EP1318351B1 - Solid fuel combustion device and method of supplying air to such a device - Google Patents
Solid fuel combustion device and method of supplying air to such a device Download PDFInfo
- Publication number
- EP1318351B1 EP1318351B1 EP20020026516 EP02026516A EP1318351B1 EP 1318351 B1 EP1318351 B1 EP 1318351B1 EP 20020026516 EP20020026516 EP 20020026516 EP 02026516 A EP02026516 A EP 02026516A EP 1318351 B1 EP1318351 B1 EP 1318351B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- air
- housing
- grate
- air amount
- total
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L1/00—Passages or apertures for delivering primary air for combustion
- F23L1/02—Passages or apertures for delivering primary air for combustion by discharging the air below the fire
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
- F23B1/00—Combustion apparatus using only lump fuel
- F23B1/16—Combustion apparatus using only lump fuel the combustion apparatus being modified according to the form of grate or other fuel support
- F23B1/24—Combustion apparatus using only lump fuel the combustion apparatus being modified according to the form of grate or other fuel support using rotating grate
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
- F23B5/00—Combustion apparatus with arrangements for burning uncombusted material from primary combustion
- F23B5/04—Combustion apparatus with arrangements for burning uncombusted material from primary combustion in separate combustion chamber; on separate grate
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
- F23G5/20—Incineration of waste; Incinerator constructions; Details, accessories or control therefor having rotating or oscillating drums
- F23G5/22—Incineration of waste; Incinerator constructions; Details, accessories or control therefor having rotating or oscillating drums the drums being conically shaped
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L9/00—Passages or apertures for delivering secondary air for completing combustion of fuel
- F23L9/02—Passages or apertures for delivering secondary air for completing combustion of fuel by discharging the air above the fire
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2202/00—Combustion
- F23G2202/10—Combustion in two or more stages
- F23G2202/103—Combustion in two or more stages in separate chambers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2203/00—Furnace arrangements
- F23G2203/20—Rotary drum furnace
- F23G2203/203—Rotary drum furnace with conically shaped drum
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2209/00—Specific waste
- F23G2209/26—Biowaste
- F23G2209/261—Woodwaste
Definitions
- the invention relates to a method for supplying air to a combustion plant according to the preamble of claim 1 and a solid fuel incineration plant according to the preamble of claim 7.
- the method and plant of the aforementioned type are made EP 0 952 398 A2 known.
- the firing cone consists of radial, hollow support arms facing inwards, i. have bores facing the fuel, and support rings carrying grate bars that form the grate surface.
- the firing cone is surrounded by a housing, and its mouth is opposite to a secondary combustion chamber in which the flame gases emerging from the firing cone are burned out.
- a second part of the combustion air is supplied to the afterburner chamber at the end remote from the firing cone via radial guide vanes, flows there helically along the wall in the direction of the firing cone and then centrally back again.
- usually 20 to 30% of the total amount of air required for combustion is supplied as primary air via the hollow support arms, while the rest, d. H. 80 to 70% of the total amount of air to be supplied as secondary air of the afterburner.
- the upper limit of the primary air quantity must not be exceeded, because otherwise slag forms on the grate bars of the firing cone, which can clog the firing cone with time.
- secondary air quantities of the order of 70 to 80% of the total amount of air necessary to avoid a lack of air at the given primary air quantities, on the support arms and support rings material temperatures of more than 900 ° C, resulting in high material stresses leads. Namely, between the end of the afterburner chamber and the outlet opening of the firing cone there is an annular gap for discharging ash into the housing surrounding the firing cone, and through this annular gap hot air from the afterburner chamber enters the housing, which leads to the overheating of the firing cone.
- the invention is therefore based on the object of specifying a method and an incinerator of the type mentioned above, with which a combustion according to the exhaust gas regulations can be achieved without overheating of the rotary grate.
- the described problem is solved according to the invention in that in the housing of the rotary grate an air inlet is arranged, is sucked by the prevailing in the housing during operation negative pressure, a third amount of air whose volume is suitably regulated by a valve disposed in the inlet flap in that the total amount of air supplied to the combustion corresponds to the quantity of air required for the combustion.
- the entry for the tertiary air into the housing of the rotary grate may be at any point, but particularly effective for the reduction of the material temperature is an arrangement of the inlet such that the tertiary air blows directly against the back of the rotary grate, d. H. the side facing away from the bearing surface for the fuel.
- the said flap in the inlet for the tertiary air is preferably an adjustable non-return valve, on the one hand, the volume flow can be influenced, but on the other hand closes automatically with a pressure increase in the housing and thereby prevents the blowing hot combustion gases into the environment.
- the material temperature of the combustion grate can be lowered even further, if one in the secondary air return gas (cold exhaust gas from the chimney) initiates.
- the drawing shows a total of 1 designated firing cone, which is surrounded by a housing 2.
- the housing 2 is expediently lined up inside, which can be seen in the drawing.
- the firing cone 1 has a frusto-conical and an adjoining cylindrical portion which narrows into a frusto-conical mouth. It is driven to rotate about an inclined axis O, wherein the drive means are not shown in the drawing for reasons of clarity.
- the inclination angle of the axis O is in the drawing indicated by ⁇ .
- At the mouth of the firing cone is axially followed by a conically narrowing afterburner chamber 3.
- the firing cone 1 consists of radial, hollow support arms 4 and extending in the circumferential direction support rings 6. These bear grate bars, which form the grate surface, but are not shown here.
- the hollow support arms 4 have inwardly, d. H. in the interior of the firing cone 1 facing openings 5 and are connected to a device, not shown here for supplying primary air L1 in their interior. Details of this can be found in the aforementioned publication.
- the afterburner 3 has at its end facing away from the fuel cone 1 means for supplying secondary air for afterburning, which is provided with vanes 7, which are directed so that the secondary air is a helical path near the peripheral wall 8 of the afterburner 3 in the direction of the Brennkegel 1 takes.
- the housing 2 is provided with a shaft-shaped inlet 9 for the supply of a third amount of air or tertiary air L3, in which there is a check valve 10, with the aid of the opening cross-section of the shaft 9 can be adjusted, recognizable in the drawing on an adjusting screw 11. Wie it can be seen, the mouth of the shaft 9 located inside the housing 2 is directed directly to the back of the firing cone 1, d. H. on the side facing away from the fuel in the firing cone (not shown).
Description
Die Erfindung bezieht sich auf ein Verfahren zum Zuführen von Luft zu einer Verbrennungsanlage nach dem Oberbegriff des Anspruchs 1 sowie eine Feststoffverbrennungsanlage nach dem Oberbegriff des Anspruchs 7. Verfahren und Anlage der vorgenannten Art sind aus
Bei der bekannten Anlage ist der Drehrost kegelstumpfartig ausgebildet, weshalb man ihn auch "Brennkegel" nennt, und rotiert um eine etwa 35° gegen die Horizontale geneigte Achse, so daß der im Brennkegel befindliche Brennstoff durch die Umlaufbewegung des Brennkegels umgewälzt wird. Der Brennkegel besteht aus radialen, hohlen Tragarmen, die nach innen, d.h. gegen den Brennstoff weisende Bohrungen haben, und Tragringen, die Roststäbe tragen, die die Rostfläche bilden. Der Brennkegel ist von einem Gehäuse umgeben, und seiner Mündung steht eine Nachbrennkammer gegenüber, in der die aus dem Brennkegel austretenden Flammgase ausgebrannt werden.In the known system of the rotary grate is frustoconical, which is why it is called "fuel cone", and rotated about an approximately 35 ° to the horizontal inclined axis, so that the fuel located in the fuel cone is circulated by the orbital motion of the firing cone. The firing cone consists of radial, hollow support arms facing inwards, i. have bores facing the fuel, and support rings carrying grate bars that form the grate surface. The firing cone is surrounded by a housing, and its mouth is opposite to a secondary combustion chamber in which the flame gases emerging from the firing cone are burned out.
Bei der bekannten Anlage wird gemäß dem bekannten Verfahren zum Zuführen von Verbrennungsluft ein erster Teil der Verbrennungsluft den hohlen Tragarmen zugeführt und durch die Bohrungen direkt in das Innere des Brennkegels unter den dort befindlichen Brennstoff geblasen. Ein zweiter Teil der Verbrennungsluft wird der Nachbrennkammer am dem Brennkegel fernen Ende über radiale Leitschaufeln zugeführt, strömt dort schraubenlinienförmig entlang der Wand in Richtung auf den Brennkegel und dann zentral wieder zurück. Dabei werden üblicherweise 20 bis 30% der für die Verbrennung notwendigen Gesamtluftmenge als Primärluft über die hohlen Tragarme zugeführt, während der Rest, d. h. 80 bis 70% der Gesamtluftmenge als Sekundärluft der Nachbrennkammer zugeführt werden.In the known system according to the known method for supplying combustion air, a first part of the combustion air supplied to the hollow support arms and blown through the holes directly into the interior of the firing cone under the fuel located there. A second part of the combustion air is supplied to the afterburner chamber at the end remote from the firing cone via radial guide vanes, flows there helically along the wall in the direction of the firing cone and then centrally back again. In this case, usually 20 to 30% of the total amount of air required for combustion is supplied as primary air via the hollow support arms, while the rest, d. H. 80 to 70% of the total amount of air to be supplied as secondary air of the afterburner.
Die obere Grenze der Primärluftmenge darf nicht überschritten werden, weil sich sonst Schlacke auf den Roststäben des Brennkegels bildet, die den Brennkegel mit der Zeit zusetzen kann. Andererseits ergeben sich bei Sekundärluftmengen in der Größenordnung von 70 bis 80% der Gesamtluftmenge, die notwendig sind, um bei den gegebenen Primärluftmengen einen Luftmangel zu vermeiden, an den Tragarmen und Tragringen Materialtemperaturen von mehr als 900°C, was zu hohen Materialbeanspruchungen führt. Zwischen dem Ende der Nachbrennkammer und der Austrittsöffnung der Brennkegels befindet sich nämlich ein Ringspalt für die Ausschleuderung von Asche in das den Brennkegel umgebende Gehäuse, und durch diesen Ringspalt tritt heiße Luft aus der Nachbrennkammer in das Gehäuse ein, die zu der Überhitzung des Brennkegels führt.The upper limit of the primary air quantity must not be exceeded, because otherwise slag forms on the grate bars of the firing cone, which can clog the firing cone with time. On the other hand, resulting in secondary air quantities of the order of 70 to 80% of the total amount of air necessary to avoid a lack of air at the given primary air quantities, on the support arms and support rings material temperatures of more than 900 ° C, resulting in high material stresses leads. Namely, between the end of the afterburner chamber and the outlet opening of the firing cone there is an annular gap for discharging ash into the housing surrounding the firing cone, and through this annular gap hot air from the afterburner chamber enters the housing, which leads to the overheating of the firing cone.
Verringert man die Sekundärluftmenge, nehmen zwar die genannten Materialtemperaturen von Tragarmen und Tragringen ab, jedoch wird die Verbrennung dadurch in den Luftmangel gebracht, was zu Abgasen führt, die den Vorschriften über die Reinhaltung von Luft nicht entsprechen.Reducing the secondary air quantity, while the mentioned material temperatures of support arms and support rings decrease, but the combustion is thereby brought to a lack of air, which leads to exhaust gases that do not comply with the regulations on the clean air.
Der Erfindung liegt daher die Aufgabe zugrunde, ein Verfahren und eine Verbrennungsanlage der Eingangs genannten Art anzugeben, mit denen eine den Abgasvorschriften entsprechende Verbrennung ohne Überhitzung des Drehrostes erreicht werden kann.The invention is therefore based on the object of specifying a method and an incinerator of the type mentioned above, with which a combustion according to the exhaust gas regulations can be achieved without overheating of the rotary grate.
Diese Aufgabe wird durch die in den Ansprüchen 1 und 7 enthaltenen Merkmale gelöst. Vorteilhafte Ausgestaltungen der Erfindung sind Gegenstand der jeweils abhängigen Ansprüche.This object is achieved by the features contained in
Das geschilderte Problem wird gemäß der Erfindung dadurch gelöst, daß im Gehäuse des Drehrostes ein Lufteintritt angeordnet ist, durch den in Folge des im Gehäuse im Betrieb herrschenden Unterdrucks eine dritte Luftmenge angesaugt wird, deren Volumen zweckmäßigerweise durch eine in dem Eintritt angeordneten Klappe so geregelt wird, daß die der Verbrennung zugeführte Gesamtluftmenge der für die Verbrennung erforderlichen Luftmenge entspricht.The described problem is solved according to the invention in that in the housing of the rotary grate an air inlet is arranged, is sucked by the prevailing in the housing during operation negative pressure, a third amount of air whose volume is suitably regulated by a valve disposed in the inlet flap in that the total amount of air supplied to the combustion corresponds to the quantity of air required for the combustion.
Günstige Werte ergeben sich für:
Untersuchungen haben ergeben, daß die Materialtemperatur bei einem Brennkegel als beispielhaftem Drehrost von über 900°C bei Zuführung nur von Primär- und Sekundärluft auf etwa 650 bis 700°C absank, wenn erfindungsgemäß die dritte Luftmenge (Tertiärluft) in das Brennkegelgehäuse zugeführt wurde. Diese Temperatur liegt auch hinreichend weit unter dem Ascheschmelzpunkt von Holz oder Biomasse, daß eine Schlackebildung vermieden ist.Investigations have shown that the material temperature dropped at a firing cone as an exemplary rotary grate of about 900 ° C with supply of primary and secondary air to about 650 to 700 ° C, according to the invention, the third air quantity (tertiary air) was fed into the Brennkegelgehäuse. This temperature is also sufficient far below the ash melting point of wood or biomass, slagging is avoided.
Der Eintritt für die Tertiärluft in das Gehäuse des Drehrostes kann an beliebiger Stelle liegen, besonders wirksam für die Verringerung der Materialtemperatur ist aber eine Anordnung des Eintritts derart, daß die Tertiärluft direkt gegen die Rückseite des Drehrostes bläst, d. h. jene Seite, die der Auflagefläche für den Brennstoff abgewandt ist.The entry for the tertiary air into the housing of the rotary grate may be at any point, but particularly effective for the reduction of the material temperature is an arrangement of the inlet such that the tertiary air blows directly against the back of the rotary grate, d. H. the side facing away from the bearing surface for the fuel.
Auch bei willkürlicher Anordnung des Eintritts für die Tertiärluft am Gehäuse bleiben auch bei kleinen O2-Gehalten im Abgas von nur 3 bis 4% die CO-Werte des Abgases deutlich unter 50 mg/m3, was bedeutet, daß die Tertiärluft vollständig an der Verbrennung teilnimmt. Dieses ist eine ganz erstaunliche Tatsache, die nicht erwartet wurde.Even with an arbitrary arrangement of the inlet for the tertiary air at the housing, the CO values of the exhaust gas remain well below 50 mg / m 3 even with small O 2 contents in the exhaust gas of only 3 to 4%, which means that the tertiary air completely at the Combustion takes part. This is a very amazing fact that was not expected.
Die genannte Klappe im Eintritt für die Tertiärluft ist vorzugsweise eine einstellbare Rückschlagklappe, mit der einerseits der Volumenstrom beeinflußt werden kann, die aber andererseits bei einem Druckanstieg im Gehäuse selbst tätig schließt und dadurch das Ausblasen heißer Brenngase in die Umgebung verhindert.The said flap in the inlet for the tertiary air is preferably an adjustable non-return valve, on the one hand, the volume flow can be influenced, but on the other hand closes automatically with a pressure increase in the housing and thereby prevents the blowing hot combustion gases into the environment.
Die Materialtemperatur des Brennrostes kann noch weiter gesenkt werden, wenn man in die Sekundärluft Rückgas (kaltes Abgas vom Kamin) einleitet. Günstig sind Rückgasmengen von 10 bis 30%, bevorzugt 15 bis 20% der Gesamtluftmenge. Weil das Rückgas ausgebranntes Gas ist und sauerstoffarm oder -frei ist, kann es zur Verbrennung nichts beitragen und wirkt daher für den Verbrennungsvorgang als Kühlgas, auch wenn es wärmer als die Umgebungsluft ist.The material temperature of the combustion grate can be lowered even further, if one in the secondary air return gas (cold exhaust gas from the chimney) initiates. Conveniently return gas quantities of 10 to 30%, preferably 15 to 20% of the total amount of air. Because the return gas is burned out gas and is oxygen lean or free, it can not contribute to the combustion and therefore acts as a cooling gas for the combustion process, even if it is warmer than the ambient air.
Die Erfindung wird nachfolgend unter Bezugnahmen auf ein in der Zeichnung dargestelltes Ausführungsbeispiel näher erläutert.The invention will be explained in more detail below with reference to an exemplary embodiment shown in the drawing.
Die Zeichnung zeigt einen insgesamt mit 1 bezeichneten Brennkegel, der von einem Gehäuse 2 umgeben ist. Das Gehäuse 2 ist im Innern zweckmäßigerweise ausgemauert, was in der Zeichnung zu erkennen ist. Der Brennkegel 1 weist einen kegelstumpfförmigen und einen sich daran anschließenden zylindrischen Abschnitt auf, der sich in eine kegelstumpfförmige Mündung verengt. Er ist um eine schrägstehende Achse O rotierend angetrieben, wobei die Antriebseinrichtungen in der Zeichnung aus Übersichtlichkeitsgründen nicht dargestellt sind. Der Neigungswinkel der Achse O ist in der Zeichnung mit α angegeben. An die Mündung des Brennkegels schließt sich axial eine sich konisch verengende Nachbrennkammer 3 an.The drawing shows a total of 1 designated firing cone, which is surrounded by a
Der Brennkegel 1 besteht aus radialen, hohlen Tragarmen 4 und im Umfangsrichtung verlaufenden Tragringen 6. Diese tragen Roststäbe, die die Rostfläche bilden, hier aber nicht dargestellt sind. Die hohlen Tragarme 4 haben nach innen, d. h. in den Innenraum des Brennkegels 1 weisende Öffnungen 5 und sind an eine hier nicht dargestellte Einrichtung zum Zuführen von Primärluft L1 in ihren Innenraum verbunden. Einzelheiten hierüber finden sich in der Eingangs erwähnten Druckschrift.The firing cone 1 consists of radial,
Die Nachbrennkammer 3 hat an ihrem dem Brennkegel 1 abgewandten Ende eine Einrichtung zum Zuführen von Sekundärluft für die Nachverbrennung, die mit Leitschaufeln 7 versehen ist, die so gerichtet sind, daß die Sekundärluft einen schraubenlinienförmigen Weg nahe der Umfangswand 8 der Nachbrennkammer 3 in Richtung auf den Brennkegel 1 nimmt.The
Das Gehäuse 2 ist mit einem schachtförmigen Eintritt 9 für die Zuführung einer dritten Luftmenge oder Tertiärluft L3 versehen, in dem sich eine Rückschlagklappe 10 befindet, mit deren Hilfe der Öffnungsquerschnitt des Schachtes 9 verstellt werden kann, in der Zeichnung erkennbar an einer Einstellschraube 11. Wie ersichtlich, ist die im Inneren des Gehäuses 2 liegende Mündung des Schachtes 9 direkt auf die Rückseite des Brennkegels 1 gerichtet, d. h. auf jene Seite, die dem im Brennkegel liegenden Brennstoff (nicht dargestellt) abgewandt ist.The
Im Betrieb stellt sich aufgrund der Art der Zuführung der Sekundärluft in bekannter Weise die schon erwähnte schraubenlinienförmige Bewegung der Sekundärluft in der Nachbrennkammer ein, die aufgrund der bekannten physikalischen Gegebenheiten im Bereich des größeren Durchmessers der Nachbrennkammer, der nahe dem Brennkegel liegt, teilweise umkehrt, so daß sich eine zentrale, in Richtung auf den Auslaß der Nachbrennkammer gerichtete Strömung ergibt, die die aus dem Brennkegel 1 entweichenden Flammgase mitreißt. Teilweise tritt die Wandnahe Strömung aber auch durch einen Ringspalt zwischen Nachbrennkammer 3 und Brennkegelmündung in das Gehäuse 2 ein, wobei mitgeführte Asche in das Gehäuse 2 ausgeschleudert wird (Zykloneffekt). Im Bereich zwischen dieser zentralen Strömung und der wandnahen Strömung findet innerhalb der Nachbrennkammer in bekannter Weise eine intensive Vermischung frischer Verbrennungsluft mit Flammgasen statt, die zu einem intensiven Ausbrand führt.In operation, due to the nature of the supply of secondary air in a known manner, the already mentioned helical movement of the secondary air in the afterburner, which partially reverses due to the known physical conditions in the region of the larger diameter of the afterburner, which is close to the fuel cone, so that results in a central, directed towards the outlet of the afterburner flow, which entrains the escaping from the fuel cone 1 flame gases. Partly enters the near-wall flow but also through an annular gap between the
Es ist anzumerken, daß die Erfindung auch bei anderen Drehrostkonstruktionen anwendbar ist, wie etwa bei Brennkörben, Trommeln und dergleichen.It should be noted that the invention is also applicable to other rotary grate designs, such as burners, drums and the like.
Claims (11)
- A method of supplying air to an installation for the combustion of solid fuel, said installation comprising a rotatable grate (1) rotating around an axis which extends horizontally or inclined with respect to the horizontal and at the same time revolving said solid fuel, a housing (2) surrounding said rotatable grate (1), and an afterburner chamber (3) opposite to said rotatable grate (1), wherein a portion (L1) of the air is blown as primary air directly below said fuel through hollow formed supporting arms (4) of said grate, said arms being provided with exit holes, and another portion (L2) of the air is blown as secondary air into the afterburner chamber (3), characterized in that the amounts of air are partitioned as follows:a) air amount blown through the supporting arms (4): L1 = 12 to 28% of the total air amount,b) air amount blown into the afterburner chamber (3): L2 = 20 to 30% of the total air amount,c) air amount supplied into the housing (2): L3 = 35 to 62% of the total air amount.
- The method of claim 1, characterized in that L1 = 20% of the total air amount.
- The method of claim 1 or 2, characterized in that L2 = 30% of the total air amount.
- The method of claim 1 or 2, characterized in that L3 = 50% of the total air amount.
- The method of claim 1 or 3, characterized in that L3 = 50% of the total air amount.
- The method of any one of the preceding claims, characterized in that the portion of the air introduced into the housing (2) is directed towards the outer side of the rotating grate (1).
- An installation for combusting solid, particulate fuel, comprising a rotating grate (1) which rotates around an axis (O) extending horizontally or inclined with respect to the horizontal and comprises hollow, air passing supporting arms (4), and further comprising a housing (2) surrounding said rotating grate and an afterburner chamber (3) opposing said rotating grate (1), characterized in that said housing is provided with an air supply opening (9) which disem-bogues into the air volume surrounding said rotating grate within said housing.
- The installation according to claim 7, characterized in that the air supply opening (9) is formed as a shaft passing through the housing wall.
- The installation according to claim 8, characterized in that the outlet of said shaft (9) is directed towards the outer side of said rotating grate (1).
- The installation according to any one of claims 7 to 9, characterized in that an adjustable device (10, 11) for influencing the air volume flow is disposed within the air supply opening (9).
- The installation according to any one of claims 7 to 10, characterized in that a check flap (10) is disposed within said air supply opening (9).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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DE10160415 | 2001-12-10 | ||
DE2001160415 DE10160415A1 (en) | 2001-12-10 | 2001-12-10 | Solid fuel incinerator and method for supplying air to it |
Publications (3)
Publication Number | Publication Date |
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EP1318351A2 EP1318351A2 (en) | 2003-06-11 |
EP1318351A3 EP1318351A3 (en) | 2003-09-10 |
EP1318351B1 true EP1318351B1 (en) | 2007-11-14 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP20020026516 Expired - Lifetime EP1318351B1 (en) | 2001-12-10 | 2002-11-27 | Solid fuel combustion device and method of supplying air to such a device |
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EP (1) | EP1318351B1 (en) |
DE (2) | DE10160415A1 (en) |
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CN103042022B (en) * | 2012-12-05 | 2015-11-25 | 广东德诚环保科技有限公司 | A kind of flyash treatment method |
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DE1751457A1 (en) * | 1968-05-31 | 1971-07-01 | Ifb Ingenieurbuero Fuer Brennt | Device for burning garbage, rubbish and the like |
DE19817122A1 (en) * | 1998-04-17 | 1999-10-21 | Kohlenstaubtechnik Dr Schoppe | Device for burning piece goods |
DE19817121A1 (en) * | 1998-04-17 | 1999-10-21 | Kohlenstaubtechnik Dr Schoppe | Method and device for feeding the wind for the combustion of lumpy fuel |
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2001
- 2001-12-10 DE DE2001160415 patent/DE10160415A1/en not_active Withdrawn
-
2002
- 2002-11-27 EP EP20020026516 patent/EP1318351B1/en not_active Expired - Lifetime
- 2002-11-27 DE DE50211198T patent/DE50211198D1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE10160415A1 (en) | 2003-06-18 |
DE50211198D1 (en) | 2007-12-27 |
EP1318351A3 (en) | 2003-09-10 |
EP1318351A2 (en) | 2003-06-11 |
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