EP0780630B1 - Brenner für einen Wärmeerzeuger - Google Patents
Brenner für einen Wärmeerzeuger Download PDFInfo
- Publication number
- EP0780630B1 EP0780630B1 EP96810827A EP96810827A EP0780630B1 EP 0780630 B1 EP0780630 B1 EP 0780630B1 EP 96810827 A EP96810827 A EP 96810827A EP 96810827 A EP96810827 A EP 96810827A EP 0780630 B1 EP0780630 B1 EP 0780630B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- burner according
- flow
- fuel
- swirl generator
- burner
- 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
Links
Images
Classifications
-
- 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
- F23D17/002—Burners for combustion conjointly or alternatively 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, e.g. burner cooling means, noise reduction means
- F23D11/40—Mixing tubes or chambers; 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.
- a swirl-stabilized burner is known from JP 07 190 308, in which a mixing tube is connected downstream of the swirl generator.
- JP 07 190 308 in which a mixing tube is connected downstream of the swirl generator.
- the invention seeks to remedy this.
- the invention how it is marked in the claims, the task lies the basis for a premix burner of the type mentioned kind of a flame stabilization with maximized efficiency and to minimize pollutant emissions.
- the essential measure of the invention relates to the position the head-side fuel nozzle, which by a certain Distance upstream from the inflow of combustion air is reset, this distance from the selected Spray angle depends.
- Mouth of the fuel nozzle in the area of a solid casing to stand which means at the same time radially around the nozzle mouth Openings can be provided through which Purge air in the cross section induced by the fuel nozzle flows in.
- the flow cross section of these openings is selected so that in gas operation through these openings flowing air mass flow is not sufficient to the To move the backflow zone further downstream.
- the fuel spray acts practically as a jet pump, with which the air mass flow through the named Openings increased. This causes a larger axial momentum which moves the backflow zone further downstream.
- Another advantage of the invention is that by the reset of the fuel nozzle with the fuel spray a larger cone radius in the main flow, i.e. in the Combustion air flowing through the tangential air inlet slots entry.
- the fuel spray is in this Layer already decayed from a film into drops and the conical surface this fuel spray has entered into the area of the combustion air from the tangential Air inlet slots enlarged by a factor of 3. Thereby the spread of the fuel spray is improved and the Combustion air inflow not impeded.
- Air mass flow sucked in in the area of the fuel nozzle prevents wetting of the inside of the cone because it lays out as a film between the fuel spray and the wall everything defines the opening angle of the spray. This remains constant over a wide load range.
- Another important advantage of the invention is that see that by varying the opening cross sections for the Air mass flow in the area of the fuel nozzle the return flow zone and thus the flame position directly during operation can be influenced.
- Fig. 1 shows the overall structure of a burner.
- a swirl generator 100a effective, the design of which in the following Fig. 2-5 shown and described in more detail becomes.
- This swirl generator 100a is a conical structure, the tangential multiple of 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 100a transitioned seamlessly into a transition piece 200, in such a way that no detachment areas occur there can.
- the configuration of this transition geometry is under Fig. 6 described in more detail.
- This transition piece is 200 downstream of the transition geometry through a pipe 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 100a. 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 100a provided a defined mixing section in which a perfect premix of Different types of fuel is achieved.
- This mixing section so the mixing tube 220, further enables one lossless flow control, so that even in operative connection initially no backflow zone with the transition geometry can form, thus over the length of the mixing tube 220 influence on the quality of the mixture for all types of fuel can be.
- This mixing tube 220 has another other property, which is that in the mixing tube 220 even the axial speed profile is a pronounced one Possesses maximum on the axis, so that a reignition of 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 shows a schematic representation of a swirl generator 100a, which is described in more detail in the following FIGS. 3-5 becomes.
- 1 is the representation of the center placed fuel nozzle 103, which is opposite the beginning 125 of the conical flow cross section set back upstream is, distance 126 from the selected spray angle 105 depends.
- the mouth 104 comes through this displacement the fuel nozzle 103 in the area of the head-side fixed casing 101a, 102a. That through the relocation of the fuel nozzle 103 arising fuel spray 105 occurs with a larger cone radius in that of the main flow of the combustion air in the interior 114 of the burner Area so that the fuel spray 105 in this area no more than a solid compact body behaves, but has already crumbled into drops and therefore is easy to penetrate.
- the inflow of combustion air 115 in the fuel spray 105 is no longer hindered what is reflected in the mix quality in a positive sense, in that the fuel spray 105 passes through more easily the combustion air can be penetrated. Furthermore, in the area of the level of the fuel spray orifice 104 radially or quasi-radially arranged openings 124 are provided, through which a purge air in the size of the Inflows cross section induced fuel nozzle 103. The Flow cross-section of these openings 124 is selected so that in gas operation of those flowing through these openings Air mass flow is not sufficient to the backflow zone (cf. Fig. 1) to move further downstream.
- the fuel spray 105 acts practically as a jet pump, with which the air mass flow through the named Openings 124 increased. This causes a larger axial Impulse that shifts the backflow zone further downstream what acts as a good measure to prevent the flame from reigniting.
- conical partial body 101, 102 is discussed in greater detail in FIGS. 2-5. There too Configuration and mode of operation of the tangential air inlet slots 119, 120 discussed in more detail.
- FIG. 2 Fig. 3 In order to better understand the structure of the swirl generator 100a, it is advantageous if at least at the same time as FIG. 2 Fig. 3 is used. Furthermore, around this Fig. 2 not to make it unnecessarily confusing are the after the baffles 121a, 121b shown schematically in FIG. 3 only have been hinted at. 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 100a.
- This consists of two hollows 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 100a are present.
- a nozzle 103 is preferred for a liquid fuel 112, the injection 104 approximately with the narrowest cross section of the formed by the conical part body 101, 102 cone cavity 114 coincides.
- the injection capacity and the type this nozzle 103 depends on the specified parameters of the respective burner.
- the swirl generator can 100a 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 100a is also particularly suitable, the Size of the tangential air inlet slots 119, 120 to change, without changing the length of the swirl generator 100a covers a relatively large operational bandwidth can be.
- the partial bodies 101, 102 can also be shifted relative to one another in another plane, thereby even overlapping them can. It is also possible to use the partial bodies 101, 102 by a counter-rotating movement in a spiral to nest.
- it is possible to shape the Size and configuration of the tangential air inlet slots 119, 120 to vary arbitrarily, with which the swirl generator 100a can be used universally without changing its overall length is.
- 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 100a can also be operated without baffles, or other aids can be provided for this.
- FIG. 5 shows that the swirl generator 100a 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. 6 differs from Fig. 5 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 100a 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. 8 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 °.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Spray-Type Burners (AREA)
- Combustion Of Fluid Fuel (AREA)
Description
- Fig. 1
- einen als Vormischbrenner ausgelegten Brenner mit einer Mischstrecke stromab eines Drallerzeugers,
- Fig. 2
- eine schematische Darstellung des Drallerzeugers mit Positionierung der Brennstoffeindüsung,
- Fig. 3
- einen Drallerzeuger als Bestandteil des Vormischbrenners nach Fig. 1, in perspektivischer Darstellung, entsprechend aufgeschnitten,
- Fig. 4
- eine Schnittebene durch den als zweischalig ausgebildeten Drallerzeuger nach Fig. 3,
- Fig. 5
- eine Schnittebene durch einen vierschaligen Drallerzeuger,
- Fig. 6
- eine Schnittebene durch einen Drallerzeuger, dessen Schalen schaufelförmig profiliert sind,
- Fig. 7
- eine Darstellung der Form der Uebergangsgeometrie zwischen Drallerzeuger und nachgeschalteter Mischstrecke und
- Fig. 8
- 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
- 100a
- 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
- 124
- Oeffnungen
- 125
- Kegelinnenspitze
- 126
- Versetzung der Brennstoffdüse 103 stromauf gegenüber 125
- 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 (18)
- Brenner für einen Wärmeerzeuger, im wesentlichen bestehend aus einem Drallerzeuger für einen Verbrennungsluftstrom und aus Mitteln zur Eindüsung eines Brennstoffes in den Verbrennungsluftstrom, wobei stromab des Drallerzeugers (100a) eine Mischstrecke (220) angeordnet ist, dadurch gekennzeichnet, dass innerhalb eines ersten Streckenteils (200) in Strömungsrichtung verlaufende Uebergangskanäle (201) zur Ueberführung einer im Drallerzeuger (100a) gebildeten Strömung (40) in ein stromab der Uebergangsgangskanäle (201) nachgeschaltetes Rohr (20) aufweist, und dass als ein Mittel zur Eindüsung eines Brennstoffes eine Düse (103) dient, welche gegenüber einem stromaufwärtigen Ende des Drallerzeugers (100a) um eine Strecke (126) stromauf versetzt ist.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass der Drallerzeuger eine Anzahl am Umfang verteilter Brennlufteinlässe aufweist, dergestalt, dass mehrere Brennluft-Teilströme gebildet werden, und dass die Anzahl der Uebergangskanäle (201) in der Mischstrecke (220) der Anzahl der vom Drallerzeuger (100a) gebildeten Teilströme entspricht.
- Brenner nach Anspruch 1, dadurch gekennzeichnet, dass die Austrittsebene des Rohres (20) mit einer Abrisskante (A) zur Stabilisierung und Vergrösserung einer sich stromab bildenden Rückströmzone (50) ausgebildet ist.
- Brenner nach Anspruch 3, dadurch gekennzeichnet, dass die Abrisskante (A) aus einem Uebergangsradius (R) im Bereich der Austrittsebene des Rohres (20) und einer von dieser Austrittsebene abgesetzten Abrissstufe (S) besteht.
- Brenner nach Anspruch 4, 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 3, dadurch gekennzeichnet, dass stromauf der Abrisskante (A) ein Diffusor und/oder eine Venturistrecke angeordnet sind.
- 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 versehen ist.
- Brenner nach Anspruch 7, dadurch gekennzeichnet, dass die Oeffnungen (21) unter einem spitzen Winkel gegenüber der Brennerachse (60) verlaufen.
- 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 (100a) 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 der Drallerzeuger (100a) 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 kopfseitig stromauf des vom Drallerzeuger (100a) induzierten Kegelanfangs die Brennstoffdüse (103) angeordnet ist.
- Brenner nach Anspruch 11, dadurch gekennzeichnet, dass die Brennstoffdüse (103) auf der Brennerachse (60) angeordnet ist.
- Brenner nach den Ansprüchen 11 und 12, dadurch gekennzeichnet, dass die Brennstoffdüse (103) mit einem flüssigen Brennstoff (112) und weitere Brennstoffdüsen (117) mit einem gasförmigen Brennstoff (113) betreibbar sind.
- Brenner nach Anspruch 13, dadurch gekennzeichnet, dass im Bereich der tangentialen Kanäle (119, 120) in deren Längserstreckung die weiteren Brennstoffdüsen (117) angeordnet sind.
- Brenner nach Anspruch 11, dadurch gekennzeichnet, dass die Teilkörper (140, 141, 142, 143) im Querschnitt eine schaufelförmige Profilierung aufweisen.
- Brenner nach Anspruch 11, dadurch gekennzeichnet, dass die Teilkörper in Strömungsrichtung einen festen Kegelwinkel, oder eine zunehmende Kegelneigung, oder eine abnehmende Kegelneigung aufweisen.
- Brenner nach Anspruch 11, dadurch gekennzeichnet, dass die Teilkörper spiralförmig ineinandergeschachtelt sind.
- Brenner nach Anspruch 11, dadurch gekennzeichnet, dass der Durchflussquerschnitt der tangentialen Lufteintrittsschlitze (119, 120) in Längsrichtung des Brenners abnimmt.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19547912A DE19547912A1 (de) | 1995-12-21 | 1995-12-21 | Brenner für einen Wärmeerzeuger |
DE19547912 | 1995-12-21 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0780630A2 EP0780630A2 (de) | 1997-06-25 |
EP0780630A3 EP0780630A3 (de) | 1998-07-29 |
EP0780630B1 true EP0780630B1 (de) | 2001-09-26 |
Family
ID=7780867
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96810827A Expired - Lifetime EP0780630B1 (de) | 1995-12-21 | 1996-11-27 | Brenner für einen Wärmeerzeuger |
Country Status (5)
Country | Link |
---|---|
US (1) | US5876196A (de) |
EP (1) | EP0780630B1 (de) |
JP (1) | JP3904644B2 (de) |
CN (1) | CN1111672C (de) |
DE (2) | DE19547912A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015055916A1 (fr) | 2013-10-14 | 2015-04-23 | Cogebio | Brûleur de gaz pauvre |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19639301A1 (de) * | 1996-09-25 | 1998-03-26 | Abb Research Ltd | Brenner zum Betrieb einer Brennkammer |
DE19640198A1 (de) * | 1996-09-30 | 1998-04-02 | Abb Research Ltd | Vormischbrenner |
DE19736902A1 (de) * | 1997-08-25 | 1999-03-04 | Abb Research Ltd | Brenner für einen Wärmeerzeuger |
DE59709791D1 (de) * | 1997-09-19 | 2003-05-15 | Alstom Switzerland Ltd | Brenner für den Betrieb eines Wärmeerzeugers |
EP0909921B1 (de) * | 1997-10-14 | 2003-01-02 | Alstom | Brenner für den Betrieb eines Wärmeerzeugers |
DE59709446D1 (de) * | 1997-10-31 | 2003-04-10 | 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 |
DE10051221A1 (de) * | 2000-10-16 | 2002-07-11 | Alstom Switzerland Ltd | Brenner mit gestufter Brennstoff-Eindüsung |
JP4524902B2 (ja) * | 2000-10-25 | 2010-08-18 | 株式会社Ihi | 予混合燃料噴射弁を備えた低NOx燃焼器 |
DE50110801D1 (de) * | 2000-12-23 | 2006-10-05 | Alstom Technology Ltd | Brenner zur Erzeugung eines Heissgases |
DE50212351D1 (de) * | 2001-04-30 | 2008-07-24 | Alstom Technology Ltd | Vorrichtung zum Verbrennen eines gasförmigen Brennstoff-Oxidator-Gemischs |
EP1262714A1 (de) | 2001-06-01 | 2002-12-04 | ALSTOM (Switzerland) Ltd | Brenner mit Abgasrückführung |
WO2005078348A1 (de) * | 2004-02-12 | 2005-08-25 | Alstom Technology Ltd | Vormischbrenneranordnung zum betreiben einer brennkammer sowie verfahren zum betreiben einer brennkammer |
US7097448B2 (en) * | 2004-05-07 | 2006-08-29 | Peter Chesney | Vortex type gas lamp |
WO2006058843A1 (de) * | 2004-11-30 | 2006-06-08 | Alstom Technology Ltd | Verfahren und vorrichtung zur verbrennung von wasserstoff in einem vormischbrenner |
JP4977522B2 (ja) * | 2007-04-25 | 2012-07-18 | 株式会社日立製作所 | ガスタービン燃焼器 |
DE102008000050A1 (de) * | 2007-08-07 | 2009-02-12 | Alstom Technology Ltd. | Brenner für eine Brennkammer einer Turbogruppe |
GB0902221D0 (en) * | 2009-02-11 | 2009-03-25 | Edwards Ltd | Pilot |
CA2786597A1 (en) | 2010-01-06 | 2011-07-14 | The Outdoor Greatroom Company LLLP | Fire container assembly |
JP5203489B2 (ja) * | 2011-06-15 | 2013-06-05 | 中外炉工業株式会社 | 燃焼装置 |
DE102014205200B3 (de) * | 2014-03-20 | 2015-06-11 | Kba-Metalprint Gmbh | Vorrichtung zur thermischen Nachverbrennung von Abluft |
DE102014205198A1 (de) | 2014-03-20 | 2015-09-24 | Kba-Metalprint Gmbh | Brenner und Vorrichtung zur thermischen Nachverbrennung von Abluft |
CN108006695B (zh) * | 2016-11-01 | 2019-12-06 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 优化用于燃气轮机的预混合燃料喷嘴的方法 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH392746A (de) * | 1962-01-12 | 1965-05-31 | Elco Oelbrennerwerk Ag | Brennerkopf |
US3656692A (en) * | 1971-01-05 | 1972-04-18 | Texaco Inc | Oil burner |
US3851466A (en) * | 1973-04-12 | 1974-12-03 | Gen Motors Corp | Combustion apparatus |
US3905192A (en) * | 1974-08-29 | 1975-09-16 | United Aircraft Corp | Combustor having staged premixing tubes |
US4014639A (en) * | 1975-04-10 | 1977-03-29 | Minnesota Mining And Manufacturing Company | Recirculating vortex burner |
US4271675A (en) * | 1977-10-21 | 1981-06-09 | Rolls-Royce Limited | Combustion apparatus for gas turbine engines |
US4561841A (en) * | 1980-11-21 | 1985-12-31 | Donald Korenyi | Combustion apparatus |
GB2175684B (en) * | 1985-04-26 | 1989-12-28 | Nippon Kokan Kk | Burner |
CH674561A5 (de) | 1987-12-21 | 1990-06-15 | Bbc Brown Boveri & Cie | |
CH680157A5 (de) * | 1989-12-01 | 1992-06-30 | Asea Brown Boveri | |
JPH07190308A (ja) * | 1993-12-28 | 1995-07-28 | Hitachi Ltd | 旋回型バーナ |
FR2717250B1 (fr) * | 1994-03-10 | 1996-04-12 | Snecma | Système d'injection à prémélange. |
DE4408136A1 (de) * | 1994-03-10 | 1995-09-14 | Bmw Rolls Royce Gmbh | Verfahren und Vorrichtung zur Kraftstoff-Aufbereitung für eine Gasturbinen-Brennkammer |
DE4416650A1 (de) * | 1994-05-11 | 1995-11-16 | Abb Management Ag | Verbrennungsverfahren für atmosphärische Feuerungsanlagen |
DE4435266A1 (de) * | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner |
-
1995
- 1995-12-21 DE DE19547912A patent/DE19547912A1/de not_active Withdrawn
-
1996
- 1996-11-27 EP EP96810827A patent/EP0780630B1/de not_active Expired - Lifetime
- 1996-11-27 DE DE59607769T patent/DE59607769D1/de not_active Expired - Lifetime
- 1996-12-04 US US08/760,410 patent/US5876196A/en not_active Expired - Lifetime
- 1996-12-19 JP JP33972796A patent/JP3904644B2/ja not_active Expired - Lifetime
- 1996-12-21 CN CN96123843A patent/CN1111672C/zh not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015055916A1 (fr) | 2013-10-14 | 2015-04-23 | Cogebio | Brûleur de gaz pauvre |
Also Published As
Publication number | Publication date |
---|---|
EP0780630A2 (de) | 1997-06-25 |
CN1157893A (zh) | 1997-08-27 |
CN1111672C (zh) | 2003-06-18 |
DE19547912A1 (de) | 1997-06-26 |
JP3904644B2 (ja) | 2007-04-11 |
EP0780630A3 (de) | 1998-07-29 |
JPH09178121A (ja) | 1997-07-11 |
DE59607769D1 (de) | 2001-10-31 |
US5876196A (en) | 1999-03-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0780630B1 (de) | Brenner für einen Wärmeerzeuger | |
EP0780629B1 (de) | Brenner für einen Wärmeerzeuger | |
EP0704657B1 (de) | Brenner | |
EP0918190A1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0899508B1 (de) | Brenner für einen Wärmeerzeuger | |
EP0918191B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0833105B1 (de) | Vormischbrenner | |
EP0797051B1 (de) | Brenner für einen Wärmeerzeuger | |
DE19757189B4 (de) | Verfahren zum Betrieb eines Brenners eines Wärmeerzeugers | |
EP0994300B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0916894B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0987493B1 (de) | Brenner für einen Wärmeerzeuger | |
EP0931980B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0909921B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0751351B1 (de) | Brennkammer | |
EP0903540B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
EP0919768B1 (de) | Brenner zum Betrieb eines Wärmeerzeugers | |
EP0833104B1 (de) | Brenner zum Betrieb einer Brennkammer | |
DE19537636B4 (de) | Kraftwerksanlage | |
EP0913630B1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
DE19914666B4 (de) | Brenner für einen Wärmeerzeuger | |
EP0780628B1 (de) | Vormischbrenner für einen Wärmeerzeuger | |
EP0899506A2 (de) | Brennervorrichtung | |
DE10042315A1 (de) | Brenner für einen Wärmeerzeuger |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE FR GB IT SE |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE FR GB IT SE |
|
17P | Request for examination filed |
Effective date: 19981223 |
|
17Q | First examination report despatched |
Effective date: 20000331 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ABB ALSTOM POWER (SCHWEIZ) AG |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ALSTROM (SCHWEIZ) AG |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ALSTOM (SCHWEIZ) AG |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB IT SE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRE;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.SCRIBED TIME-LIMIT Effective date: 20010926 |
|
REF | Corresponds to: |
Ref document number: 59607769 Country of ref document: DE Date of ref document: 20011031 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20011201 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: UWE ROESLER, DE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20120809 AND 20120815 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: RUEGER, BARTHELT & ABEL, DE Effective date: 20120713 Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: ROESLER, UWE, DIPL.-PHYS.UNIV., DE Effective date: 20120713 Ref country code: DE Ref legal event code: R081 Ref document number: 59607769 Country of ref document: DE Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: ALSTOM (SCHWEIZ) AG, BADEN, AARGAU, CH Effective date: 20120713 Ref country code: DE Ref legal event code: R081 Ref document number: 59607769 Country of ref document: DE Owner name: ALSTOM TECHNOLOGY LTD., CH Free format text: FORMER OWNER: ALSTOM (SCHWEIZ) AG, BADEN, AARGAU, CH Effective date: 20120713 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: TP Owner name: ALSTOM TECHNOLOGY LTD., CH Effective date: 20120918 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20151118 Year of fee payment: 20 Ref country code: DE Payment date: 20151119 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20151119 Year of fee payment: 20 Ref country code: SE Payment date: 20151118 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: RUEGER ABEL PATENTANWAELTE PARTGMBB, DE Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: RUEGER, BARTHELT & ABEL, DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59607769 Country of ref document: DE Representative=s name: RUEGER, BARTHELT & ABEL, DE Ref country code: DE Ref legal event code: R081 Ref document number: 59607769 Country of ref document: DE Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: ALSTOM TECHNOLOGY LTD., BADEN, CH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R071 Ref document number: 59607769 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20161126 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: CD Owner name: ALSTOM TECHNOLOGY LTD, CH Effective date: 20161124 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20161126 |