EP0981016A1 - Brenner sowie Verfahren zum Betrieb einer Brennkraftmaschine - Google Patents
Brenner sowie Verfahren zum Betrieb einer Brennkraftmaschine Download PDFInfo
- Publication number
- EP0981016A1 EP0981016A1 EP98810805A EP98810805A EP0981016A1 EP 0981016 A1 EP0981016 A1 EP 0981016A1 EP 98810805 A EP98810805 A EP 98810805A EP 98810805 A EP98810805 A EP 98810805A EP 0981016 A1 EP0981016 A1 EP 0981016A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuel
- air inlet
- combustion
- burner
- air flow
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/62—Mixing devices; Mixing tubes
- F23D14/64—Mixing devices; Mixing tubes with injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
-
- 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
- F23C2900/07002—Premix burners with air inlet slots obtained between offset curved wall surfaces, e.g. double cone burners
Definitions
- the invention relates to a burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or furnace, with at least two half, hollow partial cone bodies, which are joined together in such a way that whose axes of longitudinal symmetry are radially offset from one another and the at least two tangential air inlet slots for a combustion air flow and include a cone cavity and a nozzle assembly for injection liquid, highly reactive fuel in the cone cavity, which in the area of narrowest inside diameter of the cone cavity is arranged. Further relates the invention relates to a method for operating an internal combustion engine, a Combustion chamber of a gas turbine group or furnace.
- a burner of the type mentioned above goes for example from the EP 0321 809 B1 and is used with great success for firing gas turbine systems used.
- This type of burner is considered a successful type of burner output, those for firing with highly reactive, gaseous and liquid fuels designed with a high calorific value of around 35 to 50 MJ / kg are.
- Hirbei is using the liquid fuel inside the combustion chamber a nozzle arrangement in the center of the cone cavity in the form of a introduced conical fuel sprays.
- the conical Fuel spray is from a tangent flowing into the cone cavity rotating combustion air flow enclosed and thereby stabilized. Only in Area of the vortex runout, i.e.
- Gaseous fuel is made up of two pipes that close the air inlet slots of the Are arranged along the burner, through rows of holes transverse to the entering Air flow injected.
- the inner and outer shape of the Brenners can be seen as the end product of an extensive optimization process in which the burner from the point of view of combustion liquid fuel with a high calorific value has been optimized.
- the invention is based on the object of a generic burner the preamble of claim 1, the spatial configuration of the targeted combustion of gaseous and liquid fuel with a high calorific value is optimized to develop in such a way that the combustion of medium and / or low calorific fuels without affecting shape and Design of the burner and without deterioration of the emission values is possible.
- the measures to be taken for this should, if possible, be used for existing ones Burner can be retrofitted and have a simple design. Necessary modifications to the burner itself should be as small as possible be kept low, medium and low with the help of a single type of burner high calorific fuels can be burned.
- an injection device is in each case in the flow direction arranged in front of the air inlet slots that in the combustion air supply fuel to be introduced parallel to the flow direction of the combustion air supply is injected into the air inlet slots. Due to the parallel fuel feed any turbulence within the combustion supply air flow avoided, which does not lead to irritating eddy formation local fuel accumulations and cause uncontrolled ignition events are.
- the nozzle arrangement is particularly designed such that the exit speed the fuel from the nozzle arrangement approximately the same flow rate with which the combustion supply air flow into the Air inlet slots is introduced. Due to the isokinetic entry behavior Mass flows are also avoided any dynamic pressure differences, whereby equally disturbing eddy formation can be excluded.
- the nozzle arrangement according to the invention has that has two air inlet slots has two injection devices on, each positioned in the direction of flow in front of the air inlet slots are. Both injection devices are connected to one another via a frame firmly connected and can be attached to the corresponding connecting elements Burner can be attached detachably.
- Each of the respective injection devices provided extend longitudinally over the entire length of the air inlet slot and each have a preferably rectilinear interior Fuel supply line, which via a narrowed supply duct with the Nozzle outlet area is connected.
- the narrowed supply channel can consist of a large number of individual bores, which are distributed along the fuel supply channel, as well as a continuous feed slot that extends over the entire length of the injection device extends, be formed.
- the nozzle outlet area is preferred as a continuous slot channel that extends over the entire length of the Injection device extends and has a channel-length-width ratio on that to a directed, almost parallel fuel jet leads, which, as already mentioned above, to the flow velocity flow velocity adapted to the combustion air having.
- Figure 1 shows a schematic cross-sectional view through the air inlet slot 1 of a burner, not shown in further detail.
- the air inlet slot 1 is limited on the one hand by the outer wall of a first partial cone body 2 and through the inner wall of a second partial cone body 3.
- an injection device 7 is provided, which is parallel to its longitudinal axis
- fuel feed line 8 with a narrowed feed channel 9 the nozzle outlet area 10 of the injection device 7 is connected.
- the narrowed Supply channel 9 can be used as a multitude of side by side Single bores can be designed as well as a continuous slot opening be, which extends over the entire length of the injection device 7.
- the narrowed supply duct 9 has the task, on the one hand, of possible occurrences acoustic vibrations within the fuel feed line 8 from the nozzle outlet area 10 decouple. Secondly, the narrowed supply channel 9 a throttling of the prevailing inside the fuel feed line 8 Working pressure in the direction of the nozzle outlet area.
- the nozzle outlet area indicates one of the pressure and flow conditions of the fuel adjusted length as well as width, creating a targeted fuel flow field 13 is generated, largely as a two-dimensional flow field at the same speed to the fuel supply air flow 6 in the air inlet slot 1 can be introduced.
- FIG 2 is a side view of the burner expanded according to the invention shown, which consists of the first partial cone body 2 and the second partial cone body 3 is composed. Both partial cone bodies close two air inlet slots one, of which the air inlet slot 1 is shown in FIG. In the direction of flow An injection device 7 is provided in front of the air inlet slot 1, which can be fixed at least on one side with a base plate 10 of the burner connected is. Via a preferably ring-shaped frame 12 is the injection device 7 with its opposite on the burner (in of the rear 2) injection device connected.
- the injection device according to the invention can be installed over existing ones Burner systems are guided and suitably firmly connected to the burner become. In this way, the injection device is an additional module view that can be retrofitted as desired.
Abstract
Description
- Fig. 1
- schematischer Querschnitt durch eine Eindüsungsvorrichtung, die vor einem Lufteintrittsschlitz angeordnet ist, sowie
- Fig. 2
- schematische Seitendarstellung eines Brenners mit der erfindungsgemäßen Eindüsungsvorrichtung.
- 1
- Lufteintrittsschlitz
- 2
- erster Teilkegelkörper
- 3
- zweiter Teilkegelkörper
- 4
- Rohr für gasförmigen Brennstoff, entlang des Brenners angeordnet
- 5
- Bohrungsreihen, quer zur eintretenden Luftströmung (6)
- 6
- Verbrennungszuluftströmung
- 7
- Eindüsungsvorrichtung
- 8
- Brennstoffzuleitung
- 9
- verengter Zuleitungskanal
- 10
- Düsenauslaßbereich
- 11
- Basisplatte
- 12
- Rahmen
- 13
- Brennstoffströmungsfeld
Claims (12)
- Brenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage, mit wenigstens zwei halben, hohlen Teilkegelkörpern (2, 3), die derart ineinander gefügt sind, daß deren Längssymmetrieachsen zueinander radial versetzt verlaufen und die mindestens zwei tangentiale Lufteintrittsschlitze (1) für einen Verbrennungszuluftstrom (6) sowie einen Kegelhohlraum einschließen, einer Düsenanordnung zum Eindüsen flüssigen, hochreaktiven Brennstoffes in den Kegelhohlraum, die im Bereich des engsten Innendurchmessers des Kegelhohlraumes angeordnet ist, dadurch gekennzeichnet, daß in Richtung des Verbrennungszuluftstromes (6) vor den tangentialen Lufteintrittsschlitzen (1) jeweils eine Eindüsungsvorrichtung (7) für Brennstoff vorgesehen ist, die den Brennstoff in paralleler Strömungsrichtung zum Verbrennungszuluftstrom (6) in die Lufteintrittsschlitz (1) eindüst.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, daß die Eindüsungsvorrichtung (7) den Brennstoff isokinetisch relativ zur Verbrennungszuluft (6) eindüst.
- Brenner nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die einzelnen Eindüsungsvorrichtungen (7) pro Lufteintrittsschlitz (1) über einem zusammenhängenden Rahmen (12) miteinander verbunden sind und als einheitliches Modul ausgebildet ist, das an den Brenner befestigbar ist.
- Brenner nach Anspruch 3, dadurch gekennzeichnet, daß das Modul am Brenner nachträglich aufsetzbar und befestigbar ist.
- Brenner nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß die Eindüsungsvorrichtung (7) eine linear verlaufende Brennstoffzuleitung (8) aufweist, die über einen relativ zu einem Düsenaulaßbereich (10) verengten Zuleitungskanal (9) mit diesem verbunden ist.
- Brenner nach Anspruch 5, dadurch gekennzeichnet, daß der Düsenauslaßbereich (10) als Schlitzdüse ausgebildet ist, der sich längs über die gesamte Länge des Lufteintrittsschlitz (1) erstreckt.
- Brenner nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß die Eindüsungsvorrichtung (7) eine Vielzahl von Einzelstrahldüsen aufweist, die einen über die Länge des Lufteintrittsschlitzes (1) weitgehend homogenen Brennstoffstrahl (13) erzeugen.
- Brenner nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß die Eindüsungsvorrichtung (7) für mittel- und niederkalorische Brennstoffe vorgesehen ist.
- Brenner nach Anspruch 8, dadurch gekennzeichnet, daß der Brennstoff Heizwerte zwischen 5 und 50 MJ/kg aufweist.
- Verfahren zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage, mit wenigstens zwei halben, hohlen Teilkegelkörpern (2, 3), die derart ineinander gefügt sind, daß deren Längssymmetrieachsen zueinander radial versetzt verlaufen und die mindestens zwei tangentiale Lufteintrittsschlitze (1) für einen Verbrennungszuluftstrom (6), dadurch gekennzeichnet, daß nieder- oder mittelkalorischer, gasförmiger Brennstoff parallel zum Verbrennungszuluftstrom (6) vor oder bei Eintritt in den Lufteintrittsschlitz (1) dem Zu luftstrom beigemischt wird.
- Verfahren nach Anspruch 10, dadurch gekennzeichnet, daß der Brennstoff dem Verbrennungszuluftstrom (6) isokinetisch beigemischt wird.
- Brenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage, mit wenigstens einem tangential zur Brennkammer angeordneten Lufteintrittsschlitz (1), durch den ein Verbrennungszuluftstrom (6) in die Brennkammer einströmt, sowie einer Düsenanordnung zum Eindüsen flüssigen, hochreaktiven Brennstoffes in die Brennkammer, dadurch gekennzeichnet, daß in Richtung des Verbrennungszuluftstromes (6) vor dem tangentialen Lufteintrittsschlitz (1) jeweils eine Eindüsungsvorrichtung (7) für Brennstoff vorgesehen ist, die den Brennstoff in paralleler Strömungsrichtung zum Verbrennungszuluftstrom (6) in den Lufteintrittsschlitz (1) eindüst.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE59810551T DE59810551D1 (de) | 1998-08-19 | 1998-08-19 | Brenner zum Betrieb einer Brennkammer |
EP98810805A EP0981016B1 (de) | 1998-08-19 | 1998-08-19 | Brenner zum Betrieb einer Brennkammer |
US09/369,838 US6263676B1 (en) | 1998-08-19 | 1999-08-09 | Burner having a frame for operating an internal combustion machine |
CN99111501.5A CN1113187C (zh) | 1998-08-19 | 1999-08-17 | 运行内燃机器的燃烧器 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP98810805A EP0981016B1 (de) | 1998-08-19 | 1998-08-19 | Brenner zum Betrieb einer Brennkammer |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0981016A1 true EP0981016A1 (de) | 2000-02-23 |
EP0981016B1 EP0981016B1 (de) | 2004-01-07 |
Family
ID=8236263
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98810805A Expired - Lifetime EP0981016B1 (de) | 1998-08-19 | 1998-08-19 | Brenner zum Betrieb einer Brennkammer |
Country Status (4)
Country | Link |
---|---|
US (1) | US6263676B1 (de) |
EP (1) | EP0981016B1 (de) |
CN (1) | CN1113187C (de) |
DE (1) | DE59810551D1 (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1734306A1 (de) * | 2005-06-17 | 2006-12-20 | ALSTOM Technology Ltd | Brenner zur vormischartigen Verbrennung |
CH701905A1 (de) * | 2009-09-17 | 2011-03-31 | Alstom Technology Ltd | Verfahren zum Verbrennen wasserstoffreicher, gasförmiger Brennstoffe in einem Brenner sowie Brenner zur Durchführung des Verfahrens. |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6585784B1 (en) * | 1999-12-13 | 2003-07-01 | Exxonmobil Chemical Patents Inc. | Method for utilizing gas reserves with low methane concentrations for fueling gas turbines |
JP3940705B2 (ja) * | 2003-06-19 | 2007-07-04 | 株式会社日立製作所 | ガスタービン燃焼器及びその燃料供給方法 |
EP1614967B1 (de) * | 2004-07-09 | 2016-03-16 | Siemens Aktiengesellschaft | Verfahren und Vormischverbrennungssystem |
FR2889292B1 (fr) * | 2005-07-26 | 2015-01-30 | Optimise | Procede et installation de combustion sans soutien de gaz combustible pauvre a l'aide d'un bruleur et bruleur associe |
EP2299178B1 (de) * | 2009-09-17 | 2015-11-04 | Alstom Technology Ltd | Verfahren und Gasturbinenverbrennungssystem zum sicheren Mischen von H2-reichen Brennstoffen mit Luft |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1535610A (fr) * | 1967-06-26 | 1968-08-09 | Gaz De France | Brûleurs pour combustibles gazeux à multiple injection et mélangeur intégré |
EP0321809A1 (de) | 1987-12-21 | 1989-06-28 | BBC Brown Boveri AG | Verfahren für die Verbrennung von flüssigem Brennstoff in einem Brenner |
EP0433790A1 (de) * | 1989-12-22 | 1991-06-26 | Asea Brown Boveri Ag | Brenner |
EP0433789A1 (de) * | 1989-12-19 | 1991-06-26 | Asea Brown Boveri Ag | Verfahren für eine Vormischverbrennung eines flüssigen Brennstoffes |
DE4237187A1 (de) * | 1992-11-04 | 1994-05-05 | Raimund Prof Dr Ruderich | Wirbelerzeuger für einen Brenner |
EP0724114A2 (de) * | 1995-01-30 | 1996-07-31 | ABB Management AG | Brenner |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH682952A5 (de) * | 1991-03-12 | 1993-12-15 | Asea Brown Boveri | Brenner für eine Vormischverbrennung eines flüssigen und/oder gasförmigen Brennstoffes. |
DE4304213A1 (de) * | 1993-02-12 | 1994-08-18 | Abb Research Ltd | Brenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage |
-
1998
- 1998-08-19 EP EP98810805A patent/EP0981016B1/de not_active Expired - Lifetime
- 1998-08-19 DE DE59810551T patent/DE59810551D1/de not_active Expired - Lifetime
-
1999
- 1999-08-09 US US09/369,838 patent/US6263676B1/en not_active Expired - Lifetime
- 1999-08-17 CN CN99111501.5A patent/CN1113187C/zh not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1535610A (fr) * | 1967-06-26 | 1968-08-09 | Gaz De France | Brûleurs pour combustibles gazeux à multiple injection et mélangeur intégré |
EP0321809A1 (de) | 1987-12-21 | 1989-06-28 | BBC Brown Boveri AG | Verfahren für die Verbrennung von flüssigem Brennstoff in einem Brenner |
EP0433789A1 (de) * | 1989-12-19 | 1991-06-26 | Asea Brown Boveri Ag | Verfahren für eine Vormischverbrennung eines flüssigen Brennstoffes |
EP0433790A1 (de) * | 1989-12-22 | 1991-06-26 | Asea Brown Boveri Ag | Brenner |
DE4237187A1 (de) * | 1992-11-04 | 1994-05-05 | Raimund Prof Dr Ruderich | Wirbelerzeuger für einen Brenner |
EP0724114A2 (de) * | 1995-01-30 | 1996-07-31 | ABB Management AG | Brenner |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1734306A1 (de) * | 2005-06-17 | 2006-12-20 | ALSTOM Technology Ltd | Brenner zur vormischartigen Verbrennung |
US7975486B2 (en) | 2005-06-17 | 2011-07-12 | Alstom Technology Ltd | Burner for premix-type combustion |
CH701905A1 (de) * | 2009-09-17 | 2011-03-31 | Alstom Technology Ltd | Verfahren zum Verbrennen wasserstoffreicher, gasförmiger Brennstoffe in einem Brenner sowie Brenner zur Durchführung des Verfahrens. |
WO2011032935A3 (de) * | 2009-09-17 | 2012-03-29 | Alstom Technology Ltd. | Verfahren zum verbrennen wasserstoffreicher, gasförmiger brennstoffe in einem brenner sowie brenner zur durchführung des verfahrens |
US8549860B2 (en) | 2009-09-17 | 2013-10-08 | Alstom Technology Ltd | Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method |
DE112010003677B4 (de) | 2009-09-17 | 2023-10-26 | Ansaldo Energia Switzerland AG | Verfahren zum verbrennen wasserstoffreicher, gasförmiger brennstoffe in einem brenner sowie brenner zur durchführung des verfahrens |
Also Published As
Publication number | Publication date |
---|---|
CN1113187C (zh) | 2003-07-02 |
EP0981016B1 (de) | 2004-01-07 |
CN1245276A (zh) | 2000-02-23 |
DE59810551D1 (de) | 2004-02-12 |
US6263676B1 (en) | 2001-07-24 |
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