EP0057747B1 - Burner for the combustion of dust-like fuels - Google Patents

Burner for the combustion of dust-like fuels Download PDF

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Publication number
EP0057747B1
EP0057747B1 EP81108054A EP81108054A EP0057747B1 EP 0057747 B1 EP0057747 B1 EP 0057747B1 EP 81108054 A EP81108054 A EP 81108054A EP 81108054 A EP81108054 A EP 81108054A EP 0057747 B1 EP0057747 B1 EP 0057747B1
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EP
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Prior art keywords
fuel
duct
outlet
burner according
annular
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EP81108054A
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German (de)
French (fr)
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EP0057747A3 (en
EP0057747A2 (en
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Joachim Kümmel
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D1/00Burners for combustion of pulverulent fuel

Definitions

  • the invention relates to a burner for the combustion of dusty fuels with a central channel for the supply of a core air jet with an essentially annular primary air outlet, with a jacket channel for the supply of secondary air with an annular secondary air outlet surrounding the primary air outlet and with a fuel channel for the supply of the fuel an annular fuel outlet arranged between the primary and secondary air outlet, at least one of the two circumferential walls of the fuel outlet being rotatable and driven, and furthermore the core air jet being directed at least partially outward against the fuel and the fuel being acted on by secondary air.
  • GB-A-528 018 shows a burner which is primarily intended for the combustion of oil fuels. However, it is also considered suitable for the use of other fuels, for example dust-like fuels.
  • the burner has a central duct for the supply of core air with an annular primary air outlet which is directed slightly outwards.
  • the central channel is surrounded by a fuel channel through which the respective fuel is supplied.
  • the fuel outlet is also ring-shaped, the inner wall of the fuel outlet simultaneously forming the outer wall of the central channel.
  • the outer wall of the fuel outlet is cup-shaped and protrudes beyond the primary air outlet.
  • the primary air outlet and fuel outlet are practically parallel.
  • the fuel channel and fuel outlet are surrounded by a jacket channel for the supply of secondary air.
  • the jacket channel is divided into two ring channels, the inner ring channel being formed on the inside by the rotatable outer wall of the fuel channel and on the outside by a conically widening ring wall. This in turn forms the inner wall of the outer ring channel, the outlet for the outer ring channel opening far before the primary air outlet or fuel outlet.
  • the inner ring channel is so narrow that the vast majority of the secondary air escapes through the outer ring channel.
  • the invention is therefore based on the object of designing a burner of the type mentioned in such a way that it is also suitable for small power ranges, has a large control range and is insensitive to a wide coal dust band.
  • this object is achieved in that the core air jet at the primary air outlet is directed essentially radially to the mouth of the fuel outlet and onto the secondary air outlet.
  • the fuel is immediately deflected outwards by the core air jet after it has emerged and thus reaches the area of the secondary air outlet in the shortest possible way. This creates an intensive mixing of the fuel with the primary air and then with the secondary air. This provides enough oxygen to maintain the combustion of the outgassed coal particles. The path is so short that the flame, once started, does not go out. It has been shown that the burner is also suitable for small output ranges well below 5 Gcal / h, especially for the output range of 0.3 to 3.5 Gcal / h and has a large control range. So that with this burner opened up a new performance range for dusty fuels.
  • Another advantage of the burner according to the invention is the enlargement of the control range, which is now approximately 25% to 100%. Again, the burner is much less sensitive to a wide range of fuel dust so that mixed bed dust can also be used.
  • the fine and ultra-fine dust content is carried out of the ring nozzle with the carrier air, while the larger particles slide to the outlet due to the rotating movement of the part of the ring nozzle in question.
  • the sliding of the dust grains towards the fuel outlet is promoted by the conically widening design of the diameter of the ring nozzle.
  • This conical widening should be the same, preferably smaller than the angle of repose of the fuel in question, in order to avoid erosions and agglomerations.
  • the fuel channel should have an S-shaped cross section in the area of the ring nozzle.
  • the overall cross-section should initially widen in the area of the S-shaped course and narrow again towards the ring nozzle. This measure brings about a comparison of the fuel flow over the circumference.
  • the central channel runs out against a shielding plate to form an annular gap which opens before the exit of the ring nozzle. Since this shielding plate is very hot due to the temperatures prevailing in the combustion chamber, the core air can heat up there, which favors the initial ignition of the fuel. In addition, a deflection in the radial direction to the exit of the fuel at the ring nozzle is thereby easily achieved.
  • the core air should expediently emerge from the annular gap at approximately 20 to 100 m / s in order to achieve intensive mixing with the escaping fuel and a deflection into the secondary air flow, which likewise contributes to the mixing.
  • the mixing power achieved in this way from the three mixing pulses acting at an angle to one another is essentially load-independent.
  • the core air jet also forms a load-independent backfire shield to protect against cup fire.
  • a large number of small bores are provided in it, from which a small part of the core air can escape. These holes can be arranged at an angle in the edge area in order to compensate for the falling air pressure in the area of the exit from the annular gap.
  • gap nozzles can emanate from the central channel, in particular in the area of the annular gap, which open into the fuel channel, possibly into the middle of its S-shaped course. As a result, the fuel dust flow is evened out before entering the ring nozzle.
  • preheating should be provided.
  • This can consist, for example, of an electrical heat exchanger, the electrical connection power of which does not exceed a value of 2% of the burner output even with low-volatile coal as fuel.
  • This corresponds to the relatively small proportion of core air here, which expediently represents 10% to 15% of the total amount of combustion air.
  • Additional ignition stabilization can also be achieved by mixing the core air with steam. This steam accelerates the fuel gasification in such a way that lower temperatures are sufficient for preheating, so the heating power required for this can be reduced.
  • vibration generators can be provided in the central channel and / or in the jacket channel, which set the core air and / or the secondary air into gas dynamic vibrations before they exit.
  • These vibration generators can be designed as annular spaces surrounding the respective channel, which are connected to the respective channel via a coordinated annular gap.
  • Other embodiments for impressing a gas dynamic vibration are also possible.
  • guide vanes can also be arranged to impart a swirl.
  • a swirl contributes to the intensification of the external and internal hot gas recirculation and thereby increases the supply of ignition energy. This in turn reduces the need for preheating the core air.
  • the invention provides that an intermediate channel is provided between the fuel channel and the jacket channel. This can be supplied with cooling air during normal burner operation and with ignition gas during start-up, with a throughput that is adequate for the burner heat output for the fuel used.
  • the coal dust burner 1 shown in FIG. 1 is inserted as a whole into a conically expanding burner sleeve 2. It has an outer jacket 3, in which a jacket tube 4 is arranged at a distance from this.
  • a central tube 10 surrounding a central channel 9 and a fuel tube 11, which surrounds the central tube 10 to form an annular fuel channel 12, are arranged coaxially with the outer jacket 3 and the jacket tube 4. If necessary, heated core air 13 is conveyed via the central duct 9 and a coal dust / air mixture 14 is conveyed via the fuel duct 12.
  • the central tube 10 ends at a distance from a shielding plate 15, which on the one hand serves as protection against the heat caused by the flame and the recirculation and on the other hand redirects the core air jet 13 radially outward.
  • the core air 13 then emerges laterally from an annular gap 16.
  • the shielding plate 15 has a multiplicity of small bores 17, from which a small part of the core air 13 can flow out. In this way, the slag particles arriving there during the recirculation are cooled down to such an extent that they cannot get stuck on the shielding plate 15.
  • the fuel pipe 11 is surrounded by a drive shaft 18, which - which is not shown here - is rotatably supported and driven by an electric motor.
  • a cup 19 is fastened, which is cylindrical in the lower area and widens conically in the upper area.
  • the drive shaft 18 continues through the attachment of the cup 19 upwards.
  • a conical body 21 is arranged around this collar 20, the conical surface 22 of which, together with the conically widening region of the cup 19, forms an annular nozzle 23.
  • the fuel channel 12 receives a deflection which is S-shaped in cross section through the collar 20 or cone body 21 and the extension of the fuel tube 11 or the drive shaft 18. Coal dust settles in the pockets 24, 25 of the deflection, so that the deflection is evened out and the pockets 24, 25 are protected against erosion.
  • a slot-shaped passage 26 is kept open for a small part of the core air 13. This part of the core air 13 contributes to the coal dust being able to emerge from the ring nozzle 23 in a uniform density.
  • coal dust When operating the coal dust burner 1, coal dust is introduced into the combustion chamber via the fuel channel 12, its S-shaped deflection and the ring nozzle 23. Since this coal dust burner 1 is intended in particular for low heating outputs, the outflow speed must be relatively low, for example 3 to 8 m / s, since otherwise the flame would detach from the burner and be carried away.
  • the emerging coal dust is immediately detected by the core air 13 emerging from the annular gap 16 at speeds between 20 to 100 m / s and pressed into the region of the secondary air 7, 8 which flows out via the jacket channels 5, 6.
  • a swirl supporting the inner and outer hot gas recirculation is impressed on the secondary air portion 8 emerging from the jacket channel 6 via guide vanes 27, 28, the burner sleeve 2 stabilizing the flame.
  • the core air 13 is heated in such a way that it initiates the initial ignition, together with the radiant heat from the flame and the hot gas recirculation.
  • the heating can be done by electric heating up to 350 ° C.
  • the core air 13 is additionally heated on the shielding plate 15.
  • the rotating cup 19 reliably prevents blockages in the S-shaped deflection and the ring nozzle 23 due to the shear forces in the circumferential direction. Furthermore, it ensures sufficient heat transfer into the coal dust to prevent reignition despite the low exit speed of the coal dust.
  • FIG. 2 shows another embodiment of a coal dust burner 29. In the illustration shown, it is also inserted into a burner muffle 30, the conical design of which serves to stabilize the flame.
  • only one jacket channel 31 is provided, which is formed by an outer jacket 32 and by a jacket tube 33.
  • guide vanes 34, 35 are provided at the outlet of the jacket channel 31 in order to impart a swirl to the secondary air 36 flowing out there in order to support the recirculation.
  • a central tube 38 surrounding a central channel 37 and a fuel tube 39, which surrounds the central tube 38 to form an annular fuel channel 40, are arranged coaxially with the outer jacket 32 and jacket tube 33.
  • the core air 41 enters the central duct 37 and a carbon-air mixture 42 enters the combustion chamber via the fuel duct 40.
  • the central tube 38 ends - as in the exemplary embodiment according to FIG. 1 - at a distance from a shielding plate 43.
  • the core air 41 becomes is diverted radially outward through this shielding plate 43 and then emerges laterally from an annular gap 44.
  • the shielding plate 43 also has a large number of small bores 45 from which a small part of the core air 41 can flow out for the purpose of avoiding slag deposits.
  • the fuel pipe 39 is surrounded by a drive shaft 46, which here is rotatably supported and driven by an electric motor.
  • the upper end of the drive shaft 46 is formed into a cup 47 which widens conically towards the outside and has an annular web 48 on the inside, as a result of which an annular groove 49 is formed.
  • a collar 50 formed onto the central tube 38 and bent downward in a U-shape, projects into the annular groove 49.
  • a hollow conical body 51 is arranged around this collar 50, the conical surface 52 of which, together with the cup 47, form an annular nozzle 53.
  • the fuel channel 40 receives a deflection which is S-shaped in cross section through the collar 50 and the annular groove 49.
  • a slot-shaped passage 54 is kept free for a small part of the core air 41. It has the same task as the passage 26 in the embodiment according to FIG. 1.
  • the hollow interior 55 of the cone body 51 is connected to the annular gap 44 via slot nozzles 56.
  • the same goal is served by a vibration generator for the secondary air 36, which consists of an annular channel 57 placed around the outer jacket 32, which is connected to the jacket channel 31 by a circumferential slot nozzle 58. In this way, the secondary air 36 is set in low-frequency vibrations.
  • An intermediate tube 59 is arranged between the drive shaft 46 and the jacket tube 33, which includes a cooling channel 60 with the jacket tube 33. Cooling air 61 can be passed through it in order to cool the bearings of the drive shaft 46, which are not shown here. In the starting phase, instead of the cooling air 61, pilot gas is passed through, which emerges via the ring opening 62 and is ignited there.

Description

Die Erfindung betrifft einen Brenner für die Verbrennung staubförmiger Brennstoffe mit einem Zentralkanal für die Zuführung eines Kernluftstrahls mit im wesentlichen ringförmigem Primärluftaustritt, mit einem Mantelkanal für die Zuführung von Sekundärluft mit einem den Primärluftaustritt umgebenden, ringförmigen Sekundärluftaustritt sowie mit einem Brennstoffkanal für die Zuführung des Brennstoffs mit einem zwischen Primär- und Sekundärluftaustritt angeordneten, ringförmigen Brennstoffaustritt, wobei zumindest eine der beiden Umfangswandungen des Brennstoffaustritts drehbar und angetrieben ist, und wobei des weiteren der Kernluftstrahl zumindest teilweise nach außen gegen den Brennstoff gerichtet und der Brennstoff mit Sekundärluft beaufschlagt ist.The invention relates to a burner for the combustion of dusty fuels with a central channel for the supply of a core air jet with an essentially annular primary air outlet, with a jacket channel for the supply of secondary air with an annular secondary air outlet surrounding the primary air outlet and with a fuel channel for the supply of the fuel an annular fuel outlet arranged between the primary and secondary air outlet, at least one of the two circumferential walls of the fuel outlet being rotatable and driven, and furthermore the core air jet being directed at least partially outward against the fuel and the fuel being acted on by secondary air.

Die GB-A-528 018 zeigt einen Brenner, der vor allem für die Verbrennung von ölbrennstoffen gedacht ist. Er wird jedoch auch für die Verwendung anderer Brennstoffe, beispielsweise staubförmiger Brennstoffe, als geeignet angesehen.GB-A-528 018 shows a burner which is primarily intended for the combustion of oil fuels. However, it is also considered suitable for the use of other fuels, for example dust-like fuels.

Der Brenner hat einen Zentralkanal für die Zuführung von Kernluft mit einem ringförmigen Primärluftaustritt, der leicht nach außen gerichtet ist. Der Zentralkanal wird von einem Brennstoffkanal umgeben, über den der jeweilige Brennstoff zugeführt wird. Der Brennstoffaustritt ist ebenfalls ringförmig, wobei die Innenwandung des Brennstoffaustritts gleichzeitig die Außenwandung des Zentralkanals bildet. Die Außenwandung des Brennstoffaustritts ist kelchförmig ausgebildet und ragt über den Primärluftaustritt vor. Primärluftaustritt und Brennstoffaustritt sind praktisch parallel ausgerichtet.The burner has a central duct for the supply of core air with an annular primary air outlet which is directed slightly outwards. The central channel is surrounded by a fuel channel through which the respective fuel is supplied. The fuel outlet is also ring-shaped, the inner wall of the fuel outlet simultaneously forming the outer wall of the central channel. The outer wall of the fuel outlet is cup-shaped and protrudes beyond the primary air outlet. The primary air outlet and fuel outlet are practically parallel.

Brennstoffkanal und Brennstoffaustritt sind von einem Mantelkanal für die Zuführung von Sekundärluft umgeben. Im Bereich von Brennstoffaustritt und Primärluftaustritt ist der Mantelkanal in zwei Ringkanäle aufgeteilt, wobei der innere Ringkanal innenseitig von der drehbaren Außenwandung des Brennstoffkanals und Außenseitig von einer sich kegelförmig erweiternden Ringwandung gebildet wird. Diese wiederum bildet die Innenwandung des äußeren Ringkanals, wobei der Austritt für den äußeren Ringkanal weit vor dem Primärluftaustritt bzw. Brennstoffaustritt mündet. Der innere Ringkanal ist so eng bemessen, daß der weitaus größte Teil der Sekundärluft über den äußeren Ringkanal austritt.The fuel channel and fuel outlet are surrounded by a jacket channel for the supply of secondary air. In the area of fuel outlet and primary air outlet, the jacket channel is divided into two ring channels, the inner ring channel being formed on the inside by the rotatable outer wall of the fuel channel and on the outside by a conically widening ring wall. This in turn forms the inner wall of the outer ring channel, the outlet for the outer ring channel opening far before the primary air outlet or fuel outlet. The inner ring channel is so narrow that the vast majority of the secondary air escapes through the outer ring channel.

In der Außen- und Innenwandung des Brennstoffkanals vor dem Brennstoffaustritt befinden sich Öffnungen, die die Verbindung einerseits zum Zentralkanal und andererseits zum inneren Ringkanal des Mantelkanals herstellen. Durch diese Öffnungen gelangt Primärluft und Sekundärluft in den Brennstoff schon vor dessen Austritt.There are openings in the outer and inner walls of the fuel channel in front of the fuel outlet, which make the connection on the one hand to the central channel and on the other hand to the inner ring channel of the jacket channel. Through these openings, primary air and secondary air get into the fuel before it leaves the fuel.

Aufgrund der konstruktiven Ausbildung dieses Brenners kommt der austretende Brennstoff - abgesehen von dem über die vorgenannten Öffnungen eingetretenen Luftanteilen - zunächst nur mit dem Kernluftstrahl, also der Primärluft, in Berührung. Dies reicht bei flüssigen Brennstoffen aus, um die niedrig siedenden Bestandteile zu verbrennen. Die dabei entstehende Wärme zündet dann auch die hochsiedenden Bestandteile. Es ist dann nicht von Bedeutung, daß die für diese Verbrennung benötigte Sekundärluft erst ein gutes Stück hinter dem Austritt der Primärluft auf das Öl trifft. Dabei verhindert die Außenwandung des Brennstoffkanals, daß das Öl in den Anteil der Sekundärluft hineingedrückt werden kann, denn diese Außenwandung ist ein gutes Stück über den Primärluftaustritt hinausgezogen. Primärluft, Öl und Sekundärluft teffen also nur tangential aufeinander. Der weitaus größere Teil der Sekundärluft kommt mit dem Brennstoffgemisch erst wesentlich später in Berührung, wobei auch hier die Berührung lediglich tangential erfolgt.Due to the design of this burner, the escaping fuel - apart from the air that has entered through the aforementioned openings - initially only comes into contact with the core air jet, i.e. the primary air. With liquid fuels, this is sufficient to burn the low-boiling components. The heat generated ignites the high-boiling components. It is then not important that the secondary air required for this combustion hits the oil only a good distance behind the outlet of the primary air. The outer wall of the fuel channel prevents the oil from being forced into the portion of the secondary air, because this outer wall is pulled a good way beyond the primary air outlet. Primary air, oil and secondary air meet only tangentially. The much larger part of the secondary air comes into contact with the fuel mixture much later, although here, too, the contact is only tangential.

Bei dieser konstruktiven Gestaltung des Brenners dürfte eine Verwendung von Kohlenstaub als Brennstoff nicht zu befriedigenden Ergebnissen führen. Es kann nämlich kaum eine stabile Flamme entstehen, da die Primärluft, mit der der Kohlenstaub zunächst in Berührung käme, gerade zur Verbrennung der flüchtigen Bestandteile im Kohlenstoff ausreichen würde. Die ausgegasten Kohlepartikel würden dann erst am Ende des Brenners auf die dann noch kalte Sekundärluft treffen und können sich dann nicht mehr entzünden. Die Flamme würde wieder erlöschen.With this structural design of the burner, the use of coal dust as fuel should not lead to satisfactory results. A stable flame can hardly be created because the primary air with which the coal dust would initially come into contact would be sufficient to burn the volatile components in the carbon. The outgassed coal particles would then only hit the then still cold secondary air at the end of the burner and can then no longer ignite. The flame would go out again.

Der Erfindung liegt deshalb die Aufgabe zugrunde, einen Brenner der eingangs genannten Art so zu gestalten, daß er auch für kleine Leistungsbereiche geeignet ist, einen großen Regelbereich hat und unempfindlich gegenüber einem breiten Kohlenstaubband ist.The invention is therefore based on the object of designing a burner of the type mentioned in such a way that it is also suitable for small power ranges, has a large control range and is insensitive to a wide coal dust band.

Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß der Kernluftstrahl am Primärluftaustritt im wesentlichen radial zur Mündung des Brennstoffaustritts und auf den Sekundärluftaustritt gerichtet ist.According to the invention, this object is achieved in that the core air jet at the primary air outlet is directed essentially radially to the mouth of the fuel outlet and onto the secondary air outlet.

Auf Grund dieser Ausbildung des Brenners wird der Brennstoff nach dessen Austritt sofort durch den Kernluftstrahl nach außen abgelenkt und gelangt so auf kürzestem Weg in den Bereich des Sekundärluftaustritts. Dabei entsteht eine intensive Vermischung des Brennstoffs mit der Primärluft und anschließend mit der Sekundärluft. Diese stellt dabei genügend Sauerstoff zur Verfügung, um die Verbrennung der ausgegasten Kohlepartikel zu unterhalten. Dabei ist der Weg so kurz, daß die einmal in Gang gesetzte Flamme nicht erlischt. Dabei hat sich gezeigt, daß der Brenner auch für kleine Leistungsbereiche deutlich unter 5 Gcal/h, vor allem für den Leistungsbereich von 0,3 bis 3,5 Gcal/h geeignet ist und dabei einen großen Regelbereich hat. Damit wird mit diesem Brenner ein neuer Leistungsbereich für staubförmige Brennstoffe erschlossen.Due to this design of the burner, the fuel is immediately deflected outwards by the core air jet after it has emerged and thus reaches the area of the secondary air outlet in the shortest possible way. This creates an intensive mixing of the fuel with the primary air and then with the secondary air. This provides enough oxygen to maintain the combustion of the outgassed coal particles. The path is so short that the flame, once started, does not go out. It has been shown that the burner is also suitable for small output ranges well below 5 Gcal / h, especially for the output range of 0.3 to 3.5 Gcal / h and has a large control range. So that with this burner opened up a new performance range for dusty fuels.

Da im Gegensatz zu Großbrennern das Flammvolumen bei Brennern, die in dem vorgenannten Leistungsbereich arbeiten, entsprechend gering ist, muß der Kohlenstaub mit geringer Geschwindigkeit, die zweckmäßigerweise zwischen 3 bis 8 m/s liegt, austreten. Insbesondere bei Teillast entspricht dies der Flammen-Rückzündgeschwindigkeit. Eine Rückzündung wird jedoch durch den rotierenden Teil der Ringdüse vermieden, da hierdurch ein derart hoher Wärmeübergang zum Kohlenstaub bewirkt wird, daß dieser wie ein Flammenfilter wirkt. Dabei haben sich Umfangsgeschwindigkeiten von 12 bis 30 m/s für den rotierenden Teil bzw. die rotierenden Teile als hinreichend und zweckmäßig erwiesen.Since, in contrast to large burners, the flame volume in burners working in the aforementioned performance range is correspondingly low, the coal dust must escape at a low speed, which is expediently between 3 and 8 m / s. At partial load in particular, this corresponds to the flame reignition rate. A reignition is avoided by the rotating part of the ring nozzle, since this causes such a high heat transfer to the coal dust that it acts like a flame filter. Circumferential speeds of 12 to 30 m / s have proven to be sufficient and expedient for the rotating part or parts.

Ein weiterer Vorteil des erfindungsgemäßen Brenners liegt in der Vergrößerung des Regelbereiches, der nunmehr bei ca. 25 % bis 100 % liegt. Auch hier ist der Brenner wesentlich unempfindlicher gegenüber einem breiten Brennstoffstaubband so daß auch Mischbettstaub verwendet werden kann. Dabei wird der Fein- und Feinststaubanteil mit der Trägerluft aus der Ringdüse ausgetragen, während die größeren Körner durch die rotierende Bewegung des betreffenden Teiles der Ringdüse zum Austritt gleiten.Another advantage of the burner according to the invention is the enlargement of the control range, which is now approximately 25% to 100%. Again, the burner is much less sensitive to a wide range of fuel dust so that mixed bed dust can also be used. The fine and ultra-fine dust content is carried out of the ring nozzle with the carrier air, while the larger particles slide to the outlet due to the rotating movement of the part of the ring nozzle in question.

Das Gleiten der Staubkörner zum Brennstoffaustritt wird durch die konisch sich erweiternde Gestaltung des Durchmessers der Ringdüse begünstigt. Diese konische Erweiterung sollte dabei gleich, vorzugsweise kleiner als der Schüttwinkel des betreffenden Brennstoffes sein, um Erosionen und Agglomerationen zu vermeiden.The sliding of the dust grains towards the fuel outlet is promoted by the conically widening design of the diameter of the ring nozzle. This conical widening should be the same, preferably smaller than the angle of repose of the fuel in question, in order to avoid erosions and agglomerations.

Der Brennstoffkanal sollte im Bereich der Ringdüse einen im Querschnitt S-förmigen Verlauf haben. Dabei sollte sich der Gesamtquerschnitt im Bereich des S-förmigen Verlaufs zunächst erweitern und zur Ringdüse hin wieder verengen. Diese Maßnahme bewirkt eine Vergieichmäßigung des Brennstoffstrorqes über den Umfang.The fuel channel should have an S-shaped cross section in the area of the ring nozzle. The overall cross-section should initially widen in the area of the S-shaped course and narrow again towards the ring nozzle. This measure brings about a comparison of the fuel flow over the circumference.

Nach einem weiteren Merkmal der Erfindung ist vorgesehen, daß der Zentralkanal gegen eine Abschirmplatte zur Bildung eines vor den Austritt der Ringdüse mündenden Ringspalts ausläuft. Da diese Abschirmplatte aufgrund der im Feuerraum herrschenden Temperaturen sehr heiß ist, kann sich an ihr die Kernluft erwärmen, was die Initialzündung des Brennstoffes begünstigt. Außerdem wird hierdurch auf einfache Weise eine Umlenkung in radialer Richtung zum Austritt des Brennstoffes an der Ringdüse verwirklicht. Zweckmäßigerweise sollte dabei die Kernluft mit ca. 20 bis 100 m/s aus dem Ringspalt austreten, um eine intensive Vermischung mit dem austretenden Brennstoff und eine Ablenkung in den Sekundärluftstrom zu erreichen, der ebenfalls zu der Vermischung beiträgt. Die hierdurch erzielte Mischleistung aus den drei winklig zueinander wirkenden Mischimpulsen ist im wesentlichen lastunabhängig. Zusätzlich bildet der Kernluftstrahl einen ebenfalls lastunabhängigen Rückzündschirm zur Sicherung gegen Becherbrand.According to a further feature of the invention it is provided that the central channel runs out against a shielding plate to form an annular gap which opens before the exit of the ring nozzle. Since this shielding plate is very hot due to the temperatures prevailing in the combustion chamber, the core air can heat up there, which favors the initial ignition of the fuel. In addition, a deflection in the radial direction to the exit of the fuel at the ring nozzle is thereby easily achieved. The core air should expediently emerge from the annular gap at approximately 20 to 100 m / s in order to achieve intensive mixing with the escaping fuel and a deflection into the secondary air flow, which likewise contributes to the mixing. The mixing power achieved in this way from the three mixing pulses acting at an angle to one another is essentially load-independent. The core air jet also forms a load-independent backfire shield to protect against cup fire.

Um eine Verschlackung der Abschirmplatte zu vermeiden, sind in ihr eine Vielzahl von kleinen Bohrungen vorgesehen, aus denen ein geringfügiger Teil der Kernluft austreten kann. Im Randbereich können diese Bohrungen winklig angeordnet werden, um den abfallenden Luftdruck im Bereich des Austritts aus dem Ringspalt zu kompensieren.In order to avoid slagging of the shielding plate, a large number of small bores are provided in it, from which a small part of the core air can escape. These holes can be arranged at an angle in the edge area in order to compensate for the falling air pressure in the area of the exit from the annular gap.

Zusätzlich können vom Zentralkanal, insbesondere im Bereich des Ringspalts, Spaltdüsen ausgehen, die in den Brennstoffkanal, gegebenfalls in die Mitte dessen S-förmigen Verlaufs, münden. Hierdurch wird der Brennstoffstaubstrom vor dem Eintritt in die Ringdüse vergleichmäßigt.In addition, gap nozzles can emanate from the central channel, in particular in the area of the annular gap, which open into the fuel channel, possibly into the middle of its S-shaped course. As a result, the fuel dust flow is evened out before entering the ring nozzle.

Sofern die Temperatur des Kernluftstrahles für die Initialzündung des Brennstoffs nicht ausreicht, sollte eine entsprechende Vorwärmung vorgesehen werden. Diese kann beispielsweise aus einem elektrischen Wärmetauscher bestehen, dessen elektrische Anschlußleistung auch bei niederflüchtiger Kohle als Brennstoff einen Wert von 2 % der Brennerleistung nicht überschreitet. Dies korrespondiert mit dem hier relativ geringen Anteil der Kernluft, die zweckmäßigerweise 10 % bis 15 % der Gesamtverbrennungsluftmenge stellt. Eine zusätzliche Zündstabilisierung kann noch dadurch erreicht werden, daß die Kernluft mit Dampf vermischt wird. Diese Dampf beschleunigt die Brennstoffvergasung derart, daß für die Vorwärmung geringere Temperaturen ausreichen, die hierfür benötigte Heizleistung also verringert werden kann.If the temperature of the core air jet is not sufficient for the initial ignition of the fuel, appropriate preheating should be provided. This can consist, for example, of an electrical heat exchanger, the electrical connection power of which does not exceed a value of 2% of the burner output even with low-volatile coal as fuel. This corresponds to the relatively small proportion of core air here, which expediently represents 10% to 15% of the total amount of combustion air. Additional ignition stabilization can also be achieved by mixing the core air with steam. This steam accelerates the fuel gasification in such a way that lower temperatures are sufficient for preheating, so the heating power required for this can be reduced.

Zu einer Verbesserung der Zündstabilität des Brennstoffstaub-Luftgemisches können im Zentralkanal und/oder im Mantelkanal Schwingungsgeneratoren vorgesehen werden, die die Kernluft und/oder die Sekundärluft vor ihrem Austritt in gasdynamische Schwingungen versetzen. Diese Schwingungsgeneratoren können als den jeweiligen Kanal umgebende Ringräume ausgebildet werden, die mit dem jeweiligen Kanal über einen abgestimmten Ringspalt in Verbindung stehen. Auch andere Ausführungsformen zur Aufprägung einer gasdynamischen Schwingung sind möglich.In order to improve the ignition stability of the fuel-air mixture, vibration generators can be provided in the central channel and / or in the jacket channel, which set the core air and / or the secondary air into gas dynamic vibrations before they exit. These vibration generators can be designed as annular spaces surrounding the respective channel, which are connected to the respective channel via a coordinated annular gap. Other embodiments for impressing a gas dynamic vibration are also possible.

Am Austritt des Mantelkanals können zusätzlich Leitschaufeln zur Aufprägung eines Dralls angeordnet werden. Ein solcher Drall trägt zur Intensivierung der äußeren und inneren Heißgasrezirkulation bei und erhöht hierdurch die Zuführung von Zündenergie. Dies verringert wiederum den Bedarf an Vorwärmung für die Kernluft.At the outlet of the jacket channel, guide vanes can also be arranged to impart a swirl. Such a swirl contributes to the intensification of the external and internal hot gas recirculation and thereby increases the supply of ignition energy. This in turn reduces the need for preheating the core air.

Um die Wärmeeinwirkung der insbesondere bei Verwendung von Brennstoff mit geringen Anteilen an flüchtigen Bestandteilen relativ hoch vorgewärmten Kernluft zu verringern, ist gemäß der Erfindung vorgesehen, daß zwischen Brennstoffkanal und Mantelkanal ein Zwischenkanal vorgesehen ist. Dieser kann während des normalen Brennerbetriebes mit Kühlluft und im Anfahrbetrieb mit Zündgas beaufschlagt werden, und zwar mit einer Durchsatzleistung, welche der Brennerwärmeleistung für den jeweils verwendeten Brennstoff adäquat ist.In order to reduce the heat effect of the core air, which is preheated to a relatively high degree, particularly when using fuel with small amounts of volatile constituents, the invention provides that an intermediate channel is provided between the fuel channel and the jacket channel. This can be supplied with cooling air during normal burner operation and with ignition gas during start-up, with a throughput that is adequate for the burner heat output for the fuel used.

In der Zeichnung ist die Erfindung an Hand von zwei Ausführungsbeispielen näher veranschaulicht. Es zeigen :

  • Figur 1 einen Längsschnitt durch den oberen Teil eines Kohlenstaubbrenners in schematischer Darstellung und
  • Figur 2 einen Längsschnitt durch den oberen Teil einer anderen Ausführungsform eines Kohlenstaubbrenners in schematischer Darstellung.
In the drawing, the invention is based on two embodiments illustrated. Show it :
  • 1 shows a longitudinal section through the upper part of a coal dust burner in a schematic representation and
  • Figure 2 shows a longitudinal section through the upper part of another embodiment of a coal dust burner in a schematic representation.

Der in Figur 1 gezeigte Kohlenstaubbrenner 1 ist als Ganzes in eine sich kegelförmig erweiternde Brennermuffe 2 eingesetzt. Er hat einen Außenmantel 3, in den im Abstand zu diesem ein Mantelrohr 4 angeordnet ist.The coal dust burner 1 shown in FIG. 1 is inserted as a whole into a conically expanding burner sleeve 2. It has an outer jacket 3, in which a jacket tube 4 is arranged at a distance from this.

Hierdurch werden zwei Mantelkanäle 5, 6 gebildet, über die Sekundärluft 7, 8 in den sich in dieser Darstellung nach oben anschließenden Feuerraum einströmen kann.As a result, two jacket channels 5, 6 are formed, via which secondary air 7, 8 can flow into the combustion chamber which adjoins this illustration at the top.

Koaxial zum Außenmantel 3 und zum Mantelrohr 4 ist ein einen Zentralkanal 9 umgebendes Zentralrohr 10 sowie ein Brennstoffrohr 11 angeordnet, welches das Zentralrohr 10 unter Bildung eines ringförmigen Brennstoffkanals 12 umgibt. Über den Zentralkanal 9 wird erforderlichenfalls erwärmte Kernluft 13 und über den Brennstoffkanal 12 ein Kohlenstaub-Luftgemisch 14 befördert.A central tube 10 surrounding a central channel 9 and a fuel tube 11, which surrounds the central tube 10 to form an annular fuel channel 12, are arranged coaxially with the outer jacket 3 and the jacket tube 4. If necessary, heated core air 13 is conveyed via the central duct 9 and a coal dust / air mixture 14 is conveyed via the fuel duct 12.

Das Zentralrohr 10 endet im Abstand zu einer Abschirmplatte 15, die einerseits als Schutz gegen die durch die Flamme und die Rezirkulation bewirkte Wärme dient und andererseits den Kernluftstrahl 13 radial nach außen umleitet. Aus einem Ringspalt 16 tritt dann die Kernluft 13 seitlich aus.The central tube 10 ends at a distance from a shielding plate 15, which on the one hand serves as protection against the heat caused by the flame and the recirculation and on the other hand redirects the core air jet 13 radially outward. The core air 13 then emerges laterally from an annular gap 16.

Die Abschirmplatte 15 hat eine Vielzahl von kleinen Bohrungen 17, aus denen ein geringer Teil der Kernluft 13 herausströmen kann. Auf diese Weise werden die bei der Rezirkulation dort ankommenden Schlacketeilchen soweit abgekühlt, daß sie sich nicht auf der Abschirmplatte 15 festsetzen können.The shielding plate 15 has a multiplicity of small bores 17, from which a small part of the core air 13 can flow out. In this way, the slag particles arriving there during the recirculation are cooled down to such an extent that they cannot get stuck on the shielding plate 15.

Das Brennstoffrohr 11 ist von einer Antriebswelle 18 umgeben, die - was hier nicht näher dargestellt ist - drehbar gelagert und von einem Elektromotor angetrieben ist. Im Bereich des oberen Endes der Antriebswelle 18 ist ein Becher 19 befestigt, der im unteren Bereich zylinderförmig ausgebildet ist und sich im oberen Bereich kegelförmig erweitert.The fuel pipe 11 is surrounded by a drive shaft 18, which - which is not shown here - is rotatably supported and driven by an electric motor. In the area of the upper end of the drive shaft 18 a cup 19 is fastened, which is cylindrical in the lower area and widens conically in the upper area.

Die Antriebswelle 18 setzt sich über die Befestigung des Bechers 19 nach oben hin noch fort. In den dadurch gebildeten Zwischenraum ragt von oben ein im Querschnitt U-förmiger, nach unten umgebogener Kragen 20 des Zentralrohres 10 hinein. Um diesen Kragen 20 herum ist ein Kegelkörper 21 angeordnet, dessen Kegelfläche 22 mit dem sich kegelförmig erweiternden Bereich des Bechers 19 eine Ringdüse 23 bildet. Gleichzeitig erhält der Brennstoffkanal 12 durch den Kragen 20 bzw. Kegelkörper 21 sowie den Fortsatz des Brennstoffrohrs 11 bzw. der Antriebswelle 18 eine im Querschnitt S-förmige Umlenkung. In den Taschen 24, 25 der Umlenkung setzt sich Kohlenstaub ab, so daß die Umlenkung vergleichmäßigt wird und die Taschen 24, 25 vor Erosion geschützt werden.The drive shaft 18 continues through the attachment of the cup 19 upwards. A collar 20 of central tube 10 with a U-shaped cross section and bent downward protrudes from above into the intermediate space formed thereby. A conical body 21 is arranged around this collar 20, the conical surface 22 of which, together with the conically widening region of the cup 19, forms an annular nozzle 23. At the same time, the fuel channel 12 receives a deflection which is S-shaped in cross section through the collar 20 or cone body 21 and the extension of the fuel tube 11 or the drive shaft 18. Coal dust settles in the pockets 24, 25 of the deflection, so that the deflection is evened out and the pockets 24, 25 are protected against erosion.

Zwischen Kegelkörper 21 und Kragen 20 ist ein schlitzförmiger Durchlaß 26 für einen geringen Teil der Kernluft 13 offengehalten. Dieser Teil der Kernluft 13 trägt dazu bei, daß der Kohlenstaub in gleichmässiger Dichte aus der Ringdüse 23 austreten kann.Between the conical body 21 and the collar 20, a slot-shaped passage 26 is kept open for a small part of the core air 13. This part of the core air 13 contributes to the coal dust being able to emerge from the ring nozzle 23 in a uniform density.

Beim Betrieb des Kohlenstaubbrenners 1 wird Kohlenstaub über den Brennstoffkanal 12, seine S-förmige Umlenkung und die Ringdüse 23 in den Feuerraum eingebracht. Da dieser Kohlenstaubbrenner 1 insbesondere für kleine Heizleistungen gedacht ist, muß die Ausströmgeschwindigkeit relativ gering sein, beispielsweise 3 bis 8 m/s, da sich ansonsten die Flamme von dem Brenner lösen und weggetragen würde. Der austretende Kohlenstaub wird sofort von dem aus dem Ringspalt 16 mit Geschwindigkeiten zwischen 20 bis 100 m/s austretenden Kernluft 13 erfaßt und in den Bereich der Sekundärluft 7, 8 gedrückt, die über die Mantelkanäle 5, 6 ausströmt. Dem aus dem Mantelkanal 6 austretenden Sekundärluftanteil 8 wird dabei über Leitschaufeln 27, 28 ein die innere und äußere Heißgasrezirkulation unterstützender Drall aufgeprägt, wobei die Brennermuffe 2 die Flamme stabilisiert.When operating the coal dust burner 1, coal dust is introduced into the combustion chamber via the fuel channel 12, its S-shaped deflection and the ring nozzle 23. Since this coal dust burner 1 is intended in particular for low heating outputs, the outflow speed must be relatively low, for example 3 to 8 m / s, since otherwise the flame would detach from the burner and be carried away. The emerging coal dust is immediately detected by the core air 13 emerging from the annular gap 16 at speeds between 20 to 100 m / s and pressed into the region of the secondary air 7, 8 which flows out via the jacket channels 5, 6. A swirl supporting the inner and outer hot gas recirculation is impressed on the secondary air portion 8 emerging from the jacket channel 6 via guide vanes 27, 28, the burner sleeve 2 stabilizing the flame.

Die Kernluft 13 ist je nach dem Anteil der flüchtigen Bestandteile des Kohlenstaubes derart erhitzt, das sie - zusammen mit der Strahlungswärme aus der Flamme und der Heißgasrezirkulation - die Initialzündung einleitet. Die Erhitzung kann durch eine elektrische Beheizung bis zu 350 °C erfolgen. Zusätzlich erhitzt wird die Kernluft 13 an der Abschirmplatte 15.Depending on the proportion of volatile constituents of the coal dust, the core air 13 is heated in such a way that it initiates the initial ignition, together with the radiant heat from the flame and the hot gas recirculation. The heating can be done by electric heating up to 350 ° C. The core air 13 is additionally heated on the shielding plate 15.

Der rotierende Becher 19 verhindert aufgrund der Scherkräfte in Umfangsrichtung zuverlässig Verstopfungen in der S-förmigen Umlenkung und der Ringdüse 23. Desweiteren sorgt er für einen hinreichenden Wärmeübergang in den Kohlenstaub, um eine Rückzündung trotz der niedrigen Austrittsgeschwindigkeit des Kohlenstaubs zu verhindern.The rotating cup 19 reliably prevents blockages in the S-shaped deflection and the ring nozzle 23 due to the shear forces in the circumferential direction. Furthermore, it ensures sufficient heat transfer into the coal dust to prevent reignition despite the low exit speed of the coal dust.

Figur 2 zeigt eine andere Ausführungsform eines Kohlenstaubbrenners 29. In der gezeigten Darstellung ist auch er in eine Brennermuffel 30 eingesetzt, deren kegelförmige Gestaltung der Stabilisierung der Flamme dient.FIG. 2 shows another embodiment of a coal dust burner 29. In the illustration shown, it is also inserted into a burner muffle 30, the conical design of which serves to stabilize the flame.

Bei dieser Ausführungsform ist nur ein Mantelkanal 31 vorgesehen, der von einem Außenmantel 32 und von einem Mantelrohr 33 gebildet wird. Am Austritt des Mantelkanals 31 sind Leitschaufeln 34, 35 vorgesehen, um der dort ausströmenden Sekundärluft 36 einen Drall zur Unterstützung der Rezirkulation aufzuprägen.In this embodiment, only one jacket channel 31 is provided, which is formed by an outer jacket 32 and by a jacket tube 33. At the outlet of the jacket channel 31, guide vanes 34, 35 are provided in order to impart a swirl to the secondary air 36 flowing out there in order to support the recirculation.

Koaxial zum Außenmantel 32 und Mantelrohr 33 ist ein einen Zentralkanal 37 umgebendes Zentralrohr 38 sowie ein Brennstoffrohr 39 angeordnet, welches das Zentralrohr 38 unter Bildung eines ringförmigen Brennstoffkanals 40 umgibt. Über den Zentralkanal 37 gelangt die Kernluft 41 und über den Brennstoffkanal 40 ein Kohlenstoff-Luftgemisch 42 in den Feuerraum.A central tube 38 surrounding a central channel 37 and a fuel tube 39, which surrounds the central tube 38 to form an annular fuel channel 40, are arranged coaxially with the outer jacket 32 and jacket tube 33. The core air 41 enters the central duct 37 and a carbon-air mixture 42 enters the combustion chamber via the fuel duct 40.

Das Zentralrohr 38 endet - wie bei dem Ausführungsbeispiel gemäß Figur 1 - im Abstand zu einer Abschirmplatte 43. Die Kernluft 41 wird durch diese Abschirmplatte 43 radial nach außen umgeleitet und tritt dann aus einem Ringspalt 44 seitlich aus.The central tube 38 ends - as in the exemplary embodiment according to FIG. 1 - at a distance from a shielding plate 43. The core air 41 becomes is diverted radially outward through this shielding plate 43 and then emerges laterally from an annular gap 44.

Die Abschirmplatte 43 hat auch hier eine Vielzahl von kleinen Bohrungen 45, aus denen ein geringer Teil der Kernluft 41 zum Zwecke der Vermeidung von Schlackenablagerungen ausströmen kann.The shielding plate 43 also has a large number of small bores 45 from which a small part of the core air 41 can flow out for the purpose of avoiding slag deposits.

Das Brennstoffrohr 39 ist von einer Antriebswelle 46 umgeben, die hier erbenfalls drehbar gelagert und von einem Elektromotor angetrieben ist. Das obere Ende der Antriebswelle 46 ist zu einem Becher 47 ausgeformt, der sich nach außen hin kegelförmig erweitert und innen einen Ringsteg 48 aufweist, wodurch eine Ringnut 49 gebildet wird.The fuel pipe 39 is surrounded by a drive shaft 46, which here is rotatably supported and driven by an electric motor. The upper end of the drive shaft 46 is formed into a cup 47 which widens conically towards the outside and has an annular web 48 on the inside, as a result of which an annular groove 49 is formed.

In die Ringnut 49 ragt von oben ein an das Zentralrohr 38 angeformter, U-förmig nach unten umgebogener Kragen 50 hinein. Um diesen Kragen 50 herum ist ein hohler Kegelkörper 51 angeordnet, dessen Kegelfläche 52 mit dem Becher 47 eine Ringdüse 53 bilden. Gleichzeitig erhält der Brennstoffkanal 40 durch den Kragen 50 und die Ringnut 49 eine im Querschnitt S-förmige Umlenkung.A collar 50, formed onto the central tube 38 and bent downward in a U-shape, projects into the annular groove 49. A hollow conical body 51 is arranged around this collar 50, the conical surface 52 of which, together with the cup 47, form an annular nozzle 53. At the same time, the fuel channel 40 receives a deflection which is S-shaped in cross section through the collar 50 and the annular groove 49.

Zwischen dem Kegelkörper 51 und dem Kragen 50 ist ein schlitzförmiger Durchlaß 54 für einen geringen Teil der Kernluft 41 freigehalten. Er hat dieselbe Aufgabe wie der Durchlaß 26 bei dem Ausführungsbeispiel gemäß Figur 1.Between the cone body 51 and the collar 50, a slot-shaped passage 54 is kept free for a small part of the core air 41. It has the same task as the passage 26 in the embodiment according to FIG. 1.

Der hohle Innenraum 55 des Kegelkörpers 51 steht über Schlitzdüsen 56 mit dem Ringspalt 44 in Verbindung. Nach dem Prinzip der Flöte entsteht hierdurch ein gasdynamischer Schwingungsgenerator, der die durch den Ringspalt 44 strömende Kernluft 41 in niederfrequente Schwingungen versetz. Hierdurch wird die Mischimpulswirkung auf den austretenden Kohlenstaub intensiviert und damit die Zündstabilität verbessert. Dem gleichen Ziel dient ein Schwingungsgenerator für die Sekundärluft 36, der aus einem um den Außenmantel 32 gelegten Ringkanal 57 besteht, der mit einer umlaufenden Schlitzdüse 58 mit dem Mantelkanal 31 in Verbindung steht. Auf diese Weise wird auch die Sekundärluft 36 in niederfrequente Schwingungen versetzt.The hollow interior 55 of the cone body 51 is connected to the annular gap 44 via slot nozzles 56. According to the principle of the flute, this creates a gas dynamic vibration generator which sets the core air 41 flowing through the annular gap 44 into low-frequency vibrations. This intensifies the effect of the mixed impulses on the emerging coal dust and thus improves the ignition stability. The same goal is served by a vibration generator for the secondary air 36, which consists of an annular channel 57 placed around the outer jacket 32, which is connected to the jacket channel 31 by a circumferential slot nozzle 58. In this way, the secondary air 36 is set in low-frequency vibrations.

Zwischen der Anstriebswelle 46 und dem Mantelrohr 33 ist ein Zwischenrohr 59 angeordnet, das mit dem Mantelrohr 33 einen Kühlkanal 60 einschließt. Durch ihn kann Kühlluft 61 geleitet werden, um die hier nicht gezeigten Lager der Antriebswelle 46 zu kühlen. In der Startphase wird statt der Kühlluft 61 Zündgas hindurchgeleitet, das über die Ringöffnung 62 austritt und dort entzündet wird.An intermediate tube 59 is arranged between the drive shaft 46 and the jacket tube 33, which includes a cooling channel 60 with the jacket tube 33. Cooling air 61 can be passed through it in order to cool the bearings of the drive shaft 46, which are not shown here. In the starting phase, instead of the cooling air 61, pilot gas is passed through, which emerges via the ring opening 62 and is ignited there.

Die Funktion des in Figur 2 dargestellten Kohlenstaubbrenners 29 ist - abgesehen von der Wirkung der Schwingungsgeneratoren und des Kühlkanals 60 - die gleiche wie bei dem Kohlenstaubbrenner 1 gemäß Figur 1.The function of the coal dust burner 29 shown in FIG. 2 - apart from the effect of the vibration generators and the cooling duct 60 - is the same as that of the coal dust burner 1 according to FIG. 1.

Claims (11)

1. Burner (1, 29) for the combustion of pulverised fuels, with a central duct (9, 37) for supplying a core air jet (13, 41), with a substantially annular primary air outlet, with an envelope duct (5, 6 ; 31 ) for supplying secondary air (7, 8, 36), with an annular secondary air outlet surrounding the primary air outlet, and with a fuel duct (12, 40) for supplying the fuel and with an annular fuel outlet (23, 53) arranged between the primary and secondary air outlets, at least one of the two peripheral walls (19, 47) of the fuel outlet (23, 53) being rotatable and driven, and the core air jet (13, 41) being also directed at least partly outwardly towards the fuel, and the fuel being acted upon by secondary air (7, 8, 36), characterised in that at the primary air outlet the core air jet (13, 41) is directed substantially radially to the mouth of the fuel outlet (23, 53) and to the secondary air outlet.
2. Burner according to claim 1, characterised in that the fuel issues at speeds between 3 to 8 m/s.
3. Burner according to claim 1 or 2, characterised in that the annular nozzle (23, 53) has a conically increasing diameter.
4. Burner according to one of claims 1 to 3, characterised in that the fuel duct (12, 40) in the region of the annular nozzle has an S shape in cross-section, and preferably the overall cross-section in the region of the S-shaped course first of all widens and reduces again towards the annular nozzle (23, 53).
5. Burner according to one of claims 1 to 4, characterised in that the end of the central duct faces towards a shield plate (15, 43) for forming an annular gap (16, 44) debouching in front of the outlet of the annular nozzle (23, 53).
6. Burner according to claim 5, characterised in that the shield plate (15, 43) comprises small holes (17, 45) for the outflow of a slight proportion of the core air (13, 41).
7. Burner according to one of claims 1 to 6, characterised in that from the central duct.(9, 37) slit nozzles (26, 54) extend into the fuel duct (12, 40), into the middle of the S-shaped region of said fuel duct if appropriate.
8. Burner according to one of claims 1 to 7, characterised in that the core air jet (13, 41) is suitably pre-heated to effect initial ignigion of the fuel, possibly by an electrical heat exchanger with a connected electrical power which even when using low-volatile coal as fuel does not exceed a value of 2 % of the burner power.
9. Burner according to one of claims 1 to 8, characterised in that the central duct (9, 37) and/or the envelope duct (5, 6 ; 31) is/are provided each with an oscillation generator, constructed preferably as an annular chamber (55, 57) which surrounds the respective duct (12, 40 ; 5, 6, 31) and which communicates with the respective duct (12, 40 ; 5, 6, 31) by way of a tuned annular gap (56, 58).
10. Burner according to one of claims 1 to 9, characterised in that an intermediate duct (60) for introducing cooling air (61) and/or heating gas is provided between the fuel duct (12, 40) and the envelope duct (5, 6 ; 31).
11. Burner according to one of claims 1 to 10, characterised in that guide vanes (27, 28 ; 34. 35) are arranged at the outlet of the envelope duct (5, 6, 31) for imparting a spinning motion.
EP81108054A 1981-02-06 1981-10-08 Burner for the combustion of dust-like fuels Expired EP0057747B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3104054 1981-02-06
DE19813104054 DE3104054A1 (en) 1981-02-06 1981-02-06 BURNER FOR THE COMBUSTION OF DUST-MADE FUELS

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EP0057747A2 EP0057747A2 (en) 1982-08-18
EP0057747A3 EP0057747A3 (en) 1982-11-10
EP0057747B1 true EP0057747B1 (en) 1985-10-09

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EP (1) EP0057747B1 (en)
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DE (2) DE3104054A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4550563A (en) * 1979-11-23 1985-11-05 Marchand William C Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution
EP0114062A3 (en) * 1983-01-18 1986-02-19 Stubinen Utveckling AB Method and device for the combustion of solid fuels, particularly coal, peat or the like
SE8306652D0 (en) * 1983-12-02 1983-12-02 Insako Kb METHOD AND APPARATUS FOR ACTIVATING LARGE
US4604052A (en) * 1985-04-29 1986-08-05 The United States Of America As Represented By The United States Department Of Energy Dual-water mixture fuel burner
DE3541616A1 (en) * 1985-11-25 1987-05-27 Krupp Polysius Ag Burner for pulverulent fuel
US4628832A (en) * 1986-01-29 1986-12-16 Coen Company, Inc. Dual fuel pilot burner for a furnace
US4690074A (en) * 1986-05-02 1987-09-01 Norton Charles L Coal combustion system
US5803372A (en) * 1997-04-03 1998-09-08 Asahi Sunac Corporation Hand held rotary atomizer spray gun
GB2325729A (en) * 1997-05-29 1998-12-02 Rolls Royce Power Eng A burner
DE102008036058B4 (en) * 2008-08-01 2013-04-18 Linde Ag Method and device for starting up combustible gasification reactors
US20120003595A1 (en) * 2009-09-29 2012-01-05 Honeywell International Inc. High turn down low nox burner

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1887015A (en) * 1928-04-13 1932-11-08 Buell Comb Company Ltd Means for the combustion of pulverized fuel
US1728011A (en) * 1928-06-15 1929-09-10 John N M Shimer Centrifugal fluid-fuel burner
DE672311C (en) * 1935-10-09 1939-02-27 Oskar Jebens Oil burner with rotating atomizer beaker
CH187974A (en) * 1936-02-06 1936-12-15 Surber Hans Method and device for burning oil.
GB528018A (en) * 1938-04-26 1940-10-21 Attilio Perretti Burner for oil and other fuel
US2457067A (en) * 1938-04-26 1948-12-21 Perretti Attilio Atomizing oil burner
US2341682A (en) * 1940-08-01 1944-02-15 Riley Stoker Corp Pulverized fuel burner
DE1145736B (en) * 1956-07-03 1963-03-21 Babcock & Wilcox France Device for improving the combustion of liquid or dusty fuels
DE1551936A1 (en) * 1967-07-12 1970-03-19 Maschf Augsburg Nuernberg Ag Burners for liquid or flowable fuels
CA1060332A (en) * 1976-05-29 1979-08-14 Dowa Co. Gasified liquid fuel burner
US4113416A (en) * 1977-02-24 1978-09-12 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Rotary burner
DE2729476C3 (en) * 1977-06-30 1981-05-27 Ruhrkohle Ag, 4300 Essen Coal dust burner with central coal dust-air supply
US4270698A (en) * 1977-11-30 1981-06-02 Karl Bisa Aerosol forming device
US4150631A (en) * 1977-12-27 1979-04-24 Combustion Engineering, Inc. Coal fired furance
US4206712A (en) * 1978-06-29 1980-06-10 Foster Wheeler Energy Corporation Fuel-staging coal burner
SE421952B (en) * 1978-07-31 1982-02-08 Scaniainventor Ab BURNER FOR A SUSPENSION OF FINE CORNING COAL IN VETERIN
JPS55134212A (en) 1979-04-05 1980-10-18 Babcock Hitachi Kk Burner

Also Published As

Publication number Publication date
JPS57150708A (en) 1982-09-17
EP0057747A3 (en) 1982-11-10
EP0057747A2 (en) 1982-08-18
US4457695A (en) 1984-07-03
DE3104054A1 (en) 1982-08-12
DE3172621D1 (en) 1985-11-14

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