US20150300638A1 - Device for Centrifugal Combustion by Area Using Flow of Combustion Air - Google Patents

Device for Centrifugal Combustion by Area Using Flow of Combustion Air Download PDF

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Publication number
US20150300638A1
US20150300638A1 US14/442,839 US201314442839A US2015300638A1 US 20150300638 A1 US20150300638 A1 US 20150300638A1 US 201314442839 A US201314442839 A US 201314442839A US 2015300638 A1 US2015300638 A1 US 2015300638A1
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Prior art keywords
combustion
combustion chamber
air
ash
fuel
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Abandoned
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US14/442,839
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English (en)
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Jiwon Kim
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Posco Holdings Inc
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Individual
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Abandoned legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/24—Incineration of waste; Incinerator constructions; Details, accessories or control therefor having a vertical, substantially cylindrical, combustion chamber
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B90/00—Combustion methods not related to a particular type of apparatus
    • F23B90/04—Combustion methods not related to a particular type of apparatus including secondary combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B10/00—Combustion apparatus characterised by the combination of two or more combustion chambers
    • F23B10/02—Combustion apparatus characterised by the combination of two or more combustion chambers including separate secondary combustion chambers
    • 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
    • F23B1/30—Combustion apparatus using only lump fuel characterised by the form of combustion chamber
    • F23B1/32—Combustion apparatus using only lump fuel characterised by the form of combustion chamber rotating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B40/00—Combustion apparatus with driven means for feeding fuel into the combustion chamber
    • F23B40/04—Combustion apparatus with driven means for feeding fuel into the combustion chamber the fuel being fed from below through an opening in the fuel-supporting surface
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23B—METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B80/00—Combustion apparatus characterised by means creating a distinct flow path for flue gases or for non-combusted gases given off by the fuel
    • 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
    • F23G5/32—Incineration of waste; Incinerator constructions; Details, accessories or control therefor the waste being subjected to a whirling movement, e.g. cyclonic incinerators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J1/00—Removing ash, clinker, or slag from combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J1/00—Removing ash, clinker, or slag from combustion chambers
    • F23J1/02—Apparatus for removing ash, clinker, or slag from ash-pits, e.g. by employing trucks or conveyors, by employing suction devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J1/00—Removing ash, clinker, or slag from combustion chambers
    • F23J1/06—Mechanically-operated devices, e.g. clinker pushers
    • 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 
    • 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
    • F23L15/00—Heating of air supplied for combustion
    • 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
    • F23L15/00—Heating of air supplied for combustion
    • F23L15/04—Arrangements of recuperators
    • 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
    • F23L3/00—Arrangements of valves or dampers before the fire
    • 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 
    • F23L9/04—Passages or apertures for delivering secondary air for completing combustion of fuel  by discharging the air beyond the fire, i.e. nearer the smoke outlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, 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
    • F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
    • F23M9/02—Baffles or deflectors for air or combustion products; Flame shields in air inlets
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Definitions

  • the present invention relates to an area-specific centrifugal combustion apparatus using a flow of combustion air. More particularly, the present invention relates to an area-specific centrifugal combustion apparatus using a flow of combustion air able to perfectly burn low grade fuel containing impurities like refined fuel by centrifugally dividing a space using a strong air curtain rather than using a refractory wall.
  • the area-specific centrifugal combustion apparatus it is possible to completely divide a fuel input area, a combustion air preheating area, an ignition and combustion area, a separation and discharge area for airborne ash and nonflammable matter, and a combustion heat and gas discharge area from each other by adjusting a rate at which combustion air is input, such that perfect combustion can continuously proceed, and after the combustion, combustion heat-containing gases are discharged after being completely separated from airborne ash without contaminating heat-using facilities, thereby improving heat efficiency.
  • a flammable substance is input into a combustion chamber of a combustion furnace and is subsequently ignited using an ignition burner, and combustion air is blown into the combustion chamber in the linear direction from respective upper, middle, and lower sides of the combustion furnace, such that the flammable substance burns with the combustion air.
  • a combustion furnace for high-temperature flammable matter cannot realize high-temperature combustion without expensive construction costs or intensive labor.
  • a burner specially fabricated for use in a high-speed and high-temperature environment is disposed, high-pressure oxygen is injected, and the furnace wall is formed of refractory bricks.
  • the combustion chamber formed of a metal material suffers from corrosion since it cannot withstand a high-temperature environment. This consequently reduces the lifespan of the combustion chamber.
  • some structures such as a stoker having a shaft tunnel, a fluidized bed incinerator, a cyclone incinerator, and a rotary kiln incinerator, cannot obtain perfect combustion without a refractory wall that stores heat.
  • clinker is inevitably produced, thereby restricting continuous operation or lowering heat efficiency.
  • a centrifugal combustion method blocks heat using a flow of combustion air without the refractory wall, continuous operation is restricted due to various phenomena, such as the production of clinker.
  • FIG. 1 is a view illustrating a combustion apparatus of the related art.
  • a flange 2 protrudes outward from the lower end of a first combustion chamber 1 .
  • An upper outer tank 3 and a lower outer tank 4 are fixed to the upper surface and the lower surface of the circumference of the flange 2 .
  • a fuel tank 6 is disposed below the first combustion chamber 1 such that the upper surface of the fuel tank 6 is in close contact with the lower surface of the flange 2 of the first combustion chamber 1 .
  • the fuel tank 6 is opened upward, and a hydraulic jack 5 is coupled with the lower portion of the fuel tank 6 .
  • a flange 9 is fixedly disposed on the upper surface of the upper outer tank 3 , and protrudes outward from the lower end of a second combustion chamber 8 having an exhaust tank 7 on the upper portion thereof.
  • One or a plurality of air blowers 11 is disposed on air supply pipes 10 connected to the lower portions of the upper outer tank 3 in the tangential direction of the air blowers 11 such that the air blowers 11 communicate with air inlet pipes 12 and air connecting pipes 13 connected to the upper portions of the lower outer tank 4 .
  • a plurality of air regulating devices 16 is disposed on the upper portions of the upper outer tank 3 .
  • Each of the air regulating devices 16 includes an air regulator plate 14 positioned above the space between the first combustion chamber 1 and the upper outer tank 3 and a regulator rod 15 with which the air regulator plate 14 is fixedly and rotatably coupled.
  • an object of the present invention is to perfectly burn low grade fuel containing impurities like refined fuel by centrifugally dividing a space using a strong air curtain without a refractory wall. It is possible to completely divide a fuel input area, a combustion air preheating area, an ignition and combustion area, a separation and discharge area for airborne ash and nonflammable matter, and a combustion heat and gas discharge area from each other by adjusting a rate at which combustion air is input, such that perfect combustion can continuously proceed.
  • Another object of the present invention is to separate combustion heat-containing gas from ash, clinker, and airborne ash within the combustion chamber after the combustion, such that clean combustion heat and gas are introduced into heat-using facilities, whereby pollution is prevented and heat efficiency is maximized.
  • a further object of the present invention is to burn only flammable matter while floating nonflammable matter by preheating combustion air to an ignition temperature or higher and using the negative pressure of an ignition chamber, even in the case of using low grade fuel, such that airborne ash is perfectly separated and discharged due to centrifugation using high-speed rotation, thereby preventing clinker.
  • the present invention provides an area-specific centrifugal combustion apparatus using a flow of combustion air including: an upper combustion chamber through which combustion air is supplied to a combustion chamber, and from which a column of fire produced through perfect combustion using the combustion air is discharged; a lower combustion chamber coupled with a lower part of the upper combustion chamber, wherein fuel is supplied to the lower combustion chamber, and the lower combustion chamber supplies the fuel into the combustion chamber such that the fuel mixes with the combustion air for perfect combustion; an air supply pipe having one end divided into an upper supply pipe and a lower supply pipe, the upper supply pipe diverging upward and the lower supply pipe diverging downward, through which the combustion air is supplied to the upper combustion chamber and the lower combustion chamber; a rotary part connected to the lower combustion chamber, wherein the rotary part allows the combustion air to maintain centrifugal force when ignition proceeds in the lower combustion chamber; a fuel supply provided on a lower end of the rotary part, the fuel supply comprising a fixed quantity feeder allowing the fuel to be supplied in a fixed amount to the lower
  • the upper combustion chamber may include: an upper combustion chamber outer tank having a combustion gas discharge panel through which the column of fire is discharged, wherein the upper combustion chamber outer tank is connected to the upper supply pipe such that the combustion air that has been supplied upwardly is able to flow; a redirecting part disposed on an upper end of the upper combustion chamber outer tank, the redirecting part allowing the combustion air to flow downwardly; and an upper combustion chamber inner tank disposed at a predetermined distance from an inner circumference of the upper combustion chamber outer tank to form an upper air supply, the upper supply pipe being fixed to the upper combustion chamber inner tank in a communicating manner.
  • the lower combustion chamber may be connected to a lower end of the upper combustion chamber.
  • the lower combustion chamber may include: a lower combustion chamber outer tank, with a lower end thereof being connected to the rotary part, wherein the lower combustion chamber outer tank is connected to the lower supply pipe, causing the combustion air supplied thereto to flow downwardly; and a lower combustion chamber inner tank disposed inside the lower combustion chamber outer tank to form a lower air supply, the lower supply pipe being fixed to the lower combustion chamber inner tank in a communicating manner.
  • the area-specific centrifugal combustion apparatus may further include a regulating damper disposed at a diverging point of the air supply pipe, the regulating damper being able to regulate a temperature of air and an amount of air supplied.
  • the rotary part may include: a rotary housing connected to a lower portion of the lower combustion chamber, the rotary housing being coupled with props that fix the combustion apparatus to a ground surface; a rotary body disposed within the rotary housing, wherein the rotary body rotates forward and backward to allow the combustion air preheated while moving downward to maintain centrifugal force; and an ash treatment chamber disposed between the rotary housing and the rotary body, wherein the ash treatment chamber traps the ash, the clinker, and the airborne ash produced after perfect combustion.
  • the rotary body may include: a rotary shaft connected to a driving motor such that rotary shaft is rotatably coupled with the rotary housing, thereby providing rotating force; a guide rail connected to the rotary shaft, wherein the guide rail guides a range of rotation of the rotary body; a bearing body supporting rotation of the rotary shaft and the guide rail; crushing blades disposed on a lower portion of the rotary body, wherein the crushing blades crush the ash, the clinker, and the airborne ash produced after completion of combustion; and an opening/closing door allowing the ash, the clinker, and the airborne ash crushed by the crushing blades to be introduced to the ash treatment chamber.
  • the area-specific centrifugal combustion apparatus may further include a bidirectional-functional discharge scraper discharging the debris, the ash, and the clinker collected in the ash chamber to an ash container.
  • the fuel supply may include a fuel input cone, wherein an upper portion of the fuel input cone is in a funnel shape such that a fixed amount of fuel uniformly spreads in a hemispherical shape.
  • the present invention it is possible to perfectly burn low grade fuel containing impurities like refined fuel by centrifugally dividing a space using a strong air curtain without a refractory wall. Specifically, it is possible to completely divide a fuel input area, a combustion air preheating area, an ignition and combustion area, a separation and discharge area for airborne ash and nonflammable matter, and a combustion heat and gas discharge area from each other by adjusting a rate at which combustion air is input, such that perfect combustion can continuously proceed.
  • FIG. 1 is a view illustrating a combustion apparatus of the related art
  • FIGS. 2 and 3 are views illustrating an area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention
  • FIGS. 4 and 5 are enlarged views of the key parts illustrating the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention
  • FIGS. 6 to 13 are cross-sectional views taken along lines A-A′ to H-H′ illustrating the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention.
  • FIG. 14 is a view illustrating the operation state of the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention.
  • FIGS. 2 and 3 are views illustrating an area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention
  • FIGS. 4 and 5 are enlarged views of the key parts illustrating the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention
  • FIGS. 6 to 13 are cross-sectional views taken along A-A′ and H-H′ illustrating the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention
  • FIG. 14 is a view illustrating the operation state of the area-specific centrifugal combustion apparatus using a flow of combustion air according to an exemplary embodiment of the invention.
  • the area-specific centrifugal combustion apparatus includes an upper combustion chamber 310 , a lower combustion chamber 210 , a rotary part 410 , a fuel supply 510 , and an ash treatment chamber 420 .
  • Combustion air is rotated by a centrifugal force within the upper combustion chamber 310 , and a column of fire produced through perfect combustion with the combustion air is discharged from the upper combustion chamber 310 .
  • the lower combustion chamber 210 is coupled with the lower part of the upper combustion chamber 310 .
  • the lower combustion chamber 210 is configured such that fuel supplied to the lower combustion chamber 210 mixes with the combustion air for perfect combustion.
  • the rotary part 410 is connected to the lower combustion chamber 210 , and regulates the combustion air to maintain centrifugal force when ignition proceeds in the lower combustion chamber 210 .
  • the fuel supply 510 supplies the fuel to the lower combustion chamber 210 .
  • the ash treatment chamber 420 traps and treats ash, clinker, airborne ash, and the like produced through incineration of the fuel during the combustion.
  • the upper combustion chamber 310 includes an upper combustion chamber outer tank 318 , upper combustion chamber inner tank 316 , a combustion gas discharge panel 314 , and a coupling flange 320 .
  • the upper combustion chamber outer tank 318 is a component forming the outer shape of the area-specific centrifugal combustion apparatus.
  • the upper combustion chamber outer tank 318 is in a cylindrical shape opened in the top-bottom direction, and is configured to prevent combustion air supplied thereto from leaking.
  • the upper combustion chamber outer tank 318 having this configuration is connected to an upper air supply pipe 332 of an air supply pipe 330 through which the combustion air is supplied to the upper combustion chamber outer tank 318 .
  • the upper combustion chamber outer tank 318 allows the combustion air to flow upwardly.
  • the upper combustion chamber outer tank 318 having this configuration has a combustion gas discharge panel 314 on the upper end through which the column of fire produced through the perfect combustion can be discharged.
  • a gas discharge port 312 through which the column of fire is vertically discharged is formed in the center of the combustion gas discharge panel 314 .
  • a redirecting part 350 is provided on the upper end of the upper combustion chamber outer tank 318 .
  • the redirecting part 350 allows the combustion air supplied into the combustion chamber through an upper air supply 338 to flow downwardly.
  • the upper combustion chamber inner tank 316 is in a cylindrical shape, and is disposed at a predetermined distance from the inner circumference of the upper combustion chamber outer tank 318 .
  • the coupling flange 320 is provided on the lower end of the upper combustion chamber inner tank 316 .
  • the coupling flange 320 is coupled with the upper combustion chamber outer tank 318 , and allows the upper air supply pipe 332 of the air supply pipe 330 to be fixed in a communicating manner.
  • the air supply pipe 330 is configured such that one end thereof is divided into an upper supply pipe 332 diverging upward and a lower supply pipe 334 diverging downward, whereby the combustion air can be supplied to the upper combustion chamber 310 and the lower combustion chamber 210 .
  • a regulating damper 336 is provided at the diverging point of the air supply pipe 330 .
  • the damper 336 can regulate the temperature of the air and the amount of the air supplied.
  • the upper air supply 338 is disposed between the inner circumference of the upper combustion chamber outer tank 318 and the outer circumference of the upper combustion chamber inner tank 316 , such that the combustion air is supplied to and flows upwardly through the upper air supply 338 .
  • the lower combustion chamber 210 is a component connected to the lower end of the upper combustion chamber 310 .
  • the lower combustion chamber 210 is connected to the lower supply pipe 334 of the air supply pipe 330 such that the combustion air is supplied to the combustion chamber through the lower combustion chamber.
  • the lower combustion chamber 210 includes a lower combustion chamber outer tank 218 and a lower combustion chamber inner tank 216 .
  • a connecting flange 220 is provided on the lower end of the lower combustion chamber outer tank 218 such that the connecting flange is integrally connected to the rotary part 410 .
  • the lower combustion chamber inner tank 216 is disposed inside the lower combustion chamber outer tank 218 , thereby forming a lower air supply 238 .
  • the combustion air flows upwardly while rotating in the upper air supply 338 at a velocity with respect to the input pressure.
  • the combustion air collides against the redirecting part 350 , the direction of the combustion air is changed, and the combustion air flows downwardly toward the lower combustion chamber 210 .
  • the downwardly-flowing combustion chamber is preheated to a predetermined temperature.
  • the combustion air input into the lower air supply 238 of the lower combustion chamber 210 also flows downwardly while rotating within the lower air supply 238 at a velocity with respect to the input pressure.
  • the combustion air mixes with the above-described preheated combustion air flowing downwardly from the upper combustion chamber 310 .
  • the temperature of the air preheated in the upper combustion chamber 310 is adjusted using the combustion air supplied through the lower combustion chamber 210 .
  • the temperature of the preheated air can be adjusted in response to the operation of the regulating damper 336 .
  • the mixed combustion air rotates and flows to the rotary part 410 disposed in the lower part of the lower combustion chamber 210 .
  • the combustion air collides against a bottom plate 441 of the combustion chamber, moves upward while rotating, and completely mixes with the fuel.
  • the rotary part 410 includes a rotary housing 412 , the rotary body 440 , and an ash treatment chamber 420 .
  • the rotary housing 412 is connected to the lower portion of the lower combustion chamber 210 .
  • Props 102 fixing the combustion apparatus to the ground are coupled to the rotary housing 412 .
  • the rotary body 440 is disposed within the rotary housing 412 .
  • When the fuel is burning the rotary body 440 rotates in a predetermined direction within the rotary housing 412 , and imparts centrifugal force to the combustion air preheated while moving downward from the upper combustion chamber 310 and the lower combustion chamber 210 .
  • the ash treatment chamber 420 is disposed between the rotary housing 412 and the rotary body 440 , and traps ash, clinker, airborne ash, and the like produced after perfect combustion.
  • the rotary body 440 has a power transmission means by which the rotary body is rotatably coupled with the rotary housing 412 .
  • the power transmission means includes a rotary shaft 446 connected to a driving motor, such as a motor, to provide rotating force, a guide rail 444 with one end being connected to the rotary shaft 446 , the guide rail 444 guiding the rotary body 440 to reliably rotate based on the rotating force of the rotary shaft 446 , and a bearing body 442 supporting the rotation of the rotary shaft 446 and the guide rail 444 .
  • Crushing blades 470 are disposed on the lower portion of the rotary body 440 .
  • the crushing blades 470 crush ash, clinker, airborne ash, and the like produced after the completion of combustion.
  • An opening/closing door 430 allows the ash, clinker, airborne ash, and the like crushed by the crushing blades 470 to be introduced to the ash treatment chamber 420 therethrough.
  • the opening/closing door 430 is configured such that the opening/closing door automatically opens and closes depending on the direction of rotation of the rotary body 440 .
  • ash and clinker are discharged by centrifugation through the bottom plate 441 of the combustion chamber formed on the lower inner circumference of the rotary body 440 , and the fuel pushed by the crushing blades 470 is collected at the center.
  • the rotary body 440 rotates in the backward direction, the ash, the clinker, and the like are pushed outward by the crushing blades 470 and are introduced into the ash treatment chamber 420 as the automatic opening/closing door 430 is opened.
  • a discharge scraper 450 allows the impurities to be continuously discharged from the combustion chamber. When the trapped impurities are accumulated in a predetermined amount, the discharge scraper 450 continuously discharges the impurities through an ash outlet port 421 to an ash container 106 .
  • a machine room protector plate 413 is provided within the ash treatment chamber 420 .
  • the machine room protector plate 413 prevents the trapped impurities from reentering the combustion chamber.
  • the fuel supply 510 is disposed such that a predetermined space is defined between the fuel supply 510 and the rotary housing 412 of the rotary part 410 .
  • the fuel supply 510 has a fixed quantity feeder 530 , whereby a fixed amount of fuel can be supplied.
  • the fuel supply 510 has a fuel input cone 512 .
  • the upper portion of the fuel input cone 512 is in a funnel shape such that a fixed amount of fuel can uniformly spread in a hemispherical shape.
  • the outer circumference of the upper end of the fuel input cone 512 is positioned at the bottom, flush with an ash discharge port 460 . This allows the supplied fuel to mix with the preheated air without leakage, whereby perfect combustion is enabled.
  • the combustion air preheated through the upper combustion chamber 310 and the lower combustion chamber 210 flows downwardly while rotating along the inner circumference of the rotary part 410 , is redirected upward after colliding against the bottom plate 441 , and mixes with the fuel spreading in the hemispherical shape from the fuel supply 510 , thereby forming a first combustion area.
  • the combustion air that has moved downwardly to the middle portion mixes with the first combustion area, thereby forming a second combustion area.
  • the combustion air enters the gas discharge port 312 and mixes with the remaining combustion air supplied from the upper combustion chamber 310 , thereby forming a third combustion area.
  • the combustion apparatus forms the first to third combustion areas, whereby fuel can perfectly burn. Centrifugal force is maintained by removing or reducing obstacles against rotating force in response to the rotation of the rotary part 410 . A flame occurring during the combustion forms a column of fire, which is discharged through the gas discharge port 312 .
  • combustion heat-containing gas and nonflammable debris separated from the combustion air are separated from each other, thereby making the outer surface of the air supply clean.
  • the combustion heat-containing gas and the nonflammable debris are sucked into a column of fire within the gas discharge port 312 of the combustion gas discharge panel 314 disposed in the central upper portion of the combustion chamber while sharply rotating together with the remaining unused combustion air. Consequently, perfect combustion is performed, and a column of fire extending upward in the perfect linear shape is formed.
  • FIGS. 6 and 7 indicate the boundary between the first combustion area and the second combustion area. These figures illustrate that, after first combustion has occurred in the first combustion area, combustion migrates to the second combustion area through the boundary.
  • FIGS. 8 and 9 illustrate C-C′ and D-D′ cross-sections indicating the portions of the first combustion area where combustion is performed. The direction in which airborne ash and preheated air rotate in the first combustion area is indicated.
  • FIGS. 10 and 11 illustrate E-E′ and F-F′ cross-sections, in which the airborne ash and the preheated air are rotating in the upper end of the fuel supply part 510 .
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KR101767785B1 (ko) * 2015-12-24 2017-08-14 주식회사 포스코 연소기
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BR112015011065A2 (pt) 2017-07-11
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JP6317752B2 (ja) 2018-04-25
EP2921776A4 (en) 2016-08-10
CA2891630A1 (en) 2014-05-22
CA2891630C (en) 2020-08-18
EP2921776B1 (en) 2020-01-08
KR101307795B1 (ko) 2013-09-25
CN104919248B (zh) 2017-08-22
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CN104919248A (zh) 2015-09-16
EP2921776A1 (en) 2015-09-23

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