EP1477734B1 - Heating device - Google Patents

Heating device Download PDF

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Publication number
EP1477734B1
EP1477734B1 EP20040450070 EP04450070A EP1477734B1 EP 1477734 B1 EP1477734 B1 EP 1477734B1 EP 20040450070 EP20040450070 EP 20040450070 EP 04450070 A EP04450070 A EP 04450070A EP 1477734 B1 EP1477734 B1 EP 1477734B1
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EP
European Patent Office
Prior art keywords
chamber
burn
heating device
secondary air
flue
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
Application number
EP20040450070
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German (de)
French (fr)
Other versions
EP1477734A3 (en
EP1477734A2 (en
Inventor
Alexander Dr. Weissinger
Josef Theiler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KWB Kraft und Waerme aus Biomasse GmbH
Original Assignee
KWB Kraft und Waerme aus Biomasse GmbH
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Publication of EP1477734A2 publication Critical patent/EP1477734A2/en
Publication of EP1477734A3 publication Critical patent/EP1477734A3/en
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Publication of EP1477734B1 publication Critical patent/EP1477734B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B5/00Combustion apparatus with arrangements for burning uncombusted material from primary combustion
    • F23B5/04Combustion apparatus with arrangements for burning uncombusted material from primary combustion in separate combustion chamber; on separate grate
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B10/00Combustion apparatus characterised by the combination of two or more combustion chambers
    • F23B10/02Combustion apparatus characterised by the combination of two or more combustion chambers including separate secondary combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B80/00Combustion apparatus characterised by means creating a distinct flow path for flue gases or for non-combusted gases given off by the fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/08Incineration of waste; Incinerator constructions; Details, accessories or control therefor having supplementary heating
    • F23G5/14Incineration of waste; Incinerator constructions; Details, accessories or control therefor having supplementary heating including secondary combustion
    • F23G5/16Incineration of waste; Incinerator constructions; Details, accessories or control therefor having supplementary heating including secondary combustion in a separate combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/24Incineration of waste; Incinerator constructions; Details, accessories or control therefor having a vertical, substantially cylindrical, combustion chamber
    • F23G5/26Incineration of waste; Incinerator constructions; Details, accessories or control therefor having a vertical, substantially cylindrical, combustion chamber having rotating bottom
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/32Incineration of waste; Incinerator constructions; Details, accessories or control therefor the waste being subjected to a whirling movement, e.g. cyclonic incinerators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23JREMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J1/00Removing ash, clinker, or slag from combustion chambers
    • F23J1/06Mechanically-operated devices, e.g. clinker pushers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING 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
    • F23L1/00Passages or apertures for delivering primary air for combustion 
    • F23L1/02Passages or apertures for delivering primary air for combustion  by discharging the air below the fire
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING 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
    • F23L9/00Passages or apertures for delivering secondary air for completing combustion of fuel 
    • F23L9/04Passages or apertures for delivering secondary air for completing combustion of fuel  by discharging the air beyond the fire, i.e. nearer the smoke outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00Casings; Linings; Walls
    • F23M5/08Cooling thereof; Tube walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G2205/00Waste feed arrangements
    • F23G2205/12Waste feed arrangements using conveyors
    • F23G2205/121Screw conveyor

Definitions

  • the invention relates to a heating device according to the preamble of claim 1.
  • the burn-out space is usually formed by a multiplicity of pulls, which generally run essentially parallel to one another and have a generally relatively small cross section, through which fuel gases flow and are introduced into the secondary air.
  • a heating device wherein parallel to a vertical combustion chamber, a Ausbrennhunt provided, wherein the combustion chamber via a horizontal train through which fuel gases flow is in communication with the Ausbrennhunt.
  • a heating device in which a combustion chamber aligned in parallel with a vertical combustion chamber is provided.
  • the aim of the invention is to avoid these disadvantages and to propose a heating device of the type mentioned, in which the possibly entrained ashes can be discharged quickly and easily.
  • the proposed measures ensure that the fuel channel is forced into a helical motion by the introduction of secondary air or a mixture of secondary air with fuel gases in the Ausbrennraum in the tangential direction.
  • the ash parts are urged against the wall of Ausbrennraumes due to their relative to the fuel gases of higher specific mass and are slowed down at this due to the friction and the lower velocity of the voltage applied to the wall layers of the fuel gases.
  • the ash can be discharged very easily, for example with a discharge screw.
  • the heater has a combustion chamber 20, as shown in Fig. 3 can be seen, is closed at the top with a cover 4 made of a refractory material, which in turn is covered by a protective cover 21.
  • the walls 23 of the combustion chamber 20 are provided with a lining 22 made of refractory material, wherein the wall 23 is formed as a double jacket, which is traversed by water, via connections 24, 25th can be discharged, wherein the supply via the top, not shown, arranged region of the double jacket connections.
  • the Double coat provided in a conventional manner with beads to secure the distance between the two walls of the double jacket and to increase its mechanical strength.
  • a closable service opening 14 is provided.
  • a rotary grate 3 is arranged, which is closer to the basis of Fig. 4 and 5 will be explained.
  • This rotary grate 3 is driven by a geared motor, not shown.
  • a primary air duct 1 ( Fig. 3 ) to which a blower 26 is connected. Furthermore, a drivable ash discharge screw 16 is provided, which projects into a space below the rotary grate 3 and is stirred in a nozzle 48.
  • a fuel feed screw protrudes, which is guided in an opening 27 of the combustion chamber 20 passing through, not shown pipe and extending above the rotary grate 3. offset in the direction of rotation of the rotary grate 3 by an angular amount relative to this fuel feed screw a Ableymschnecke (not shown) is provided, which guided in a bearing, not shown, the wall 23 passes through together with lining.
  • This clearance screw runs in accordance with the generatrices of the substantially conical rotary grate 3 and serves to clear the burnt-out fuel in order to transport it into the area of the ash discharge screw 16.
  • a Ausbrennraum 10 is provided, which is arranged parallel to the combustion chamber 20 and is connected thereto via a train 8, which tapers against the Ausbrennraum 10 and is surrounded by a double jacket 7, which serves for feeding of secondary air, wherein at the the Ausbrennraum 10 facing end face air nozzles 6 are provided which in the Fig. 3 only partially shown.
  • the Ausbrennraum 10 has a substantially circular cross section, wherein the axis of the train 8 extends substantially in the tangential direction to the cross section of the Ausbrennraumes 10.
  • This Ausbrennraum 10 is provided with a closable service opening 14 '. In addition to this service opening 14 'arranged in a socket 60 viewing opening is arranged.
  • an ash compartment 28 is provided, which is bounded by a substantially at the mouth of the train 8 in the Ausbrennraum 10 attached separating plate 9, which extends obliquely downwards.
  • This separating plate 9 is double-walled ( Fig. 3 ) and serves to supply secondary air to the double jacket 7 of the train. 8
  • This secondary air is the separating plate 9 via a secondary air channel 29 ( Fig. 3 ) supplied from a blower 30.
  • the interior of the double-walled separating plate 9, which also extends under the underside of the train 8, is connected via an opening 31 to the interior of the double jacket 7 of the train 8.
  • the secondary air flows through the interior of the double-walled separating plate 9 and the interior of the double jacket 7 of the train 8, whereby the secondary air is heated by the fuel gases flowing through the train 8 before it flows via the nozzles 6 in the Ausbrennraum 10.
  • the Ausbrennraum 10 whose wall is also provided with a lining 4 made of a refractory material, extends through the protective cover 21 therethrough upwards.
  • a heat exchanger assembly 12 of any type and a water-cooled cover 13 is provided in this upper region 11 of the Ausbrennhunt 10 and a heat exchanger assembly 12 of any type and a water-cooled cover 13 is provided.
  • the burnout chamber 10, 11 is connected via a deduction, not shown, with a chimney (not shown).
  • the rotary grate 3 eight partitions 37 which extend radially from a sleeve 36 'away to the outside and the tops are made trepanned.
  • the sleeve 36 ' is rotatably connected to a shaft 36 which is driven by a geared motor, not shown.
  • the radially outer end faces of the partition walls 37 are connected to each other via an annular wall 43.
  • the sectors 34, which are each defined by the two dividing walls 37, are therefore practically closed and, as a result, virtually no air can flow over from one sector 34 into the adjacent sector 34.
  • the partitions 37 are further connected to an Aschering 39, which is provided with annular openings 42, between which only relatively narrow webs remain.
  • Aschering 39 which is provided with annular openings 42, between which only relatively narrow webs remain.
  • rust rings 46 are attached.
  • the up to smaller diameter having rust rings 46 are spaced apart from each other in the vertical direction, so that between the individual rust rings 46 column 47 remain. Through this column, primary air can flow into the combustion chamber 20 and thereby flow through the solid fuel lying on the grate rings 46.
  • the grid rings are usually provided with slots, not shown, to avoid distortions due to thermal stresses.
  • the Aschering 39 which is fixedly connected to the annular wall 43 and the sleeve 36 ', rotates a short distance above a fixed primary air chamber 40, which is closed at the top by a diaphragm 33 which is provided with arranged in a circular arc openings 44.
  • the apertures 44 of the aperture 33 are arranged on a circular arc, which is connected to the circular arc on which the openings 42nd the Ascheringes 39 are arranged, covers substantially.
  • the cross sections of the apertures 44 of the aperture 33 are steadily decreasing ( Fig. 4 ) from the area of the fuel feed screw (not shown) away against the Abhoffmschnecke (not shown), wherein in the illustrated embodiment, the openings extend over an angle of about 240 °. In this case, a portion of the aperture 33 is kept free of openings 44.
  • solid fuel e.g. Pellets with the fuel supply screw, which projects through the opening 27 into the combustion chamber 20, introduced and applied to the rotary grate 3. Due to the temperatures prevailing in the combustion chamber 20, the fuel gas is exhausted and the gases ignite. In the vicinity of the fuel supply screw area, the openings 44 of the aperture 33 are located with the largest cross sections. As a result, a lot of primary air is supplied in this area.
  • the sector 34 of the rotary grate 3 on which the fuel material has been applied reaches into regions of the perforations 44 of the diaphragm 33 with smaller cross sections, whereby less and less air is supplied to the slowly burning fuel material, as a result of which the fuel material In the course of its progressive combustion, it is always supplied essentially optimally with air, since in the course of progressive combustion the demand for air is reduced.
  • the flames and fuel gases flow through the train 8 through into the Ausbrennraum 10, wherein the fuel gases flow due to the orientation of the train 8 substantially tangentially into the Ausbrennraum 10.
  • the ash particles contained in the combustion gases are specifically heavier than the gases and are therefore forced to the wall of the Ausbrennraumes 10 due to the swirl of the flow. Since the gases move due to the friction in a voltage applied to the wall boundary layer much slower than towards the middle of the gas stream, coming on the wall of the Ausbrennraumes 10 ash parts falling down into the ash chamber 28 and are out of this with a discharge screw 50 ( Fig. 3 ).

Description

Die Erfindung betrifft eine Heizeinrichtung gemäß dem Oberbegriff des Anspruches 1.The invention relates to a heating device according to the preamble of claim 1.

Bei bekannten derartigen Heizeinrichtungen ist der Ausbrennraum meist durch eine Vielzahl an Zügen, die meist im wesentlichen parallel zueinander verlaufen und einen meist relativ kleinen Querschnitt aufweisen gebildet, die von Brenngasen durchströmt werden und in die Sekundärluft eingebracht wird.In known heating devices of this type, the burn-out space is usually formed by a multiplicity of pulls, which generally run essentially parallel to one another and have a generally relatively small cross section, through which fuel gases flow and are introduced into the secondary air.

Aus der Gemäß der EP 1 085 259 A1 ist eine Heizvorrichtung bekannt, wobei parallel zu einer vertikalen Brennkammer eine Ausbrennkammer vorgesehen, wobei die Brennkammer über einen horizontalen Zug, durch den Brenngase strömen mit der Ausbrennkammer in Verbindung steht.From According to the EP 1 085 259 A1 a heating device is known, wherein parallel to a vertical combustion chamber, a Ausbrennkammer provided, wherein the combustion chamber via a horizontal train through which fuel gases flow is in communication with the Ausbrennkammer.

Aus der Gemäß der DE 296 05 801 U1 ist eine Heizvorrichtung bekannt, wobei eine zu einer vertikalen Brennkammer parallel ausgerichtete Ausbrennkammer vorgesehen ist.From According to the DE 296 05 801 U1 For example, a heating device is known in which a combustion chamber aligned in parallel with a vertical combustion chamber is provided.

Dabei ergibt sich jedoch der Nachteil, dass Ascheteile mitgerissen werden und sich meist in Umlenkungen der Züge ablagern, sodass die Asche aus einer Vielzahl von solchen Umlenkstellen ausgetragen werden muss. Dies ist jedoch mit einem erheblichen konstruktiven Aufwand verbunden, oder es ist in relativ kurzen zeitlichen Abständen eine Stillsetzung der Anlage zu Reinigungszwecken erforderlich.However, there is the disadvantage that ash parts are entrained and usually deposit in deflections of the trains, so that the ashes must be discharged from a variety of such deflection. However, this is associated with a considerable design effort, or it is necessary in relatively short time intervals, a shutdown of the system for cleaning purposes.

Ziel der Erfindung ist es, diese Nachteile zu vermeiden und eine Heizeinrichtung der eingangs erwähnten Art vorzuschlagen, bei dem die allenfalls mitgerissene Asche rasch und einfach ausgetragen werden kann.The aim of the invention is to avoid these disadvantages and to propose a heating device of the type mentioned, in which the possibly entrained ashes can be discharged quickly and easily.

Erfindungsgemäß wird dies bei einer Heizeinrichtung der eingangs erwähnten Art durch die kennzeichnenden Merkmale des Anspruches 1 erreicht.This is achieved according to the invention in a heating device of the type mentioned by the characterizing features of claim 1.

Durch die vorgeschlagenen Maßnahmen wird sichergestellt, dass die Brenngasse durch die Einbringung von Sekundärluft oder eines Gemisches von Sekundärluft mit Brenngasen in den Ausbrennraum in tangentialer Richtung in eine schraubenlinienförmige Bewegung gedrängt werden. Dadurch werden aber auch die Ascheteile aufgrund ihres gegenüber den Brenngasen höherer spezifischer Masse gegen die Wand des Ausbrennraumes gedrängt und werden an dieser aufgrund der Reibung und der geringeren Geschwindigkeit der an der Wand anliegenden Schichten der Brenngase gebremst und fallen nach unten. Aus dem untersten Bereich des Ausbrennraumes kann die Asche sehr einfach ausgetragen werden, z.B. mit einer Austragschnecke. Außerdem kommt es bei der Strömung der Sekundärluft durch das Innere des Doppelmantels des Zuges zu einer Erwärmung derselben durch die den Zug durchströmenden Brenngase.The proposed measures ensure that the fuel channel is forced into a helical motion by the introduction of secondary air or a mixture of secondary air with fuel gases in the Ausbrennraum in the tangential direction. As a result, however, the ash parts are urged against the wall of Ausbrennraumes due to their relative to the fuel gases of higher specific mass and are slowed down at this due to the friction and the lower velocity of the voltage applied to the wall layers of the fuel gases. From the bottom of the Ausbrennraumes the ash can be discharged very easily, for example with a discharge screw. In addition, it comes in the flow of secondary air through the interior the double mantle of the train to a heating of the same by the flowing through the train fuel gases.

Durch die Merkmale des Anspruches 2 ergibt sich der Vorteil, dass sich die Brenngase samt der Sekundärluft praktisch über die gesamte Höhe des Ausbrennraumes in einer schraubenlinienförmigen Bewegung befinden und es dabei zu einer sehr guten Abscheidung der Ascheteile und einer guten Vermischung der Brenngase mit der Sekundärluft kommt, wodurch die Brenngase praktisch vollkommen ausbrennen.Due to the features of claim 2, there is the advantage that the fuel gases including the secondary air are practically over the entire height of Ausbrennraumes in a helical motion and it comes to a very good separation of the ash parts and a good mixing of the fuel gases with the secondary air , whereby the combustion gases practically burn out completely.

In diesem Zusammenhang ist es vorteilhaft die Merkmale des Anspruches 3 vorzusehen, wodurch eine weitere Erwärmung der Sekundärluft ermöglicht wird.In this context, it is advantageous to provide the features of claim 3, whereby a further heating of the secondary air is made possible.

Durch die Merkmale des Anspruches 4 ergibt sich der Vorteil, dass die an der Wand des Ausbrennraumes abgeschiedene Asche in den Ascheraum abgleiten kann.Due to the features of claim 4, there is the advantage that the deposited ash on the wall of Ausbrennraumes can slide into the ash space.

Durch die Merkmale des Anspruches 5 ergibt sich eine in konstruktiver Hinsicht sehr einfache Lösung, bei der auch sichergestellt ist, dass die gesamten Brenngase im Bereich des Ausbrennraumes in eine schraubenlinieförmige Bewegung gezwungen werden, wodurch auf einfache Weise ein hoher Grad der Abscheidung von mitgerissenen Aschepartikel erreicht wird.Due to the features of claim 5 results in a structurally very simple solution, in which it is also ensured that the entire fuel gases are forced in the region of Ausbrennraumes in a helical motion, which achieved in a simple way a high degree of deposition of entrained ash particles becomes.

In diesem Zusammenhang ist es besonders vorteilhaft die Merkmale des Anspruches 6 vorzusehen, durch welche Maßnahmen die Einströmgeschwindigkeit der Brenngase in den Ausbrennraum erhöht wird.In this context, it is particularly advantageous to provide the features of claim 6, by which measures the inflow velocity of the fuel gases is increased in the Ausbrennraum.

Die Erfindung wird unter Bezugnahme auf die beigeschlossenen Zeichnungen, in welchen besonders bevorzugte Ausführungsbeispiele dargestellt sind, näher beschrieben. Dabei zeigt:

  • Fig. 1 und 2 schematische axonometrische Ansichten einer erfindungsgemäßen Heizeinrichtung mit abgenommener oberer Abdeckung und ohne Wärmetauscher,
  • Fig. 3 schematisch einen Vertikalschnitt entlang der Linie III-III in der Fig. 2,
  • Fig. 4 schematisch einen Horizontalschnitt entlang der Linie V-V in der Fig. 3 durch einen Drehrost und
  • Fig. 5 einen Vertikalschnitt durch den Drehrost samt Primärluftkammer und Primärluftkanal.
The invention will be described in more detail with reference to the accompanying drawings, in which particularly preferred embodiments are shown. Showing:
  • Fig. 1 and 2 schematic axonometric views of a heater according to the invention with removed top cover and without heat exchanger,
  • Fig. 3 schematically a vertical section along the line III-III in the Fig. 2 .
  • Fig. 4 schematically a horizontal section along the line VV in the Fig. 3 through a rotating grate and
  • Fig. 5 a vertical section through the rotary grate together with primary air chamber and primary air duct.

Die Heizeinrichtung weist einen Brennraum 20 auf, der wie aus der Fig. 3 zu ersehen ist, nach oben zu mit einer Abdeckung 4 aus einem feuerfesten Material abgeschlossen ist, die ihrerseits von einem Schutzdeckel 21 abgedeckt ist. Die Wände 23 des Brennraumes 20 sind mit einer Auskleidung 22 aus feuerfestem Material versehen, wobei die Wand 23 als ein Doppelmantel ausgebildet ist, der von Wasser durchströmt ist, das über Anschlüsse 24, 25 abführbar ist, wobei die Zufuhr über im obersten, nicht dargestellten, Bereich des Doppelmantels angeordnete Anschlüsse erfolgt. Wie aus der Fig. 3 zu ersehen ist, ist der Doppelmantel in üblicher Weise mit Sicken zur Sicherung des Abstandes zwischen den beiden Wänden des Doppelmantels und zur Erhöhung seiner mechanischen Festigkeit versehen.The heater has a combustion chamber 20, as shown in Fig. 3 can be seen, is closed at the top with a cover 4 made of a refractory material, which in turn is covered by a protective cover 21. The walls 23 of the combustion chamber 20 are provided with a lining 22 made of refractory material, wherein the wall 23 is formed as a double jacket, which is traversed by water, via connections 24, 25th can be discharged, wherein the supply via the top, not shown, arranged region of the double jacket connections. Like from the Fig. 3 is to be seen is the Double coat provided in a conventional manner with beads to secure the distance between the two walls of the double jacket and to increase its mechanical strength.

Um einen Zugang zum Brennraum 20 zu ermöglichen, ist eine verschließbare Serviceöffnung 14 vorgesehen.In order to allow access to the combustion chamber 20, a closable service opening 14 is provided.

In dem Brennraum 20 ist ein Drehrost 3 angeordnet, der näher anhand der Fig. 4 und 5 erläutert werden wird. Dieser Drehrost 3 ist von einem nicht dargestellten Getriebemotor angetrieben.In the combustion chamber 20, a rotary grate 3 is arranged, which is closer to the basis of Fig. 4 and 5 will be explained. This rotary grate 3 is driven by a geared motor, not shown.

Unterhalb des Drehrostes 3 verläuft ein Primärluftkanal 1 (Fig. 3), an dem ein Gebläse 26 angeschlossen ist. Weiters ist eine antreibbare Ascheaustragsschnecke 16 vorgesehen, die in einen Raum unterhalb des Drehrostes 3 hineinragt und in einem Stutzen 48 gerührt ist.Below the rotary grate 3 runs a primary air duct 1 ( Fig. 3 ) to which a blower 26 is connected. Furthermore, a drivable ash discharge screw 16 is provided, which projects into a space below the rotary grate 3 and is stirred in a nozzle 48.

In den Brennraum 20 ragt eine Brennstoff-Zuführschnecke (nicht dargestellt) hinein, die in einem eine Öffnung 27 des Brennraumes 20 durchsetzenden, nicht dargestellten Rohr geführt ist und oberhalb des Drehrostes 3 verläuft. in Drehrichtung des Drehrostes 3 um einen Winkelbetrag gegenüber dieser Brennstoff-Zuführschnecke versetzt ist eine Abräumschnecke (nicht dargestellt) vorgesehen, die in einem nicht dargestellten Lager geführt die Wand 23 samt Auskleidung durchsetzt. Diese Abräumschnecke verläuft entsprechend den Mantellinien des im wesentlichen kegelförmigen Drehrostes 3 und dient zum Abräumen des ausgebrannten Brennstoffes, um diesen in den Bereich der Ascheaustragsschnecke 16 zu befördern.In the combustion chamber 20, a fuel feed screw (not shown) protrudes, which is guided in an opening 27 of the combustion chamber 20 passing through, not shown pipe and extending above the rotary grate 3. offset in the direction of rotation of the rotary grate 3 by an angular amount relative to this fuel feed screw a Abräumschnecke (not shown) is provided, which guided in a bearing, not shown, the wall 23 passes through together with lining. This clearance screw runs in accordance with the generatrices of the substantially conical rotary grate 3 and serves to clear the burnt-out fuel in order to transport it into the area of the ash discharge screw 16.

Weiters ist ein Ausbrennraum 10 vorgesehen, der parallel zum Brennraum 20 angeordnet ist und mit diesem über einen Zug 8 verbunden ist, der sich gegen den Ausbrennraum 10 zu verjüngt und von einem Doppelmantel 7 umgeben ist, der zum Einspeisen von Sekundärluft dient, wobei an der dem Ausbrennraum 10 zugekehrten Stirnseite Luftdüsen 6 vorgesehen sind, die in der Fig. 3 nur teilweise dargestellt sind. Der Ausbrennraum 10 weist einen im wesentlichen kreisrunden Querschnitt auf, wobei die Achse des Zuges 8 im wesentlichen in tangentialer Richtung zum Querschnitt des Ausbrennraumes 10 verläuft.Furthermore, a Ausbrennraum 10 is provided, which is arranged parallel to the combustion chamber 20 and is connected thereto via a train 8, which tapers against the Ausbrennraum 10 and is surrounded by a double jacket 7, which serves for feeding of secondary air, wherein at the the Ausbrennraum 10 facing end face air nozzles 6 are provided which in the Fig. 3 only partially shown. The Ausbrennraum 10 has a substantially circular cross section, wherein the axis of the train 8 extends substantially in the tangential direction to the cross section of the Ausbrennraumes 10.

Dieser Ausbrennraum 10 ist mit einer verschließbaren Serviceöffnung 14' versehen. Neben dieser Serviceöffnung 14' ist ein in einem Stutzen 60 angeordnete Sichtöffnung angeordnet.This Ausbrennraum 10 is provided with a closable service opening 14 '. In addition to this service opening 14 'arranged in a socket 60 viewing opening is arranged.

Im Bereich des Ausbrennraumes 10 ist ein Ascheraum 28 vorgesehen, der durch ein im wesentlichen an der Mündung des Zuges 8 in den Ausbrennraum 10 ansetzendes Trennblech 9 begrenzt ist, das sich schräg nach unten zu erstreckt. Dieses Trennblech 9 ist doppelwandig ausgebildet (Fig. 3) und dient zur Zufuhr von Sekundärluft zum Doppelmantel 7 des Zuges 8.In the area of Ausbrennraumes 10 an ash compartment 28 is provided, which is bounded by a substantially at the mouth of the train 8 in the Ausbrennraum 10 attached separating plate 9, which extends obliquely downwards. This separating plate 9 is double-walled ( Fig. 3 ) and serves to supply secondary air to the double jacket 7 of the train. 8

Diese Sekundärluft wird dem Trennblech 9 über einen Sekundärluftkanal 29 (Fig. 3) von einem Gebläse 30 zugeführt. Dabei ist das Innere des doppelwandigen Trennbleches 9, das sich auch unter der Unterseite des Zuges 8 erstreckt, über eine Öffnung 31 mit dem Inneren des Doppelmantels 7 des Zuges 8 verbunden. Dadurch durchströmt die Sekundärluft das Innere des doppelwandigen Trennblechs 9 und das Innere des Doppelmantels 7 des Zuges 8, wodurch die Sekundärluft durch die den Zug 8 durchströmenden Brenngase erwärmt wird, bevor sie über die Düsen 6 in den Ausbrennraum 10 strömt.This secondary air is the separating plate 9 via a secondary air channel 29 ( Fig. 3 ) supplied from a blower 30. In this case, the interior of the double-walled separating plate 9, which also extends under the underside of the train 8, is connected via an opening 31 to the interior of the double jacket 7 of the train 8. As a result, the secondary air flows through the interior of the double-walled separating plate 9 and the interior of the double jacket 7 of the train 8, whereby the secondary air is heated by the fuel gases flowing through the train 8 before it flows via the nozzles 6 in the Ausbrennraum 10.

Der Ausbrennraum 10, dessen Wand ebenfalls mit einer Auskleidung 4 aus einem feuerfesten Material versehen ist, erstreckt sich durch den Schutzdeckel 21 hindurch nach oben. In diesem oberen Bereich 11 der Ausbrennkammer 10 ist auch eine Wärmetauscher-Anordnung 12 beliebiger Bauart und ein wassergekühlter Deckel 13 vorgesehen. Die Ausbrennkammer 10, 11 ist über einen nicht dargestellten Abzug mit einem Kamin (nicht dargestellt) verbunden.The Ausbrennraum 10, whose wall is also provided with a lining 4 made of a refractory material, extends through the protective cover 21 therethrough upwards. In this upper region 11 of the Ausbrennkammer 10 and a heat exchanger assembly 12 of any type and a water-cooled cover 13 is provided. The burnout chamber 10, 11 is connected via a deduction, not shown, with a chimney (not shown).

Wie aus den Fig. 4 und 5 zu ersehen ist, weist der Drehrost 3 acht Trennwände 37 auf, die sich radial von einer Hülse 36' weg nach außen erstrecken und deren Oberseiten getreppt ausgeführt sind. Die Hülse 36' ist drehfest mit einer Welle 36 verbunden, die von einem nicht dargestellten Getriebemotor angetrieben ist. Die radial äußeren Stirnseiten der Trennwände 37 sind über eine Ringwand 43 miteinander verbunden. Die durch die je zwei Trennwände 37 bestimmten Sektoren 34 sind daher praktisch abgeschlossen und es kann daher praktisch keine Luft von einem Sektor 34 in den benachbarten Sektor 34 überströmen.Like from the Fig. 4 and 5 can be seen, the rotary grate 3 eight partitions 37 which extend radially from a sleeve 36 'away to the outside and the tops are made trepanned. The sleeve 36 'is rotatably connected to a shaft 36 which is driven by a geared motor, not shown. The radially outer end faces of the partition walls 37 are connected to each other via an annular wall 43. The sectors 34, which are each defined by the two dividing walls 37, are therefore practically closed and, as a result, virtually no air can flow over from one sector 34 into the adjacent sector 34.

Die Trennwände 37 sind weiters mit einem Aschering 39 verbunden, der mit ringförmig angeordneten Durchbrechungen 42 versehen ist, zwischen denen nur relativ schmale Stege verbleiben. An den oberen getreppten Rändern der Trennwände 37 sind Rostringe 46 befestigt. Dabei sind die nach oben zu kleinere Durchmesser aufweisenden Rostringe 46 voneinander in vertikaler Richtung distanziert, sodass zwischen den einzelnen Rostringen 46 Spalte 47 verbleiben. Über diese Spalte kann Primärluft in den Brennraum 20 einströmen und dabei das auf den Rostringen 46 liegende feste Brennmaterial durchströmen. Die Rostringe sind üblicherweise mit nicht dargestellten Schlitzen versehen, um Verwerfungen aufgrund von thermischen Spannungen zu vermeiden.The partitions 37 are further connected to an Aschering 39, which is provided with annular openings 42, between which only relatively narrow webs remain. At the top stepped edges of the partitions 37 rust rings 46 are attached. In this case, the up to smaller diameter having rust rings 46 are spaced apart from each other in the vertical direction, so that between the individual rust rings 46 column 47 remain. Through this column, primary air can flow into the combustion chamber 20 and thereby flow through the solid fuel lying on the grate rings 46. The grid rings are usually provided with slots, not shown, to avoid distortions due to thermal stresses.

Der Aschering 39, der mit der Ringwand 43 und der Hülse 36' fest verbunden ist, dreht sich in geringem Abstand oberhalb einer fest angeordneten Primärluftkammer 40, die oben durch eine Blende 33 abgeschlossen ist, die mit in einem Kreisbogen angeordneten Durchbrechungen 44 versehen ist. Dabei sind die Durchbrechungen 44 der Blende 33 auf einen Kreisbogen angeordnet, der sich mit dem Kreisbogen, auf dem die Durchbrechungen 42 des Ascheringes 39 angeordnet sind, im wesentlichen deckt. Die Querschnitte der Durchbrechungen 44 der Blende 33 vermindern sich stetig (Fig. 4) vom Bereich der Brennstoff-Zufuhrschnecke (nicht dargestellt) weg gegen die Abräumschnecke (nicht dargestellt) zu, wobei sich beim dargestellten Ausführungsbeispiel die Durchbrechungen über einen Winkel von ca. 240° erstrecken. Dabei ist ein Teilbereich der Blende 33 frei von Durchbrechungen 44 gehalten.The Aschering 39, which is fixedly connected to the annular wall 43 and the sleeve 36 ', rotates a short distance above a fixed primary air chamber 40, which is closed at the top by a diaphragm 33 which is provided with arranged in a circular arc openings 44. The apertures 44 of the aperture 33 are arranged on a circular arc, which is connected to the circular arc on which the openings 42nd the Ascheringes 39 are arranged, covers substantially. The cross sections of the apertures 44 of the aperture 33 are steadily decreasing ( Fig. 4 ) from the area of the fuel feed screw (not shown) away against the Abräumschnecke (not shown), wherein in the illustrated embodiment, the openings extend over an angle of about 240 °. In this case, a portion of the aperture 33 is kept free of openings 44.

Die Zufuhr von Primärluft zur Primärluftkammer 40 erfolgt über den Primärluftkanal 1, wobei die Primärluftkammer 40 an ihrer Unterseite im Bereich des Primärluftkanals 1 Durchbrüche 41 aufweist, über die die Luft einströmen kann.The supply of primary air to the primary air chamber 40 via the primary air duct 1, wherein the primary air chamber 40 has on its underside in the region of the primary air duct 1 openings 41 through which the air can flow.

Im Betrieb wird festes Brennmaterial, z.B. Pellets mit der Brennstoff-Zufuhrschnecke, die durch die Öffnung 27 in den Brennraum 20 hineinragt, eingebracht und auf dem Drehrost 3 aufgebracht. Das Brennmaterial gast aufgrund der im Brennraum 20 herrschenden Temperaturen aus und die Gase entzünden sich. In dem der Brennstoff-Zufuhrschnecke nahen Bereich befinden sich die Durchbrechungen 44 der Blende 33 mit den größten Querschnitten. Dadurch wird in diesem Bereich viel Primärluft zugeführt.In operation, solid fuel, e.g. Pellets with the fuel supply screw, which projects through the opening 27 into the combustion chamber 20, introduced and applied to the rotary grate 3. Due to the temperatures prevailing in the combustion chamber 20, the fuel gas is exhausted and the gases ignite. In the vicinity of the fuel supply screw area, the openings 44 of the aperture 33 are located with the largest cross sections. As a result, a lot of primary air is supplied in this area.

Beim Weiterdrehen des Drehrostes 3 gelangt der durch die Trennwände 37 bestimmte Sektor 34 des Drehrostes 3, auf welchem das Brennmaterial aufgebracht wurde in Bereiche der Durchbrechungen 44 der Blende 33 mit kleineren Querschnitten, wodurch dem langsam ausbrennenden Brennmaterial immer weniger Luft zugeführt wird, wodurch das Brennmaterial im Zuge seiner fortschreitenden Verbrennung stets im wesentlichen optimal mit Luft versorgt wird, da sich eben im Zuge der fortschreitenden Verbrennung der Luftbedarf vermindert.As the rotary grate 3 continues to rotate, the sector 34 of the rotary grate 3 on which the fuel material has been applied reaches into regions of the perforations 44 of the diaphragm 33 with smaller cross sections, whereby less and less air is supplied to the slowly burning fuel material, as a result of which the fuel material In the course of its progressive combustion, it is always supplied essentially optimally with air, since in the course of progressive combustion the demand for air is reduced.

Im Bereich der nicht dargestellten Abräumschnecke, die im Bereich des Zuges 8 angeordnet ist, weist die Blende 39 keine Durchbrüche mehr auf. Dadurch herrscht im Bereich jenes Sektors 34, über dem sich die Abräumschnecke befindet, wenn überhaupt, so nur eine sehr geringe Luftströmung, wodurch nur wenige Ascheteile mitgerissen werden.In the region of the removal screw, not shown, which is arranged in the region of the train 8, the diaphragm 39 no breakthroughs on more. As a result, prevails in the area of that sector 34, over which the Abräumschnecke is, if at all, so only a very small flow of air, causing only a few ash parts are entrained.

Die Flammen und Brenngase strömen durch den Zug 8 hindurch in den Ausbrennraum 10, wobei die Brenngase aufgrund der Ausrichtung des Zuges 8 im wesentlichen tangential in den Ausbrennraum 10 einströmen.The flames and fuel gases flow through the train 8 through into the Ausbrennraum 10, wherein the fuel gases flow due to the orientation of the train 8 substantially tangentially into the Ausbrennraum 10.

Gleichzeitig wird Sekundärluft über den Sekundärluftkanal 29 und das doppelwandige Trennblech 9 in den Doppelmantel 7 des Zuges 8 eingebracht und strömt über die Düsen 6 in den Ausbrennraum 10 in tangentialer Richtung ein und vermischt sich mit den Brenngasen.At the same time secondary air is introduced via the secondary air duct 29 and the double-walled separating plate 9 in the double jacket 7 of the train 8 and flows through the nozzles 6 in the Ausbrennraum 10 in the tangential direction and mixes with the fuel gases.

Dadurch brennen diese auf ihrem im wesentlichen schraubenlinienförmigen Weg durch den Ausbrennraum 10 aus.As a result, they burn out on their essentially helical path through the Ausbrennraum 10.

Die in den Brenngasen enthaltenen Ascheteilchen sind spezifisch schwerer als die Gase und werden daher aufgrund des Dralls der Strömung an die Wand des Ausbrennraumes 10 gedrängt. Da die Gase aufgrund der Reibung sich in einer an der Wand anliegenden Grenzschicht wesentlich langsamer bewegen als gegen die Mitte des Gasstromes zu, fallen die an der Wand des Ausbrennraumes 10 zur Anlage kommenden Ascheteile nach unten in den Ascheraum 28 und werden aus diesem mit einer Austragschnecke 50 (Fig. 3) ausgetragen.The ash particles contained in the combustion gases are specifically heavier than the gases and are therefore forced to the wall of the Ausbrennraumes 10 due to the swirl of the flow. Since the gases move due to the friction in a voltage applied to the wall boundary layer much slower than towards the middle of the gas stream, coming on the wall of the Ausbrennraumes 10 ash parts falling down into the ash chamber 28 and are out of this with a discharge screw 50 ( Fig. 3 ).

Im oberen Bereich des Ausbrennraumes wird den Brenngasen durch die Wärmetauscher-Anordnung 12 und den wassergekühlten Deckel 13 Wärme entzogen. Die abgekühlten Brenngase gelangen anschließend in einen Kamin und werden über diesen abgeführt.In the upper part of the Ausbrennraumes the fuel gases through the heat exchanger assembly 12 and the water-cooled cover 13 heat is removed. The cooled fuel gases then pass into a chimney and are discharged via this.

Claims (6)

  1. A heating device, comprising a combustion chamber (20), into which a fuel feed pipe opens and which is connected via a substantially horizontal flue (8) with burn-up chamber (10), into which at least one inlet (6) opens for secondary air and/or a mixture of secondary air and combustion gases, wherein the burn-up chamber (10) is aligned vertically and has a substantially circular cross section, wherein the inlet (6) opens tangentially into the burn-up chamber (10), characterized in that the flue (8) is arranged with a double jacket (7), the interior of which can be supplied with secondary air, wherein nozzles (6) are arranged on the face side facing the burn-up chamber (10).
  2. A heating device according to claim 1, characterized in that the inlet (6) is arranged in the bottom region of the burn-up chamber (10).
  3. A heating device according to claim 1 or 2, characterized in that the supply of secondary air to the interior of the double jacket (7) of the flue (8) occurs via a double-walled separating plate (9) which separates the combustion chamber (20) from the burn-up chamber (10) beneath the flue (8).
  4. A heating device according to claim 3, characterized in that the double-walled separating plate (9) is arranged diagonally downwards and delimits an ash chamber (28) in the region of the burn-up chamber (10).
  5. A heating device according to one of the claims 1 to 4, characterized in that the flue (8) opens tangentially into the burn-up chamber (10).
  6. A heating device according to one of the claims 1 to 5, characterized in that the flue (8) has a cross-section which tapers in the direction towards the burn-up chamber.
EP20040450070 2003-05-14 2004-03-29 Heating device Expired - Lifetime EP1477734B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT2003739 2003-05-14
AT7392003A AT412308B (en) 2003-05-14 2003-05-14 HEATING DEVICE

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EP1477734A2 EP1477734A2 (en) 2004-11-17
EP1477734A3 EP1477734A3 (en) 2007-05-30
EP1477734B1 true EP1477734B1 (en) 2013-11-13

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITVR20060191A1 (en) * 2006-12-13 2008-06-14 Cola S R L PORTABRACHIER, PARTICULARLY FOR STOVES
AT504652B1 (en) * 2007-03-29 2008-07-15 Windhager Zentralheizung Techn Burning chamber for boiler with heated solid fuel, has multiple burning chamber bricks which are covered by base plate , where base plate has multiple combustion bricks
FR2917486B1 (en) * 2007-06-15 2009-09-25 Ct Internat De Traitement Et D PROCESS FOR GASIFYING WASTE IN A ROTATING SOAK OVEN, AND OVEN FOR ITS IMPLEMENTATION
CN102128719B (en) * 2010-12-13 2012-10-24 中国航空动力机械研究所 Sectorial reverse flow combustor and split combustor case thereof
CN102330970B (en) * 2011-09-20 2014-11-05 魏广廷 Boiler combustor
CN103851626A (en) * 2014-03-18 2014-06-11 郑敏 Trash burning furnace

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ210243A (en) * 1984-11-19 1988-01-08 Waterwide Dev New Zealand Ltd Extraction zone for solid fuel burner
AT402098B (en) * 1995-02-16 1997-01-27 Georg Fischer Maschinen Und Ke BOILER
DE29605801U1 (en) 1996-03-28 1996-06-27 Fischer Georg Gmbh & Co boiler
DE19817885A1 (en) * 1998-04-22 1999-10-28 Bosch Gmbh Robert Arrangement for rebuilding the torque of a supercharged internal combustion engine after an ASR intervention
EP1085259B1 (en) 1999-09-15 2004-01-14 LIGNOTECH Entwicklung von Biomassefeuerungsanlagen GmbH Device for burning biogenous fuels

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AT412308B (en) 2004-12-27
EP1477734A2 (en) 2004-11-17
ATA7392003A (en) 2004-05-15

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