JP2013096324A - ガスタービンシステム - Google Patents
ガスタービンシステム Download PDFInfo
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- JP2013096324A JP2013096324A JP2011240818A JP2011240818A JP2013096324A JP 2013096324 A JP2013096324 A JP 2013096324A JP 2011240818 A JP2011240818 A JP 2011240818A JP 2011240818 A JP2011240818 A JP 2011240818A JP 2013096324 A JP2013096324 A JP 2013096324A
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- fuel
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- gas turbine
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Classifications
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- 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
- F02C9/40—Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
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- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
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- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
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- 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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
- F02C7/1435—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages by water injection
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C99/00—Subject-matter not provided for in other groups of this subclass
- F23C99/008—Combustion methods wherein flame cooling techniques other than fuel or air staging or fume recirculation are used
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
- F23L7/002—Supplying water
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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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
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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
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2203/00—Flame cooling methods otherwise than by staging or recirculation
- F23C2203/30—Injection of tempering fluids
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/9901—Combustion process using hydrogen, hydrogen peroxide water or brown gas as fuel
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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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
【解決手段】水素ガスHおよび純水Wを噴射する燃料噴射ノズル4を有する燃焼器2と、燃焼器2に供給する純水Wを貯留する貯留水槽12と、燃焼器2に供給する水素ガスHを昇圧するガス圧縮装置10と、昇圧された水素ガスHを燃焼器2に導く燃料供給通路6と、貯留水槽12と燃料供給通路6とを連通して、昇圧された水素ガスHによって純水Wを加圧する導圧通路16とを備えている。
【選択図】図1
Description
図1は本発明の第1実施形態のガスタービンシステムの概略構成図を示す。同図において、ガスタービンエンジンGTは、圧縮機1と、燃焼器2と、タービン3とを主な構成要素とし、このガスタービンエンジンGTに発電機PUが連結されている。燃焼器2は燃料噴射ノズル4を有し、この燃料噴射ノズル弁4に燃料供給通路6と噴射水導入通路8とが接続されている。燃料供給通路6は、燃焼器2に気体燃料である水素ガスHを供給する通路で、噴射水導入通路8は、燃焼器2に噴射水である純水Wを供給する通路である。純水Wは、燃焼器2内の火炎温度を下げて低NOxを図るために供給される。
まず、ガスタービンエンジンGTの稼動しない夜間に、図1に示す純水製造装置14を外部の夜間電力で運転して、1日分の純水Wを製造して貯留水槽12に貯留しておく。
2 燃焼器
3 タービン
4 燃料噴射ノズル
6 燃料供給通路
10 ガス圧縮装置(燃料昇圧手段)
12 貯留水槽
14 純水製造装置
16 導圧通路
40 液体水素圧縮装置(燃料昇圧手段)
GT ガスタービンエンジン
H 水素ガス(気体燃料)
W 純水(噴射水)
Claims (4)
- 気体燃料および噴射水を噴射する燃料噴射ノズルを有する燃焼器と、
前記燃焼器に供給する前記噴射水を貯留する貯留水槽と、
前記燃焼器に供給する気体燃料を昇圧する燃料昇圧手段と、
昇圧された前記気体燃料を前記燃焼器に導く燃料供給通路と、
前記貯留水槽と前記燃料供給通路とを連通して、昇圧された前記気体燃料によって前記噴射水を加圧する導圧通路と、
を備えたガスタービンシステム。 - 請求項1において、前記燃焼器は、前記気体燃料と前記噴射水とを予混合する予混合型であるガスタービンシステム。
- 請求項2において、前記気体燃料は水素ガスであるガスタービンシステム。
- 請求項1,2または3において、さらに、純水からなる前記噴射水を製造する純水製造装置を備えたガスタービンシステム。
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011240818A JP5816522B2 (ja) | 2011-11-02 | 2011-11-02 | ガスタービンシステム |
PCT/JP2012/077849 WO2013065624A1 (ja) | 2011-11-02 | 2012-10-29 | ガスタービンシステム |
EP12846297.5A EP2775120B1 (en) | 2011-11-02 | 2012-10-29 | Gas turbine system |
RU2014119542/06A RU2014119542A (ru) | 2011-11-02 | 2012-10-29 | Газотурбинная система |
CA2854079A CA2854079C (en) | 2011-11-02 | 2012-10-29 | Gas turbine system |
US14/355,774 US10041417B2 (en) | 2011-11-02 | 2012-10-29 | Gas turbine system with injection water pressurization passage |
AU2012333652A AU2012333652B2 (en) | 2011-11-02 | 2012-10-29 | Gas turbine system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011240818A JP5816522B2 (ja) | 2011-11-02 | 2011-11-02 | ガスタービンシステム |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2013096324A true JP2013096324A (ja) | 2013-05-20 |
JP2013096324A5 JP2013096324A5 (ja) | 2014-08-07 |
JP5816522B2 JP5816522B2 (ja) | 2015-11-18 |
Family
ID=48191971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011240818A Active JP5816522B2 (ja) | 2011-11-02 | 2011-11-02 | ガスタービンシステム |
Country Status (7)
Country | Link |
---|---|
US (1) | US10041417B2 (ja) |
EP (1) | EP2775120B1 (ja) |
JP (1) | JP5816522B2 (ja) |
AU (1) | AU2012333652B2 (ja) |
CA (1) | CA2854079C (ja) |
RU (1) | RU2014119542A (ja) |
WO (1) | WO2013065624A1 (ja) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015166597A1 (ja) * | 2014-04-30 | 2015-11-05 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器、ガスタービン、制御装置及び制御方法 |
WO2016051758A1 (ja) * | 2014-09-29 | 2016-04-07 | 川崎重工業株式会社 | ガスタービン |
WO2021234979A1 (ja) * | 2020-05-18 | 2021-11-25 | 国立大学法人東北大学 | ガスタービン |
Families Citing this family (14)
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JP6327826B2 (ja) * | 2013-10-11 | 2018-05-23 | 川崎重工業株式会社 | ガスタービンの燃料噴射装置 |
US20160348911A1 (en) * | 2013-12-12 | 2016-12-01 | Siemens Energy, Inc. | W501 d5/d5a df42 combustion system |
CN106574775B (zh) * | 2014-08-14 | 2019-10-18 | 西门子公司 | 具有双孔口雾化器的多功能燃料喷嘴 |
CN107735555A (zh) * | 2015-07-24 | 2018-02-23 | 陈俊廷 | 以水作为辅助动力的内燃机引擎 |
KR101835421B1 (ko) * | 2015-12-31 | 2018-03-08 | 한국항공우주연구원 | 습식 압축용 환형 분사 장치 |
US20170254264A1 (en) | 2016-03-03 | 2017-09-07 | Technische Universität Berlin | Swirl-stabilised burner having an inertisation front and related methods |
JP6722491B2 (ja) * | 2016-04-01 | 2020-07-15 | 川崎重工業株式会社 | ガスタービンの燃焼器 |
DE102018126496A1 (de) * | 2018-10-24 | 2020-04-30 | HK Innovation UG (haftungsbeschränkt) | Vorrichtung und Verfahren zum Antreiben eines Fahrzeugs, Flugzeugs, Schiffs oder dergleichen sowie Fahrzeug, Flugzeug, Schiff oder dergleichen, welches eine derartige Vorrichtung aufweist und/oder mit einem solchen Verfahren betreibbar ist |
US11286884B2 (en) * | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
WO2020242556A1 (en) * | 2019-05-30 | 2020-12-03 | Siemens Aktiengesellschaft | Gas turbine water injection for emissions reduction |
US11306661B1 (en) | 2020-12-04 | 2022-04-19 | General Electric Company | Methods and apparatus to operate a gas turbine engine with hydrogen gas |
EP4056903A1 (en) * | 2021-03-07 | 2022-09-14 | CPS-Holding Limited | Hydrogen-fueled combustor for gas turbines |
US11692709B2 (en) | 2021-03-11 | 2023-07-04 | General Electric Company | Gas turbine fuel mixer comprising a plurality of mini tubes for generating a fuel-air mixture |
WO2024116966A1 (ja) * | 2022-12-01 | 2024-06-06 | 三菱重工業株式会社 | ガスタービンの運転方法 |
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2012
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- 2012-10-29 AU AU2012333652A patent/AU2012333652B2/en active Active
- 2012-10-29 US US14/355,774 patent/US10041417B2/en active Active
- 2012-10-29 RU RU2014119542/06A patent/RU2014119542A/ru unknown
- 2012-10-29 WO PCT/JP2012/077849 patent/WO2013065624A1/ja active Application Filing
- 2012-10-29 CA CA2854079A patent/CA2854079C/en active Active
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WO2015166597A1 (ja) * | 2014-04-30 | 2015-11-05 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器、ガスタービン、制御装置及び制御方法 |
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WO2021234979A1 (ja) * | 2020-05-18 | 2021-11-25 | 国立大学法人東北大学 | ガスタービン |
US11959417B2 (en) | 2020-05-18 | 2024-04-16 | Tohoku University | Ammonia-fueled gas turbine |
Also Published As
Publication number | Publication date |
---|---|
RU2014119542A (ru) | 2015-12-10 |
EP2775120A1 (en) | 2014-09-10 |
WO2013065624A1 (ja) | 2013-05-10 |
CA2854079C (en) | 2016-08-16 |
AU2012333652A1 (en) | 2014-06-19 |
EP2775120A4 (en) | 2015-04-29 |
AU2012333652B2 (en) | 2015-11-05 |
US10041417B2 (en) | 2018-08-07 |
JP5816522B2 (ja) | 2015-11-18 |
CA2854079A1 (en) | 2013-05-10 |
EP2775120B1 (en) | 2017-11-29 |
US20140283498A1 (en) | 2014-09-25 |
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