SE7513777L - Forfarande och brennkammare for lagemissionsforbrenning - Google Patents
Forfarande och brennkammare for lagemissionsforbrenningInfo
- Publication number
- SE7513777L SE7513777L SE7513777A SE7513777A SE7513777L SE 7513777 L SE7513777 L SE 7513777L SE 7513777 A SE7513777 A SE 7513777A SE 7513777 A SE7513777 A SE 7513777A SE 7513777 L SE7513777 L SE 7513777L
- Authority
- SE
- Sweden
- Prior art keywords
- procedure
- low emission
- fire chamber
- emission combustion
- combustion
- Prior art date
Links
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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/533,921 US3973390A (en) | 1974-12-18 | 1974-12-18 | Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones |
Publications (1)
Publication Number | Publication Date |
---|---|
SE7513777L true SE7513777L (sv) | 1976-06-21 |
Family
ID=24127990
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7513777A SE7513777L (sv) | 1974-12-18 | 1975-12-08 | Forfarande och brennkammare for lagemissionsforbrenning |
Country Status (9)
Country | Link |
---|---|
US (1) | US3973390A (xx) |
JP (1) | JPS5189018A (xx) |
CA (1) | CA1051674A (xx) |
CH (1) | CH618780A5 (xx) |
DE (1) | DE2555007A1 (xx) |
FR (1) | FR2295235A1 (xx) |
GB (1) | GB1530146A (xx) |
IT (1) | IT1054444B (xx) |
SE (1) | SE7513777L (xx) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4201047A (en) * | 1976-06-10 | 1980-05-06 | Morgan J Randolph | Low emission combustors |
US4145879A (en) * | 1977-12-15 | 1979-03-27 | United Technologies Corp. | Modified vorbix burner concept |
US4145880A (en) * | 1977-12-15 | 1979-03-27 | United Technologies Corp. | Vorbix augmenter configuration with diffuser and vorbix swirler |
US4215535A (en) * | 1978-01-19 | 1980-08-05 | United Technologies Corporation | Method and apparatus for reducing nitrous oxide emissions from combustors |
US4226083A (en) * | 1978-01-19 | 1980-10-07 | United Technologies Corporation | Method and apparatus for reducing nitrous oxide emissions from combustors |
US4249373A (en) * | 1978-01-28 | 1981-02-10 | Rolls-Royce Ltd. | Gas turbine engine |
US4253301A (en) * | 1978-10-13 | 1981-03-03 | General Electric Company | Fuel injection staged sectoral combustor for burning low-BTU fuel gas |
GB2098720B (en) * | 1979-01-12 | 1983-04-27 | Gen Electric | Stationary gas turbine combustor arrangements |
GB2043868B (en) * | 1979-03-08 | 1982-12-15 | Rolls Royce | Gas turbine |
DE2937631A1 (de) * | 1979-09-18 | 1981-04-02 | Daimler-Benz Ag, 7000 Stuttgart | Brennkammer fuer gasturbinen |
US4312185A (en) * | 1980-02-19 | 1982-01-26 | General Electric Company | Low profile fuel injection system |
JPS5741524A (en) * | 1980-08-25 | 1982-03-08 | Hitachi Ltd | Combustion method of gas turbine and combustor for gas turbine |
DE3331989A1 (de) * | 1983-09-05 | 1985-04-04 | L. & C. Steinmüller GmbH, 5270 Gummersbach | Verfahren zur verminderung der no(pfeil abwaerts)x(pfeil abwaerts)-emission bei der verbrennung von stickstoffhaltigen brennstoffen |
DE3662462D1 (en) * | 1985-07-30 | 1989-04-20 | Bbc Brown Boveri & Cie | Dual combustor |
US4967562A (en) * | 1988-12-12 | 1990-11-06 | Sundstrand Corporation | Turbine engine with high efficiency fuel atomization |
US5261224A (en) * | 1989-12-21 | 1993-11-16 | Sundstrand Corporation | High altitude starting two-stage fuel injection apparatus |
US5205117A (en) * | 1989-12-21 | 1993-04-27 | Sundstrand Corporation | High altitude starting two-stage fuel injection |
US5092128A (en) * | 1989-12-22 | 1992-03-03 | Sundstrand Corporation | Stored energy combustor |
US5216876A (en) * | 1990-11-05 | 1993-06-08 | Consolidated Natural Gas Service Company, Inc. | Method for reducing nitrogen oxide emissions from gas turbines |
US5207064A (en) * | 1990-11-21 | 1993-05-04 | General Electric Company | Staged, mixed combustor assembly having low emissions |
US5685156A (en) * | 1996-05-20 | 1997-11-11 | Capstone Turbine Corporation | Catalytic combustion system |
US5983642A (en) * | 1997-10-13 | 1999-11-16 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel tube with concentric members and flow regulating |
US6286298B1 (en) * | 1998-12-18 | 2001-09-11 | General Electric Company | Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity |
US6295801B1 (en) * | 1998-12-18 | 2001-10-02 | General Electric Company | Fuel injector bar for gas turbine engine combustor having trapped vortex cavity |
US6453658B1 (en) | 2000-02-24 | 2002-09-24 | Capstone Turbine Corporation | Multi-stage multi-plane combustion system for a gas turbine engine |
EP1659339A1 (de) * | 2004-11-18 | 2006-05-24 | Siemens Aktiengesellschaft | Verfahren zum Anfahren eines Brenners |
US8511094B2 (en) * | 2006-06-16 | 2013-08-20 | Siemens Energy, Inc. | Combustion apparatus using pilot fuel selected for reduced emissions |
US8769955B2 (en) * | 2010-06-02 | 2014-07-08 | Siemens Energy, Inc. | Self-regulating fuel staging port for turbine combustor |
US9194586B2 (en) * | 2011-12-07 | 2015-11-24 | Pratt & Whitney Canada Corp. | Two-stage combustor for gas turbine engine |
US9062609B2 (en) | 2012-01-09 | 2015-06-23 | Hamilton Sundstrand Corporation | Symmetric fuel injection for turbine combustor |
US20130180248A1 (en) * | 2012-01-18 | 2013-07-18 | Nishant Govindbhai Parsania | Combustor Nozzle/Premixer with Curved Sections |
US9677766B2 (en) * | 2012-11-28 | 2017-06-13 | General Electric Company | Fuel nozzle for use in a turbine engine and method of assembly |
US9677513B2 (en) | 2014-07-08 | 2017-06-13 | David L. Wilson | Mechanically induced vacuum driven delivery system providing pre-vaporized fuel to an internal combustion engine |
CN113432150B (zh) * | 2021-06-29 | 2022-04-22 | 中国人民解放军国防科技大学 | 可控火焰稳定器、发动机以及飞行器 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2955420A (en) * | 1955-09-12 | 1960-10-11 | Phillips Petroleum Co | Jet engine operation |
US3046731A (en) * | 1955-10-07 | 1962-07-31 | Edward Pohlmann | Flame stabilization in jet engines |
US2922279A (en) * | 1956-02-02 | 1960-01-26 | Power Jets Res & Dev Ltd | Combustion apparatus and ignitor employing vaporized fuel |
FR1166154A (fr) * | 1957-02-01 | 1958-11-04 | Snecma | Brûleur à semi-vaporisation |
US2974487A (en) * | 1957-10-19 | 1961-03-14 | Bristol Siddeley Engines Ltd | Combustion system for a gas turbine engine |
GB854135A (en) * | 1958-03-05 | 1960-11-16 | Rolls Royce | Improvements in or relating to combustion equipment |
FR1206830A (fr) * | 1958-05-19 | 1960-02-11 | Rolls Royce | Perfectionnements aux appareillages de combustion des moteurs à turbine à gaz |
US3074668A (en) * | 1958-12-10 | 1963-01-22 | Snecma | Burner for hot fuel |
US3531937A (en) * | 1968-09-24 | 1970-10-06 | Curtiss Wright Corp | Fuel vaporizer for gas turbine engines |
GB1357533A (en) * | 1970-09-11 | 1974-06-26 | Lucas Industries Ltd | Combustion equipment for gas turbine engines |
US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
JPS4724483Y1 (xx) * | 1970-12-22 | 1972-08-02 | ||
DE2403657A1 (de) * | 1973-02-28 | 1974-09-12 | United Aircraft Corp | Brennkammer mit vormischung fuer gasturbinentriebwerke |
US3872664A (en) * | 1973-10-15 | 1975-03-25 | United Aircraft Corp | Swirl combustor with vortex burning and mixing |
GB1489339A (en) * | 1973-11-30 | 1977-10-19 | Rolls Royce | Gas turbine engine combustion chambers |
IT1048356B (it) * | 1974-10-30 | 1980-11-20 | Engelhard Min & Chem | Procedimento termodinamico per generare prodotti di combustione di elevata energia termica e produrre da essi energia meccanica in una turbina a gas e relativo impianto a turbina |
-
1974
- 1974-12-18 US US05/533,921 patent/US3973390A/en not_active Expired - Lifetime
-
1975
- 1975-10-31 CA CA238,795A patent/CA1051674A/en not_active Expired
- 1975-12-03 CH CH1575175A patent/CH618780A5/de not_active IP Right Cessation
- 1975-12-06 DE DE19752555007 patent/DE2555007A1/de not_active Withdrawn
- 1975-12-08 SE SE7513777A patent/SE7513777L/xx unknown
- 1975-12-12 GB GB51084/75A patent/GB1530146A/en not_active Expired
- 1975-12-15 FR FR7538258A patent/FR2295235A1/fr not_active Withdrawn
- 1975-12-17 IT IT30400/75A patent/IT1054444B/it active
- 1975-12-18 JP JP50151740A patent/JPS5189018A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2295235A1 (fr) | 1976-07-16 |
US3973390A (en) | 1976-08-10 |
JPS5189018A (xx) | 1976-08-04 |
GB1530146A (en) | 1978-10-25 |
IT1054444B (it) | 1981-11-10 |
DE2555007A1 (de) | 1976-07-01 |
CH618780A5 (xx) | 1980-08-15 |
CA1051674A (en) | 1979-04-03 |
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