EP0849532A2 - Verfahren zum Betrieb eines Brenners - Google Patents
Verfahren zum Betrieb eines Brenners Download PDFInfo
- Publication number
- EP0849532A2 EP0849532A2 EP97810891A EP97810891A EP0849532A2 EP 0849532 A2 EP0849532 A2 EP 0849532A2 EP 97810891 A EP97810891 A EP 97810891A EP 97810891 A EP97810891 A EP 97810891A EP 0849532 A2 EP0849532 A2 EP 0849532A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- burner
- gas
- fuel
- auxiliary gas
- auxiliary
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/22—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour the gaseous medium being vaporised fuel, e.g. for a soldering lamp, or other gaseous fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/101—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
- F23D11/102—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2206/00—Burners for specific applications
- F23D2206/10—Turbines
Definitions
- the invention relates to a method for operating a burner, according to the Preamble of claim 1.
- the nozzle can also be used with a so-called Ignition level can be provided. It is a second Atomizer, which is designed for correspondingly small throughputs and therefore at Partial load ensures a sufficiently fine atomization of the liquid fuel.
- a second Atomizer which is designed for correspondingly small throughputs and therefore at Partial load ensures a sufficiently fine atomization of the liquid fuel.
- This nozzle with their two fuel supply lines and with two radially one above the other Fuel channels, which act on depending on the required fuel mass flow , but requires a relatively large amount of space. They are also components used are naturally filigree, which makes the nozzle more susceptible to failure.
- pp. 142-144 and Fig. 4.50 is an atomizer for liquid fuels known, in which an auxiliary gas upstream of the injection opening is introduced into the liquid flow.
- a gas pipe is arranged which ends upstream of the injection opening and is provided with a plurality of outlet openings for the auxiliary gas.
- the injection of the auxiliary gas in the liquid flow takes place at low speed and with only slightly higher pressure than the liquid flow.
- This in the auxiliary gas emerging from the liquid forms gas bubbles, due to their influence relatively thin scraps of liquid and bands appear in the liquid flow. Because such Liquid flows with a smaller diameter easier to a fine Spray can be dissolved, this will atomize the liquid Improved fuel.
- With the injection of the auxiliary gas into the liquid fuel pipe the total volume flow to be atomized is increased so that sufficient atomization even with partial load using a full jet atomizer of the fuel is available.
- the invention tries to avoid all of these disadvantages. You have the task is based on a simple and suitable method for all operating conditions To create operation of a burner.
- this is achieved in that in a method according to the preamble of claim 1, the auxiliary gas only in the ignition and at Partial load of the burner fed and the supply interrupted at high load ranges becomes.
- the atomizer nozzle which is known per se, can now be used both on ignition and Low load conditions as well as under high load conditions and of course at Full load can be optimally adjusted. In this way the respective range of applications such an atomizer nozzle or one equipped with it Brenners significantly expanded. Your use with one with different combustion air pressures, such as. in a gas turbine, operated combustion chamber is only made possible by this.
- the premixing of the liquid in the burner can Low-emission combustion can be achieved with the auxiliary gas.
- An additional advantage results when using the method in axially mounted Combustion chambers where the burners are at different geodetic heights are arranged.
- the supply of the auxiliary gas can, in particular, otherwise uneven distribution of the liquid fuel that occurs during ignition significantly reduced, thus increasing the functional reliability of the combustion chamber will.
- auxiliary gas from a pressure vessel or Auxiliary compressor is supplied to the burner. According to the specific conditions of use the burner is therefore a suitable source for the auxiliary gas given.
- Compressed air is particularly advantageously supplied as auxiliary gas. This is done at Requires either compressed ambient air or compressed air from the already filled pressure vessel before igniting the burner.
- the stake of ambient air as auxiliary gas is particularly cheap because it is constantly is available.
- the invention can also be used with inert gases, e.g. Nitrogen, with ignition gases (e.g. propane) or with fuel gases (e.g. natural gas) will be realized.
- inert gases e.g. Nitrogen
- ignition gases e.g. propane
- fuel gases e.g. natural gas
- a plurality of burners 1 are arranged in the gas turbine system, not shown, which are operated with a liquid fuel 2, more precisely with fuel oil. Naturally other suitable fuels can also be used.
- Each burner 1 consists of an outer air tube 3 and a coaxial inside the air tube 3 arranged atomizer nozzle 4, both in one Combustion chamber 5 of the gas turbine system open out.
- the atomizer nozzle 4 has a Liquid fuel tube 6 with an interior 7, a fuel feed line 8 and one circular injection opening 9.
- a gas pipe 11 connected to a feed line 10 is arranged, which several Has outlet openings 12 in the interior 7.
- the interior 7 is in the direction the injection opening 9 tapers, i.e. with a guide piece 13 for that Fuel oil 2 trained.
- the feed line 10 has a control valve 14 with which the Gas pipe 1 can be opened or blocked.
- each burner 1 When operating the gas turbine system, each burner 1 is switched over the corresponding one Fuel supply line 8 supplied with fuel oil 2.
- the fuel oil 2 comes first in the interior 7 of the liquid fuel tube 6, where it through the Fuel pressure is further promoted in the direction of the injection opening 9.
- Gas turbine system is arranged via the feed line 10 and in the gas pipe 11 Outlet openings 12 serving as auxiliary gas 15, compressed air into the Interior 7 located fuel oil 2 initiated.
- This injection takes place with less Speed and with an insignificant compared to the fuel oil 2 higher pressure of about 0.1 to 3.0 bar.
- the air serving as auxiliary gas 15 becomes the compressor section, not shown removed from the gas turbine system pre-compressed and, if necessary, also via one brought auxiliary compressor, not shown, to the required pressure.
- the air 15 can also be supplied from a pressure vessel.
- the fuel throughput of the Brenner 1 constantly.
- the fuel pressure increases in line with the fuel throughput in the burner 1 and in the atomizing nozzle 4. If the atomization is sufficient required fuel pressure is reached, the air supply is through Closing the control valve 14 interrupted. With the control valve closed 14, i.e. at high fuel pressure, the fuel oil 2 is by means of the circular Injection opening 9 distributed to a fine, suitable for combustion spray.
- auxiliary gases such as inert gases (nitrogen) or ignition gases (propane) or fuel gases (Natural gas) can be used.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
Description
- 1
- Brenner
- 2
- flüssiger Brennstoff, Brennöl
- 3
- Luftrohr, äusseres
- 4
- Zerstäuberdüse
- 5
- Brennkammer
- 6
- Flüssigbrennstoffrohr
- 7
- Innenraum
- 8
- Brennstoffzuleitung
- 9
- Einspritzöffnung, kreisförmig
- 10
- Zuleitung
- 11
- Gasrohr
- 12
- Austrittsöffnung
- 13
- Führungsstück
- 14
- Steuerventil
- 15
- Hilfsgas, Luft
Claims (9)
- Verfahren zum Betrieb eines Brenners (1), bei dem mit einem aktuellen Brennstoffdruck in eine Zerstäuberdüse (4) des Brenners (1) einströmender flüssiger Brennstoff (2) durch eine Einspritzöffnung (9) ausgestossen, zuvor jedoch ein Hilfsgas (15) mit einem nur geringfügig höheren Druck als der Brennstoffdruck in den flüssigen Brennstoff (2) eingebracht wird, dadurch gekennzeichnet, dass das Hilfsgas (15) bei der Zündung und bei Teillast des Brenners (1) zugeführt, die Zufuhr bei hohen Lastbereichen des Brenners (1) jedoch unterbrochen wird.
- Verfahren nach Anspruch 1, dadurch gekennzeichnet, dass das Hilfsgas (15) auch bei Unterbrechung der Versorgung des Brenners (1) mit flüssigem Brennstoff (2) weiterhin zugeführt wird.
- Verfahren nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das Hilfsgas (15) aus einem Druckbehälter oder einem Hilfsverdichter zum Brenner (1) geliefert wird.
- Verfahren nach Anspruch 3, dadurch gekennzeichnet, dass verdichtete Luft als Hilfsgas (15) zugeführt wird.
- Verfahren nach Anspruch 4, dadurch gekennzeichnet, dass während der Zündung und/oder dem Teillastbetrieb des Brenners (1) Umgebungsluft (15) verdichtet und zum Brenner (1) geliefert wird.
- Verfahren nach Anspruch 3, dadurch gekennzeichnet, dass komprimierte Luft (15) aus einem vor dem Zünden des Brenners (1) befüllten Druckbehälter zum Brenner (1) geliefert wird.
- Verfahren nach Anspruch 3, dadurch gekennzeichnet, dass als Hilfsgas (15) ein inertes Gas, vorzugsweise Stickstoff, zum Brenner (1) geliefert wird.
- Verfahren nach Anspruch 3, dadurch gekennzeichnet, dass als Hilfsgas (15) ein Zündgas, vorzugsweise Propan zum Brenner (1) geliefert wird.
- Verfahren nach Anspruch 3, dadurch gekennzeichnet, dass als Hilfsgas (15) ein Brenngas, vorzugsweise Erdgas, verwendet wird.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19653059A DE19653059A1 (de) | 1996-12-19 | 1996-12-19 | Verfahren zum Betrieb eines Brenners |
DE19653059 | 1996-12-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0849532A2 true EP0849532A2 (de) | 1998-06-24 |
EP0849532A3 EP0849532A3 (de) | 1999-05-26 |
EP0849532B1 EP0849532B1 (de) | 2002-04-10 |
Family
ID=7815390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97810891A Expired - Lifetime EP0849532B1 (de) | 1996-12-19 | 1997-11-21 | Verfahren zum Betrieb eines Brenners |
Country Status (5)
Country | Link |
---|---|
US (1) | US6128894A (de) |
EP (1) | EP0849532B1 (de) |
JP (1) | JPH10185109A (de) |
CN (1) | CN1119568C (de) |
DE (2) | DE19653059A1 (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19855069A1 (de) * | 1998-11-28 | 2000-05-31 | Asea Brown Boveri | Flüssigbrennstoffaufbereitungseinheit für einen Brenner und Verfahren zum Betrieb derselben |
EP2469167A1 (de) * | 2010-12-22 | 2012-06-27 | Siemens Aktiengesellschaft | System zum Belüften von flüssigem Brennstoff mit Gas für eine Gasturbine und Verfahren zum Belüften von flüssigem Brennstoff mit Gas für eine Gasturbine |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE514341C2 (sv) * | 1998-06-18 | 2001-02-12 | Abb Ab | Förfarande för start av en brännaranordning till en gasturbin |
US6450108B2 (en) * | 2000-03-24 | 2002-09-17 | Praxair Technology, Inc. | Fuel and waste fluid combustion system |
US6796129B2 (en) * | 2001-08-29 | 2004-09-28 | Catalytica Energy Systems, Inc. | Design and control strategy for catalytic combustion system with a wide operating range |
US20040255588A1 (en) * | 2002-12-11 | 2004-12-23 | Kare Lundberg | Catalytic preburner and associated methods of operation |
BRPI0406806A (pt) * | 2003-01-17 | 2005-12-27 | Catalytica Energy Sys Inc | Sistema e método de controle dinâmico para multicombustor catalìtico para motor de turbina a gás |
WO2005026675A2 (en) * | 2003-09-05 | 2005-03-24 | Catalytica Energy Systems, Inc. | Catalyst module overheating detection and methods of response |
US7390189B2 (en) * | 2004-08-16 | 2008-06-24 | Air Products And Chemicals, Inc. | Burner and method for combusting fuels |
FR2875584B1 (fr) * | 2004-09-23 | 2009-10-30 | Snecma Moteurs Sa | Injecteur a effervescence pour systeme aeromecanique d'injection air/carburant dans une chambre de combustion de turbomachine |
FR2875585B1 (fr) * | 2004-09-23 | 2006-12-08 | Snecma Moteurs Sa | Systeme aerodynamique a effervescence d'injection air/carburant dans une chambre de combustion de turbomachine |
CN100441949C (zh) * | 2005-01-24 | 2008-12-10 | 张鹏飞 | 醇基液体燃料燃烧器 |
US7963096B2 (en) * | 2006-11-02 | 2011-06-21 | Vanholstyn Alex | Reflective pulse rotary engine |
US8454354B2 (en) * | 2008-05-08 | 2013-06-04 | Air Products And Chemicals, Inc. | Highly radiative burner and combustion process |
IT1400384B1 (it) * | 2010-05-26 | 2013-05-31 | Ansaldo Energia Spa | Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore. |
JP2015505595A (ja) * | 2012-02-01 | 2015-02-23 | ゼネラル・エレクトリック・カンパニイ | 液体燃料始動システムを備えるガスターボ機械の燃焼装置アセンブリ |
US10634358B2 (en) | 2017-06-16 | 2020-04-28 | General Electric Company | System and method for igniting liquid fuel in a gas turbine combustor |
CN107035533B (zh) * | 2017-06-23 | 2018-06-29 | 王冠霖 | 基于plc的多功能燃气轮机燃料控制装置 |
WO2019104614A1 (zh) * | 2017-11-30 | 2019-06-06 | 乔治洛德方法研究和开发液化空气有限公司 | 一种能用于固体燃料和气体燃料的氧化剂-多燃料烧嘴 |
FR3105985B1 (fr) * | 2020-01-03 | 2023-11-24 | Safran Aircraft Engines | Circuit multipoint d’injecteur amélioré |
US11326521B2 (en) | 2020-06-30 | 2022-05-10 | General Electric Company | Methods of igniting liquid fuel in a turbomachine |
Family Cites Families (26)
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US1995099A (en) * | 1930-03-10 | 1935-03-19 | Frank E Herr | Burner |
US2319591A (en) * | 1941-05-09 | 1943-05-18 | Nat Airoil Burner Company Inc | Method of treating imperfectly combustible liquids or semiliquids |
US2635425A (en) * | 1949-09-07 | 1953-04-21 | Westinghouse Electric Corp | Dual flow fuel nozzle system having means to inject air in response to low fuel pressure |
US3236281A (en) * | 1963-12-19 | 1966-02-22 | United States Steel Corp | Method and apparatus for burning a mixture of liquid and gaseous fuels |
NL130010C (de) * | 1966-01-27 | |||
US3426527A (en) * | 1966-12-28 | 1969-02-11 | United Aircraft Corp | Starting system for gas turbine engines |
GB1377184A (en) * | 1971-02-02 | 1974-12-11 | Secr Defence | Gas turbine engine combustion apparatus |
US3748087A (en) * | 1971-10-14 | 1973-07-24 | Pyronics Inc | Burner apparatus and method for flame propagation control |
BE794642A (fr) * | 1972-01-28 | 1973-05-16 | Arbed | Injecteur de combustibles pour les hauts fourneaux |
US3785570A (en) * | 1972-08-30 | 1974-01-15 | Us Army | Dual orifice fuel nozzle with air-assisted primary at low flow rates |
US3982878A (en) * | 1975-10-09 | 1976-09-28 | Nissan Motor Co., Ltd. | Burning rate control in hydrogen fuel combustor |
US4201553A (en) * | 1976-06-16 | 1980-05-06 | Hans Osborg | Method of improving combustion of fuels and novel fuel compositions |
US4105163A (en) * | 1976-10-27 | 1978-08-08 | General Electric Company | Fuel nozzle for gas turbines |
US4293230A (en) * | 1978-04-12 | 1981-10-06 | Tan Lu J | Apparatus for providing fuel for an oil burner |
US4443180A (en) * | 1981-05-11 | 1984-04-17 | Honeywell Inc. | Variable firing rate oil burner using aeration throttling |
US4655706A (en) * | 1982-09-27 | 1987-04-07 | Otis Engineering Corporation | Burner |
US4600151A (en) * | 1982-11-23 | 1986-07-15 | Ex-Cell-O Corporation | Fuel injector assembly with water or auxiliary fuel capability |
JPS60235910A (ja) * | 1984-05-09 | 1985-11-22 | Nippon Furnace Kogyo Kaisha Ltd | 低負荷燃焼対策のバ−ナ |
GB2161915B (en) * | 1984-07-20 | 1988-07-27 | Council Scient Ind Res | Film burner |
US4643666A (en) * | 1984-10-09 | 1987-02-17 | Mobil Oil Corporation | Method of burning hydrogen deficient fuels |
DE4014185A1 (de) * | 1990-05-03 | 1991-11-07 | Webasto Ag Fahrzeugtechnik | Verfahren zum betreiben eines mit fluessigbrennstoff gespeisten brenners |
US5222357A (en) * | 1992-01-21 | 1993-06-29 | Westinghouse Electric Corp. | Gas turbine dual fuel nozzle |
US5450724A (en) * | 1993-08-27 | 1995-09-19 | Northern Research & Engineering Corporation | Gas turbine apparatus including fuel and air mixer |
DE69409049T3 (de) * | 1993-08-31 | 2001-09-13 | Praxair Technology, Inc. | Verbrennungsverfahren unter Verwendung von Argon und Sauerstoff |
DE4446609B4 (de) * | 1994-12-24 | 2005-10-06 | Alstom | Vorrichtung zur Brennstoffzuführung zu einem sowohl für flüssige als auch für gasförmige Brennstoffe geeigneten Brenner |
US5701732A (en) * | 1995-01-24 | 1997-12-30 | Delavan Inc. | Method and apparatus for purging of gas turbine injectors |
-
1996
- 1996-12-19 DE DE19653059A patent/DE19653059A1/de not_active Withdrawn
-
1997
- 1997-11-21 EP EP97810891A patent/EP0849532B1/de not_active Expired - Lifetime
- 1997-11-21 DE DE59706957T patent/DE59706957D1/de not_active Expired - Fee Related
- 1997-12-03 US US08/984,424 patent/US6128894A/en not_active Expired - Fee Related
- 1997-12-19 CN CN97108594A patent/CN1119568C/zh not_active Expired - Fee Related
- 1997-12-19 JP JP9351295A patent/JPH10185109A/ja active Pending
Non-Patent Citations (2)
Title |
---|
A. LEFEBVRE: "ATOMIZATION AND SPRAYS", 1989, WEST LAFAYETTE, INDIANA, pages: 120+ FIG - 4.21 |
A. LEFEBVRE: "ATOMIZATION AND SPRAYS", 1989, WEST LAFAYETTE, INDIANA, pages: FIG4.50+ - 142-144 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19855069A1 (de) * | 1998-11-28 | 2000-05-31 | Asea Brown Boveri | Flüssigbrennstoffaufbereitungseinheit für einen Brenner und Verfahren zum Betrieb derselben |
EP2469167A1 (de) * | 2010-12-22 | 2012-06-27 | Siemens Aktiengesellschaft | System zum Belüften von flüssigem Brennstoff mit Gas für eine Gasturbine und Verfahren zum Belüften von flüssigem Brennstoff mit Gas für eine Gasturbine |
WO2012084347A2 (en) | 2010-12-22 | 2012-06-28 | Siemens Aktiengesellschaft | Gas turbine and method for oparating said gas turbine |
WO2012084347A3 (en) * | 2010-12-22 | 2012-08-16 | Siemens Aktiengesellschaft | Gas turbine and method for oparating said gas turbine |
Also Published As
Publication number | Publication date |
---|---|
CN1186928A (zh) | 1998-07-08 |
EP0849532B1 (de) | 2002-04-10 |
DE59706957D1 (de) | 2002-05-16 |
JPH10185109A (ja) | 1998-07-14 |
EP0849532A3 (de) | 1999-05-26 |
DE19653059A1 (de) | 1998-06-25 |
US6128894A (en) | 2000-10-10 |
CN1119568C (zh) | 2003-08-27 |
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