JP6030919B2 - タービンエンジンで使用する燃焼器アセンブリ及びその組立方法 - Google Patents

タービンエンジンで使用する燃焼器アセンブリ及びその組立方法 Download PDF

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Publication number
JP6030919B2
JP6030919B2 JP2012238466A JP2012238466A JP6030919B2 JP 6030919 B2 JP6030919 B2 JP 6030919B2 JP 2012238466 A JP2012238466 A JP 2012238466A JP 2012238466 A JP2012238466 A JP 2012238466A JP 6030919 B2 JP6030919 B2 JP 6030919B2
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Japan
Prior art keywords
fuel
cooling fluid
plenum
cooling
fuel nozzle
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Application number
JP2012238466A
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English (en)
Japanese (ja)
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JP2013139993A (ja
JP2013139993A5 (enExample
Inventor
ジョン・ホー・ウーム
トーマス・エドワード・ジョンソン
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General Electric Co
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General Electric Co
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Publication of JP2013139993A5 publication Critical patent/JP2013139993A5/ja
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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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/10—Flame flashback
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/20—Flame lift-off / stability
    • 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
    • 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
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts

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)
  • Gas Burners (AREA)
  • Fuel-Injection Apparatus (AREA)
JP2012238466A 2012-01-03 2012-10-30 タービンエンジンで使用する燃焼器アセンブリ及びその組立方法 Active JP6030919B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/342,303 2012-01-03
US13/342,303 US8438851B1 (en) 2012-01-03 2012-01-03 Combustor assembly for use in a turbine engine and methods of assembling same

Publications (3)

Publication Number Publication Date
JP2013139993A JP2013139993A (ja) 2013-07-18
JP2013139993A5 JP2013139993A5 (enExample) 2015-12-03
JP6030919B2 true JP6030919B2 (ja) 2016-11-24

Family

ID=47172450

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012238466A Active JP6030919B2 (ja) 2012-01-03 2012-10-30 タービンエンジンで使用する燃焼器アセンブリ及びその組立方法

Country Status (5)

Country Link
US (1) US8438851B1 (enExample)
EP (1) EP2613083B1 (enExample)
JP (1) JP6030919B2 (enExample)
CN (1) CN103185353B (enExample)
RU (1) RU2605164C2 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220117567A (ko) * 2021-02-17 2022-08-24 두산에너빌리티 주식회사 마이크로 믹서모듈 및 이를 포함하는 연소기

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8984888B2 (en) * 2011-10-26 2015-03-24 General Electric Company Fuel injection assembly for use in turbine engines and method of assembling same
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US9163839B2 (en) * 2012-03-19 2015-10-20 General Electric Company Micromixer combustion head end assembly
US9267690B2 (en) * 2012-05-29 2016-02-23 General Electric Company Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same
US9212822B2 (en) * 2012-05-30 2015-12-15 General Electric Company Fuel injection assembly for use in turbine engines and method of assembling same
US9151503B2 (en) * 2013-01-04 2015-10-06 General Electric Company Coaxial fuel supply for a micromixer
CN106907740B (zh) * 2013-10-18 2019-07-05 三菱重工业株式会社 燃料喷射器
US9664392B2 (en) * 2013-12-13 2017-05-30 General Electric Company Bundled tube fuel injector with outer shroud and outer band connection
US20150198332A1 (en) * 2014-01-16 2015-07-16 General Electric Company Channel defining fuel nozzle of combustion system
US9657642B2 (en) 2014-03-27 2017-05-23 Honeywell International Inc. Turbine sections of gas turbine engines with dual use of cooling air
US10605457B2 (en) 2014-05-19 2020-03-31 Siemens Aktiengesellschaft Burner arrangement with resonator
JP6437099B2 (ja) * 2014-08-26 2018-12-12 シーメンス エナジー インコーポレイテッド タービンエンジンの燃焼器内における燃料ノズル用の冷却システム
JP6551820B2 (ja) * 2014-09-29 2019-07-31 三菱日立パワーシステムズ株式会社 燃焼器、及びこれを備えているガスタービン
US20170227225A1 (en) * 2016-02-09 2017-08-10 General Electric Company Fuel injectors and methods of fabricating same
US10670271B2 (en) * 2016-09-30 2020-06-02 DOOSAN Heavy Industries Construction Co., LTD Acoustic dampening liner cap and gas turbine combustor including the same
US10788215B2 (en) * 2016-12-21 2020-09-29 General Electric Company Fuel nozzle assembly with flange orifice
JP6822894B2 (ja) * 2017-04-28 2021-01-27 三菱パワー株式会社 燃料噴射器及びガスタービン
JP6979343B2 (ja) 2017-11-30 2021-12-15 三菱パワー株式会社 燃料噴射器、燃焼器、及びガスタービン
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly
JP7270517B2 (ja) * 2019-10-01 2023-05-10 三菱重工業株式会社 ガスタービン燃焼器
EP4027059A1 (en) * 2021-01-12 2022-07-13 Crosstown Power GmbH Burner, combustor, and method for retrofitting a combustion appliance
KR102490477B1 (ko) * 2021-02-03 2023-01-19 두산에너빌리티 주식회사 분사노즐, 연소기 및 이를 포함하는 가스터빈
DE102022103746A1 (de) 2022-02-17 2023-08-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennersystem zur Erzeugung von Heißgas
US12215866B2 (en) 2022-02-18 2025-02-04 General Electric Company Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages
CN115031259B (zh) * 2022-03-18 2023-06-02 北京航空航天大学 一种燃气轮机燃烧室及其设计方法
US12313004B2 (en) 2022-08-26 2025-05-27 Collins Engine Nozzles, Inc. Proportional force modification of passive spool for control of secondary nozzle circuits
US11970977B2 (en) 2022-08-26 2024-04-30 Hamilton Sundstrand Corporation Variable restriction of a secondary circuit of a fuel injector
US12270343B2 (en) 2022-08-26 2025-04-08 Collins Engine Nozzles, Inc. Proportional restriction of fuel nozzle with an auxiliary circuit
US12286931B2 (en) 2022-08-26 2025-04-29 Collins Engine Nozzles, Inc. Variable restriction of a fuel circuit of a fuel nozzle
US12305581B2 (en) 2022-08-26 2025-05-20 Collins Engine Nozzles, Inc. Proportional restriction of a secondary circuit of a fuel injector
KR102733280B1 (ko) 2022-11-30 2024-11-25 두산에너빌리티 주식회사 노즐 어셈블리, 연소기 및 이를 포함하는 가스터빈
US20240271571A1 (en) * 2023-02-14 2024-08-15 Collins Engine Nozzles, Inc. Proportional control of cooling circuit of fuel nozzle
US20240271790A1 (en) * 2023-02-14 2024-08-15 Collins Engine Nozzles, Inc. Variable cooling of secondary circuit of fuel nozzles
KR102814686B1 (ko) 2023-05-02 2025-05-28 두산에너빌리티 주식회사 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈
KR102863422B1 (ko) * 2023-12-08 2025-09-22 두산에너빌리티 주식회사 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈
US12281795B1 (en) * 2024-03-11 2025-04-22 Rtx Corporation Cluster of swirled mini-mixers for fuel-staged, axially staged combustion

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3943705A (en) * 1974-11-15 1976-03-16 Westinghouse Electric Corporation Wide range catalytic combustor
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
RU2145039C1 (ru) * 1999-03-18 2000-01-27 Федеральное государственное унитарное предприятие "Исследовательский центр им.М.В.Келдыша" Способ подачи горючего в камеру теплового двигателя и устройство для его реализации
EP1742868A2 (en) 2004-04-27 2007-01-17 Velocys, Inc. Hydrogen peroxide production in microchannel reactors
US7513115B2 (en) 2005-05-23 2009-04-07 Power Systems Mfg., Llc Flashback suppression system for a gas turbine combustor
US7878000B2 (en) * 2005-12-20 2011-02-01 General Electric Company Pilot fuel injector for mixer assembly of a high pressure gas turbine engine
EP1990578A1 (de) 2007-05-08 2008-11-12 ALSTOM Technology Ltd Gasturbine mit Wassereinspritzung
US20100180564A1 (en) 2009-01-21 2010-07-22 General Electric Company Systems and Methods for Mitigating a Flashback Condition in a Premixed Combustor
US7942038B2 (en) 2009-01-21 2011-05-17 General Electric Company Systems and methods of monitoring acoustic pressure to detect a flame condition in a gas turbine
US8424311B2 (en) * 2009-02-27 2013-04-23 General Electric Company Premixed direct injection disk
US8157189B2 (en) * 2009-04-03 2012-04-17 General Electric Company Premixing direct injector
US8234872B2 (en) * 2009-05-01 2012-08-07 General Electric Company Turbine air flow conditioner
US8276385B2 (en) * 2009-10-08 2012-10-02 General Electric Company Staged multi-tube premixing injector
US20110162377A1 (en) * 2010-01-06 2011-07-07 General Electric Company Turbomachine nozzle
JP5372814B2 (ja) * 2010-03-17 2013-12-18 株式会社日立製作所 ガスタービン燃焼器、及び運転方法
US8307655B2 (en) * 2010-05-20 2012-11-13 General Electric Company System for cooling turbine combustor transition piece
US20120058437A1 (en) * 2010-09-08 2012-03-08 General Electric Company Apparatus and method for mixing fuel in a gas turbine nozzle
US8322143B2 (en) * 2011-01-18 2012-12-04 General Electric Company System and method for injecting fuel
US20120192566A1 (en) * 2011-01-28 2012-08-02 Jong Ho Uhm Fuel injection assembly for use in turbine engines and method of assembling same
US8875516B2 (en) * 2011-02-04 2014-11-04 General Electric Company Turbine combustor configured for high-frequency dynamics mitigation and related method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220117567A (ko) * 2021-02-17 2022-08-24 두산에너빌리티 주식회사 마이크로 믹서모듈 및 이를 포함하는 연소기
KR102460001B1 (ko) 2021-02-17 2022-10-26 두산에너빌리티 주식회사 마이크로 믹서모듈 및 이를 포함하는 연소기
US12049844B2 (en) 2021-02-17 2024-07-30 Doosan Enerbility Co., Ltd. Micro-mixer module and combustor having the same

Also Published As

Publication number Publication date
JP2013139993A (ja) 2013-07-18
RU2012146617A (ru) 2014-05-10
US8438851B1 (en) 2013-05-14
EP2613083A2 (en) 2013-07-10
RU2605164C2 (ru) 2016-12-20
CN103185353A (zh) 2013-07-03
CN103185353B (zh) 2016-12-21
EP2613083B1 (en) 2020-08-12
EP2613083A3 (en) 2017-12-20

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