RU2605164C2 - Блок топливных форсунок и блок камеры сгорания - Google Patents

Блок топливных форсунок и блок камеры сгорания Download PDF

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Publication number
RU2605164C2
RU2605164C2 RU2012146617/06A RU2012146617A RU2605164C2 RU 2605164 C2 RU2605164 C2 RU 2605164C2 RU 2012146617/06 A RU2012146617/06 A RU 2012146617/06A RU 2012146617 A RU2012146617 A RU 2012146617A RU 2605164 C2 RU2605164 C2 RU 2605164C2
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RU
Russia
Prior art keywords
pressure chamber
cooling fluid
fuel
wall
chamber
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RU2012146617/06A
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English (en)
Russian (ru)
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RU2012146617A (ru
Inventor
Цзон Хо АХМ
Томас Эдвард ДЖОНСОН
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Дженерал Электрик Компани
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Publication of RU2012146617A publication Critical patent/RU2012146617A/ru
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Publication of RU2605164C2 publication Critical patent/RU2605164C2/ru

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    • 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

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  • 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)
RU2012146617/06A 2012-01-03 2012-11-02 Блок топливных форсунок и блок камеры сгорания RU2605164C2 (ru)

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 (2)

Publication Number Publication Date
RU2012146617A RU2012146617A (ru) 2014-05-10
RU2605164C2 true RU2605164C2 (ru) 2016-12-20

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012146617/06A RU2605164C2 (ru) 2012-01-03 2012-11-02 Блок топливных форсунок и блок камеры сгорания

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)

Families Citing this family (41)

* 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
WO2015056337A1 (ja) 2013-10-18 2015-04-23 三菱重工業株式会社 燃料噴射器
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
KR102460001B1 (ko) * 2021-02-17 2022-10-26 두산에너빌리티 주식회사 마이크로 믹서모듈 및 이를 포함하는 연소기
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
US12305581B2 (en) 2022-08-26 2025-05-20 Collins Engine Nozzles, Inc. Proportional restriction of a secondary circuit of a fuel injector
US12286931B2 (en) 2022-08-26 2025-04-29 Collins Engine Nozzles, Inc. Variable restriction of a fuel circuit of a fuel nozzle
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
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

Citations (5)

* 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
US7513115B2 (en) * 2005-05-23 2009-04-07 Power Systems Mfg., Llc Flashback suppression system for a gas turbine combustor
US7959880B2 (en) * 2004-04-27 2011-06-14 Velocys, Inc. Hydrogen peroxide production in microchannel reactors

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Patent Citations (5)

* 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
US7959880B2 (en) * 2004-04-27 2011-06-14 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

Also Published As

Publication number Publication date
EP2613083B1 (en) 2020-08-12
JP6030919B2 (ja) 2016-11-24
CN103185353A (zh) 2013-07-03
EP2613083A3 (en) 2017-12-20
CN103185353B (zh) 2016-12-21
EP2613083A2 (en) 2013-07-10
US8438851B1 (en) 2013-05-14
JP2013139993A (ja) 2013-07-18
RU2012146617A (ru) 2014-05-10

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Effective date: 20171103