RU2618765C2 - Система для подачи топлива в камеру сгорания (варианты) - Google Patents
Система для подачи топлива в камеру сгорания (варианты) Download PDFInfo
- Publication number
- RU2618765C2 RU2618765C2 RU2013119328A RU2013119328A RU2618765C2 RU 2618765 C2 RU2618765 C2 RU 2618765C2 RU 2013119328 A RU2013119328 A RU 2013119328A RU 2013119328 A RU2013119328 A RU 2013119328A RU 2618765 C2 RU2618765 C2 RU 2618765C2
- Authority
- RU
- Russia
- Prior art keywords
- chamber
- combustion chamber
- liquid fuel
- channels
- partition
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 118
- 239000000446 fuel Substances 0.000 title claims abstract description 112
- 239000007788 liquid Substances 0.000 claims abstract description 59
- 239000012530 fluid Substances 0.000 claims abstract description 40
- 238000004891 communication Methods 0.000 claims abstract description 23
- 238000005192 partition Methods 0.000 claims description 25
- 230000000694 effects Effects 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 description 14
- 238000002156 mixing Methods 0.000 description 11
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 9
- 239000007789 gas Substances 0.000 description 8
- 230000007704 transition Effects 0.000 description 7
- 239000003570 air Substances 0.000 description 6
- 230000005611 electricity Effects 0.000 description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 3
- 229910002091 carbon monoxide Inorganic materials 0.000 description 3
- 239000000295 fuel oil Substances 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 239000003949 liquefied natural gas Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000004939 coking Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
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
- F23R3/346—Feeding into different combustion zones for staged 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/36—Supply of different fuels
-
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Spray-Type Burners (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/457,726 | 2012-04-27 | ||
| US13/457,726 US9200808B2 (en) | 2012-04-27 | 2012-04-27 | System for supplying fuel to a late-lean fuel injector of a combustor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2013119328A RU2013119328A (ru) | 2014-11-10 |
| RU2618765C2 true RU2618765C2 (ru) | 2017-05-11 |
Family
ID=48182805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2013119328A RU2618765C2 (ru) | 2012-04-27 | 2013-04-26 | Система для подачи топлива в камеру сгорания (варианты) |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9200808B2 (enExample) |
| EP (1) | EP2657611B1 (enExample) |
| JP (1) | JP6203528B2 (enExample) |
| CN (1) | CN103375816B (enExample) |
| RU (1) | RU2618765C2 (enExample) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9297534B2 (en) | 2011-07-29 | 2016-03-29 | General Electric Company | Combustor portion for a turbomachine and method of operating a turbomachine |
| US8904796B2 (en) * | 2011-10-19 | 2014-12-09 | General Electric Company | Flashback resistant tubes for late lean injector and method for forming the tubes |
| US20130111918A1 (en) * | 2011-11-07 | 2013-05-09 | General Electric Company | Combustor assembly for a gas turbomachine |
| US9097424B2 (en) * | 2012-03-12 | 2015-08-04 | General Electric Company | System for supplying a fuel and working fluid mixture to a combustor |
| US8745986B2 (en) * | 2012-07-10 | 2014-06-10 | General Electric Company | System and method of supplying fuel to a gas turbine |
| WO2014092185A1 (ja) * | 2012-12-13 | 2014-06-19 | 川崎重工業株式会社 | マルチ燃料対応のガスタービン燃焼器 |
| US10139111B2 (en) * | 2014-03-28 | 2018-11-27 | Siemens Energy, Inc. | Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine |
| EP2902708B1 (en) * | 2014-06-12 | 2017-02-01 | Kawasaki Jukogyo Kabushiki Kaisha | Multi-fuel-supporting gas-turbine combustor |
| CN106574777B (zh) * | 2014-08-26 | 2020-02-07 | 西门子能源公司 | 用于涡轮发动机中的燃烧器内的燃料喷嘴的冷却系统 |
| FR3029271B1 (fr) * | 2014-11-28 | 2019-06-21 | Safran Aircraft Engines | Paroi annulaire de deflection pour systeme d'injection de chambre de combustion de turbomachine offrant une zone etendue d'atomisation de carburant |
| JP2016109309A (ja) * | 2014-12-02 | 2016-06-20 | 川崎重工業株式会社 | ガスタービン用燃焼器、及びガスタービン |
| US10837641B2 (en) | 2014-12-25 | 2020-11-17 | Kawasaki Jukogyo Kabushiki Kaisha | Burner, combustor, and gas turbine |
| US10054314B2 (en) * | 2015-12-17 | 2018-08-21 | General Electric Company | Slotted injector for axial fuel staging |
| US20170260866A1 (en) * | 2016-03-10 | 2017-09-14 | Siemens Energy, Inc. | Ducting arrangement in a combustion system of a gas turbine engine |
| US20170268776A1 (en) * | 2016-03-15 | 2017-09-21 | General Electric Company | Gas turbine flow sleeve mounting |
| WO2018026382A1 (en) * | 2016-08-03 | 2018-02-08 | Siemens Aktiengesellschaft | Ducting arrangement with injector assemblies configured to form a shielding flow of air injected into a combustion stage in a gas turbine engine |
| CN109563996B (zh) * | 2016-08-03 | 2021-03-12 | 西门子股份公司 | 具有设置成重新捕获燃烧器壁中的冷却空气以在燃烧工段形成防护空气流的喷射器组件的燃烧系统 |
| US10502426B2 (en) | 2017-05-12 | 2019-12-10 | General Electric Company | Dual fuel injectors and methods of use in gas turbine combustor |
| US20180340689A1 (en) * | 2017-05-25 | 2018-11-29 | General Electric Company | Low Profile Axially Staged Fuel Injector |
| US10690349B2 (en) * | 2017-09-01 | 2020-06-23 | General Electric Company | Premixing fuel injectors and methods of use in gas turbine combustor |
| US11187415B2 (en) * | 2017-12-11 | 2021-11-30 | General Electric Company | Fuel injection assemblies for axial fuel staging in gas turbine combustors |
| US11137144B2 (en) * | 2017-12-11 | 2021-10-05 | General Electric Company | Axial fuel staging system for gas turbine combustors |
| US10816203B2 (en) * | 2017-12-11 | 2020-10-27 | General Electric Company | Thimble assemblies for introducing a cross-flow into a secondary combustion zone |
| US11022308B2 (en) | 2018-05-31 | 2021-06-01 | Honeywell International Inc. | Double wall combustors with strain isolated inserts |
| US11933223B2 (en) * | 2019-04-18 | 2024-03-19 | Rtx Corporation | Integrated additive fuel injectors for attritable engines |
| KR102164620B1 (ko) * | 2019-06-19 | 2020-10-12 | 두산중공업 주식회사 | 연소기 및 이를 포함하는 가스터빈 |
| US11333360B2 (en) * | 2020-09-25 | 2022-05-17 | General Electric Company | Fuel injector for a turbomachine |
| US11846426B2 (en) | 2021-06-24 | 2023-12-19 | General Electric Company | Gas turbine combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel |
| CN114909675B (zh) * | 2022-04-07 | 2024-03-01 | 中国联合重型燃气轮机技术有限公司 | 用于燃气涡轮机的燃烧室和燃气轮机 |
| CN117109030B (zh) * | 2022-05-16 | 2025-09-19 | 通用电气公司 | 燃烧器衬里中的热声阻尼器 |
| CA3257195A1 (en) * | 2022-05-23 | 2023-11-30 | Casale Sa | BURNER FOR REFORMING REACTOR |
| CN115059544A (zh) * | 2022-07-01 | 2022-09-16 | 星辰萌想科技(北京)有限公司 | 一种具有双燃烧部的燃气轮机 |
| CN115075946B (zh) * | 2022-07-01 | 2024-11-01 | 星辰萌想科技(北京)有限公司 | 一种双燃烧部燃气轮机 |
| DE102022208339A1 (de) * | 2022-08-10 | 2024-02-15 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammeranordnung zum Betrieb mit flüssigem und/oder gasförmigem Kraftstoff, Gasturbinenanordnung und Verfahren |
| US12188658B1 (en) | 2023-07-07 | 2025-01-07 | Ge Infrastructure Technology Llc | Fuel injection assembly for a combustor |
| US12467630B2 (en) | 2023-07-07 | 2025-11-11 | Ge Vernova Infrastructure Technology Llc | Fuel injection assembly having a boss with a serpentine cooling passage |
| US12429224B1 (en) * | 2024-05-09 | 2025-09-30 | Ge Infrastructure Technology Llc | Axial fuel stage injector with fuel injection in same direction as high-pressure air flow |
| US12449128B1 (en) | 2024-11-27 | 2025-10-21 | Ge Vernova Infrastructure Technology Llc | Boss for a fuel injection assembly having cooling circuit and combustor provided therewith |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2135898C1 (ru) * | 1994-05-21 | 1999-08-27 | Роллс-Ройс Лимитид | Камера сгорания газовой турбины и топливный инжектор газотурбинного двигателя |
| US20060156734A1 (en) * | 2005-01-15 | 2006-07-20 | Siemens Westinghouse Power Corporation | Gas turbine combustor |
| US20070022758A1 (en) * | 2005-06-30 | 2007-02-01 | General Electric Company | Reverse-flow gas turbine combustion system |
| US20070151251A1 (en) * | 2006-01-03 | 2007-07-05 | Haynes Joel M | Counterflow injection mechanism having coaxial fuel-air passages |
| RU86280U1 (ru) * | 2009-04-10 | 2009-08-27 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Устройство сжигания топлива в камере сгорания |
| US20110179803A1 (en) * | 2010-01-27 | 2011-07-28 | General Electric Company | Bled diffuser fed secondary combustion system for gas turbines |
Family Cites Families (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2221621B1 (enExample) * | 1973-03-13 | 1976-09-10 | Snecma | |
| US3901445A (en) * | 1974-11-08 | 1975-08-26 | Pullman Inc | Gas burner - lance construction |
| JPS6143637U (ja) * | 1984-08-21 | 1986-03-22 | 三菱重工業株式会社 | ガスタ−ビンの燃焼バ−ナ |
| US5749219A (en) * | 1989-11-30 | 1998-05-12 | United Technologies Corporation | Combustor with first and second zones |
| US5207064A (en) | 1990-11-21 | 1993-05-04 | General Electric Company | Staged, mixed combustor assembly having low emissions |
| US5235813A (en) * | 1990-12-24 | 1993-08-17 | United Technologies Corporation | Mechanism for controlling the rate of mixing in combusting flows |
| DE4411623A1 (de) * | 1994-04-02 | 1995-10-05 | Abb Management Ag | Vormischbrenner |
| JP3346034B2 (ja) * | 1994-06-30 | 2002-11-18 | 石川島播磨重工業株式会社 | ガスタービン用燃焼装置 |
| JPH08145361A (ja) * | 1994-11-16 | 1996-06-07 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービン用燃料噴射弁 |
| JP3012166B2 (ja) * | 1995-02-01 | 2000-02-21 | 川崎重工業株式会社 | ガスタービン燃焼システム |
| US5622054A (en) * | 1995-12-22 | 1997-04-22 | General Electric Company | Low NOx lobed mixer fuel injector |
| US6122916A (en) * | 1998-01-02 | 2000-09-26 | Siemens Westinghouse Power Corporation | Pilot cones for dry low-NOx combustors |
| GB9813972D0 (en) * | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
| DE59910909D1 (de) * | 1998-08-20 | 2004-11-25 | Siemens Ag | Verfahren zum betrieb eines hybridbrenners |
| US6868676B1 (en) * | 2002-12-20 | 2005-03-22 | General Electric Company | Turbine containing system and an injector therefor |
| JP2005147459A (ja) * | 2003-11-13 | 2005-06-09 | Hitachi Ltd | ガスタービン燃焼器及びガスタービン燃焼器の燃料供給方法 |
| JP4670035B2 (ja) * | 2004-06-25 | 2011-04-13 | 独立行政法人 宇宙航空研究開発機構 | ガスタービン燃焼器 |
| JP2006090602A (ja) * | 2004-09-22 | 2006-04-06 | Japan Aerospace Exploration Agency | ローブミキサー及び予混合器 |
| US8387390B2 (en) * | 2006-01-03 | 2013-03-05 | General Electric Company | Gas turbine combustor having counterflow injection mechanism |
| CN101235969B (zh) * | 2007-01-31 | 2014-11-26 | 通用电气公司 | 具有同轴燃料-空气通道的逆流喷射机构 |
| JP5193695B2 (ja) * | 2008-06-17 | 2013-05-08 | 新潟原動機株式会社 | 燃料噴射装置 |
| RU2506497C2 (ru) * | 2008-09-29 | 2014-02-10 | Сименс Акциенгезелльшафт | Топливная форсунка |
| US20100223930A1 (en) * | 2009-03-06 | 2010-09-09 | General Electric Company | Injection device for a turbomachine |
| US8991192B2 (en) * | 2009-09-24 | 2015-03-31 | Siemens Energy, Inc. | Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine |
| EP2362148A1 (en) * | 2010-02-23 | 2011-08-31 | Siemens Aktiengesellschaft | Fuel injector and swirler assembly with lobed mixer |
| US8752386B2 (en) * | 2010-05-25 | 2014-06-17 | Siemens Energy, Inc. | Air/fuel supply system for use in a gas turbine engine |
| US8769955B2 (en) * | 2010-06-02 | 2014-07-08 | Siemens Energy, Inc. | Self-regulating fuel staging port for turbine combustor |
-
2012
- 2012-04-27 US US13/457,726 patent/US9200808B2/en active Active
-
2013
- 2013-04-24 EP EP13165222.4A patent/EP2657611B1/en active Active
- 2013-04-25 JP JP2013091859A patent/JP6203528B2/ja not_active Expired - Fee Related
- 2013-04-26 CN CN201310149399.5A patent/CN103375816B/zh not_active Expired - Fee Related
- 2013-04-26 RU RU2013119328A patent/RU2618765C2/ru not_active IP Right Cessation
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2135898C1 (ru) * | 1994-05-21 | 1999-08-27 | Роллс-Ройс Лимитид | Камера сгорания газовой турбины и топливный инжектор газотурбинного двигателя |
| US20060156734A1 (en) * | 2005-01-15 | 2006-07-20 | Siemens Westinghouse Power Corporation | Gas turbine combustor |
| US20070022758A1 (en) * | 2005-06-30 | 2007-02-01 | General Electric Company | Reverse-flow gas turbine combustion system |
| US20070151251A1 (en) * | 2006-01-03 | 2007-07-05 | Haynes Joel M | Counterflow injection mechanism having coaxial fuel-air passages |
| RU86280U1 (ru) * | 2009-04-10 | 2009-08-27 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Устройство сжигания топлива в камере сгорания |
| US20110179803A1 (en) * | 2010-01-27 | 2011-07-28 | General Electric Company | Bled diffuser fed secondary combustion system for gas turbines |
Also Published As
| Publication number | Publication date |
|---|---|
| US9200808B2 (en) | 2015-12-01 |
| US20130283801A1 (en) | 2013-10-31 |
| CN103375816A (zh) | 2013-10-30 |
| RU2013119328A (ru) | 2014-11-10 |
| JP6203528B2 (ja) | 2017-09-27 |
| JP2013231580A (ja) | 2013-11-14 |
| EP2657611B1 (en) | 2019-11-20 |
| EP2657611A3 (en) | 2017-11-22 |
| CN103375816B (zh) | 2016-08-17 |
| EP2657611A2 (en) | 2013-10-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2618765C2 (ru) | Система для подачи топлива в камеру сгорания (варианты) | |
| RU2613764C2 (ru) | Система для подачи рабочей текучей среды в камеру сгорания (варианты) | |
| RU2614887C2 (ru) | Камера сгорания (варианты) | |
| RU2611135C2 (ru) | Система (варианты) и способ для подачи рабочей текучей среды в камеру сгорания | |
| US9284888B2 (en) | System for supplying fuel to late-lean fuel injectors of a combustor | |
| US8677753B2 (en) | System for supplying a working fluid to a combustor | |
| US8479518B1 (en) | System for supplying a working fluid to a combustor | |
| US8745986B2 (en) | System and method of supplying fuel to a gas turbine | |
| US9188337B2 (en) | System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20200427 |