ES2712867A1 - MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) - Google Patents
MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) Download PDFInfo
- Publication number
- ES2712867A1 ES2712867A1 ES201731328A ES201731328A ES2712867A1 ES 2712867 A1 ES2712867 A1 ES 2712867A1 ES 201731328 A ES201731328 A ES 201731328A ES 201731328 A ES201731328 A ES 201731328A ES 2712867 A1 ES2712867 A1 ES 2712867A1
- Authority
- ES
- Spain
- Prior art keywords
- gas
- module
- modular reactor
- treatment
- reactor
- 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.)
- Withdrawn
Links
- 238000011282 treatment Methods 0.000 title claims abstract description 18
- 239000007789 gas Substances 0.000 claims abstract description 43
- 238000002485 combustion reaction Methods 0.000 claims abstract description 22
- 239000000463 material Substances 0.000 claims abstract description 20
- 230000005855 radiation Effects 0.000 claims abstract description 14
- 239000002250 absorbent Substances 0.000 claims abstract description 9
- 230000002745 absorbent Effects 0.000 claims abstract description 9
- 239000012535 impurity Substances 0.000 claims abstract description 5
- 230000014759 maintenance of location Effects 0.000 claims abstract description 3
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 claims description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 6
- 239000002737 fuel gas Substances 0.000 claims description 6
- 239000000567 combustion gas Substances 0.000 claims description 4
- 239000000839 emulsion Substances 0.000 claims description 4
- 239000010457 zeolite Substances 0.000 claims description 4
- 229910021536 Zeolite Inorganic materials 0.000 claims description 3
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 claims description 3
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 claims description 2
- 239000008187 granular material Substances 0.000 claims description 2
- 229910001172 neodymium magnet Inorganic materials 0.000 claims description 2
- 230000003068 static effect Effects 0.000 claims description 2
- 238000005457 optimization Methods 0.000 claims 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 6
- 229910052760 oxygen Inorganic materials 0.000 abstract description 6
- 239000001301 oxygen Substances 0.000 abstract description 6
- 230000004913 activation Effects 0.000 abstract description 4
- 230000004888 barrier function Effects 0.000 abstract description 4
- 230000003993 interaction Effects 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 9
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 6
- 230000007423 decrease Effects 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 239000003915 liquefied petroleum gas Substances 0.000 description 3
- 239000003345 natural gas Substances 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 238000006722 reduction reaction Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 229910052779 Neodymium Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M27/00—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
- F02M27/04—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by electric means, ionisation, polarisation or magnetism
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
- B01D53/02—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by adsorption, e.g. preparative gas chromatography
- B01D53/04—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by adsorption, e.g. preparative gas chromatography with stationary adsorbents
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10K—PURIFYING OR MODIFYING THE CHEMICAL COMPOSITION OF COMBUSTIBLE GASES CONTAINING CARBON MONOXIDE
- C10K3/00—Modifying the chemical composition of combustible gases containing carbon monoxide to produce an improved fuel, e.g. one of different calorific value, which may be free from carbon monoxide
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M27/00—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
- F02M27/06—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by rays, e.g. infrared and ultraviolet
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- General Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Organic Chemistry (AREA)
- Analytical Chemistry (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
Description
REACTOR MODULAR PARA TRATAMIENTO DE GAS COMBUSTIBLEMODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT
DESCRIPCIONDESCRIPTION
OBJETO DE LA INVENCIONOBJECT OF THE INVENTION
La presente invention se refiere en particular a un reactor modular para tratamiento en llnea de gases combustibles, especialmente concebido para gas natural y gases licuados de petroleo.The present invention relates in particular to a modular reactor for the in-line treatment of combustible gases, especially designed for natural gas and liquefied petroleum gases.
ANTECEDENTES DE LA INVENCIONBACKGROUND OF THE INVENTION
Los sistemas actualmente existentes para la combustion de gases combustibles, en especial gas natural (GN) y gases licuados de petroleo (GLP) no logran alcanzar las eficiencias operacionales optimas establecidas en la fase de diseno debido, entre otros factores, al contenido de compuestos de bajo valor energetico que presentan los combustibles empleados.Currently existing systems for the combustion of combustible gases, especially natural gas (NG) and liquefied petroleum gases (LPG), fail to achieve the optimum operational efficiencies established in the design phase due, among other factors, to the content of low energetic value presented by the fuels used.
Elementos como el azufre, el hierro, el nitrogeno, los solidos residuales, el agua, el dioxido de carbono y otros compuestos, incorporados al gas combustible durante su procesado y transporte, tienen un pobre valor energetico. Dichos elementos contribuyen asimismo a la creation de aglomerados moleculares de elevado tamano, los cuales aumentan las temperaturas de ignition del combustible y dificultan su mezclado con el oxlgeno en el aire. Todo esto contribuye a ocasionar una combustion incompleta en los sistemas, lo cual da como resultado altas concentraciones de inquemados, elevadas emisiones al medio ambiente de productos toxicos, excesivos consumos de combustible.Elements such as sulfur, iron, nitrogen, residual solids, water, carbon dioxide and other compounds, incorporated into the fuel gas during processing and transport, have a poor energy value. These elements also contribute to the creation of high molecular agglomerates, which increase the ignition temperatures of the fuel and make it difficult to mix with the oxygen in the air. All this contributes to an incomplete combustion in the systems, which results in high concentrations of unburned, high emissions to the environment of toxic products, excessive fuel consumption.
Se conocen en el actual estado de la tecnica dispositivos destinados a aumentar la eficiencia termica de los combustibles mediante tratamientos previos a la combustion. Por ejemplo, existen mecanismos de tratamiento mediante la action combinada de irradiacion con infrarrojo visible y creacion de campos magneticos que dan como resultado una mayor eficiencia en la quema y una reduction de las emisiones contaminantes. Se conocen asimismo dispositivos para filtrado previo del combustible destinados a eliminar las impurezas mediante su retention flsica en mallas con un tam ano de poro inferior al de dichas impurezas.Devices intended to increase the thermal efficiency of fuels by means of pre-combustion treatments are known in the current state of the art. For example, there are treatment mechanisms through the combined action of irradiation with visible infrared and creation of magnetic fields that result in greater efficiency in burning and a reduction of pollutant emissions. Devices for prefiltering the fuel are also known for eliminating impurities by their physical retention in meshes with a a pore size smaller than said impurities.
DESCRIPCION DE LA INVENCIONDESCRIPTION OF THE INVENTION
El objeto de la inven tion consiste en un reactor m odular para tratam iento fls ico-qulm ico de gas combustible, destinado a ser instalado en sistemas de com bustion abiertos tales com o hornos o calderas, para elim inar los com puestos de bajo valor energetico contenidos en el gas em pleado como com bustib le para de esa form a aum entar su poder calorlfico, d ism inuir su tem peratura de ign ition y prom over la mezcla entre el gas y el aire saturada de oxlgeno.The object of the invention consists of a modular reactor for physical-chemical treatment of combustible gas, intended to be installed in open com bustion systems such as furnaces or boilers, to eliminate low value com ponents. energetic contained in the gas used as a com bustib le for that way increase its calorific power, d ism inuir its ign ition temperature and prom otes the mixture between gas and air saturated with oxygen.
Para ello, el reactor m odular com bina una prim era fase en la que se pone en contacto al gas combustib le con materiales absorbentes, preferentem ente zeolitas y oxido de hierro, y una segunda fase posterior en la que se expone al gas combustib le a materiales em isores de radiaciones en la franja del infrarrojo lejano, preferentemente tierras raras, y a medios magneticos, preferentemente imanes de neodim io, capaces de crear un campo magnetico. Se contem pla asim ism o la adicion de carbon activado al gas para m ejorar los resultados obtenidos. La exposition del gas a las dos fases del reactor produce cambios fls ico-qulm icos que duran hasta el inicio de la combustion, perm itiendo que los sistemas de com bustion trabajen a la m axim a eficiencia de su diseno.For this purpose, the mechanical reactor combines a first phase in which the fuel gas is brought into contact with absorbent materials, preferably zeolites and iron oxide, and a second subsequent phase in which it is exposed to the combustion gas. to radiation materials in the far infrared range, preferably rare earths, and to magnetic media, preferably neodymium magnets, capable of creating a magnetic field. The addition of activated carbon to the gas was also contemplated to improve the results obtained. The exposure of the gas to the two phases of the reactor produces physical-chemical changes that last until the start of the combustion, allowing the commuting systems to work at the maximum efficiency of their design.
En su rea liza tion preferente, el reactor presenta una geom etrla esencialm ente cillndrica que le perm ite disponerse coaxialm ente al exterior de un conducto del sistem a de com bustion por cuyo interior fluye el gas. Dicho reactor presenta dos cuerpos cillndricos vinculados entre si, preferentemente mediante machihembrado, los cuales se corresponden con las fases del tratam iento al cual se va a som eter al gas. El reactor m odular as! descrito esta destinado a ser instalado en el conducto, preferentemente antes del ultimo regulador de presion.In its preferred embodiment, the reactor has an essentially cylindrical geometry that allows it to be arranged coaxially outside a conduit of the combustion system through which the gas flows. Said reactor has two cylindrical bodies linked together, preferably by tongue and groove, which correspond to the phases of the treatment to which the gas is to be gassed. The reactor as odd! described is intended to be installed in the conduit, preferably before the last pressure regulator.
En la primera fase del reactor, un prim er m odulo contiene los materiales absorbentes, Zeolita y oxido de hierro, con un tam ano de m icro-poros inferior a un nanometro. En esta primera fase, el com bustib le aum enta su poder calorlfico y d ism inuye su tem peratura de ignicion de la combustion. La du ra tion efectiva aproxim ada de este prim er m odulo se estima en hasta dos anos. En el analisis de la com bustion de los gases tratados con la primera fase del reactor, la de tec tion de increm entos superiores al 2% en el consum o del com bustib le indica la posibilidad de que los materiales absorbentes se hayan agotado o colmatado, lo que determ ina la necesidad de reemplazarlo.In the first phase of the reactor, a first module contains the absorbent materials, Zeolite and iron oxide, with a micro pore size less than one nanometer. In this first phase, the combustion increases its calorific power and reduces its temperature of combustion ignition. The approximate effective duration of this first module is estimated at up to two years. In the analysis of the combustion of the gases treated with the The first phase of the reactor, the one of increase of more than 2% in the consumption of the com bustib indicates the possibility that the absorbent materials have been exhausted or clogged, which determines the need to replace it.
En la segunda fase del reactor, un segundo m odulo contiene los medios m agneticos y el material em isor de radiaciones en la franja del infrarrojo, para exponer el com bustib le a cam pos m agneticos y radiaciones lR-Lejano para cam biar su caracter flsico. Los materiales de la rea liza tion preferente tipo "Tierras Raras" son capaces de generar una rad ia tion infrarroja de una longitud de onda entre 3.3 y 3.6 m icrometros. La rad ia tion generada por los fotones de los materiales usados increm enta la energla cinetica de las moleculas, las cuales vibran. Estas vibraciones reducen las fuerzas de Van Der W aals entre las moleculas, lo que facilita la reac tion de reduction ox ida tion de combustion.In the second phase of the reactor, a second module contains the magnetic media and the emulsion material of radiation in the infrared range, to expose the com bustib le to m agnetic fields and IR-Far radiations to change its character. physical The materials of the "Rare Earth" type preferential area are capable of generating an infrared radiation of a wavelength between 3.3 and 3.6 meters. The radiation generated by the photons of the materials used increases the kinetic energy of the molecules, which vibrate. These vibrations reduce the Van Der W aals forces between the molecules, which facilitates the combustion reduction reaction.
En cuanto a los imanes, estos se disponen preferentemente por pares, enfrentados entre si y perpendiculares al flujo de combustible. Los cam pos magneticos que generan cada par de imanes pueden ser tanto de repulsion com o de atraccion. Los imanes cam bian el m om ento d ipolar de las moleculas de hidrocarburo y reducen el tam ano de los agregados moleculares, lo cual facilita posteriorm ente la mezcla del gas con el oxlgeno y dism inuye la barrera de activa tion de los enlaces moleculares, catalizando asl la reaccion de combustion.As for the magnets, these are preferably arranged in pairs, facing each other and perpendicular to the fuel flow. The magnetic fields generated by each pair of magnets can be both repulsion and attraction. The magnets change the polarity of the hydrocarbon molecules and reduce the size of the molecular aggregates, which subsequently facilitates the mixing of the gas with the oxygen and decreases the barrier of activation of the molecular bonds, catalyzing asl the combustion reaction.
La com b ina tion de la tecnolog la m agnetica con la radiacion infrarroja asegura que los cam bios fls ico-qulm icos logrados en el com bustib le duren varias horas, haciendo asl que su reaccion de oxidacion de com bustion sea lo mas com pleta posible. La du ra tion efectiva de este segundo m odulo se estima aproxim adam ente en 10 anos.The combination of m agnetic technology with infrared radiation ensures that the physico-chemical changes achieved in the com bustib lasts for several hours, thus making its reaction of oxidation of combustion as complete as possible. possible. The effective duration of this second module is estimated approximately in 10 years.
DESCRIPCION DE LOS DIBUJOSDESCRIPTION OF THE DRAWINGS
Para com plem entar la descrip tion que se esta realizando y con objeto de ayudar a una m ejor com prension de las caracterlsticas de la invention , de acuerdo con un ejemplo preferente de realizacion practica de la misma, se acom pana como parte integrante de dicha descripcion, un juego de dibujos en donde con caracter ilustrativo y no lim itativo, se ha representado lo siguiente: In order to complement the description that is being made and in order to help a better understanding of the characteristics of the invention, according to a preferred example of practical realization thereof, it is included as an integral part of said description. description, a set of drawings in which, with illustrative and not limitative character, the following has been represented:
Figura 1.- Muestra una vista en perspectiva del reactor modular.Figure 1 shows a perspective view of the modular reactor.
Figura 2.- Muestra una vista frontal de un corte longitudinal realizado en el reactor modular.Figure 2 shows a front view of a longitudinal section made in the modular reactor.
Figura 3.- Muestra una vista en perspectiva del difusor.Figure 3.- Shows a perspective view of the diffuser.
REALIZACION PREFERENTE DE LA INVENCIONPREFERRED EMBODIMENT OF THE INVENTION
Seguidamente se proporciona, con ayuda de las figuras anteriormente referidas, una explication detallada de un ejemplo de realization preferente del objeto de la presente invention.Next, with the help of the aforementioned figures, a detailed explanation of an example of a preferred embodiment of the object of the present invention is provided.
El reactor modular para tratamiento de gas combustible que se describe esta destinado a interponerse en un conducto (1) de un dispositivo de combustion abierto como un horno, conducto (1) por cuyo interior fluye un gas combustible. En el interior de dicho reactor se realizan una serie de tratamientos sobre el gas para aumentar su poder calorlfico, disminuir su temperatura de ignition y facilitar la interaction entre las moleculas del gas y el oxlgeno del aire, reduciendo asl la barrera de activation de la reaction de combustion.The modular fuel gas treatment reactor described is intended to be interposed in a conduit (1) of an open combustion device such as an oven, conduit (1) through which a combustible gas flows. In the interior of said reactor a series of treatments are carried out on the gas to increase its calorific power, decrease its ignition temperature and facilitate the interaction between the molecules of the gas and the oxygen of the air, thus reducing the barrier of activation of the reaction of combustion.
Para ello, el reactor comprende un primer modulo (2) y un segundo modulo (3) vinculados temporalmente entre si mediante unos elementos de union (4) que en esta realizacion preferente son de tipo machihembrado. Como se observa en la figura 1, ambos modulos (2,3) presentan una geometrla esencialmente cillndrica y se disponen coaxialmente interpuestos al conducto (1).For this, the reactor comprises a first module (2) and a second module (3) temporarily linked together by means of joining elements (4) which in this preferred embodiment are tongue-and-groove type. As seen in Figure 1, both modules (2,3) have an essentially cylindrical geometry and are arranged coaxially interposed to the conduit (1).
El reactor comprende una entrada (5) para paso del flujo de combustible desde el conducto (1) hacia el interior del reactor, y una salida (6) para paso del combustible tratado desde el interior del reactor hacia el conducto (1), desde el cual continua fluyendo hacia un regulador de presion del dispositivo de combustion. En la realizacion preferente aqul descrita y mostrada en las figuras adjuntas, la entrada (5) es de tipo macho, y la salida (6) es de tipo hembra para facilitar la vinculacion con el conducto (1). The reactor comprises an inlet (5) for passage of fuel flow from the conduit (1) into the reactor, and an outlet (6) for passage of the fuel treated from the interior of the reactor to the conduit (1), from which continues to flow towards a pressure regulator of the combustion device. In the preferred embodiment here described and shown in the attached figures, the inlet (5) is of the male type, and the outlet (6) is female in order to facilitate the connection with the duct (1).
La figura 2 m uestra un corte transversal realizado en el reactor, en la que se aprecian los elem entos del interior y su d isposition . Com o se observa en dicha figura 2, el primer m odulo (1) com prende una primera carcasa (7) cillndrica y hueca, en cuyo interior hueco se dispone en prim er lugar, en la d irec tion del flujo de gas procedente del conducto (1), un d ifusor (8), para para reduction de la velocidad y aum ento de la presion estatica de dicho gas.Figure 2 shows a cross section made in the reactor, in which the interior elements and their position are appreciated. As seen in said figure 2, the first module (1) comprises a first cylindrical and hollow casing (7), in whose hollow interior it is first arranged, in the direction of the gas flow coming from the duct (1), a d ifusor (8), to reduce the speed and increase the static pressure of said gas.
Dicho difusor (8), m ostrado en la figura 3, presenta una geom etrla circular, e incorpora unas respectivas juntas (9) toricas para asegurar su vinculacion a las paredes internas de la carcasa (7) y m antener la estanqueidad. En esta rea liza tion preferente, el d ifusor (8) tiene una pluralidad de orificios uniform em ente repartidos por su superficie con un diam etro de 100 m icrones.Said diffuser (8), shown in Figure 3, has a circular geometry, and incorporates respective toric seals (9) to ensure its connection to the internal walls of the casing (7) and to maintain tightness. In this preferred embodiment, the driver (8) has a plurality of holes uniformly distributed over its surface with a diameter of 100 microns.
Posteriorm ente al d ifusor (8) se disponen en el interior hueco de la primera carcasa (7) una pluralidad de materiales absorbentes (10), a traves de los cuales fluye el gas a alta presion. Dichos materiales absorbentes (10), que en esta realizacion preferente son respectivam ente zeolita (11), oxido de hierro (12) granulado y carbon activado (13) con un tam ano de m icro-poros inferior a un nanometro, retienen parte de las im purezas del gas para aum entar su poder calorlfico y dism inuir su tem peratura de ign ition de la combustion.Subsequently to the diffuser (8) a plurality of absorbent materials (10) are arranged in the hollow interior of the first casing (7), through which the gas flows at high pressure. Said absorbent materials (10), which in this preferred embodiment are respectively zeolite (11), iron oxide (12) granulate and activated carbon (13) with a micro pore size less than one nanometer, retain part of the im purities of the gas to increase its calorific power and decrease its ignition temperature of the combustion.
Tras los materiales absorbentes (10) se dispone otro d ifusor (8) previo al paso del flujo de gas parcialm ente tratado hacia el interior del segundo m odulo (2) a traves de un canal (14) definido en los elem entos de union (4) que vinculan a am bos m odulos (2,3) entre si.Beyond the absorbent materials (10) another d isusor (8) is provided prior to the passage of the gas flow partially treated towards the interior of the second module (2) through a channel (14) defined in the joint elements. (4) that link the two modules (2.3) to each other.
El segundo modulo (3) com prende una segunda carcasa (15) cillndrica y hueca, en cuyo interior hueco se disponen, fijados a las paredes internas, una pluralidad de medios m agneticos (16), que en esta realizacion preferente son unos imanes de neodimio, alternados con una correspondiente pluralidad de recipientes (17) con paredes de material metalico poroso no inductivo, en cuyo interior se alojan materiales em isores de rad ia tion infrarroja (18), que en esta realizacion preferente son T ierras Raras capaces de generar una radiacion infrarroja de una longitud de onda entre 3.3 y 3.6 m icrometros. The second module (3) comprises a second cylindrical and hollow housing (15), inside which hollow are disposed, fixed to the internal walls, a plurality of m agnetic means (16), which in this preferred embodiment are magnetic neodymium, alternating with a corresponding plurality of containers (17) with walls of non-inductive porous metal material, inside which infrared radiation emulsion materials (18) are housed, which in this preferred embodiment are rare machines capable of generating an infrared radiation of a wavelength between 3.3 and 3.6 meters.
Com o se ilustra en dicha figura 2, en el interior de la segunda carcasa (15) se dispone una agrupacion superior (19), paralela a un eje longitudinal de la segunda carcasa (15), que com prende medios m agneticos (16) y recipientes (17) dispuestos alternativamente, y una agrupacion inferior (20), paralela a la agrupacion superior (19) y que com prende unos correspondientes medios magneticos (16) y recipientes (17) dispuestos alternativamente. Los medios m agneticos (16) de cada agrupacion (19,20) se disponen enfrentados entre si para crear un cam po magnetico perpendicular al flujo del gas. Asim ism o, entre am bas agrupaciones (19,20) se dispone un serpentln (21) longitudinal a traves del cual fluye el gas a tratar.As illustrated in said figure 2, inside the second housing (15) there is an upper group (19), parallel to a longitudinal axis of the second housing (15), which comprises m agnetic means (16) and recipients (17) arranged alternately, and a lower group (20), parallel to the upper group (19) and comprising corresponding magnetic means (16) and recipients (17) arranged alternately. The m agnetic means (16) of each group (19, 20) are arranged facing each other to create a magnetic field perpendicular to the gas flow. Also, between the two groups (19, 20) there is a longitudinal serpentine (21) through which the gas to be treated flows.
Los medios m agneticos (16) cam bian el m om ento d ipolar de las moleculas del gas y reducen el tam ano de posibles agregados m oleculares de impurezas, lo cual facilita posteriorm ente la mezcla del gas con el oxlgeno y dism inuye la barrera de activacion de los enlaces moleculares, catalizando asl la reac tion de combustion. Adicionalm ente, la rad ia tion generada por los fotones de los materiales em isores de rad ia tion infrarroja (18) incrementa la energla cinetica de las m oleculas del gas, las cuales vibran. Estas vibraciones reducen las fuerzas de Van Der W aals entre moleculas, lo que facilita la reaccion de reduction ox ida tion de combustion.The m agnetic means (16) change the dipolar m omet of the gas molecules and reduce the size of possible molecular aggregates of impurities, which subsequently facilitates the mixing of the gas with the oxygen and decreases the barrier Activation of molecular bonds, thus catalyzing the combustion reaction. Additionally, the radiation generated by the photons of the infrared radiation emulsion materials (18) increases the kinetic energy of the gas molecules, which vibrate. These vibrations reduce Van Der W aals forces between molecules, which facilitates the combustion reduction reaction.
El reactor reduce el consum o del combustib le (gas) entre un 5 y 15% y dism inuyen la con tam ina tion ambiental hasta un 40%. The reactor reduces fuel consumption (gas) by 5 to 15% and decreases environmental pollution by up to 40%.
Claims (7)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201731328A ES2712867A1 (en) | 2017-11-15 | 2017-11-15 | MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201731328A ES2712867A1 (en) | 2017-11-15 | 2017-11-15 | MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2712867A1 true ES2712867A1 (en) | 2019-05-16 |
Family
ID=66442000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES201731328A Withdrawn ES2712867A1 (en) | 2017-11-15 | 2017-11-15 | MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES2712867A1 (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2280862Y (en) * | 1996-10-26 | 1998-05-06 | 马和中 | Domestic gas purifying energy-saving device |
| CN1587185A (en) * | 2004-07-06 | 2005-03-02 | 北京联飞翔科技有限公司 | Ceramic material with activated fluid fuel molecule and combustion aid function and its preparing method and use |
| CN200955457Y (en) * | 2006-06-24 | 2007-10-03 | 杜望月 | Taxi rare earth permanent magnet gasoline-saving device |
| CN201553636U (en) * | 2009-10-29 | 2010-08-18 | 王健慧 | Far infrared ray strong magnetizing treater |
| CN102399081A (en) * | 2010-09-15 | 2012-04-04 | 黄学鸿 | Trace element energy-saving and purifying ceramic |
| KR20140001614A (en) * | 2012-06-28 | 2014-01-07 | 백완복 | Energy saved-fuel activation devices |
| CN204003168U (en) * | 2014-07-14 | 2014-12-10 | 郑铁 | A kind of vehicle economizer |
| CN204253238U (en) * | 2014-11-07 | 2015-04-08 | 康佳翔 | Motor Synergistic and energy-saving environmental protecting device |
-
2017
- 2017-11-15 ES ES201731328A patent/ES2712867A1/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2280862Y (en) * | 1996-10-26 | 1998-05-06 | 马和中 | Domestic gas purifying energy-saving device |
| CN1587185A (en) * | 2004-07-06 | 2005-03-02 | 北京联飞翔科技有限公司 | Ceramic material with activated fluid fuel molecule and combustion aid function and its preparing method and use |
| CN200955457Y (en) * | 2006-06-24 | 2007-10-03 | 杜望月 | Taxi rare earth permanent magnet gasoline-saving device |
| CN201553636U (en) * | 2009-10-29 | 2010-08-18 | 王健慧 | Far infrared ray strong magnetizing treater |
| CN102399081A (en) * | 2010-09-15 | 2012-04-04 | 黄学鸿 | Trace element energy-saving and purifying ceramic |
| KR20140001614A (en) * | 2012-06-28 | 2014-01-07 | 백완복 | Energy saved-fuel activation devices |
| CN204003168U (en) * | 2014-07-14 | 2014-12-10 | 郑铁 | A kind of vehicle economizer |
| CN204253238U (en) * | 2014-11-07 | 2015-04-08 | 康佳翔 | Motor Synergistic and energy-saving environmental protecting device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ES2235938T3 (en) | DEVICE FOR HOUSING AN ADDITIVE IN AN EXHAUST GAS. | |
| ES2567200T3 (en) | Stage combustion process with assisted ignition fuel lances | |
| ES2358328T3 (en) | PROCEDURE AND APPLIANCE FOR REDUCING NOx OF EXHAUST GASES INJECTING REDUCING AGENT IN THE AIR OF FIRE. | |
| ES2395148T3 (en) | Exhaust system | |
| ES2607695T3 (en) | Kettle and integrated air pollution control systems | |
| WO2013183981A1 (en) | Gaseous fuel burner with high energy and combustion efficiency, low pollutant emission and increased heat transfer | |
| ES2711318T3 (en) | Axial piston engine and method to operate an axial piston engine | |
| ES2910504T3 (en) | Procedure and device for adjusting the ignition property of a fuel, in particular, for the reduction of polluting emissions from combustion installations | |
| ES2260452T3 (en) | METHOD AND DEVICE FOR LITTLE NON-CATALYTIC CONTAMINANT COMBUSTION OF A LIQUID FUEL. | |
| ES2601702T3 (en) | Combustion with reduced carbon in the ash | |
| ES2089699T3 (en) | LOW EMISSION COMBUSTION SYSTEM FOR GAS TURBINES. | |
| BRPI0721244A2 (en) | shrink-fit shrink tunnel, Hot shrink wrapping films or packaging units | |
| ES2712867A1 (en) | MODULAR REACTOR FOR COMBUSTIBLE GAS TREATMENT (Machine-translation by Google Translate, not legally binding) | |
| US3838193A (en) | Method of treating nitrogen oxide generating substances by combustion | |
| ES2611106T3 (en) | Lance of a gas turbine burner | |
| ES2361041T3 (en) | TREATMENT OF EXHAUST CURRENTS. | |
| WO2022049314A1 (en) | Device for generating hydroxyl radicals | |
| ES2593202T3 (en) | Device for the magnetic treatment of a fluid with hydrocarbons | |
| ES2813361T3 (en) | Low NOx Premix Gas Burner Combustion Procedure | |
| ES2563453T3 (en) | Combination of fuel cells | |
| ES2397591T3 (en) | Device for supplying water vapor through a heat exchanger to a combustion chamber and associated procedure | |
| ES2781312T3 (en) | A system and method for purifying gas | |
| CN201003820Y (en) | Polluted air ion reaction chamber | |
| ES2921256T3 (en) | NOx removal system for a stationary combustion system | |
| ES2755325T3 (en) | Combustion procedure for solid, liquid, or gaseous hydrocarbon (HC) starting materials in a heat engine, heat engine, and system for producing energy from hydrocarbon (HC) materials |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| BA2A | Patent application published |
Ref document number: 2712867 Country of ref document: ES Kind code of ref document: A1 Effective date: 20190516 |
|
| FA2A | Application withdrawn |
Effective date: 20191010 |