418A (ja) * 1999-07-27 2001-02-13 Noritz Corp バーナ
CN1468352A (zh) * 2000-10-05 2004-01-14 ����˹��ķ(��ʿ)���޹�˾ 预混合燃烧器的燃料供给方法和装置
JP2004360944A (ja) * 2003-06-02 2004-12-24 National Aerospace Laboratory Of Japan ガスタービン用燃料ノズル
JP2005315473A (ja) * 2004-04-27 2005-11-10 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP2006029677A (ja) * 2004-07-15 2006-02-02 Hitachi Ltd 複数のバーナを備えた燃焼器
JP2011102669A (ja) * 2009-11-10 2011-05-26 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器及びガスタービン
US20130008167A1 (en) * 2011-07-07 2013-01-10 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
CN103134081A (zh) * 2011-12-01 2013-06-05 通用电气公司 用于脉冲爆震燃烧器的可变引发位置系统
JP5743122B2 (ja) * 2012-02-28 2015-07-01 三菱日立パワーシステムズ株式会社 燃焼器及びガスタービン
US20170299182A1 (en) * 2014-09-25 2017-10-19 Mitsubishi Hitachi Power Systems, Ltd. Combustor and gas turbine comprising same
CN108779919A (zh) * 2016-03-29 2018-11-09 三菱日立电力系统株式会社 燃烧器、燃烧器的性能提高方法
JP2019020071A (ja) * 2017-07-19 2019-02-07 三菱重工業株式会社 燃焼器及びガスタービン

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4356698A (en) * 1980-10-02 1982-11-02 United Technologies Corporation Staged combustor having aerodynamically separated combustion zones
JP2005076982A (ja) * 2003-08-29 2005-03-24 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP6508470B2 (ja) 2015-07-31 2019-05-08 三菱日立パワーシステムズ株式会社 燃料流量設定方法、この方法を実行する装置、この装置を備えるガスタービンプラント

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4490156A (en) * 1981-06-10 1984-12-25 Texaco Inc. Partial oxidation system
JPH11166707A (ja) * 1997-12-04 1999-06-22 Sanyo Electric Co Ltd ロータリーバーナ
JP2001041418A (ja) * 1999-07-27 2001-02-13 Noritz Corp バーナ
CN1468352A (zh) * 2000-10-05 2004-01-14 ����˹��ķ(��ʿ)���޹�˾ 预混合燃烧器的燃料供给方法和装置
JP2004360944A (ja) * 2003-06-02 2004-12-24 National Aerospace Laboratory Of Japan ガスタービン用燃料ノズル
JP2005315473A (ja) * 2004-04-27 2005-11-10 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP2006029677A (ja) * 2004-07-15 2006-02-02 Hitachi Ltd 複数のバーナを備えた燃焼器
JP2011102669A (ja) * 2009-11-10 2011-05-26 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器及びガスタービン
US20130008167A1 (en) * 2011-07-07 2013-01-10 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
CN103134081A (zh) * 2011-12-01 2013-06-05 通用电气公司 用于脉冲爆震燃烧器的可变引发位置系统
JP5743122B2 (ja) * 2012-02-28 2015-07-01 三菱日立パワーシステムズ株式会社 燃焼器及びガスタービン
US20170299182A1 (en) * 2014-09-25 2017-10-19 Mitsubishi Hitachi Power Systems, Ltd. Combustor and gas turbine comprising same
CN108779919A (zh) * 2016-03-29 2018-11-09 三菱日立电力系统株式会社 燃烧器、燃烧器的性能提高方法
JP2019020071A (ja) * 2017-07-19 2019-02-07 三菱重工業株式会社 燃焼器及びガスタービン

Also Published As

Publication number Publication date
US20240027069A1 (en) 2024-01-25
WO2021201093A1 (ja) 2021-10-07
DE112021002128T5 (de) 2023-03-09
JPWO2021201093A1 (https=) 2021-10-07
KR20220160546A (ko) 2022-12-06
JP7386325B2 (ja) 2023-11-24
KR102693689B1 (ko) 2024-08-08

Similar Documents

Publication Publication Date Title
JP5947515B2 (ja) 渦発生装置を有する混合管要素を備えたターボ機械
JP6335903B2 (ja) 火炎シート燃焼器ドーム
CN102378878B (zh) 旋流器、燃烧腔以及具有改善的涡流的燃气涡轮机
CN109804200B (zh) 旋流器、燃烧装置组件以及具有改善燃料/空气混合的燃气涡轮
CN101688670B (zh) 燃气轮机燃烧器
US11859822B2 (en) Burner assembly, gas turbine combustor, and gas turbine
US20130283805A1 (en) Fuel/air premixing system for turbine engine
JP2002039533A (ja) 燃焼器、ガスタービン及びジェットエンジン
US11692710B2 (en) Burner, combustor including same, and gas turbine
US20250179960A1 (en) Burner assembly, gas turbine combustor, and gas turbine
KR102154220B1 (ko) 연소기 및 이를 포함하는 가스터빈
CN107466354A (zh) 用于燃气涡轮发动机的旋流器、燃烧器和燃烧装置
CN115335638A (zh) 燃气轮机的燃烧器以及燃气轮机
CN107850308B (zh) 用于燃气轮机的燃烧器
US11209163B2 (en) Gas turbine combustor, manufacturing method for gas turbine and gas turbine combustor
CN115989383A (zh) 用于燃气涡轮机的燃烧器
JP6692847B2 (ja) ガスタービン燃焼器及びこれを備えたガスタービン機関
CN102692036A (zh) 具有带有人字形肋的燃料喷嘴衬套的燃烧器
CN118829827A (zh) 燃气涡轮机燃烧器及燃气涡轮机
EP4592597A1 (en) Fuel injection assembly for a combustor and axial fuel staging combustor comprising the fuel injection assembly
JP7154984B2 (ja) タービン静翼及びガスタービン
CN108431503A (zh) 用于燃气轮机的燃烧器
WO2024202124A1 (ja) バーナー集合体、ガスタービン燃焼器及びガスタービン

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination