EP0952398B1 - Air supply method and device for burning particulate fuel - Google Patents
Air supply method and device for burning particulate fuel Download PDFInfo
- Publication number
- EP0952398B1 EP0952398B1 EP99107650A EP99107650A EP0952398B1 EP 0952398 B1 EP0952398 B1 EP 0952398B1 EP 99107650 A EP99107650 A EP 99107650A EP 99107650 A EP99107650 A EP 99107650A EP 0952398 B1 EP0952398 B1 EP 0952398B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion
- fuel
- grate
- cone
- combustion grate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 63
- 238000000034 method Methods 0.000 title claims description 11
- 238000002485 combustion reaction Methods 0.000 claims abstract description 81
- 239000007789 gas Substances 0.000 claims abstract description 31
- 230000008878 coupling Effects 0.000 claims abstract 2
- 238000010168 coupling process Methods 0.000 claims abstract 2
- 238000005859 coupling reaction Methods 0.000 claims abstract 2
- 239000002699 waste material Substances 0.000 claims description 4
- 239000002023 wood Substances 0.000 claims description 4
- 230000000284 resting effect Effects 0.000 claims 3
- 230000000630 rising effect Effects 0.000 claims 1
- 238000005096 rolling process Methods 0.000 claims 1
- 239000004449 solid propellant Substances 0.000 abstract 1
- 238000010304 firing Methods 0.000 description 43
- 239000002956 ash Substances 0.000 description 12
- 239000002245 particle Substances 0.000 description 10
- 239000000463 material Substances 0.000 description 4
- 241001156002 Anthonomus pomorum Species 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 235000002918 Fraxinus excelsior Nutrition 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000010791 domestic waste Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000010881 fly ash Substances 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000002440 industrial waste Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000004056 waste incineration Methods 0.000 description 1
Images
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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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 and an apparatus to feed the wind for the combustion of lumpy 3.
- the method according to the preamble of claim 1 and 3, respectively and device of this type are from the essay "The development of the fuel cone for incineration of waste "by the inventor in the magazine “Fuel-Heat-Power", 19 (1967), No. 10, Pages 469 to 473 known.
- This essay largely describes an incinerator for the automatic, universal and inexpensive waste incineration for municipalities and small and medium-sized industrial companies.
- she includes a firing cone that is about an inclined axis rotates, and an afterburner that is vertically above the opening the firing cone is arranged.
- the firing cone has a frustoconical shape Section, one located at the top larger diameter adjoining cylindrical section and a frustoconical one adjoining its free end Attachment whose small diameter is the free end of the Firing cone and its opening forms.
- the frustoconical section consists of itself radial / axial extending, mutually spaced bars, the of several outer circumferential rings of different diameters are mutually supported.
- the frustoconical section of the fuel cone is blown from below by the downwind, which is the Gaps between the bars must pass to the firing material to reach, which is in the firing cone and due to this its orbital movement is circulated.
- the one above the The afterburner arranged in the opening of the firing cone attachment has one Afterburning chamber which is frusto-conical in the upper section narrowed and provided with a facility there the upper wind leads tangentially into the afterburning chamber so that a turbulent flow forms in it, which the Exhaust gases emerging from the firing cone and burns out.
- a firing cone firing system of this type is. also in US 3,599,581 A.
- EP 0 754 907 A2 describes a method for influencing combustion known in a boiler with shaking grate, in which the Supply of primary air and / or fuel during and briefly after shaking the grate is reduced to one by the Shaking causes the burn rate to increase suddenly to avoid. A sudden drop in oxygen levels in the exhaust gas, which would otherwise occur because of the overall control of the Fuel supply too slow due to sudden changes in combustion conditions is avoided.
- the combustion system shown is the primary air from below blown against the rust and the gaps between the Grate bars pass to the firing material lying on the grate to get to the firing material while secondary air from above is blown, which is fed through nozzles, which at least one of the boiler walls arranged and directed against the grate are.
- the air volumes supplied depend on the result ongoing measurements of the boiler state variables, the excess air and heat absorption.
- GB 1,141,562 A describes a domestic or industrial waste incinerator, consisting of a lying, rotating Grid drum made of axially extending and circular tubes trending rings is formed. Inside the drum are on small tubes attached to the tubes, which are radial into the drum protrude and are connected to the interior of the tube to which they are attached.
- the tubes are on one arranged helically and through plates connected to each other to form a screw conveyor for the firing material to form, which is attached to the drum by a front Pilot burner can be ignited.
- the tubes are on the face open to allow the entry of air through the Tubes can escape into the interior of the drum.
- the drum is surrounded by a double-walled jacket, the outer wall is open at the top. Below in the area of one under the drum Ash box are the jacket and its interior completely open.
- air is introduced into the interior of the jacket from above, that flows through the coat and cools its walls, exits in the ash box at the bottom and from there the bottom Gaps between the tubes of the drum and as primary air in the combustion chamber enclosed by the drum arrives.
- An external suction fan in the combustion chamber Vacuum generated by this primary air and by the Tubes and secondary air supplied through the tubes, which at the same time cools the pipes, sucks them in.
- a significant disadvantage is also that in the above Way deflected underwind entrained gas and it contains dusty fuel that burns.
- the the resulting flame rays overheat and corrode the metallic material of the combustion grate, in particular its consisting of radial arms and circular rings Supporting structure. As the heating value of the fuel increases such overheating and corrosion are more serious.
- Flame gases are known to supply this upper air. at known method, this was done in such a way that the flame gas flow the upper air sucked in by itself.
- the invention has for its object a method in The preamble of claim 1 to specify the outlined type sufficient for the complete burnout of the fuel Air supply ensures overheating of the combustion grate avoids and without dust filtering of the combustion exhaust gases gets along.
- the invention achieves the desired success apparatus in that the support arms of the combustion grate are hollow are executed and flowed through by the downwind, making them be cooled.
- the downwind is forced on the top the combustion grate, i.e. directly on the fuel, so that the possibility of deflecting the underwind under the combustion grate is greatly reduced.
- the aim of the post-combustion of the flame gases generated by that on the Burn out burning rust burning fuel special attention given.
- the flame gases the upper air is supplied in the form of a high-speed flow, which surrounds the flame gases helically and itself propagates towards the combustion grate, the Increased diameter of this vortex.
- the headwind current describes, for example, the surface of a truncated cone, whose larger diameter faces the combustion grate.
- the headwind is due to the smaller diameter of this truncated cone blown. This results in a negative pressure in the center, the sucks in the flame gases. Between the center of the towards this vacuum point flowing flame gas flow and this A zone is formed around the toroidal headwind current intense turbulence from where the flame gases with the headwind be mixed thoroughly. This zone of turbulence is outside of surrounded by a cold air flow of fresh head wind.
- the head wind is at a speed of 40 to 100 m / s, preferably 60 to 80 m / s, which is thus so high, that the thereby acting on the particles in the flame gases Centrifugal force the particles into the cold air flow mentioned ejected, where they are cooled so far that they dry fail. In this way, not only the afterburner becomes escaping exhaust gas flow without the use of filters of particles exempt, but is also a slagging of the incinerator avoided.
- the air duct described in the afterburner is achieved with the help of a truncated cone-shaped afterburner into which the upper wind at the smaller end facing away from the combustion grate The same diameter is blown in via an introducer which is the upper wind tangential to the wall of the afterburner leads into this, where it is inclined at an angle to the Axis of the afterburning chamber spreads out in this.
- At the introduction of the headwind into the afterburning chamber can also be from a flow direction obliquely from the outset by means of guide devices to the axis of the afterburning chamber.
- each hollow support arm at least one further opening on the side facing away from the fuel Side so that it has fallen through the combustion grate Ash or fine amounts of fuel in the combustion air ashes get to burn out completely. Through these openings can also penetrate into the pipes fuel or Ash particles are blown out.
- the combustion grate is advantageously covered by a jacket hollow (burning) cone, which rotates around a executes an inclined axis.
- the afterburner is in this Most conveniently arranged coaxially to the axis of rotation of the cone.
- the coaxial arrangement of the afterburning chamber just above the firing cone also has the consequence that the heat radiation in the Afterburning chamber burning flame gases on the in the burning cone located fuel acts advantageously and the taking place there Smoldering and combustion process supported.
- the lower diameter of the afterburning chamber should expediently be used slightly larger than the diameter of the top edge of the fuel cone. This will close the afterburner wall downward blown dust from the afterburner past the firing cone into the ash room below blown.
- Fig. 1 shows a complete incinerator consisting of a firing cone K rotating about an inclined axis O and one coaxial to the exit end of the firing cone K. subsequent afterburner N, which is enclosed by a housing G. are.
- the fuel cone K has a frustoconical section 1, a cylindrical one adjoining it towards the open end Section 2 and an adjoining one section 3 narrowing in diameter.
- the combustion grate this fuel cone K consists of grate bars 4 made of heat-resistant cast and from hollow, radial support arms 5 and ring carriers (not shown), that connect the support arms 5 to each other.
- the firing cone K is smaller in diameter at the end of several hollow axially parallel legs 6 held with an air collection box 7 are connected, which has radial partitions, that each close one air collection chamber per support arm 5.
- the Air collection box 7 is firmly connected to a race 8, the of several stationary rollers (not shown) is stored.
- the race 8 has one opening per support arm 5 on.
- the number of connectors is preferably as large as the number of hollow support arms 5th
- a shaft 12 is rigidly connected on the side of the race 8 facing away from the firing cone K of this extends away and in its free end area by means of a spherical roller bearing 13 is mounted.
- a drive motor 14 which has a spur gear Race 8 and thus the burning cone K in rotation on the axis O added.
- the coaxial is arranged to the firing cone K.
- Afterburner N has one frustoconical afterburner 15, which is in the direction of the firing cone K extends and the lower edge 16 one has a larger diameter than the free edge of the narrowing Section 3 of the firing cone K.
- the afterburning chamber 15 closes an air collection space 17, arranged in the radially adjustable guide vanes 18 are. By adjusting the guide vanes 18, the effective one Opening cross section of the air plenum 17 changeable.
- the Air collecting space 17 has an opening (not shown), through the upper air tangentially into the air collecting space 17 can be blown.
- a narrowed collar 19 with an outlet cross section 20 leaves free.
- the frustoconical wall 21 of the afterburning chamber 15 is from surrounded by a jacket 22 with the wall 21 one of coolant flowed through chamber and can be part of the housing G. Through this jacket 22 and the wall 21 extends Feed shaft 23, which is vertically above the opening of the firing cone K lies and the supply of fuel into the fuel cone K serves. Suitable closing flaps (not shown) arranged.
- the axis of the afterburning chamber 15 against the Axis of the firing cone K can be inclined, especially after above, but the edge 16 of the afterburning chamber 15 should be parallel to the opposite edge of the firing cone K, to avoid the uncontrolled escape of flame gases or at least to decrease.
- Fig. 2 shows a section through the conical section of the Brennkegels K. You can see the support arms 5, which are hollow are and are arranged at uniform angular intervals. The Reference numerals of the individual support arms 5 are here for later Provide an explanation of the operational sequence with suffixes a to 1. Between the support arms 5 there are the grate bars 4 made of heat-resistant Greetings, which are essentially T-shaped in cross-section, the wide leg of the T being the bearing surface for the fuel B forms while the protruding rib not only stiffening, but also dissipating heat.
- the Grate bars 4 have a mutual distance, which is chosen is that ash, but not too large pieces of fuel through the the space formed by the distance can fall through. The The distance is expediently of the order of 4 mm.
- Fig. 3 one of the support arms 5 is enlarged in cross section shown. It can be seen that the same from the hollow interior openings 26 inclined at the top in the from the firing cone K lead enclosed combustion chamber. Another opening 27 can open be formed on the opposite side. Their purpose is still explained.
- the firing cone K rotates about its axis O.
- This Orbital movement is shown in Fig. 2 with the arrow.
- the one in Fuel cone K located fuel B is thereby from the fuel cone entrained so that there is an inclined slope results, as Fig. 2 indicates.
- This embankment is in circulation around the Brennkegels K ever steeper and then collapses, resulting in The consequence is that the fuel B circulates continuously in the fuel cone becomes.
- the fuel B is ignited at the beginning of the combustion process by an ignition flame which is supplied by a lance (not shown). If the fuel B burns sufficiently, the combustion flame can be dispensed with. With constant circulation due to the movement of the fuel cone, the fuel B burns in the fuel cone K. Fuel can be added through the shaft 23 at the appropriate time. The metering of the fuel per unit of time is expediently carried out by monitoring the O 2 content contained in the combustion exhaust gases.
- the flame gases emanating from the firing cone K are replaced by the the negative pressure caused by the upstream flow into the afterburning chamber 15 sucked in, being intense with that there swirling headwind. Flammable components the flame gases are completely burned out. Ash particles are thrown out in the direction of the wall 21 and fall down at the edge 16 into the housing G.
- the support arms 5k, 5l and 5a to 5d in Fig. 2. This can be controlled in such a way that only those connecting pieces with Air supply can be supplied, which are arranged at the positions are who are currently taking the aforementioned arms.
- the support arm 5j Upon further rotation of the firing cone in Fig. 2 counterclockwise the support arm 5j then enters the combustion zone a while the support arm 5d leaves it. Then the later arrives Support arm 5i in the combustion zone, while the support arm 5c them leaves, etc.
- this weak supply serves one certain cooling, but mainly the prevention of particles penetrate through openings 26.
- the layer thickness of the fuel over the Combustion grate is different. For example, it is on Transition between the conical section 1 and the cylindrical Section 2 largest and near the center of the tapered Section 1, i.e. smallest at its smallest diameter.
- which is in the different Height of the support arms during the rotation of the firing cone resulting different coverage of the support arms can by appropriately throttling the downwind supply to the something higher connecting pieces are taken into account.
- the openings 26 and 27 in the support arms 5 are preferably so dimensioned that at full load the speed of the exiting from them Underwind between 20 and 60 m / s, preferably at 40 m / s lies.
- openings 27 in the support arms 5 serve to on the one hand blow out particles that have penetrated into the support arms 5, and on the other hand, which in the ash receiving room in Housing G particles that may have fallen are not completely burned out, to supply them with combustion air. Therefore, the openings 27 are on the outside of the firing cone K. formed in the support arms 5, expediently on the point at the lowest surface line of the Firing cone is lowest. In the example shown would be that in the area of the transition between the tapered section 1 and the cylindrical section 2 of the firing cone K.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Solid-Fuel Combustion (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combustion Of Fluid Fuel (AREA)
Abstract
Description
Die Erfindung bezieht sich auf ein Verfahren und eine Vorrichtung
zu Zuführung des Windes zur Verbrennung von stückigem
Brennstoff nach dem Oberbegriff des Anspruchs 1 bzw. 3. Verfahren
und Vorrichtung dieser Art sind aus dem Aufsatz "Die Entwicklung
des Brennkegels zur Abfallveraschung" des Erfinders in
der Zeitschrift "Brennstoff-Wärme-Kraft", 19 (1967), Nr. 10,
Seiten 469 bis 473 bekannt.The invention relates to a method and an apparatus
to feed the wind for the combustion of
Dieser Aufsatz beschreibt eine Verbrennungsanlage für die weitgehend selbsttätige, universale und preisgünstige Müllverbrennung für Kommunen und kleine und mittlere Industriebetriebe. Sie umfaßt einen Brennkegel, der um eine schrägstehende Achse rotiert, und eine Nachbrennkammer, die vertikal über der Öffnung des Brennkegels angeordnet ist. Der Brennkegel hat einen kegelstumpfförmigen Abschnitt, einen sich an dessen oben angeordneten größeren Durchmesser anschließenden zylindrischen Abschnitt und einen sich an dessen freies Ende anschließenden kegelstumpfförmigen Aufsatz, dessen kleiner Durchmesser das freie Ende des Brennkegels und dessen Öffnung bildet.This essay largely describes an incinerator for the automatic, universal and inexpensive waste incineration for municipalities and small and medium-sized industrial companies. she includes a firing cone that is about an inclined axis rotates, and an afterburner that is vertically above the opening the firing cone is arranged. The firing cone has a frustoconical shape Section, one located at the top larger diameter adjoining cylindrical section and a frustoconical one adjoining its free end Attachment whose small diameter is the free end of the Firing cone and its opening forms.
Der kegelstumpfförmige Abschnitt besteht aus sich radial/axial erstreckenden, in gegenseitigem Abstand verlaufenden Stäben, die von mehreren äußeren Umfangsringen unterschiedlicher Durchmesser gegenseitig abgestützt werden. Der kegelstumpfförmige Abschnitt des Brennkegels wird von unten vom Unterwind angeblasen, der die Zwischenräume zwischen den Stäben passieren muß, um das Brenngut zu erreichen, der in dem Brennkegel liegt und von diesem aufgrund seiner Umlaufbewegung umgewälzt wird. Der oberhalb der Öffnung des Brennkegelaufsatzes angeordnete Nachbrenner hat eine Nachbrennkammer, die sich im oberen Abschnitt nach oben kegelstumpfförmig verengt und dort mit einer Einrichtung versehen ist, die Oberwind tangential in die Nachbrennkammer einleitet, so daß sich in ihr eine turbulente Strömung ausbildet, die die aus dem Brennkegel austretenden Abgase aufnimmt und ausbrennt.The frustoconical section consists of itself radial / axial extending, mutually spaced bars, the of several outer circumferential rings of different diameters are mutually supported. The frustoconical section of the fuel cone is blown from below by the downwind, which is the Gaps between the bars must pass to the firing material to reach, which is in the firing cone and due to this its orbital movement is circulated. The one above the The afterburner arranged in the opening of the firing cone attachment has one Afterburning chamber which is frusto-conical in the upper section narrowed and provided with a facility there the upper wind leads tangentially into the afterburning chamber so that a turbulent flow forms in it, which the Exhaust gases emerging from the firing cone and burns out.
Für eine konkret angegebene Brennkegelkonstruktion mit einem größten Durchmesser von 1870 mm, einem kleinsten Durchmesser von 530 mm und einer Länge von 460 mm des kegelstumpfförmigen Abschnitts des Brennkegels, die gemäß dem zitierten Aufsatz für die Verbrennung von 1,2 bis 1,4 t/h Kommunalmüll bestimmt ist - der zum Zeitpunkt der Veröffentlichung des Aufsatzes in Deutschland einen Heizwert von etwa 1,7 bis 1,9 MWh/t hatte - errechnet sich eine Feuerungsleistung von 3,58 MW. Für die Erzielung größerer Leistungen wird wegen der mechanischen Schwierigkeiten, die sich mit einer Vergrößerung der Brennkegeldurchmesser ergeben, in dem Aufsatz eine Parallelschaltung mehrerer Anlagen der beschriebenen Art empfohlen.For a specific firing cone design with a largest diameter of 1870 mm, a smallest diameter of 530 mm and a length of 460 mm of the frustoconical Section of the fuel cone, which according to the article cited for the incineration of 1.2 to 1.4 t / h municipal waste is determined - the at the time of publication of the essay in Germany had a calorific value of around 1.7 to 1.9 MWh / t a combustion output of 3.58 MW. For achieving bigger ones Achievements is because of the mechanical difficulties which result from an increase in the diameter of the firing cone, in the article a parallel connection of several systems of the described type recommended.
Eine Brennkegel-Feuerungsanlage dieser Art ist. auch in US 3,599,581 A beschrieben.A firing cone firing system of this type is. also in US 3,599,581 A.
Aus EP 0 754 907 A2 ist ein Verfahren zum Beeinflussen der Verbrennung in einem Kessel mit Schüttelrost bekannt, bei dem die Zuführung von Primärluft und/oder Brennstoff während und kurz nach dem Schütteln des Rostes vermindert wird, um ein durch das Schütteln verursachtes plötzliches Ansteigen der Verbrennungsrate zu vermeiden. Ein plötzlicher Abfall des Sauerstoffgehalts im Abgas, der sonst auftreten würde, weil die Gesamtregelung der Brennstoffzufuhr zu langsam auf plötzliche Änderungen der Verbrennungsbedingungen reagiert, wird dadurch vermieden. Bei der dargestellten Feuerungsanlage wird die Primärluft von unten gegen den Rost geblasen und muß die Zwischenräume zwischen den Roststäben passieren, um zu dem auf dem Rost liegenden Brenngut zu gelangen, während Sekundärluft von oben auf das Brenngut geblasen wird, die durch Düsen zugeführt wird, die an wenigstens einer der Kesselwände angeordnet und gegen den Rost gerichtet sind. Die zugeführten Luftmengen werden abhängig vom Ergebnis laufender Messungen der Kesselzustandvariablen, des Luftüberschusses und der Wärmeabsorption bestimmt.EP 0 754 907 A2 describes a method for influencing combustion known in a boiler with shaking grate, in which the Supply of primary air and / or fuel during and briefly after shaking the grate is reduced to one by the Shaking causes the burn rate to increase suddenly to avoid. A sudden drop in oxygen levels in the exhaust gas, which would otherwise occur because of the overall control of the Fuel supply too slow due to sudden changes in combustion conditions is avoided. In the The combustion system shown is the primary air from below blown against the rust and the gaps between the Grate bars pass to the firing material lying on the grate to get to the firing material while secondary air from above is blown, which is fed through nozzles, which at least one of the boiler walls arranged and directed against the grate are. The air volumes supplied depend on the result ongoing measurements of the boiler state variables, the excess air and heat absorption.
Die GB 1,141,562 A beschreibt eine Haus- oder Industriemüllverbrennungsvorrichtung, bestehend aus einer liegenden, rotierenden Gittertrommel, die von axial verlaufenden Rohren und zirkular verlaufenden Ringen gebildet ist. Im Inneren der Trommel sind an den Rohren kleine Röhrchen angebracht, die radial in die Trommel vorstehen und mit dem Innenraum des Rohres verbunden sind, an dem sie jeweils angebracht sind. Die Röhrchen sind auf einer wendelförmig verlaufenden Linie angeordnet und durch Platten miteinander verbunden, um eine Förderschnecke für das Brenngut zu bilden, das durch einen stirnseitig an die Trommel angesetzten Zündbrenner gezündet werden kann. Die Rohre sind stirnseitig offen, um den Eintritt von Luft zu ermöglichen, die durch die Röhrchen in den Innenraum der Trommel entweichen kann. Die Trommel ist von einem doppelwandigem Mantel umgeben, dessen Außenwand oben offen ist. Unten im Bereich eines unter der Trommel befindlichen Aschekastens sind der Mantel und sein Innenraum vollständig offen.GB 1,141,562 A describes a domestic or industrial waste incinerator, consisting of a lying, rotating Grid drum made of axially extending and circular tubes trending rings is formed. Inside the drum are on small tubes attached to the tubes, which are radial into the drum protrude and are connected to the interior of the tube to which they are attached. The tubes are on one arranged helically and through plates connected to each other to form a screw conveyor for the firing material to form, which is attached to the drum by a front Pilot burner can be ignited. The tubes are on the face open to allow the entry of air through the Tubes can escape into the interior of the drum. The drum is surrounded by a double-walled jacket, the outer wall is open at the top. Below in the area of one under the drum Ash box are the jacket and its interior completely open.
Im Betrieb wird Luft von oben in den Innenraum des Mantels eingeleitet, die den Mantel durchströmt und dessen Wände kühlt, unten in den Aschekasten austritt und von dort aus von unten die Zwischenräume zwischen den Rohren der Trommel durchströmt und als Primärluft in den von der Trommel umschlossenen Brennraum gelangt. Im Brennraum ist durch ein äußeres Sauggebläse ein Unterdruck erzeugt, der diese Primärluft und die durch die Röhrchen und durch die Rohre hindurch zugeführte Sekundärluft, die zugleich die Rohre kühlt, ansaugt.In operation, air is introduced into the interior of the jacket from above, that flows through the coat and cools its walls, exits in the ash box at the bottom and from there the bottom Gaps between the tubes of the drum and as primary air in the combustion chamber enclosed by the drum arrives. An external suction fan in the combustion chamber Vacuum generated by this primary air and by the Tubes and secondary air supplied through the tubes, which at the same time cools the pipes, sucks them in.
Allen bekannte Verbrennungsanlagen der vorgenannten Art ist gemeinsam, daß bei ihnen der Unterwind aufwärts gegen die Unterseite des Verbrennungsrostes geblasen wird. Der Verbrennungsrost hat Öffnungen zwischen den ihn bildenden Roststäben bzw. -rohren, durch den der Unterwind jedoch nur zum kleinen Teil strömen kann, weil der auf dem Verbrennungsrost liegende Brennstoff diese Öffnungen teilweise versperrt. Der größere Teil des Unterwindes wird daher gewöhnlich seitlich und nach unten abgelenkt. Der auf dem Verbrennungsrost liegende Brennstoff erhält dadurch nicht genügend Verbrennungsluft.All known incinerators of the aforementioned type is common that with them the underwind upwards towards the bottom the combustion grate is blown. The combustion grate has openings between the grate bars or tubes forming it, through which the underwind flows only to a small extent can, because the fuel lying on the combustion grate these openings partially blocked. The greater part of the downwind is therefore usually deflected sideways and downwards. This gives the fuel lying on the combustion grate not enough combustion air.
Ein erheblicher Nachteil ist ferner, daß in dem in der vorgenannten Weise abgelenkten Unterwind mitgerissene gas- und staubförmige Brennstoffanteile enthalten sind, die brennen. Die dadurch entstehenden Flammstrahlen überhitzen und korrodieren das metallische Material des Verbrennungsrostes, insbesondere dessen aus radialen Tragarmen und zirkularen Ringen bestehende Tragstruktur. Mit steigendem Heizwert des Brennstoffs werden solche Überhitzungen und Korrosionen gravierender. A significant disadvantage is also that in the above Way deflected underwind entrained gas and it contains dusty fuel that burns. The the resulting flame rays overheat and corrode the metallic material of the combustion grate, in particular its consisting of radial arms and circular rings Supporting structure. As the heating value of the fuel increases such overheating and corrosion are more serious.
Zur Nachverbrennung der vom Verbrennungsrost aufsteigenden Flammgase ist es bekannt, diesen Oberluft zuzuführen. Bei bekannten Verfahren erfolgte dieses in der Weise, daß die Flammgasströmung die Oberluft von selbst ansaugte.For post-combustion of the ascending from the combustion grate Flame gases are known to supply this upper air. at known method, this was done in such a way that the flame gas flow the upper air sucked in by itself.
Nachteilig bei solchen Rostfeuerungen war ein noch immer unvollständiger Ausbrand des Brennstoffs, der sich in einem entsprechend hohen CO-Anteil in den Verbrennungsabgasen äußerte. Schließlich enthielten diese auch noch einen erheblichen Anteil mitgerissener Feststoffpartikel, insbesondere Flugasche, die eine Abscheidung mittels Filteranlagen und dgl. erforderlich machten. Rostfeuerungen der beschriebenen Art, insbesondere mit Drehkegeln, haben sich daher in der Praxis nicht durchsetzen können.A disadvantage of such grate furnaces was that they were still incomplete Burning out of the fuel, resulting in a corresponding expressed a high proportion of CO in the combustion exhaust gases. Finally, they also contained a significant proportion entrained solid particles, especially fly ash, the separation by means of filter systems and the like is required made. Grate firing of the type described, especially with Cones, therefore, have not become established in practice can.
Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren der im Oberbegriff des Anspruchs 1 umrissenen Art anzugeben, das eine für den vollständigen Ausbrand des Brennstoffs ausreichende Luftzuführung gewährleistet, eine Überhitzung des Verbrennungsrostes vermeidet und ohne Staubfilterung der Verbrennungsabgase auskommt. Außerdem soll eine zur Durchführung des Verfahrens geeignete Vorrichtung angegeben werden.The invention has for its object a method in The preamble of claim 1 to specify the outlined type sufficient for the complete burnout of the fuel Air supply ensures overheating of the combustion grate avoids and without dust filtering of the combustion exhaust gases gets along. In addition, one is said to carry out the procedure suitable device can be specified.
Diese Aufgabe wird hinsichtlich des Verfahrens durch die im Anspruch 1, hinsichtlich der Vorrichtung durch die im Anspruch 2 angegebenen Merkmale gelöst. Vorteilhafte Ausgestaltungen der Erfindung sind Gegenstand der Unteransprüche.This task is carried out with regard to the procedure by the Claim 1, with respect to the device by the in claim 2 specified features solved. Advantageous embodiments of the Invention are the subject of the dependent claims.
Die Erfindung erreicht den von ihr angestrebten Erfolg zum einen apparativ dadurch, daß die Tragarme des Verbrennungsrostes hohl ausgeführt und vom Unterwind durchströmt sind, wodurch sie gekühlt werden. Der Unterwind tritt zwangsweise an der Oberseite des Verbrennungsrostes, d.h. direkt am Brennstoff aus, so daß die Möglichkeit einer Ablenkung des Unterwindes unter den Verbrennungsrost stark vermindert ist.On the one hand, the invention achieves the desired success apparatus in that the support arms of the combustion grate are hollow are executed and flowed through by the downwind, making them be cooled. The downwind is forced on the top the combustion grate, i.e. directly on the fuel, so that the possibility of deflecting the underwind under the combustion grate is greatly reduced.
Zum anderen ist zur Erreichung des von der Erfindung angestrebten Ziels der Nachverbrennung der Flammgase, die von dem auf dem Verbrennungsrost brennenden Brennstoff ausgehen, besondere Aufmerksamkeit geschenkt. Gemäß der Erfindung wird den Flammgasen die Oberluft in Form einer Hochgeschwindigkeitsströmung zugeführt, die die Flammgase schraubenlinienförmig umgibt und sich in Richtung auf den Verbrennungsrost fortpflanzt, wobei sich der Durchmesser dieses Strömungswirbels vergrößert. Die Oberwindströmung beschreibt somit etwa den Mantel eines Kegelstumpfes, dessen größerer Durchmesser dem Verbrennungsrost zugewandt ist.On the other hand, to achieve what is sought by the invention The aim of the post-combustion of the flame gases generated by that on the Burn out burning rust burning fuel, special attention given. According to the invention, the flame gases the upper air is supplied in the form of a high-speed flow, which surrounds the flame gases helically and itself propagates towards the combustion grate, the Increased diameter of this vortex. The headwind current describes, for example, the surface of a truncated cone, whose larger diameter faces the combustion grate.
Der Oberwind wird am kleineren Durchmesser dieses Kegelstumpfes eingeblasen. Dadurch ergibt sich im Zentrum ein Unterdruck, der die Flammgase ansaugt. Zwischen dem Zentrum der in Richtung auf diesen Unterdruckpunkt strömenden Flammgasströmung und der diese umgebenden torusförmigen Oberwindströmung bildet sich eine Zone intensiver Turbulenz aus, wo die Flammgase mit dem Oberwind intensiv durchmischt werden. Diese Turbulenzzone ist außen von einer Kaltluftströmung frischen Oberwindes umgeben.The headwind is due to the smaller diameter of this truncated cone blown. This results in a negative pressure in the center, the sucks in the flame gases. Between the center of the towards this vacuum point flowing flame gas flow and this A zone is formed around the toroidal headwind current intense turbulence from where the flame gases with the headwind be mixed thoroughly. This zone of turbulence is outside of surrounded by a cold air flow of fresh head wind.
Der Oberwind wird mit einer Geschwindigkeit von 40 bis 100 m/s, bevorzugt 60 bis 80 m/s, zugeführt, die somit derart hoch ist, daß die dadurch auf die Partikel in den Flammgasen einwirkende Zentrifugalkraft die Partikel in die erwähnte Kaltluftströmung ausschleudert, wo sie soweit abgekühlt werden, daß sie trocken ausfallen. Auf diese Weise wird nicht nur die aus dem Nachbrenner austretende Abgasströmung ohne Einsatz von Filtern von Partikeln befreit, sondern ist auch eine Verschlackung der Verbrennungsanlage vermieden.The head wind is at a speed of 40 to 100 m / s, preferably 60 to 80 m / s, which is thus so high, that the thereby acting on the particles in the flame gases Centrifugal force the particles into the cold air flow mentioned ejected, where they are cooled so far that they dry fail. In this way, not only the afterburner becomes escaping exhaust gas flow without the use of filters of particles exempt, but is also a slagging of the incinerator avoided.
Tatsächlich ergibt sich eine so weitgehende Heißentstaubung der Flammgase, daß die aus dem Nachbrenner austretenden Abgase - z.B. bei Ausblasen ins Freie - für das Auge klar und optisch staubfrei erscheinen, was beim heutigen Stand der Heißentstaubungstechnik bislang als unmöglich angesehen worden ist.In fact, there is such a large amount of hot dedusting Flame gases that the exhaust gases emerging from the afterburner - e.g. when blowing out into the open - clear and visual to the eye appear dust-free, what with the current state of hot dedusting technology has so far been considered impossible.
Versuche mit Abfallholz in Form von Holzschnitzeln als Brennstoff haben gezeigt, daß die vorgenannten Ergebnisse mit einer Luftführung erreicht werden, bei der etwa 30 bis 40% der zur vollständigen Verbrennung des Brennstoffs erforderlichen Luftmenge als Unterwind zugeführt werden, während der notwendige Restanteil von 70 bis 60% der Luftmenge als Oberwind zugeführt wird. Man erkennt hieraus, daß der Nachverbrennung auch unter dem Gesichtspunkt der Brennstoffausnutzung eine wesentliche Bedeutung zukommt.Experiments with waste wood in the form of wood chips as fuel have shown that the above results with a Air flow can be achieved in which about 30 to 40% of the complete combustion of the fuel required air quantity be fed as a downwind while the necessary Remaining portion of 70 to 60% of the air volume supplied as head wind becomes. It can be seen from this that the afterburning also under an essential one from the point of view of fuel efficiency Importance.
Apparativ erreicht man die beschriebene Luftführung im Nachbrenner mit Hilfe einer kegelstumpfförmigen Nachbrennkammer, in die der Oberwind am dem Verbrennungsrost abgewandten Ende kleineren Durchmessers derselben über eine Einleitvorrichtung eingeblasen wird, die den Oberwind tangential zur Wand der Nachbrennkammer in diese einleitet, wo er sich unter einem Winkel schräg zur Achse der Nachbrennkammer in dieser ausbreitet. Bei der Einleitung des Oberwindes in die Nachbrennkammer kann diesem auch von vornherein durch Leiteinrichtungen eine Strömungsrichtung schräg zur Achse der Nachbrennkammer vermittelt werden. In terms of apparatus, the air duct described in the afterburner is achieved with the help of a truncated cone-shaped afterburner into which the upper wind at the smaller end facing away from the combustion grate The same diameter is blown in via an introducer which is the upper wind tangential to the wall of the afterburner leads into this, where it is inclined at an angle to the Axis of the afterburning chamber spreads out in this. At the introduction of the headwind into the afterburning chamber can also be from a flow direction obliquely from the outset by means of guide devices to the axis of the afterburning chamber.
Vorteilhafterweise wird im Betrieb nur denjenigen Tragarmen des Verbrennungsrostes Unterluft zugeführt, auf denen Brennstoff liegt, und vorzugsweise nach Maßgabe der Dicke der Brennstoffschicht. Die anderen, nicht von Brennstoff bedeckten Tragarme erhalten keine Luft. Man kann ihnen aber auch eine geringe Luftmenge zuführen, um das Eindringen korrodierender Brenngase und von Brennstoff- oder Aschepartikeln zu verhindern. Eine geringe Durchströmung der nicht von Brennstoff bedeckten Tragarme verbessert auch die Kühlung derselben.Advantageously, only those support arms of the Combustion grate fed under air on which fuel lies, and preferably in accordance with the thickness of the fuel layer. The other brackets not covered by fuel get no air. You can also give them a small amount of air lead to the penetration of corrosive fuel gases and to prevent fuel or ash particles. A minor one Flow through the support arms not covered by fuel improved also cooling them.
Gemäß einer Weiterbildung der Erfindung hat jeder hohle Tragarm wenigstens eine weitere Öffnung auf der dem Brennstoff abgewandten Seite, so daß durch den Verbrennungsrost hindurchgefallene Asche oder feine Brennstoffanteile im Aschenraum Verbrennungsluft erhalten, um vollständig auszubrennen. Durch diese Öffnungen können außerdem in die Rohre eingedrungene Brennstoff- oder Aschepartikel ausgeblasen werden.According to a development of the invention, each hollow support arm at least one further opening on the side facing away from the fuel Side so that it has fallen through the combustion grate Ash or fine amounts of fuel in the combustion air ashes get to burn out completely. Through these openings can also penetrate into the pipes fuel or Ash particles are blown out.
Vorteilhafterweise wird der Verbrennungsrost vom Mantel eines hohlen (Brenn-) Kegels gebildet, der eine Drehbewegung um eine schrägstehende Achse ausführt. Die Nachbrennkammer ist in diesem Falle am günstigsten koaxial zur Drehachse des Kegels angeordnet. Hierdurch werden die aus dem Brennkegel austretenden Flammgase besonders gut in das Zentrum des Nachbrenners geleitet, wo ein gegenüber dem im Brennkegel herrschenden Druck verminderter Druck herrscht, was die Überleitung der aus dem Brennkegel austretenden Flammgase in die Nachverbrennung begünstigt und ein unkontrolliertes Entweichen dieser Flammgase nach außen bzw. in ein die Verbrennungsanlage aus Brennkegel und Nachbrennkammer umschließendes Gehäuse verhindert. The combustion grate is advantageously covered by a jacket hollow (burning) cone, which rotates around a executes an inclined axis. The afterburner is in this Most conveniently arranged coaxially to the axis of rotation of the cone. As a result, the flame gases emerging from the firing cone particularly well directed to the center of the afterburner, where a reduced compared to the pressure prevailing in the firing cone Pressure prevails, which is the conduction of those emerging from the firing cone Flame gases favored in the post-combustion and one uncontrolled escape of these flame gases to the outside or in a the incinerator from the fuel cone and afterburner enclosing housing prevented.
Die koaxiale Anordnung der Nachbrennkammer dicht über dem Brennkegel hat ferner zur Folge, daß die Wärmestrahlung der in der Nachbrennkammer brennenden Flammgase auf den im Brennkegel befindlichen Brennstoff vorteilhaft einwirkt und den dort stattfindenden Verschwelungs- und Verbrennungsvorgang unterstützt.The coaxial arrangement of the afterburning chamber just above the firing cone also has the consequence that the heat radiation in the Afterburning chamber burning flame gases on the in the burning cone located fuel acts advantageously and the taking place there Smoldering and combustion process supported.
Dabei sollte zweckmäßigerweise der untere Durchmesser der Nachbrennkammer etwas größer als der Durchmesser des oberen Randes des Brennkegels sein. Dadurch wird der in der Nähe der Nachbrennkammerwand abwärts geblasene Staub aus der Nachbrennkammer am Brennkegel vorbei in den darunter befindlichen Ascheraum geblasen.The lower diameter of the afterburning chamber should expediently be used slightly larger than the diameter of the top edge of the fuel cone. This will close the afterburner wall downward blown dust from the afterburner past the firing cone into the ash room below blown.
Die Erfindung wird nachfolgend unter Bezugnahme auf in den
Zeichnungen dargestelltes Ausführungsbeispiel näher erläutert.
Es zeigt:
Fig. 1 zeigt eine vollständige Verbrennungsanlage, bestehend aus einem um eine schrägstehende Achse O rotierenden Brennkegel K und einem sich an das Austrittsende des Brennkegels K koaxial anschließenden Nachbrenner N, die von einem Gehäuse G umschlossen sind. Fig. 1 shows a complete incinerator consisting of a firing cone K rotating about an inclined axis O and one coaxial to the exit end of the firing cone K. subsequent afterburner N, which is enclosed by a housing G. are.
Der Brennkegel K weist einen kegelstumpfförmigen Abschnitt 1,
einen sich daran zum offenen Ende hin anschließenden zylindrischen
Abschnitt 2 und einen sich an diesen anschließenden, sich
im Durchmesser verengenden Abschnitt 3 auf. Der Verbrennungsrost
dieses Brennkegels K besteht aus Roststäben 4 aus warmfestem Guß
und aus hohlen, radialen Tragarmen 5 und Ringträgern (nicht dargestellt),
die die Tragarme 5 miteinander verbinden. Der Brennkegel
K ist an seinem Ende kleineren Durchmessers von mehreren
hohlen achsparallelen Beinen 6 gehalten, die mit einem Luftsammelkasten
7 verbunden sind, der radiale Zwischenwände aufweist,
die pro Tragarm 5 je eine Luftsammelkammer abschließen. Der
Luftsammelkasten 7 ist mit einem Laufring 8 fest verbunden, der
von mehreren stationär gelagerten Laufrollen (nicht dargestellt)
gelagert ist. Der Laufring 8 weist je eine Öffnung pro Tragarm 5
auf.The fuel cone K has a frustoconical section 1,
a cylindrical one adjoining it towards the open end
Section 2 and an adjoining one
Gegen die dem Brennkegel K abgewandte Seite des Laufrings 8 ist
von Federn ein Gleitring 9 gedrückt, der mehrere Anschlußstutzen
trägt, die über Schlauchleitungen 10 mit einer gemeinsamen Luftzuführkammer
11 verbunden sind. Die Anzahl der Anschlußstutzen
ist vorzugsweise ebenso groß wie die Anzahl der hohlen Tragarme
5.Against the side of the
Mit dem Laufring 8 ist eine Welle 12 starr verbunden, die sich
auf der dem Brennkegel K abgewandten Seite des Laufrings 8 von
diesem weg erstreckt und in ihrem freien Endbereich mittels
eines Pendelrollenlagers 13 gelagert ist. Man erkennt ferner
einen Antriebsmotor 14, der über eine Stirnverzahnung den
Laufring 8 und damit den Brennkegel K in Drehung am die Achse O
versetzt. With the
Im Abstand über dem Ende größeren Durchmessers des Brennkegels K
befindet sich der kegelstumpfförmige Nachbrenner N, der koaxial
zum Brennkegel K angeordnet ist. Der Nachbrenner N hat eine
kegelstumpfförmige Nachbrennkammer 15,die sich in Richtung auf
den Brennkegel K erweitert und deren unterer Rand 16 einen
größeren Durchmesser hat, als der freie Rand des sich verengenden
Abschnitts 3 des Brennkegels K. An das Ende kleineren Durchmessers
der Nachbrennkammer 15 schließt sich ein Luftsammelraum
17 an, in dem radial verstellbare Leitschaufeln 18 angeordnet
sind. Durch Verstellen der Leitschaufeln 18 ist der wirksame
Öffnungsquerschnitt des Luftsammelraums 17 veränderbar. Der
Luftsammelraum 17 weist eine Öffnung (nicht dargestellt) auf,
durch die hindurch Oberluft tangential in den Luftsammelraum 17
eingeblasen werden kann. Nach außen, also auf der der Nachbrennkammer
15 abgewandten Seite schließt sich an den Luftsammelraum
17 ein verengter Kragen 19 an, der einen Austrittsquerschnitt 20
frei läßt.At a distance above the end of the larger diameter of the firing cone K
is the truncated cone-shaped afterburner N, the coaxial
is arranged to the firing cone K. Afterburner N has one
Die kegelstumpfförmige Wand 21 der Nachbrennkammer 15 ist von
einem Mantel 22 umgeben, der mit der Wand 21 eine von Kühlmittel
durchströmte Kammer begrenzt und Teil des Gehäuses G sein kann.
Durch diesen Mantel 22 und die Wand 21 erstreckt sich ein
Zuführschacht 23, der vertikal über der Öffnung des Brennkegels
K liegt und der Zuführung von Brennstoff in den Brennkegel K
dient. In dem Schacht 23 sind geeignete Schließklappen (nicht
dargestellt) angeordnet.The
Man erkennt in Fig. 1 ferner im Gehäuse G unterhalb des Brennkegels
K eine Förderschneckenanordnung 24, die dem Transport von
sich im Gehäuse G ansammelnder Asche in einen Ascheauslaß 25
dient.It can also be seen in FIG. 1 in the housing G below the firing cone
K is a
Es sei angemerkt, daß die Achse der Nachbrennkammer 15 gegen die
Achse des Brennkegels K geneigt sein kann, insbesondere nach
oben, doch sollte dabei der Rand 16 der Nachbrennkammer 15 parallel
zum gegenüberstehenden Rand des Brennkegels K verbleiben,
um das unkontrollierte Austreten von Flammgasen zu vermeiden
oder wenigstens zu vermindern.It should be noted that the axis of the afterburning
Fig. 2 zeigt einen Schnitt durch den konischen Abschnitt des
Brennkegels K. Man erkennt die Tragarme 5, die hohl ausgebildet
sind und in gleichmäßigen Winkelabständen angeordnet sind. Die
Bezugszeichen der einzelnen Tragarme 5 sind hier zur späteren
Erläuterung des Betriebsablaufs mit Suffixen a bis 1 versehen.
Zwischen den Tragarmen 5 befinden sich die Roststäbe 4 aus warmfestem
Gruß, die im Querschnitt im wesentlichen T-förmig sind,
wobei der breite Schenkel des T die Auflagefläche für den Brennstoff
B bildet, während die davon hochstehende Rippe nicht nur
der Aussteifung, sondern auch der Abführung von Wärme dient. Die
Roststäbe 4 haben einen gegenseitigen Abstand, der so gewählt
ist, daß Asche, nicht aber zu große Brennstoffstücke durch den
vom Abstand gebildeten Zwischenraum hindurchfallen kann. Der
Abstand liegt zweckmäßigerweise in der Größenordnung von 4mm.Fig. 2 shows a section through the conical section of the
Brennkegels K. You can see the
In Fig. 3 ist einer der Tragarme 5 im Querschnitt vergrößert
dargestellt. Man erkennt, daß aus dem hohlen Innenraum desselben
oben schrägstehende Öffnungen 26 in den von dem Brennkegel K
umschlossenen Brennraum führen. Eine weitere Öffnung 27 kann auf
der entgegengesetzten Seite ausgebildet sein. Deren Zweck wird
noch erläutert. In Fig. 3 one of the
Im Betrieb läuft der Brennkegel K um seine Achse O um. Diese Umlaufbewegung ist in Fig. 2 mit dem Pfeil dargestellt. Der im Brennkegel K befindliche Brennstoff B wird dadurch vom Brennkegel mitgenommen, so daß sich eine schrägverlaufende Böschung ergibt, wie Fig. 2 andeutet. Diese Böschung wird beim Umlauf des Brennkegels K immer steiler und bricht dann zusammen, was zur Folge hat, daß der Brennstoff B im Brennkegel ständig umgewälzt wird.In operation, the firing cone K rotates about its axis O. This Orbital movement is shown in Fig. 2 with the arrow. The one in Fuel cone K located fuel B is thereby from the fuel cone entrained so that there is an inclined slope results, as Fig. 2 indicates. This embankment is in circulation around the Brennkegels K ever steeper and then collapses, resulting in The consequence is that the fuel B circulates continuously in the fuel cone becomes.
Der Brennstoff B wird zu Beginn des Verbrennungsvorgangs durch
eine Zündflamme, die von einer Lanze (nicht dargestellt) zugeführt
wird, gezündet. Wenn der Brennstoff B ausreichend brennt,
kann auf die Unterstützung der Verbrennung durch die Zündflamme
verzichtet werden. Unter ständiger Umwälzung aufgrund der
Brennkegelbewegung brennt der Brennstoff B im Brennkegel K ab.
Durch den Schacht 23 kann zum geeigneten Zeitpunkt Brennstoff
neu zugegeben werden. Die Dosierung des Brennstoffs pro Zeiteinheit
erfolgt zweckmäßigerweise durch Überwachung des in den Verbrennungsabgasen
enthaltenen O2-Anteils.The fuel B is ignited at the beginning of the combustion process by an ignition flame which is supplied by a lance (not shown). If the fuel B burns sufficiently, the combustion flame can be dispensed with. With constant circulation due to the movement of the fuel cone, the fuel B burns in the fuel cone K. Fuel can be added through the
Die vom Brennkegel K ausgehenden Flammgase werden durch den von
der Oberwindströmung hervorgerufenen Unterdruck in die Nachbrennkammer
15 hineingesaugt, wobei sie mit dem dort intensiv
wirbelnden Oberwind durchmischt werden. Noch brennbare Bestandteile
der Flammgase werden dadurch vollständig ausgebrannt.
Ascheteilchen werden in die Richtung der Wand 21 ausgeschleudert
und fallen am Rand 16 nach unten in das Gehäuse G.The flame gases emanating from the firing cone K are replaced by the
the negative pressure caused by the upstream flow into the afterburning
Für den Betrieb ist es zweckmäßig, wenn nur die in der Verbrennungszone
befindlichen Tragarme 5 mit Unterwind versorgt sind. For operation it is useful if only those in the combustion
Das sind in Fig. 2 die Tragarme 5k, 5lund 5a bis 5d. Dieses kann
in der Weise gesteuert werden, daß nur jene Anschlußstutzen mit
Unterluft versorgt werden, die an den Positionen angeordnet
sind, die augenblicklich die vorgenannten Tragarme einnehmen.
Bei weiterer Drehung des Brennkegels in Fig. 2 entgegen dem Uhrzeigersinn
tritt dann der Tragarm 5j in die Verbrennungszone
ein, während der Tragarm 5d sie verläßt. Später gelangt dann der
Tragarm 5i in die Verbrennungszone, während der Tragarm 5c sie
verläßt, usw.. Die übrigen, nicht in der Verbrennungszone
befindlichen Tragarme, das sind in der in Fig. 2 dargestellten
Situation die Tragarme 5d bis 5h, werden nicht oder nur schwach
mit Luft versorgt, beispielsweise über entsprechende Drosselstellen.
Diese schwache Versorgung dient einerseits einer
gewissen Kühlung, hauptsächlich aber der Verhinderung, daß Partikel
durch die Öffnungen 26 in sie eindringen.These are the support arms 5k, 5l and 5a to 5d in Fig. 2. This can
be controlled in such a way that only those connecting pieces with
Air supply can be supplied, which are arranged at the positions
are who are currently taking the aforementioned arms.
Upon further rotation of the firing cone in Fig. 2 counterclockwise
the support arm 5j then enters the combustion zone
a while the support arm 5d leaves it. Then the later arrives
Support arm 5i in the combustion zone, while the support arm 5c them
leaves, etc. The rest, not in the combustion zone
located support arms, that are shown in Fig. 2
Situation the support arms 5d to 5h, do not become weak or only
supplied with air, for example via appropriate throttling points.
On the one hand, this weak supply serves one
certain cooling, but mainly the prevention of particles
penetrate through
Durch die dargestellte Gestaltung und Anordnung des Brennkegels
K ergibt sich, daß die Schichtdicke des Brennstoffs über dem
Verbrennungsrost unterschiedlich ist. Sie ist beispielsweise am
Übergang zwischen dem kegeligen Abschnitt 1 und dem zylindrischen
Abschnitt 2 am größten und nahe dem Zentrum des kegeligen
Abschnitts 1, d.h. an dessen kleinsten Durchmesser am geringsten.
Um dem beim Verbrennungsvorgang Rechnung zu tragen, können
die Öffnungen 26, die längs jedes Tragarms 5 angeordnet sind, in
Durchmesser und/oder Längsverteilung derart ausgebildet sein,
daß die Summe der Öffnungsquerschnitte pro Längeneinheit jedes
Tragarms näherungsweise proportional der Schichtdicke der auf
der jeweiligen Längeneinheit des Tragarms liegenden
Brennstoffmenge ist. Der sich in den unterschiedlichen
Höhenlagen der Tragarme während des Umlaufs des Brennkegels
ergebende unterschiedliche Bedeckungsgrad der Tragarme kann
durch entsprechende Drosselung der Unterwindzufuhr an den etwas
höher gelegenen Anschlußstutzen berücksichtigt werden.Through the design and arrangement of the firing cone shown
K shows that the layer thickness of the fuel over the
Combustion grate is different. For example, it is on
Transition between the conical section 1 and the cylindrical
Section 2 largest and near the center of the tapered
Section 1, i.e. smallest at its smallest diameter.
To take this into account during the combustion process, you can
the
Vorzugsweise sind die Öffnungen 26 und 27 in den Tragarmen 5 so
bemessen, daß bei Vollast die Geschwindigkeit des aus ihnen austretenden
Unterwindes zwischen 20 und 60 m/s, bevorzugt bei 40
m/s liegt.The
Die letztgenannten Öffnungen 27 in den Tragarmen 5 dienen dazu,
einerseits etwa in die Tragarme 5 eingedrungene Partikel auszublasen,
und andererseits, die in den Ascheaufnahmeraum im
Gehäuse G hineingefallenen Partikel, die möglicherweise noch
nicht vollständig ausgebrannt sind, mit Brennluft zu versorgen.
Daher sind die Öffnungen 27 auf der Außenseite des Brennkegel K
in den Tragarmen 5 ausgebildet, und zwar zweckmäßigerweise an
derjenigen Stelle, die bei der tiefstliegenden Mantellinie des
Brennkegels am tiefsten liegt. Im dargestellten Beispiel wäre
das im Bereich des Überganges zwischen dem kegeligen Abschnitt 1
und dem zylindrischen Abschnitt 2 des Brennkegels K.The
Claims (8)
- A method of supplying a blast for the combustion of a particulate fuel resting on a surface of a rotational-symmetrical combustion grate comprising a surface portion located in a combustion zone and covered by the fuel and a surface portion not covered by the fuel, said grate performing a rotary movement around its axis, causing a rolling movement of the fuel across the entire surface of the combustion grate, wherein a blast is supplied to the fuel in the combustion zone from below (under blast), and flame gases emerging from the combustion zone are mixed at a distance to the combustion zone with an overfire air, which is routed in a rotating flow in a helically extending path having an expaning diameter and enclosing the flame gases emerging from the combustion zone, towards the combustion zone,
characterized in that
the under blast is blown above the combustion grate below the fuel, and
the overfire air is supplied in a path surrounding the rotational axis of the combustion grate at a speed of 40 to 100 m/s,
wherein for the complete combustion of waste wood, in particular wood chips, as the fuel to be burnt, an air quantity proportion supplied along with the under blast is approximately 30 to 40 % and an air quantity proportion supplied with the overfire air is approximately 70 to 60%. - The method as claimed in claim 1, characterized in that the under blast is supplied to the fuel resting on the combustion grate at a speed of 20 to 60 m/s.
- An apparatus for carrying out the method as set forth in one of claims 1 and 2, comprising
a movable, rotational-symmetrical combustion grate (K) having partially radially extending arms (4,5), a combustion zone covering a partial region of the combustion grate (K), and a drive means (14) which sets the combustion grate (K) into a rotary movement around its axis (O), said rotary movement successively routing all partial regions of the combustion grate (K) through the combustion zone,
an air source which supplies an under blast to the combustion zone,
and an afterburner chamber (N) arranged above the combustion grate (K) and receiving the flame gases rising from the combustion grate (K) and mixing said flame gases with combustion air freshly supplied as overfire air and burning them out,
characterized in that
some of the arms of the combustion grate are hollow supporting arms (5) regularly distributed over the combustion grate (K) and each comprising a plurality of blow openings (26) disposed at the surface of the combustion grate (K) bearing the fuel and directed towards said fuel,
a movable coupling means (7,8) is provided through which the air source is pneumatically connected at least to the supporting arms located in the combustion zone for supplying under blast, and
the afterburner chamber (15) is formed rotational-symmetrical and is arranged coaxial with respect to the combustion grate (K). - The apparatus as set forth in claim 3, in which the hollow supporting arms (5) not located in the combustion zone are pneumatically connected to the air source via a throttling means.
- The apparatus as set forth in one of claims 3 and 4, in which the blow openings (26) directed against the fuel are distributed at the hollow supporting arms (5) and are dimensioned in a manner that the sum of the opening cross sections per length unit of each supporting arm (5) is approximately proportional to the nominal layer thickness of the fuel quantity resting on the respective length section of the supporting arm (5).
- The apparatus as set forth in one of claims 3 to 5, in which the combustion grate is a shell of a truncated cone (K) which comprises an axis of rotation (O) extending obliquely with respect to a horizontal, and in which the supporting arms (5) extend radially, characterized in that at least one blow opening (27) directed away from the fuel supporting surface of the combustion grate is formed at a position of each supporting arm (5) that is located the deepest when the shell line, in which the supporting arm is located, takes a lowermost position during the rotation of the truncated cone (K).
- The apparatus as set forth in claim 6, characterized in that a rotationally-symmetrically formed afterburner chamber (N) confronts the opening of the cone (K) at the base thereof as an afterburner chamber (15), which has an inlet opening (16) facing the cone (K) which has a diameter larger than the opening of the cone (K), and which comprises means (17,18) for tangentially supplying an overfire air disposed in the area of the outlet end distal to the cone (K), and wherein a collar (19) is connected to this means (17,18) in the direction towards the outlet end, said collar encompassing an opening that has a smaller diameter than the smallest cross section of the afterburner chamber (15).
- The apparatus as set forth in claim 7, characterized in that said means (17,18) for tangentially supplying the overfire air has a variable opening cross section.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19817121A DE19817121A1 (en) | 1998-04-17 | 1998-04-17 | Method and device for feeding the wind for the combustion of lumpy fuel |
DE19817121 | 1998-04-17 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0952398A2 EP0952398A2 (en) | 1999-10-27 |
EP0952398A3 EP0952398A3 (en) | 2000-03-08 |
EP0952398B1 true EP0952398B1 (en) | 2003-08-20 |
Family
ID=7864880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP99107650A Expired - Lifetime EP0952398B1 (en) | 1998-04-17 | 1999-04-16 | Air supply method and device for burning particulate fuel |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0952398B1 (en) |
AT (1) | ATE247800T1 (en) |
DE (2) | DE19817121A1 (en) |
DK (1) | DK0952398T3 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10160415A1 (en) | 2001-12-10 | 2003-06-18 | Fritz Schoppe | Solid fuel incinerator and method for supplying air to it |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1327662A (en) * | 1962-07-04 | 1963-05-17 | Device for burning lean coals or other applications | |
FR1487371A (en) * | 1966-05-09 | 1967-07-07 | Gen Thermique | Household or industrial waste incinerator |
US3599581A (en) * | 1969-05-20 | 1971-08-17 | Fritz Schoppe | Incinerator |
AT402965B (en) * | 1993-09-02 | 1997-10-27 | List Guenther Ing | AFTERBURNING DEVICE FOR A FAN BOILER OR COOKER |
EP0741267B1 (en) * | 1995-05-05 | 2001-08-01 | BBP Environment GmbH | Method and furnace for incinerating waste |
DK172248B1 (en) * | 1995-07-18 | 1998-02-02 | Burmeister & Wains Energi | Method of controlling combustion in a boiler with a vibration grate |
-
1998
- 1998-04-17 DE DE19817121A patent/DE19817121A1/en not_active Withdrawn
-
1999
- 1999-04-16 AT AT99107650T patent/ATE247800T1/en not_active IP Right Cessation
- 1999-04-16 DK DK99107650T patent/DK0952398T3/en active
- 1999-04-16 EP EP99107650A patent/EP0952398B1/en not_active Expired - Lifetime
- 1999-04-16 DE DE59906632T patent/DE59906632D1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE59906632D1 (en) | 2003-09-25 |
EP0952398A3 (en) | 2000-03-08 |
DE19817121A1 (en) | 1999-10-21 |
DK0952398T3 (en) | 2003-12-15 |
ATE247800T1 (en) | 2003-09-15 |
EP0952398A2 (en) | 1999-10-27 |
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