NO913362D0 - Gassturbin for kraftproduksjon. - Google Patents
Gassturbin for kraftproduksjon.Info
- Publication number
- NO913362D0 NO913362D0 NO913362A NO913362A NO913362D0 NO 913362 D0 NO913362 D0 NO 913362D0 NO 913362 A NO913362 A NO 913362A NO 913362 A NO913362 A NO 913362A NO 913362 D0 NO913362 D0 NO 913362D0
- Authority
- NO
- Norway
- Prior art keywords
- gas turbine
- power production
- production
- power
- turbine
- Prior art date
Links
Classifications
-
- 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
-
- 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
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
-
- 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
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/36—Supply of different fuels
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/573,727 US5203796A (en) | 1990-08-28 | 1990-08-28 | Two stage v-gutter fuel injection mixer |
Publications (2)
Publication Number | Publication Date |
---|---|
NO913362D0 true NO913362D0 (no) | 1991-08-27 |
NO913362L NO913362L (no) | 1992-03-02 |
Family
ID=24293151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO91913362A NO913362L (no) | 1990-08-28 | 1991-08-27 | Gassturbin for kraftproduksjon. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5203796A (no) |
EP (1) | EP0473371A1 (no) |
JP (1) | JPH04244511A (no) |
KR (1) | KR940001926B1 (no) |
NO (1) | NO913362L (no) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2696502B1 (fr) * | 1992-10-07 | 1994-11-04 | Snecma | Dispositif de post-combustion pour turbo réacteur double flux. |
FR2706588B1 (fr) * | 1993-06-16 | 1995-07-21 | Snecma | Système d'injection de carburant pour chambre de combustion. |
US5927076A (en) * | 1996-10-22 | 1999-07-27 | Westinghouse Electric Corporation | Multiple venturi ultra-low nox combustor |
US5782079A (en) * | 1997-02-25 | 1998-07-21 | Industrial Technology Research Institute | Miniature liquid-fueled turbojet engine |
WO2000019081A2 (en) * | 1998-08-17 | 2000-04-06 | Ramgen Power Systems, Inc. | Fuel supply and fuel - air mixing for a ram jet combustor |
FR2835906B1 (fr) * | 2002-02-13 | 2004-06-04 | Saint Gobain Isover | Bruleur a combustion interne, notamment pour l'etirage de fibres minerales |
US7308793B2 (en) * | 2005-01-07 | 2007-12-18 | Power Systems Mfg., Llc | Apparatus and method for reducing carbon monoxide emissions |
US8671658B2 (en) * | 2007-10-23 | 2014-03-18 | Ener-Core Power, Inc. | Oxidizing fuel |
US20090111063A1 (en) * | 2007-10-29 | 2009-04-30 | General Electric Company | Lean premixed, radial inflow, multi-annular staged nozzle, can-annular, dual-fuel combustor |
US9822649B2 (en) * | 2008-11-12 | 2017-11-21 | General Electric Company | Integrated combustor and stage 1 nozzle in a gas turbine and method |
US8701413B2 (en) | 2008-12-08 | 2014-04-22 | Ener-Core Power, Inc. | Oxidizing fuel in multiple operating modes |
EP2208934A1 (en) * | 2009-01-15 | 2010-07-21 | ALSTOM Technology Ltd | Burner of a gas turbine for a reactive fuel air mixture |
US8616002B2 (en) * | 2009-07-23 | 2013-12-31 | General Electric Company | Gas turbine premixing systems |
US8763400B2 (en) * | 2009-08-04 | 2014-07-01 | General Electric Company | Aerodynamic pylon fuel injector system for combustors |
WO2011054771A2 (en) | 2009-11-07 | 2011-05-12 | Alstom Technology Ltd | Premixed burner for a gas turbine combustor |
WO2011054766A2 (en) | 2009-11-07 | 2011-05-12 | Alstom Technology Ltd | Reheat burner injection system |
EP2496885B1 (en) | 2009-11-07 | 2019-05-29 | Ansaldo Energia Switzerland AG | Burner with a cooling system allowing an increased gas turbine efficiency |
WO2011054757A2 (en) | 2009-11-07 | 2011-05-12 | Alstom Technology Ltd | Reheat burner injection system with fuel lances |
EP2496880B1 (en) | 2009-11-07 | 2018-12-05 | Ansaldo Energia Switzerland AG | Reheat burner injection system |
US9027324B2 (en) * | 2010-12-28 | 2015-05-12 | Rolls-Royce North American Technologies, Inc. | Engine and combustion system |
US8863525B2 (en) | 2011-01-03 | 2014-10-21 | General Electric Company | Combustor with fuel staggering for flame holding mitigation |
US20120167578A1 (en) * | 2011-01-04 | 2012-07-05 | General Electric Company | Flame holding inhibitor for a lean pre-nozzle fuel injection diffuser and related method |
US8955329B2 (en) | 2011-10-21 | 2015-02-17 | General Electric Company | Diffusion nozzles for low-oxygen fuel nozzle assembly and method |
US11015808B2 (en) | 2011-12-13 | 2021-05-25 | General Electric Company | Aerodynamically enhanced premixer with purge slots for reduced emissions |
US9359947B2 (en) | 2012-03-09 | 2016-06-07 | Ener-Core Power, Inc. | Gradual oxidation with heat control |
US9353946B2 (en) | 2012-03-09 | 2016-05-31 | Ener-Core Power, Inc. | Gradual oxidation with heat transfer |
US9567903B2 (en) | 2012-03-09 | 2017-02-14 | Ener-Core Power, Inc. | Gradual oxidation with heat transfer |
US9328660B2 (en) | 2012-03-09 | 2016-05-03 | Ener-Core Power, Inc. | Gradual oxidation and multiple flow paths |
US9347664B2 (en) | 2012-03-09 | 2016-05-24 | Ener-Core Power, Inc. | Gradual oxidation with heat control |
US9381484B2 (en) | 2012-03-09 | 2016-07-05 | Ener-Core Power, Inc. | Gradual oxidation with adiabatic temperature above flameout temperature |
US9359948B2 (en) | 2012-03-09 | 2016-06-07 | Ener-Core Power, Inc. | Gradual oxidation with heat control |
US9534780B2 (en) | 2012-03-09 | 2017-01-03 | Ener-Core Power, Inc. | Hybrid gradual oxidation |
US9328916B2 (en) | 2012-03-09 | 2016-05-03 | Ener-Core Power, Inc. | Gradual oxidation with heat control |
US9726374B2 (en) | 2012-03-09 | 2017-08-08 | Ener-Core Power, Inc. | Gradual oxidation with flue gas |
US9371993B2 (en) | 2012-03-09 | 2016-06-21 | Ener-Core Power, Inc. | Gradual oxidation below flameout temperature |
US10094289B2 (en) * | 2012-09-06 | 2018-10-09 | United Technologies Corporation | Cavity swirl fuel injector for an augmentor section of a gas turbine engine |
CA2830031C (en) * | 2012-10-23 | 2016-03-15 | Alstom Technology Ltd. | Burner for a can combustor |
US10436117B2 (en) * | 2013-01-18 | 2019-10-08 | United Technologies Corporation | Carbureted fuel injection system for a gas turbine engine |
JP6206648B2 (ja) * | 2013-07-08 | 2017-10-04 | 三菱日立パワーシステムズ株式会社 | チップホルダ、これを備える燃焼器ノズル、この燃焼器ノズルを備える燃焼器、及び燃焼器ノズルの製造方法 |
CA2988555C (en) * | 2015-06-16 | 2019-03-26 | Ihi Corporation | Engine aft section structure |
US11149948B2 (en) | 2017-08-21 | 2021-10-19 | General Electric Company | Fuel nozzle with angled main injection ports and radial main injection ports |
WO2023033855A1 (en) * | 2021-08-31 | 2023-03-09 | Siemens Energy, Inc. | Combustor having bluff bodies |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2632300A (en) * | 1949-08-03 | 1953-03-24 | Thermal Res & Engineering Corp | Combustion stabilization means having igniter grill heated by pilotburner |
US2771743A (en) * | 1951-08-10 | 1956-11-27 | Rolls Royce | Gas-turbine engine with reheat combustion equipment |
GB709452A (en) * | 1951-10-16 | 1954-05-26 | Napier & Son Ltd | Improvements in or relating to liquid fuel combustion apparatus more particularly for gas turbine plant |
US2948117A (en) * | 1956-10-01 | 1960-08-09 | Gen Electric | Afterburner flameholder |
US3018626A (en) * | 1960-02-02 | 1962-01-30 | Gen Electric | Vapor combustion system |
FR1321385A (fr) * | 1962-05-09 | 1963-03-15 | Rolls Royce | Réchauffeur à combustion pour turbine à gaz ou analogue |
US3176465A (en) * | 1962-08-27 | 1965-04-06 | Gen Electric | Vapor fuel injector flameholder |
FR1364192A (fr) * | 1963-05-22 | 1964-06-19 | Bristol Siddeley Engines Ltd | Perfectionnements apportés aux moteurs de propulsion par réaction |
US3153324A (en) * | 1963-05-29 | 1964-10-20 | Robert E Meyer | Simplified primary fuel system |
US3315468A (en) * | 1965-10-01 | 1967-04-25 | Gen Electric | Cooled flameholder assembly |
US3777983A (en) * | 1971-12-16 | 1973-12-11 | Gen Electric | Gas cooled dual fuel air atomized fuel nozzle |
JPS5026880B2 (no) * | 1973-05-08 | 1975-09-03 | ||
US4445339A (en) * | 1980-11-24 | 1984-05-01 | General Electric Co. | Wingtip vortex flame stabilizer for gas turbine combustor flame holder |
GB2175993B (en) * | 1985-06-07 | 1988-12-21 | Rolls Royce | Improvements in or relating to dual fuel injectors |
US4893468A (en) * | 1987-11-30 | 1990-01-16 | General Electric Company | Emissions control for gas turbine engine |
-
1990
- 1990-08-28 US US07/573,727 patent/US5203796A/en not_active Expired - Fee Related
-
1991
- 1991-04-30 KR KR1019910006928A patent/KR940001926B1/ko active IP Right Grant
- 1991-08-12 JP JP3225339A patent/JPH04244511A/ja active Pending
- 1991-08-23 EP EP91307762A patent/EP0473371A1/en not_active Ceased
- 1991-08-27 NO NO91913362A patent/NO913362L/no unknown
Also Published As
Publication number | Publication date |
---|---|
KR920020066A (ko) | 1992-11-20 |
EP0473371A1 (en) | 1992-03-04 |
JPH04244511A (ja) | 1992-09-01 |
US5203796A (en) | 1993-04-20 |
KR940001926B1 (ko) | 1994-03-11 |
NO913362L (no) | 1992-03-02 |
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