ES2637192T3 - Burner and combustion device comprising said burner - Google Patents
Burner and combustion device comprising said burner Download PDFInfo
- Publication number
- ES2637192T3 ES2637192T3 ES09812447.2T ES09812447T ES2637192T3 ES 2637192 T3 ES2637192 T3 ES 2637192T3 ES 09812447 T ES09812447 T ES 09812447T ES 2637192 T3 ES2637192 T3 ES 2637192T3
- Authority
- ES
- Spain
- Prior art keywords
- reagent
- operating cavity
- burner
- feeding means
- main body
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C1/00—Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel being either a fluid fuel or a solid fuel suspended in a carrier gas or air
- F23C1/08—Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel being either a fluid fuel or a solid fuel suspended in a carrier gas or air liquid and gaseous fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
- F23C3/002—Combustion apparatus characterised by the shape of the combustion chamber the chamber having an elongated tubular form, e.g. for a radiant tube
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/002—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space spraying nozzle arranged within furnace openings
- F23D11/004—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space spraying nozzle arranged within furnace openings for producing radiant heat
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/12—Radiant burners
- F23D14/126—Radiant burners cooperating with refractory wall surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
- F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
- F23C2700/04—Combustion apparatus using gaseous fuel
- F23C2700/046—Combustion apparatus using gaseous fuel generating heat by heating radiant bodies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/002—Radiant burner mixing tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2204/00—Burners adapted for simultaneous or alternative combustion having more than one fuel supply
- F23D2204/10—Burners adapted for simultaneous or alternative combustion having more than one fuel supply gaseous and liquid fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Wick-Type Burners And Burners With Porous Materials (AREA)
Abstract
Un quemador (1) para producir un dispositivo de combustión (100), en el que dicho quemador (1) comprende: - un cuerpo principal que comprende una cavidad operativa (11) de forma sustancialmente cilíndrica que se extiende a lo largo de una dirección axial (X) que tiene la misma dimensión diametral, estando dicha cavidad operativa abierta por lo menos en un primer lado y cerrada en el otro lado por una pared de carcasa (12); - primeros medios de alimentación para introducir un flujo de un primer reactivo en dicha cavidad operativa (11) en una posición de admisión de dicho primer reactivo (P1), configurando dichos primeros medios de alimentación (20) una admisión tangencial de dicho primer reactivo en dicha cavidad operativa (11); - segundos medios de alimentación para introducir un flujo de un segundo reactivo en dicha cavidad operativa (11) en una posición de admisión (P2) de dicho segundo flujo, introduciendo dicho segundo medio de alimentación dicho flujo de segundo reactivo de acuerdo con una dirección sustancialmente paralela a dicha dirección axial (X) a lo largo de la que se extiende dicha cavidad operativa (11), dicho segundo medio de alimentación (30) comprende una lanza (30) que se extiende a través de dicha pared de carcasa (12) de dicho cuerpo principal, comprendiendo dicha lanza (30) una porción (30B) fuera de dicho cuerpo principal y una porción (30A) dentro de dicho cuerpo principal y coaxial con dicha cavidad operativa (11), y medios de encendido por combustión dispuestos dentro de dicha lanza en el que dicha cavidad operativa (11) comprende una primera porción (11A) entre dicha posición de admisión (P1) de dicho primer reactivo y dicha posición de admisión (P2) de dicho segundo reactivo, definiendo dicha primera porción una cámara de estabilización del movimiento de dicho primer reactivo, comprendiendo dicha cavidad operativa (11) una segunda porción (11B) que define una cámara de combustión aguas abajo de dicha posición de admisión (P2) de dicho segundo reactivo.A burner (1) for producing a combustion device (100), wherein said burner (1) comprises: - a main body comprising an operating cavity (11) of substantially cylindrical shape extending along a direction axial (X) having the same diametrical dimension, said operating cavity being open on at least one first side and closed on the other side by a casing wall (12); - first feeding means for introducing a flow of a first reagent into said operating cavity (11) in an admission position for said first reagent (P1), said first feeding means (20) configuring a tangential admission of said first reagent in said operating cavity (11); - second feeding means for introducing a flow of a second reagent into said operating cavity (11) at an admission position (P2) of said second flow, said second feeding means introducing said flow of second reagent according to a direction substantially parallel to said axial direction (X) along which said operating cavity (11) extends, said second feeding means (30) comprises a lance (30) extending through said casing wall (12) of said main body, said lance (30) comprising a portion (30B) outside said main body and a portion (30A) inside said main body and coaxial with said operating cavity (11), and combustion ignition means disposed inside of said lance in which said operating cavity (11) comprises a first portion (11A) between said admission position (P1) of said first reagent and said admission position (P2) of said second reagent, defined said first portion being a chamber for stabilizing the movement of said first reagent, said operating cavity (11) comprising a second portion (11B) defining a combustion chamber downstream of said admission position (P2) of said second reagent.
Description
anteriormente. El elemento tubular 10 del quemador 1 está situado al menos parcialmente dentro del revestimiento de carcasa 50 a través de la primera pared 51 de manera que la cámara de combustión primaria 11B es sustancialmente coaxial con el revestimiento 50 de la carcasa o con la cámara 18 de combustión secundaria. Como puede verse, el elemento tubular 10 está distanciado de la segunda pared 52 de modo que los productos de previously. The tubular element 10 of the burner 1 is located at least partially inside the carcass liner 50 through the first wall 51 so that the primary combustion chamber 11B is substantially coaxial with the casing 50 of the casing or with the chamber 18 of secondary combustion As can be seen, the tubular element 10 is distanced from the second wall 52 so that the products of
5 combustión suministrados desde la cámara de combustión primaria 11A pueden liberarse dentro de la cámara de combustión secundaria 18. 5 combustion supplied from the primary combustion chamber 11A can be released into the secondary combustion chamber 18.
[0036] La primera pared 51 del revestimiento de carcasa 50 comprende una abertura de descarga 55 para descargar productos derivados de la segunda combustión. En particular, en la solución ilustrada, la abertura de 10 descarga 55 es coaxial con el revestimiento de carcasa 50 o con el elemento tubular 10 del quemador 1. El dispositivo de combustión 5 puede comprender ventajosamente un elemento de transporte 58 para transportar los productos de la segunda combustión. En el caso ilustrado, el elemento de transporte 58 comprende una salida de descarga 59 que se puede conectar, a través de un elemento de brida 59B, a un conducto de evacuación, no mostrado en las figuras. Según los requisitos, estos productos pueden ser transportados a una etapa de combustión [0036] The first wall 51 of the housing liner 50 comprises a discharge opening 55 for discharging products derived from the second combustion. In particular, in the illustrated solution, the discharge opening 55 is coaxial with the housing liner 50 or with the tubular element 10 of the burner 1. The combustion device 5 can advantageously comprise a transport element 58 for transporting the products of The second combustion. In the illustrated case, the transport element 58 comprises a discharge outlet 59 that can be connected, through a flange element 59B, to an evacuation conduit, not shown in the figures. According to the requirements, these products can be transported to a combustion stage
15 adicional del dispositivo de combustión 5 o dentro de otro dispositivo. Alternativamente, los productos de combustión podrían liberarse directamente en la atmósfera si su temperatura es suficientemente baja. 15 additional combustion device 5 or within another device. Alternatively, combustion products could be released directly into the atmosphere if their temperature is sufficiently low.
[0037] Las figuras 10 y 11 se refieren a una segunda realización de un dispositivo de combustión 5 de acuerdo con la posición que difiere de la anterior mediante el uso de un quemador de combustible líquido 1. Por comparación de [0037] Figures 10 and 11 refer to a second embodiment of a combustion device 5 according to the position that differs from the previous one by using a liquid fuel burner 1. By comparison of
20 las figuras 8 y 9, puede entenderse que en las dos realizaciones del dispositivo de combustión 5 su estructura es sustancialmente idéntica con ventajas evidentes desde el punto de vista de los costes de fabricación. Naturalmente, las dimensiones de los dos dispositivos se establecen en función del tipo de combustible a utilizar y de las condiciones de funcionamiento requeridas. 20 Figures 8 and 9, it can be understood that in the two embodiments of the combustion device 5 its structure is substantially identical with advantages evident from the point of view of manufacturing costs. Naturally, the dimensions of the two devices are set according to the type of fuel to be used and the required operating conditions.
25 [0038] Las soluciones técnicas adoptadas para el quemador permiten alcanzar plenamente los objetivos y objetos. En particular, el quemador de acuerdo con la invención tiene una alta versatilidad funcional, lo que lo hace adecuado para su uso en diferentes aplicaciones. En particular, puede utilizarse para la combustión parcial o total o, alternativamente, como elemento de calentamiento de fluidos que transportan calor o de masas sólidas. La estructura del quemador de acuerdo con la invención permite que se utilice para producir dispositivos de combustión [0038] The technical solutions adopted for the burner allow the objectives and objects to be fully achieved. In particular, the burner according to the invention has a high functional versatility, which makes it suitable for use in different applications. In particular, it can be used for partial or total combustion or, alternatively, as a heating element for fluids that transport heat or solid masses. The burner structure according to the invention allows it to be used to produce combustion devices
30 de varias etapas, particularmente compactos y eficientes, con costes de fabricación extremadamente limitados. 30 multi-stage, particularly compact and efficient, with extremely limited manufacturing costs.
[0039] El quemador y el dispositivo de combustión así concebidos son susceptibles a numerosas modificaciones y variantes, todas ellas dentro del alcance del concepto inventivo; Además todos los detalles pueden ser reemplazados por otros detalles técnicamente equivalentes. [0039] The burner and the combustion device thus conceived are susceptible to numerous modifications and variants, all of them within the scope of the inventive concept; In addition all the details can be replaced by other technically equivalent details.
35 [0040] En la práctica, los materiales utilizados y las dimensiones y formas contingentes pueden ser cualesquiera, de acuerdo con los requisitos y el estado de la técnica. [0040] In practice, the materials used and the contingent dimensions and shapes may be any, in accordance with the requirements and prior art.
7 7
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IT2009/000599 WO2011080780A1 (en) | 2009-12-30 | 2009-12-30 | Burner and combustion device comprising said burner |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2637192T3 true ES2637192T3 (en) | 2017-10-11 |
Family
ID=42731824
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES09812447.2T Active ES2637192T3 (en) | 2009-12-30 | 2009-12-30 | Burner and combustion device comprising said burner |
Country Status (4)
Country | Link |
---|---|
US (1) | US20120276490A1 (en) |
EP (1) | EP2519770B1 (en) |
ES (1) | ES2637192T3 (en) |
WO (1) | WO2011080780A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101870969B1 (en) * | 2017-08-22 | 2018-07-19 | 한국남동발전 주식회사 | Torch assembly for seperating ignition plug |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3301639A (en) * | 1963-03-20 | 1967-01-31 | Columbian Carbon | Method and apparatus for the manufacture of carbon black |
US3576384A (en) * | 1968-11-29 | 1971-04-27 | British American Oil Co | Multinozzle system for vortex burners |
US3658289A (en) * | 1969-12-22 | 1972-04-25 | Cities Service Co | Control of fluid dynamics in spiraling gas streams |
FR2402831A1 (en) * | 1977-09-12 | 1979-04-06 | Utilisation Ration Gaz | RADIANT BURNER WITH LOW THERMAL INERTIA |
US4623521A (en) * | 1985-09-30 | 1986-11-18 | Phillips Petroleum Company | Carbon black reactor |
DE4113412C2 (en) * | 1991-04-20 | 1999-04-01 | Saacke Gmbh & Co Kg | Device for burning liquid or gaseous fuel for a furnace |
DE4316946A1 (en) * | 1993-05-20 | 1994-11-24 | Colsman & Co Gmbh | Gas powered infrared heater for heating purposes |
US5761897A (en) * | 1996-12-20 | 1998-06-09 | United Technologies Corporation | Method of combustion with a two stream tangential entry nozzle |
US5899076A (en) * | 1996-12-20 | 1999-05-04 | United Technologies Corporation | Flame disgorging two stream tangential entry nozzle |
DE19925875A1 (en) * | 1999-06-07 | 2000-12-14 | Krupp Polysius Ag | Tubular burner for industrial furnaces |
US6872070B2 (en) * | 2001-05-10 | 2005-03-29 | Hauck Manufacturing Company | U-tube diffusion flame burner assembly having unique flame stabilization |
US6773256B2 (en) * | 2002-02-05 | 2004-08-10 | Air Products And Chemicals, Inc. | Ultra low NOx burner for process heating |
DE60308071T3 (en) | 2002-01-31 | 2012-10-25 | Air Products And Chemicals, Inc. | Burner for process heating with very low NOx emission |
FI20021223A (en) * | 2002-06-24 | 2003-12-25 | Andritz Oy | Procedure and burner for rotary kilns |
DE102004003343A1 (en) * | 2004-01-22 | 2005-08-11 | Linde Ag | Flexible parallel flow burner with swirl chamber |
US7303388B2 (en) * | 2004-07-01 | 2007-12-04 | Air Products And Chemicals, Inc. | Staged combustion system with ignition-assisted fuel lances |
-
2009
- 2009-12-30 ES ES09812447.2T patent/ES2637192T3/en active Active
- 2009-12-30 WO PCT/IT2009/000599 patent/WO2011080780A1/en active Application Filing
- 2009-12-30 US US13/520,086 patent/US20120276490A1/en not_active Abandoned
- 2009-12-30 EP EP09812447.2A patent/EP2519770B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2011080780A1 (en) | 2011-07-07 |
EP2519770A1 (en) | 2012-11-07 |
EP2519770B1 (en) | 2017-05-31 |
US20120276490A1 (en) | 2012-11-01 |
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