EP0780629B1 - Brenner für einen Wärmeerzeuger - Google Patents
Brenner für einen Wärmeerzeuger Download PDFInfo
- Publication number
- EP0780629B1 EP0780629B1 EP96810804A EP96810804A EP0780629B1 EP 0780629 B1 EP0780629 B1 EP 0780629B1 EP 96810804 A EP96810804 A EP 96810804A EP 96810804 A EP96810804 A EP 96810804A EP 0780629 B1 EP0780629 B1 EP 0780629B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- burner according
- tube
- flow
- swirl generator
- section
- 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.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion simultaneously or alternately of gaseous or liquid or pulverulent fuel
- F23D17/002—Burners for combustion simultaneously or alternately of gaseous or liquid or pulverulent fuel gaseous or liquid 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
- 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
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details
- F23D11/40—Mixing tubes; Burner heads
- F23D11/402—Mixing chambers downstream of the nozzle
-
- 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 present invention relates to a burner according to the preamble of claim 1.
- EP-B1-0 321 809 describes a shell made of several shells conical burner, so-called double cone burner, for Generation of a closed swirl flow in the cone head has become known, which due to the increasing swirl along the cone tip becomes unstable and into an annular swirl flow with reverse flow in the core.
- Fuels such as gaseous fuels are produced along the the individual adjacent shells formed channels, too Called air inlet slots, injected and homogeneous with the Air mixes before combustion by ignition at the stagnation point the backflow zone or backflow bubble, which acts as a flame holder is used.
- Liquid fuels will be preferably injected via a central nozzle on the burner head and then evaporate in the cone cavity.
- JP 07190308 A discloses one Burner with a swirl generator for application of a combustion air-fuel mixture with one Swirl. Following this swirl generator closes a tubular mixing section, which opens into a combustion chamber. Because of the geometric Design of the swirl generator is a conical Vortex formed at a point on the burner axis collapsed in the combustion chamber and there one circular flow to form a stable backflow zone evokes the stabilization of the flame serves.
- the invention seeks to remedy this.
- the invention how it is characterized in the claims, the task lies based on precautions for a burner of the type mentioned propose by which a perfect premix of fuels of various types and achieved which are reliable and optimal flame positioning is achieved.
- the proposed burner has one on the head side and upstream Mixing section on a swirl generator, which is preferred can be interpreted in such a way that the aerodynamic Basic principles of the so-called double-cone burner according to EP-A1-0 321 809 can be used. Basically, however, is that Use of an axial or radial swirl generator possible.
- the mixing section itself preferably consists of a tubular one Mixing element, hereinafter called mixing tube, which a perfect premixing of different fuelskind allowed.
- the flow from the swirl generator is seamless into the mixing tube initiated: This happens through a transition geometry, which consists of transition channels, which in the initial phase this mixing tube are excluded, and which the flow in the subsequent effective flow cross-section transfer the mixing tube.
- This low loss Flow initiation between swirl generator and mixing tube prevented first the immediate formation of a backflow zone at the exit of the swirl generator.
- the swirl strength in the swirl generator is above its Geometry chosen so that the vertebra does not burst in the mixing tube, but further downstream at the combustion chamber inlet takes place, the length of this mixing tube dimensioned so is that there is sufficient mix quality for everyone Fuel types results.
- the twist strength results from the design the corresponding cone angle, the air inlet slots and their number.
- the axial speed profile has a pronounced profile in the mixing tube Maximum on the axis and thereby prevents backfire in this area.
- the axial speed drops down to the wall.
- various measures are provided: For example, on the one hand, the entire speed level by using a mixing tube with a sufficient Lift small diameter.
- Another possibility consists of only the outside speed of the Increase mixing tube by a small part of the combustion air over an annular gap or through filming holes flows into the mixing tube downstream of the transition channels.
- transition channels to initiate the flow affects from the swirl generator in the mixing tube, so to say that the course of these transition channels is spiral can be constricting or expanding accordingly the effective subsequent flow cross-section of the mixing tube.
- Part of the pressure loss that may be generated can be caused by Attachment of a diffuser at the end of the mixing tube compensated become. In this area or upstream one can also Venturi range can be provided.
- the combustion chamber closes at the end of the mixing tube a cross-sectional leap.
- a central one is formed here Backflow zone, the properties of which are those of a flame holder are.
- the creation of a stable backflow zone requires one sufficiently high swirl number in the mixing tube. But it is one Initially undesirable, stable backflow zones can occur the supply of small, strongly swirled air volumes, 5-20% of the Total air volume generated at the end of the pipe.
- Fig. 1 shows the overall structure of a burner.
- a swirl generator 100 effective, the design of which in the following Fig. 2-5 shown and described in more detail becomes.
- This swirl generator 100 is a conical one Formations that are tangential multiple times from a tangential inflowing combustion air flow 115 is applied becomes.
- the flow that forms here is based on a transition geometry provided downstream of the swirl generator 100 transitioned seamlessly into a transition piece 200, in such a way that no separation areas can occur there.
- the configuration of this transition geometry is under Fig. 6 described in more detail.
- This transition piece 200 is on the outflow side the transition geometry through a tube 20 extended, both parts of the actual mixing tube 220, also called mixing section, form the burner.
- the mixing tube 220 may consist of a single piece, i.e. then that the transition piece 200 and pipe 20 merged into a single coherent structure with the characteristics of each part preserved stay. Become transition piece 200 and tube 20 from two parts created, they are connected by a socket ring 10, the same bushing ring 10 on the head side as the anchoring surface serves for the swirl generator 100. Such a Socket ring 10 also has the advantage that different Mixing tubes can be used. Outflow side of the tube 20 is the actual combustion chamber 30, which only symbolizes here through the flame tube is.
- the mixing tube 220 meets the condition that downstream of the swirl generator 100 provides a defined mixing section in which a perfect premix of fuels of different types is achieved.
- This mixing section so the mixing tube 220, furthermore enables a loss-free Flow guidance, so that also in operative connection do not initially form a backflow zone with the transition geometry can, which over the length of the mixing tube 220 to the Mix quality for all types of fuel influence can be exercised can.
- This mixing tube 220 has yet another Property, which is that in the mixing tube 220 even the axial speed profile is a pronounced maximum owns on the axis, so that the Flame from the combustion chamber is not possible. However it is correct that with such a configuration this axial speed drops to the wall.
- the mixing tube 220 in Flow and circumferential direction with a number regularly or irregularly distributed holes 21 of the most varied Provide cross sections and directions through which an amount of air flows into the interior of the mixing tube 220, and along the wall in the sense of a filming an increase in speed induce.
- Another way the same To achieve effect is that the flow cross section of the mixing tube 220 on the outflow side of the transition channels 201, which has the transition geometry already mentioned form, narrowing, causing the whole Speed level increased within the mixing tube 220 becomes.
- these bores 21 run under one acute angle with respect to the burner axis 60.
- the outlet of the transition channels 201 corresponds to the narrowest Flow cross section of the mixing tube 220.
- the above Transition channels 201 therefore bridge the respective cross-sectional difference, without making the flow negative to influence. If the precaution chosen by the Guiding the pipe flow 40 along the mixing pipe 220 triggers intolerable pressure loss, can counter this Remedial action can be taken by placing one at the end of the mixing tube Diffuser not shown in the figure is provided. At the A combustion chamber 30 closes at the end of the mixing tube 220 , with a between the two flow cross-sections Cross-sectional jump is present. Only here does one form central backflow zone 50, which has the properties of a Has flame holder.
- FIG. 2 In order to better understand the structure of the swirl generator 100 it is advantageous if, at the same time as FIG. 2, at least FIG. 3 is used. Furthermore, this Fig. 2 is not unnecessary to be confusing, they are those according to the Figure 3 schematically shown guide plates 121a, 121b only hinted been recorded. In the following, the Description of Fig. 2 as required on the figures mentioned pointed out.
- the first part of the burner according to FIG. 1 forms the one according to FIG. 2 shown swirl generator 100.
- This consists of two hollow conical partial bodies 101, 102 which are offset from one another are nested.
- the number of conical Partial body can of course be larger than two, such as Figures 4 and 5 show; this depends on how each further will be explained in more detail below, depending on the type of debt collection of the whole burner. It is with certain operating constellations not excluded one from one single spiral existing swirl generator.
- the Offset of the respective central axis or longitudinal symmetry axes 201b, 202b of the tapered partial bodies 101, 102 to one another creates a mirror image of the neighboring wall Arrangement, each a tangential channel, i.e.
- the cone shape of the one shown Partial body 101, 102 has a flow direction certain fixed angle. Of course, depending on the operational use, can the partial body 101, 102 in the direction of flow have an increasing or decreasing taper similar to a trumpet or Tulip. The latter two Shapes are not included in the drawing as they are for the expert can be easily understood.
- the two tapered partial bodies 101, 102 each have a cylindrical Initial part 101a, 102a, which also, analogous to the tapered Partial bodies 101, 102, offset from one another, so that the tangential air inlet slots 119, 120 via the entire length of the swirl generator 100 are present.
- a nozzle 103 is preferred for a liquid fuel 112, the injection of which 104 with the narrowest cross section of the through conical partial body 101, 102 formed conical cavity 114 coincides.
- the injection capacity and the type of this Nozzle 103 depends on the specified parameters of the respective burner.
- the swirl generator can 100 purely conical, i.e. without cylindrical starting parts 101a, 102a.
- the tapered body 101, 102 also each have a fuel line 108, 109 on which along the tangential air inlet slots 119, 120 arranged and provided with injection openings 117 are, by which preferably a gaseous fuel 113 injected into the combustion air 115 flowing through there is how the arrows 116 symbolize this.
- This Fuel lines 108, 109 are preferably at the latest End of tangential inflow, before entering the cone cavity 114, placed, this for an optimal Obtain air / fuel mixture.
- fuel introduced 112 normally a liquid fuel, whereby a mixture formation with another medium without any problems is possible. This fuel 112 will tip under one Angle injected into the cone cavity 114.
- the construction of the swirl generator 100 is also excellent, the size to change the tangential air inlet slots 119, 120, with which without changing the overall length of the swirl generator 100 a relatively wide range of operations can be covered can.
- the partial bodies 101, 102 are also in another level slidable to each other, which even an overlap of the same can be provided. It is further possible, the partial body 101, 102 by an opposite to interleave rotating movement in a spiral. So it is possible to change the shape, size and the configuration of the tangential air inlet slots 119, 120 to vary arbitrarily, with which the swirl generator 100 without Changing its overall length is universally applicable.
- FIG Baffles 121a, 121b The geometric configuration of FIG Baffles 121a, 121b. They have a flow initiation function these, according to their length, the respective End of the tapered partial body 101, 102 in the direction of flow extend towards the combustion air 115.
- the Channeling the combustion air 115 into the cone cavity 114 can by opening or closing the guide plates 121a, 121b by one in the area of the entry of this channel into the Cone cavity 114 placed pivot point 123 can be optimized, this is particularly necessary if the original gap size of the tangential air inlet slots 119, 120 dynamic should be changed.
- you can dynamic arrangements can also be provided statically by required guide plates with a fixed component form the tapered partial bodies 101, 102.
- the can also Swirl generator 100 can also be operated without baffles, or other aids can be provided for this.
- FIG. 4 shows that the swirl generator 100 now made up of four partial bodies 130, 131, 132, 133 is.
- the associated longitudinal symmetry axes for each partial body are marked with the letter a.
- This configuration can be said that because of the generated lower twist strength and in cooperation with one suitably suitably enlarged slot width, the bursting of the vortex flow on the downstream side of the To prevent swirl in the mixing tube, making the mixing tube can best fulfill the role intended for him.
- Fig. 5 differs from Fig. 4 in so far as here the partial bodies 140, 141, 142, 143 have a blade profile shape, which is intended to provide a certain flow becomes. Otherwise, the mode of operation of the swirl generator stayed the same.
- the admixture of fuel 116 in the combustion air flow 115 happens from the inside the blade profiles out, i.e. the fuel line 108 is now integrated in the individual blades. Also here are the longitudinal axes of symmetry to the individual partial bodies marked with the letter a.
- the transition geometry is for a swirl generator 100 with four partial bodies, corresponding to FIG. 4 or 5, built up. Accordingly, the transition geometry points as natural extension of the upstream parts four transition channels 201 on, making up the cone quarter area the partial body mentioned is extended until it hits the wall of the tube 20 respectively. of the mixing tube 220 cuts.
- the same Considerations also apply when the swirl generator is off another principle than that described under Fig. 2, is constructed.
- the one running downward in the direction of flow The area of the individual transition channels 201 has an in Flow direction on a spiral shape, which describes a crescent shape, corresponding to the The fact that the flow cross section of the Transition piece 200 flared in the direction of flow.
- the swirl angle of the transition channels 201 in the flow direction is selected so that the pipe flow then up to A cross-sectional jump at the combustion chamber inlet is still sufficient large distance remains to make a perfect premix with to manage the injected fuel. Further increases the axial speed is also affected by the above-mentioned measures on the mixing tube wall downstream of the swirl generator.
- the transition geometry and the measures in the area of the mixing tube cause a significant increase in the axial speed profile towards the center of the mixing tube, so that the danger of early ignition is decisively counteracted becomes.
- Fig. 7 shows the tear-off edge already mentioned, which on Burner outlet is formed.
- the flow cross section of the Tube 20 is given a transition radius R in this area, whose size basically depends on the flow within the Tube 20 depends.
- This radius R is chosen so that the flow applies to the wall and so the swirl number strong can rise.
- the size of the radius can be quantified Define R so that it is> 10% of the inner diameter d of the tube is 20. Opposite a flow without a radius Now the backflow bladder 50 increases enormously.
- This Radius R extends to the exit plane of the tube 20, wherein the angle ⁇ between the beginning and end of the curvature is ⁇ 90 °.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray-Type Burners (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Sorption Type Refrigeration Machines (AREA)
- Gas Burners (AREA)
Description
- Fig. 1
- einen Brenner mit anschliessender Brennkammer,
- Fig. 2
- einen Drallerzeuger in perspektivischer Darstellung, entsprechend aufgeschnitten,
- Fig. 3
- einen Schnitt durch den 2-Schalen-Drallerzeuger, nach Fig. 2,
- Fig. 4
- einen Schnitt durch einen 4-Schalen-Drallerzeuger,
- Fig. 5
- einen Schitt durch einen Drallerzeuger, dessen Schalen schaufelförmig profiliert sind,
- Fig. 6
- eine Darstellung der Form der Uebergangsgeometrie zwischen Drallerzeuger und Mischrohr und
- Fig. 7
- eine Abrisskante zur räumlichen Stabilisierung der Rückströmzone.
- 10
- Buchenring
- 20
- Rohr
- 21
- Bohrungen, Oeffnungen
- 30
- Brennkammer
- 31
- Oeffnungen
- 40
- Strömung, Rohrströmung im Mischrohr
- 50
- Rückströmzone, Rückströmblase
- 60
- Brennerachse
- 100
- Drallerzeuger
- 101, 102
- Teilkörper
- 101a, 102b
- Zylindrische Anfangsteile
- 101b, 102b
- Längssymmetrieachsen
- 103
- Brennstoffdüse
- 104
- Brennstoffeindüsung
- 105
- Brennstoffspray (Brennstoffeindüsungsprofil)
- 108, 109
- Brennstoffleitungen
- 112
- Flüssiger Brennstoff
- 113
- Gasförmiger Brennstoff
- 114
- Kegelhohlraum
- 115
- Verbrennungsluft (Verbrennungsluftstrom)
- 116
- Brennstoff-Eindüsung aus den Leitungen 108, 109
- 117
- Brennstoffdüsen
- 119, 120
- Tangentiale Lufteintrittsschlitze
- 121a, 121b
- Leitbleche
- 123
- Drehpunkt der Leitbleche
- 130, 131, 132, 133
- Teilkörper
- 131a, 131a, 132a, 133a
- Längssymmetrieachsen
- 140, 141, 142, 143
- Schaufelprofilförmige Teilkörper
- 140a, 141a, 142a, 143a
- Längssymmetrieachsen
- 200
- Uebergangsstück
- 201
- Uebergangskanäle
- 220
- Mischrohr
- d
- Innendurchmesser des Rohres 20
- R
- Uebergangsradius
- T
- Tangentiale der Abrisskante
- A
- Abrisskante
- S
- Abrissstufe
- β
- Uebergangswinkel von R
- β'
- Winkel zwischen T und A
Claims (14)
- Brenner für einen Wärmeerzeuger, im wesentlichen bestehend aus einem Drallerzeuger (100) für einen Verbrennungsluftstrom und aus Mitteln zur Eindüsung eines Brennstoffes in den Verbrennungsluftstrom, wobei stromab des Drallerzeugers (100) eine Mischstrecke (220) angeordnet ist,
dadurch gekennzeichnet,
dass die Mischstrecke (220) innerhalb eines ersten Streckenteils (200) in Strömungsrichtung verlaufende Übergangskanäle (201) zur Überführung einer im Drallerzeuger (100) gebildeten Strömung (40) in ein stromab der Übergangskanäle (201) nachgeschaltetes Rohr (20) aufweist, und dass die Austrittsebene dieses Rohres (20) zur Brennkammer (30) mit einer Abrisskante (A) zur Stabilisierung und Vergrößerung eines sich stromab bildenden Rückströmzone (50) ausgebildet ist. - Brenner nach Anspruch 1, dadurch gekennzeichnet, dass die Anzahl der Uebergangskanäle (201) in der Mischstrecke (220) der Anzahl der vom Drallerzeuger (100) gebildeten Teilströme entspricht.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass das der Uebergangskanäle (201) nachgeschaltete Rohr (20) in Strömungs- und Umfangsrichtung mit Oeffnungen (21) zur Eindüsung eines Luftstromes ins Innere des Rohres (20) versehen ist.
- Brenner nach Anspruch 3, dadurch gekennzeichnet, dass die Oeffnungen (21) unter einem spitzen Winkel gegenüber der Brennerachse (60) des Rohres (20) verlaufen.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass die Abrisskante (A) aus einem Uebergangsradius (R) im Bereich der Austrittsebene des Rohres (20) und einer von der Austrittsebene des Rohres (20) abgesetzten Abrissstufe (S) besteht.
- Brenner nach Anspruch 5, dadurch gekennzeichnet, dass der Uebergangsradius (R) > 10% des Innendurchmessers des Rohres (20) beträgt, und dass die Abrissstufe (S) eine Tiefe > 3 mm aufweist.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass der Durchflussquerschnitt des Rohres (20) stromab der Uebergangskanäle (201) kleiner, gleich gross oder grösser als der Querschnitt der im Drallerzeuger (100) gebildeten Strömung (40) ist.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass stromab der Mischstrecke (220) eine Brennkammer (30) angeordnet ist, dass zwischen der Mischstrecke (220) und der Brennkammer (30) ein Querschnittssprung vorhanden ist, der den anfänglichen Strömungsquerschnitt der Brennkammer (30) induziert, und dass im Bereich dieses Querschnittssprunges eine Rückströmzone (50) wirkbar ist.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass stromauf der Abrisskante (A) ein Diffusor und/oder eine Venturistrecke vorhanden ist.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass der Drallerzeuger (100) aus mindestens zwei hohlen, kegelförmigen, in Strömungsrichtung ineinandergeschachtelten Teilkörpern (101, 102; 130, 131, 132, 133; 140, 141, 142, 143) besteht, dass die jeweiligen Längssymmetrieachsen (101b, 102b; 130a, 131a, 132a, 133a; 140a, 141a, 142a, 143a) dieser Teilkörper gegeneinander versetzt verlaufen, dergestalt, dass die benachbarten Wandungen der Teilkörper in deren Längserstreckung tangentiale Kanäle (119, 120) für einen Verbrennungsluftstromes (115) bilden, und dass im von den Teilkörpern gebildeten Kegelhohlraum (114) mindestens eine Brennstoffdüse (103) angeordnet ist.
- Brenner nach Anspruch 10, dadurch gekennzeichnet, dass im Bereich der tangentialen Kanäle (119, 120) in deren Längserstreckung weitere Brennstoffdüsen (117) angeordnet sind.
- Brenner nach Anspruch 10, dadurch gekennzeichnet, dass die Teilkörper (140, 141, 142, 143) im Querschnitt eine schaufelförmige Profilierung aufweisen.
- Brenner nach Anspruch 10, dadurch gekennzeichnet, dass die Teilkörper in Strömungsrichtung einen festen Kegelwinkel, oder eine zunehmende Kegelneigung, oder eine abnehmende Kegelneigung aufweisen.
- Brenner nach Anspruch 10, dadurch gekennzeichnet, dass die Teilkörper spiralförmig ineinandergeschachtelt sind.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19547913A DE19547913A1 (de) | 1995-12-21 | 1995-12-21 | Brenner für einen Wärmeerzeuger |
| DE19547913 | 1995-12-21 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0780629A2 EP0780629A2 (de) | 1997-06-25 |
| EP0780629A3 EP0780629A3 (de) | 1998-08-19 |
| EP0780629B1 true EP0780629B1 (de) | 2001-07-11 |
Family
ID=7780868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP96810804A Expired - Lifetime EP0780629B1 (de) | 1995-12-21 | 1996-11-18 | Brenner für einen Wärmeerzeuger |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5735687A (de) |
| EP (1) | EP0780629B1 (de) |
| JP (1) | JPH09184606A (de) |
| KR (1) | KR970046984A (de) |
| AT (1) | ATE203101T1 (de) |
| CA (1) | CA2190805A1 (de) |
| DE (2) | DE19547913A1 (de) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6834504B2 (en) | 2001-07-26 | 2004-12-28 | Alstom Technology Ltd | Premix burner with high flame stability having a net-like structure within the mixing section |
| US7424804B2 (en) | 2003-03-07 | 2008-09-16 | Alstom Technology Ltd | Premix burner |
| US7584616B2 (en) | 2004-12-23 | 2009-09-08 | Alstom Technology Ltd | Method for the operation of a gas turbo group |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5954496A (en) * | 1996-09-25 | 1999-09-21 | Abb Research Ltd. | Burner for operating a combustion chamber |
| DE19736902A1 (de) * | 1997-08-25 | 1999-03-04 | Abb Research Ltd | Brenner für einen Wärmeerzeuger |
| DE19737998A1 (de) * | 1997-08-30 | 1999-03-04 | Abb Research Ltd | Brennervorrichtung |
| DE59709791D1 (de) * | 1997-09-19 | 2003-05-15 | Alstom Switzerland Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0908671B1 (de) | 1997-10-08 | 2003-05-14 | ALSTOM (Switzerland) Ltd | Verfahren zur Verbrennung von gasförmigen, flüssigen sowie mittel-oder niederkalorischen Brennstoffen in einem Brenner |
| EP0909921B1 (de) | 1997-10-14 | 2003-01-02 | Alstom | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0913630B1 (de) * | 1997-10-31 | 2003-03-05 | ALSTOM (Switzerland) Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0916894B1 (de) | 1997-11-13 | 2003-09-24 | ALSTOM (Switzerland) Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
| DE59710380D1 (de) * | 1997-11-21 | 2003-08-07 | Alstom | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0918190A1 (de) * | 1997-11-21 | 1999-05-26 | Abb Research Ltd. | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0919768B1 (de) * | 1997-11-25 | 2003-02-05 | Alstom | Brenner zum Betrieb eines Wärmeerzeugers |
| DE19757189B4 (de) * | 1997-12-22 | 2008-05-08 | Alstom | Verfahren zum Betrieb eines Brenners eines Wärmeerzeugers |
| EP0931980B1 (de) | 1998-01-23 | 2003-04-09 | ALSTOM (Switzerland) Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
| EP0987493B1 (de) | 1998-09-16 | 2003-08-06 | Abb Research Ltd. | Brenner für einen Wärmeerzeuger |
| EP0994300B1 (de) | 1998-10-14 | 2003-11-26 | ALSTOM (Switzerland) Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
| DE19859829A1 (de) | 1998-12-23 | 2000-06-29 | Abb Alstom Power Ch Ag | Brenner zum Betrieb eines Wärmeerzeugers |
| DE19914666B4 (de) | 1999-03-31 | 2009-08-20 | Alstom | Brenner für einen Wärmeerzeuger |
| EP1065346A1 (de) | 1999-07-02 | 2001-01-03 | Asea Brown Boveri AG | Gasturbinenbrennkammer |
| DE59909531D1 (de) | 1999-07-22 | 2004-06-24 | Alstom Technology Ltd Baden | Vormischbrenner |
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| JP5453322B2 (ja) * | 2008-03-07 | 2014-03-26 | アルストム テクノロジー リミテッド | バーナ装置並びにバーナ装置の使用 |
| US8561602B2 (en) * | 2008-12-24 | 2013-10-22 | Agio International Company, Ltd. | Gas feature and method |
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| 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. |
| RU2561956C2 (ru) * | 2012-07-09 | 2015-09-10 | Альстом Текнолоджи Лтд | Газотурбинная система сгорания |
| EP2685160B1 (de) * | 2012-07-10 | 2018-02-21 | Ansaldo Energia Switzerland AG | Multikonus-Vormischungsbrenner für eine Gasturbine |
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| JP6602004B2 (ja) * | 2014-09-29 | 2019-11-06 | 川崎重工業株式会社 | 燃料噴射器及びガスタービン |
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| US2183596A (en) * | 1938-01-28 | 1939-12-19 | Eastman Kodak Co | Burner construction |
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| DE4435266A1 (de) * | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner |
-
1995
- 1995-12-21 DE DE19547913A patent/DE19547913A1/de not_active Withdrawn
-
1996
- 1996-11-18 AT AT96810804T patent/ATE203101T1/de not_active IP Right Cessation
- 1996-11-18 EP EP96810804A patent/EP0780629B1/de not_active Expired - Lifetime
- 1996-11-18 DE DE59607269T patent/DE59607269D1/de not_active Expired - Lifetime
- 1996-11-20 CA CA002190805A patent/CA2190805A1/en not_active Abandoned
- 1996-11-22 US US08/753,330 patent/US5735687A/en not_active Expired - Lifetime
- 1996-12-17 KR KR1019960066837A patent/KR970046984A/ko not_active Withdrawn
- 1996-12-24 JP JP8343827A patent/JPH09184606A/ja active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6834504B2 (en) | 2001-07-26 | 2004-12-28 | Alstom Technology Ltd | Premix burner with high flame stability having a net-like structure within the mixing section |
| US7424804B2 (en) | 2003-03-07 | 2008-09-16 | Alstom Technology Ltd | Premix burner |
| US7584616B2 (en) | 2004-12-23 | 2009-09-08 | Alstom Technology Ltd | Method for the operation of a gas turbo group |
Also Published As
| Publication number | Publication date |
|---|---|
| DE19547913A1 (de) | 1997-06-26 |
| KR970046984A (ko) | 1997-07-26 |
| CA2190805A1 (en) | 1997-06-22 |
| EP0780629A3 (de) | 1998-08-19 |
| US5735687A (en) | 1998-04-07 |
| DE59607269D1 (de) | 2001-08-16 |
| EP0780629A2 (de) | 1997-06-25 |
| ATE203101T1 (de) | 2001-07-15 |
| JPH09184606A (ja) | 1997-07-15 |
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