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EP1144915B1 - Burner-type apparatus and fuel combustion method - Google Patents

Burner-type apparatus and fuel combustion method Download PDF

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Publication number
EP1144915B1
EP1144915B1 EP99961180A EP99961180A EP1144915B1 EP 1144915 B1 EP1144915 B1 EP 1144915B1 EP 99961180 A EP99961180 A EP 99961180A EP 99961180 A EP99961180 A EP 99961180A EP 1144915 B1 EP1144915 B1 EP 1144915B1
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EP
European Patent Office
Prior art keywords
gas
tubes
tube
axis
devices
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
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EP99961180A
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German (de)
French (fr)
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EP1144915A1 (en
Inventor
Gérard Mougey
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TotalEnergies Marketing Services SA
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TotalFinaElf France SA
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/06Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
    • F23G7/08Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases using flares, e.g. in stacks
    • F23G7/085Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases using flares, e.g. in stacks in stacks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • F04F5/466Arrangements of nozzles with a plurality of nozzles arranged in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • F23D14/64Mixing devices; Mixing tubes with injectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L5/00Blast-producing apparatus before the fire
    • F23L5/04Blast-producing apparatus before the fire by induction of air for combustion, e.g. using steam jet

Definitions

  • An apparatus and method allowing better gas combustion containing in particular hydrocarbons can be used, for example, in torches from an oil refinery or on the fields of oil and gas production, for burning gases waste or gaseous emissions without emissions unburnt hydrocarbons.
  • Oil processing in a refinery results the production of waste gases and gaseous emissions, whose elimination by combustion in gas burning, called “torches” or “gas flares” in the profession, can cause emissions toxic and smelly, fumes or noise, harmful to the environment.
  • the excess gas to be burned has a relatively low pressure and a high flow rate of up to 10 000 000 Nm 3 / day, consecutive for example, to a malfunction on a refining unit of the petroleum or at an oil or gas production site. Since the pressure of the gas to be burnt remains generally low, this does not allow aeration of the flame sufficiently activated by the pressure of the gas leaving the torch supply tube. Since the fuel-oxidant mixture in the combustion zone becomes deficient in the amount of air necessary for perfect combustion, an external supply of oxidant is therefore necessary by any means available in the art to improve the combustion of the gas.
  • GB 1,323,674 describes an apparatus of the flare type, supplied with combustible gas by at least one tube gas inlet to burn.
  • the end of the tube is surrounded of a plurality of devices arranged around it and each comprising a venturi and a supply of motor fluid.
  • FR 573 059 A describes a blowing device in which we use a pressurized fluid to drive a other fluid and give it speed.
  • a plurality of motor fluid supply tubes are arranged with substantially annularly around the axis of at least one venturi, in view of sucking the second fluid before injection in a combustion zone.
  • US 1,443,315 A and US 3,554,681 also describe devices in which injection devices of a first gas arranged in a ring at the entrance of a venturi cause a second gas in it.
  • Torch manufacturers have also considered solution which consists in bringing air into the zone of combustion by means of power fan groups high, arranged for example under the torch, and to stagger the gas distribution using automatic valves controlled by complex instrumentation.
  • This solution is difficult to apply because of the cost investment and high operating costs, and more it is made unreliable by the installation of fans under the flame in a warm atmosphere and corrosive, and also raises safety concerns due to possible fallout from liquid hydrocarbons easily flammable on hot fans.
  • the Applicant therefore carried out research with a view to to find solutions that are, at the same time, technically satisfactory, simple, reliable and whose corresponding investment cost is low, in refinery as on a production site, to obtain smoke-free combustion of a gas which may contain liquid hydrocarbons.
  • This device has the major advantage of allowing smokeless combustion even when the gas pressure is low and high throughput, and that it contains liquid hydrocarbons.
  • the invention also relates to the use of the apparatus defined above to facilitate the combustion in the atmosphere of a combustible gas supplying the gas inlet tube, while the tubes of the supply devices of the working fluid are supplied by a fluid chosen from the group consisting of air, air enriched with oxygen, water vapor or a combustible gas, this use being characterized in that the pressure of the working fluid is between 0.5 and 6.10 5 Pa and, preferably, between 1 and 3.10 5 Pa, and in that each tube transports between 1% and 33% and, preferably, between 5% and 33% of this working fluid.
  • This use eliminates the need for fans and noise from passing a fluid such as water vapor in injectors.
  • the apparatus allows, on the one hand, to reduce the consumption of engine fluid, for example the water vapor, and on the other hand to increase the reliability of installation by the absence of moving parts, such that fans, to have an implementation process easy, and offer installation costs and relatively weak operational.
  • engine fluid for example the water vapor
  • the combustion apparatus according to the invention is shown in Figure 1 as it can be installed on the top of a gas flare.
  • combustion zone 1 with an inlet of combustible gas constituted by a tube 2 of gas to burn.
  • a plurality of devices 3 for supplying working fluid under pressure.
  • the devices 3 are inclined towards the combustion zone, i.e. towards the axis BB of tube 2, their axes of symmetry AA forming an angle ⁇ with the axis of symmetry BB of the tube 2 of arrival of the gas to be burned between 1 ° and 70 °, and preferably between 5 ° and 60 °.
  • FIG. 2 illustrates an embodiment of a device 3.
  • the latter consists of an arrival of working fluid 4, at the outlet of which is placed a body forming venturi 5, itself made up of a part tapered lower 6, generally called “converging”, and which is extended by a part cylindrical 7 called “neck”, the latter being extended by an upper frustoconical part 8 called “divergent”.
  • the supply of engine fluid 4 of each of the venturis 5, from the supply tube 13, comprises a central tube 9, which is usually of section transverse annular and arranged substantially coaxially to the axis AA of the venturi 5.
  • the central tube 9 extends from outside, passing through converging 6, to a point located in the venturi 5, generally at the level of the junction of convergent 6 and neck 7.
  • a plurality of tubes 10 is advantageously provided around the central tube 9.
  • the arrangement of these tubes 10 is generally regular and annular, the tubes 10 may be arranged in at least one ring, the center is located on the axis AA of the venturi body.
  • the tubes 10 and the central tube 9 are identical to each other, have a cross section generally circular and are arranged in an annular manner, following at least one crown whose center is located on the axis AA of the venturi.
  • the number of tubes 10 is calculated according to the flow air required for combustion and the internal diameter of the venturi body.
  • all of the feed tubes 13 are connected to the same source of pressurized working fluid.
  • At least the tubes 10 so arranged substantially annular around the axis AA of the venturi 5 and located furthest from this axis inject the motive fluid in the venturi at an angle ⁇ , formed with the axis AA of the venturi 5, greater than 3 °, and preference substantially equal to that formed by the divergent 8 with said axis.
  • Their lower part 12 can be cylindrical and substantially parallel to the axis AA of the venturi 5, while, as can be seen in FIG. 2, the angle of inclination ⁇ of their upper part 11 by relation to the axis AA is substantially equal to the angle of inclination of the diverging 8 with respect to this same axis AA.
  • the axes of the tubes 10 can form with the axis AA of the venturi 5 an angle substantially equal to that that forms the divergent with the axis of said venturi.
  • the tubes 10 all generally enter the venturi 5 of the same depth, which can be the same or less than the penetration depth of the central tube 9 in the venturi 5.
  • the central tube 9 is replaced by a second plurality of tubes arranged annularly around the axis AA, of so that they are surrounded by the tubes 10.
  • the tubes 10 as well as the central tube 9 may be identical others have a cross section overall circular and are preferably all connected to the tube power supply 13, itself being connected to a source of motor fluid. They are sized so that they transport between 1% and 33% of the working fluid and, from preferably between 5% and 33% of said fluid.
  • the devices 3 arranged so annular around the end of the gas inlet tube 2 to burn are all identical.
  • a variant of the invention can also be used, as shown in this figure 3, for burning gases requiring a high combustion temperature, for example hydrogen sulfide, whose temperature oxidation is greater than 700 ° C.
  • the area of combustion 1 is covered by a venturi body 15, into which the gas to be burned is injected via of tube 2, said body making it possible to maintain a higher temperature and residence time while preserving the flame from external disturbances.
  • a plurality of devices is arranged annularly around the end of the tube 2 for supplying the gas to be burned, so that the motor fluid exiting from each of the diverging the plurality of devices is injected into the body forming venturi 15, thereby improving the combustion of the gas to be burned.
  • the working fluid air, air enriched with oxygen, a gas which is itself combustible or steam is generally used.
  • the pressure of the working fluid is usually between 0.5 and 6.10 5 Pa (0.5 to 6 bars) and, preferably, between 1 and 3.10 5 Pa (1 to 3 bars).
  • the combustible gas is introduced coaxially in combustion zone 1 according to the arrows G. Combustion occurs in the area of combustion 1. It is favored by devices 3, which, thanks to the introduction of a working fluid, alone or in mixture, following the arrows H, cause air to through the venturi 5, following the arrows I. This air driven spring by the divergent 8 of the device concerned and then comes to improve the combustion of gases.
  • the use of the devices 3 therefore allows a complete combustion of a gas containing a hydrocarbon, a mixture of hydrocarbons, an acid gas or a mixture of these gas, thanks to a high air entrainment with low amount of working fluid.
  • the noise is due to the trigger of the working fluid in the tubes, the use of a less amount of working fluid leads to a reduction in noise.
  • the Applicant has found, during tests it has that the use of the device according to the invention requires a flow rate of the steam necessary for ensure smoke-free combustion, which is 14 times lower than the flow required by conventional torches for obtaining the same result.
  • the apparatus according to the invention also has the advantage of be easily achievable on a platform, shortly, by simply fitting out a torch classic, which only causes a short stop the operation of the refining unit, or on a site oil or gas production. Operating losses are therefore minimal.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Incineration Of Waste (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)
  • Air Supply (AREA)

Description

L'invention concerne un appareil et un procédé permettant d'obtenir une meilleure combustion de gaz contenant notamment des hydrocarbures. Ces appareil et procédé peuvent être utilisés, par exemple, dans les torches d'une raffinerie de pétrole ou sur les champs de production d'huile et de gaz, pour brûler des gaz résiduaires ou des émissions gazeuses sans émissions d'hydrocarbures imbrûlés.An apparatus and method allowing better gas combustion containing in particular hydrocarbons. These devices and process can be used, for example, in torches from an oil refinery or on the fields of oil and gas production, for burning gases waste or gaseous emissions without emissions unburnt hydrocarbons.

ETAT DE LA TECHNIQUESTATE OF THE ART

Le traitement du pétrole dans une raffinerie entraíne la production de gaz résiduaires et d'émissions gazeuses, dont l'élimination par combustion dans des systèmes de brûlage de gaz, appelés " torches " ou " torchères à gaz " dans la profession, peuvent être à l'origine d'émissions toxiques et malodorantes, de fumées ou de bruit, préjudiciables à l'environnement.Oil processing in a refinery results the production of waste gases and gaseous emissions, whose elimination by combustion in gas burning, called "torches" or "gas flares" in the profession, can cause emissions toxic and smelly, fumes or noise, harmful to the environment.

Ces nuisances et notamment celles apportées par la combustion incomplète de gaz, par exemple riches en hydrogène sulfuré (H2S), se manifestent généralement, lorsque la quantité d'air nécessaire à une parfaite combustion est insuffisante, c'est-à-dire quand le rapport entre le débit de gaz à brûler et le débit d'air nécessaire à la combustion est inférieur au rapport stoechiométrique, et lorsque les trois conditions nécessaires à une combustion optimale, appelées " les trois T ", à savoir la Température de la flamme, le Temps de mélange air/gaz avant brûlage et la Turbulence appliquée à ce mélange, sont insuffisamment remplies.These nuisances, and in particular those caused by the incomplete combustion of gases, for example rich in hydrogen sulphide (H 2 S), generally appear, when the quantity of air necessary for perfect combustion is insufficient, that is to say when the ratio between the flow rate of gas to be burned and the air flow rate required for combustion is less than the stoichiometric ratio, and when the three conditions necessary for optimal combustion, called "the three T", namely the T emperature of the flame, the T emps of air / gas mixture before burning and the T urbulence applied to this mixture, are insufficiently filled.

Ceci est généralement dû au fait que les excédents de gaz à brûler ont une pression relativement faible et un débit élevé pouvant aller jusqu'à 10 000 000 Nm3/jour, consécutif par exemple, à un défaut de fonctionnement sur une unité de raffinage du pétrole ou sur un site de production d'huile ou de gaz. La pression du gaz à brûler demeurant globalement faible, celle-ci ne permet pas une aération de la flamme suffisamment activée par la pression du gaz en sortie du tube d'alimentation de la torche. Le mélange combustible-comburant dans la zone de combustion devenant déficitaire au niveau de la quantité d'air nécessaire à une parfaite combustion, il faut par conséquent un apport extérieur de comburant par tout moyen disponible dans la technique pour améliorer la combustion du gaz.This is generally due to the fact that the excess gas to be burned has a relatively low pressure and a high flow rate of up to 10 000 000 Nm 3 / day, consecutive for example, to a malfunction on a refining unit of the petroleum or at an oil or gas production site. Since the pressure of the gas to be burnt remains generally low, this does not allow aeration of the flame sufficiently activated by the pressure of the gas leaving the torch supply tube. Since the fuel-oxidant mixture in the combustion zone becomes deficient in the amount of air necessary for perfect combustion, an external supply of oxidant is therefore necessary by any means available in the art to improve the combustion of the gas.

Jusqu'à présent, on a fait appel à des dispositifs d'injection alimentés, par exemple, par de la vapeur d'eau traversant des injecteurs, ou d'autres fluides moteurs tels que l'air ou un gaz, qui induisent l'air et les turbulences nécessaires à la combustion. Cependant, ces dispositifs ont des rendements faibles, ce qui impose d'utiliser des quantités importantes de fluides pour compenser leur manque d'efficacité.So far, devices have been used injection fueled, for example, by steam passing through injectors, or other working fluids such than air or gas, which induce air and turbulence necessary for combustion. However, these devices have low yields, which requires the use of large quantities of fluids to compensate for their lack efficiency.

Il en résulte, en raffinerie, dans le cas par exemple d'utilisation de la vapeur d'eau comme fluide moteur, une forte consommation ayant pour effets :

  • une émission importante de bruit, due au passage de la vapeur d'eau dans les tubes et les injecteurs ;
  • un refroidissement de la flamme, qui ne permet pas d'assurer les conditions correctes de combustion des gaz, par exemple les gaz acides comme H2S, pour lequel la température de 700°C requise pour sa complète oxydation n'est, dans ces conditions, pas atteinte, produisant ainsi des émissions toxiques et malodorantes ;
  • un bilan énergétique du site pouvant être déficitaire, car dépendant de la production de la vapeur d'eau.
This results in a refinery, in the case for example of the use of water vapor as a working fluid, a high consumption having the effects:
  • a significant emission of noise, due to the passage of water vapor through the tubes and the injectors;
  • a cooling of the flame, which does not make it possible to ensure the correct conditions for combustion of the gases, for example the acid gases such as H 2 S, for which the temperature of 700 ° C. required for its complete oxidation is not, in these conditions, not reached, thus producing toxic and smelly emissions;
  • an energy balance of the site can be in deficit, because dependent on the production of water vapor.

Sur les champs de production d'huile et de gaz, il n'y a généralement pas de vapeur d'eau disponible et la pression du gaz à brûler est trop faible pour être utilisable comme source d'énergie de mélange combustibe-comburant suffisante. Par conséquent, la combustion des rejets, qui sont des gaz riches en hydrocarbures et parfois en hydrocarbures liquides appelés condensats, devient incomplète et s'accompagne habituellement d'épaisses fumées noires.On the oil and gas production fields, there usually has no steam available and the pressure of the gas to be burned is too low to be usable as a fuel-oxidizer mixture energy source sufficient. Therefore, the combustion of discharges, which are gases rich in hydrocarbons and sometimes into liquid hydrocarbons called condensates, becomes incomplete and usually accompanied by thick smoke black.

GB 1 323 674 décrit un appareil du type torchère, alimenté en un gaz combustible par au moins un tube d'arrivée de gaz à brûler. L'extrémité du tube est entourée d'une pluralité de dispositifs disposés autour de celle-ci et comprenant chacun un venturi et une alimentation en fluide moteur.GB 1,323,674 describes an apparatus of the flare type, supplied with combustible gas by at least one tube gas inlet to burn. The end of the tube is surrounded of a plurality of devices arranged around it and each comprising a venturi and a supply of motor fluid.

FR 573 059 A décrit un appareil de soufflage dans lequel on utilise un fluide sous pression pour entraíner un autre fluide et lui imprimer de la vitesse. Une pluralité de tubes d'alimentation en fluide moteur sont disposés de façon sensiblement annulaire autour de l'axe d'au moins un venturi, en vu d'aspirer le second fluide avant injection dans une zone de combustion.FR 573 059 A describes a blowing device in which we use a pressurized fluid to drive a other fluid and give it speed. A plurality of motor fluid supply tubes are arranged with substantially annularly around the axis of at least one venturi, in view of sucking the second fluid before injection in a combustion zone.

US 1 443 315 A et US 3 554 681 décrivent eux aussi des dispositifs dans lesquels des dispositifs d'injection d'un premier gaz disposés en couronne à l'entrée d'un venturi entraínent un second gaz dans celui-ci.US 1,443,315 A and US 3,554,681 also describe devices in which injection devices of a first gas arranged in a ring at the entrance of a venturi cause a second gas in it.

Les constructeurs de torches ont aussi envisagé une solution qui consiste à apporter de l'air dans la zone de combustion au moyen de groupes de ventilateurs de puissance élevée, disposés par exemple sous la torche, et à étager la distribution du gaz à l'aide de vannes automatiques commandées par une instrumentation complexe. Cette solution s'avère difficilement applicable, car d'un coût d'investissement et de frais opératoires élevé, et de plus, elle est rendue peu fiable par l'installation des ventilateurs sous la flamme dans une atmosphère chaude et corrosive, et soulève également des problèmes de sécurité dus à des retombées possibles d'hydrocarbures liquides facilement inflammables sur les ventilateurs chauds.Torch manufacturers have also considered solution which consists in bringing air into the zone of combustion by means of power fan groups high, arranged for example under the torch, and to stagger the gas distribution using automatic valves controlled by complex instrumentation. This solution is difficult to apply because of the cost investment and high operating costs, and more it is made unreliable by the installation of fans under the flame in a warm atmosphere and corrosive, and also raises safety concerns due to possible fallout from liquid hydrocarbons easily flammable on hot fans.

La Demanderesse a donc effectué des recherches en vue de trouver des solutions qui soient, à la fois, satisfaisantes sur le plan technique, simples, fiables et dont le coût d'investissement correspondant soit faible, en raffinerie comme sur un site de production, pour obtenir une combustion sans fumées d'un gaz pouvant contenir des hydrocarbures liquides.The Applicant therefore carried out research with a view to to find solutions that are, at the same time, technically satisfactory, simple, reliable and whose corresponding investment cost is low, in refinery as on a production site, to obtain smoke-free combustion of a gas which may contain liquid hydrocarbons.

EXPOSE SOMMAIRE DE L'INVENTIONSUMMARY OF THE INVENTION

La Demanderesse est ainsi parvenue à mettre au point un appareil de type torchère à gaz, pour faciliter la combustion de gaz combustibles dans l'atmosphère, comprenant une zone de combustion alimentée en au moins un gaz combustible par au moins un tube d'arrivée de gaz à brûler, caractérisé :

  • en ce que l'extrémité dudit tube est entourée d'une pluralité de dispositifs disposés autour de cette extrémité, composés chacun d'un venturi et d'une alimentation en fluide moteur ;
  • en ce que chacun des dispositifs comporte une pluralité de tubes disposés de façon sensiblement annulaire autour de l'axe AA du venturi ;
  • et en ce que l'ensemble des tubes de chaque dispositif, qui injectent le fluide moteur dans le venturi, divergent les uns des autres en formant un angle α avec l'axe AA du venturi, supérieur à 3° et, de préférence, sensiblement égal à celui que forme le divergent avec ledit axe.
The Applicant has thus succeeded in developing an apparatus of the gas flare type, to facilitate the combustion of combustible gases in the atmosphere, comprising a combustion zone supplied with at least one combustible gas by at least one inlet tube of gas to be burned, characterized:
  • in that the end of said tube is surrounded by a plurality of devices arranged around this end, each composed of a venturi and a supply of working fluid;
  • in that each of the devices comprises a plurality of tubes arranged substantially annularly around the axis AA of the venturi;
  • and in that the set of tubes of each device, which inject the working fluid into the venturi, diverge from each other by forming an angle α with the axis AA of the venturi, greater than 3 ° and, preferably, substantially equal to that formed by the divergent with said axis.

Cet appareil a pour avantage majeur de permettre une combustion sans fumée, même lorsque la pression du gaz est faible et le débit élevé, et que celui-ci contient des hydrocarbures liquides.This device has the major advantage of allowing smokeless combustion even when the gas pressure is low and high throughput, and that it contains liquid hydrocarbons.

L'invention a également pour objet l'utilisation de l'appareil défini ci-dessus pour faciliter la combustion dans l'atmosphère d'un gaz combustible alimentant le tube d'arrivée de gaz, tandis que les tubes des dispositifs d'amenée du fluide moteur sont alimentés par un fluide choisi dans le groupe constitué par l'air, l'air enrichi avec de l'oxygène, la vapeur d'eau ou un gaz combustible, cette utilisation étant caractérisée en ce que la pression du fluide moteur est comprise entre 0,5 et 6.105 Pa et, de préférence, entre 1 et 3.105 Pa, et en ce que chaque tube transporte entre 1 % et 33 % et, de préférence, entre 5 % et 33 % de ce fluide moteur.The invention also relates to the use of the apparatus defined above to facilitate the combustion in the atmosphere of a combustible gas supplying the gas inlet tube, while the tubes of the supply devices of the working fluid are supplied by a fluid chosen from the group consisting of air, air enriched with oxygen, water vapor or a combustible gas, this use being characterized in that the pressure of the working fluid is between 0.5 and 6.10 5 Pa and, preferably, between 1 and 3.10 5 Pa, and in that each tube transports between 1% and 33% and, preferably, between 5% and 33% of this working fluid.

Cette utilisation supprime le recours à des ventilateurs ainsi que le bruit résultant du passage d'un fluide tel que la vapeur d'eau dans des injecteurs.This use eliminates the need for fans and noise from passing a fluid such as water vapor in injectors.

En plus d'une combustion complète sans fumée, l'appareil conforme à l'invention permet, d'une part, de diminuer la consommation de fluide moteur, par exemple la vapeur d'eau, et, d'autre part d'augmenter la fiabilité de l'installation par l'absence de pièces en mouvement, tels que des ventilateurs, d'avoir un procédé de mise en oeuvre aisée, et d'offrir des coûts d'installation et opérationnels relativement faibles.In addition to complete smoke-free combustion, the apparatus according to the invention allows, on the one hand, to reduce the consumption of engine fluid, for example the water vapor, and on the other hand to increase the reliability of installation by the absence of moving parts, such that fans, to have an implementation process easy, and offer installation costs and relatively weak operational.

D'autres avantages et caractéristiques de l'appareil et du procédé selon l'invention ressortiront de la suite de la présente description, dans laquelle on se réfèrera aux figures 1 à 3 des dessins annexés, qui n'ont pas de caractère limitatif.Other advantages and features of the device and of the method according to the invention will emerge from the rest of the present description, in which reference will be made to Figures 1 to 3 of the accompanying drawings, which have no limiting character.

DESCRIPTION SOMMAIRE DES FIGURESSUMMARY DESCRIPTION OF FIGURES

  • La figure 1 représente schématiquement un appareil selon l'invention, en vue de face et en coupe ;Figure 1 shows schematically an apparatus according to the invention, in front view and in section;
  • La figure 2 est une vue schématique détaillée de l'un des dispositifs de la figure 1, en vue de face et en coupe ; Figure 2 is a detailed schematic view of one of the devices of FIG. 1, in front view and in chopped off ;
  • La figure 3 illustre une utilisation particulière de l'invention pour brûler des gaz acides tels que l'hydrogène sulfuré.Figure 3 illustrates a particular use of the invention for burning acid gases such as hydrogen sulfide.
  • EXPOSE DETAILLE DE L'INVENTIONDETAILED DESCRIPTION OF THE INVENTION Appareil selon l'inventionApparatus according to the invention

    L'appareil de combustion selon l'invention est représenté sur la figure 1 tel qu'il peut être installé sur la partie supérieure d'une torchère à gaz.The combustion apparatus according to the invention is shown in Figure 1 as it can be installed on the top of a gas flare.

    Il comporte une zone de combustion 1, avec une arrivée de gaz combustible constituée par un tube 2 de gaz à brûler. Autour de l'extrémité de ce tube d'arrivée de gaz à brûler 2 sont disposés de façon sensiblement annulaire une pluralité de dispositifs 3 d'amenée de fluide moteur sous pression.It has a combustion zone 1, with an inlet of combustible gas constituted by a tube 2 of gas to burn. Around the end of this gas inlet tube to burn 2 are arranged substantially annularly a plurality of devices 3 for supplying working fluid under pressure.

    Comme on peut le voir sur la figure 1, les dispositifs 3 sont inclinés vers la zone de combustion, c'est-à-dire vers l'axe BB du tube 2, leurs axes de symétrie AA formant un angle β avec l'axe de symétrie BB du tube 2 d'arrivée du gaz à brûler compris entre 1° et 70°, et de préférence entre 5° et 60°.As can be seen in Figure 1, the devices 3 are inclined towards the combustion zone, i.e. towards the axis BB of tube 2, their axes of symmetry AA forming an angle β with the axis of symmetry BB of the tube 2 of arrival of the gas to be burned between 1 ° and 70 °, and preferably between 5 ° and 60 °.

    La figure 2 illustre une forme de réalisation d'un dispositif 3. Ce dernier est composé d'une arrivée de fluide moteur 4, à la sortie de laquelle est placé un corps formant venturi 5, lui-même constitué d'une partie tronconique inférieure 6, appelée généralement " convergent ", et qui se prolonge par une partie cylindrique 7 appelée " col ", cette dernière étant prolongée par une partie tronconique supérieure 8 appelée " divergent".Figure 2 illustrates an embodiment of a device 3. The latter consists of an arrival of working fluid 4, at the outlet of which is placed a body forming venturi 5, itself made up of a part tapered lower 6, generally called "converging", and which is extended by a part cylindrical 7 called "neck", the latter being extended by an upper frustoconical part 8 called "divergent".

    L'alimentation en fluide moteur 4 de chacun des venturis 5, à partir du tube d'alimentation 13, comporte un tube central 9, qui est habituellement de section transversale annulaire et disposé sensiblement coaxialement à l'axe AA du venturi 5. Le tube central 9 s'étend depuis l'extérieur, en passant dans le convergent 6, jusqu'à un point situé dans le venturi 5, en général au niveau de la jonction du convergent 6 et du col 7.The supply of engine fluid 4 of each of the venturis 5, from the supply tube 13, comprises a central tube 9, which is usually of section transverse annular and arranged substantially coaxially to the axis AA of the venturi 5. The central tube 9 extends from outside, passing through converging 6, to a point located in the venturi 5, generally at the level of the junction of convergent 6 and neck 7.

    Une pluralité de tubes 10 est avantageusement prévue autour du tube central 9. La disposition de ces tubes 10 est généralement régulière et annulaire, les tubes 10 pouvant être disposés suivant au moins une couronne dont le centre est situé sur l'axe AA du corps formant venturi.A plurality of tubes 10 is advantageously provided around the central tube 9. The arrangement of these tubes 10 is generally regular and annular, the tubes 10 may be arranged in at least one ring, the center is located on the axis AA of the venturi body.

    De préférence, les tubes 10 et le tube central 9 sont identiques entre eux, présentent une section transversale globalement circulaire et sont disposés de façon annulaire, suivant au moins une couronne dont le centre est situé sur l'axe AA du venturi.Preferably, the tubes 10 and the central tube 9 are identical to each other, have a cross section generally circular and are arranged in an annular manner, following at least one crown whose center is located on the axis AA of the venturi.

    Le nombre de tubes 10 est calculé en fonction du débit d'air nécessaire à la combustion et du diamètre interne du corps du venturi.The number of tubes 10 is calculated according to the flow air required for combustion and the internal diameter of the venturi body.

    Avantageusement, tous les tubes d'alimentation 13 sont reliés à une même source de fluide moteur sous pression.Advantageously, all of the feed tubes 13 are connected to the same source of pressurized working fluid.

    De préférence, au moins les tubes 10 disposés de façon sensiblement annulaire autour de l'axe AA du venturi 5 et situés les plus à l'extérieur de cet axe injectent le fluide moteur dans le venturi suivant un angle α, formé avec l'axe AA du venturi 5, supérieur à 3°, et de préférence sensiblement égal à celui que forme le divergent 8 avec ledit axe. Leur partie inférieure 12 peut être cylindrique et sensiblement parallèle à l'axe AA du venturi 5, tandis que, comme cela est visible sur la figure 2, l'angle d'inclinaison α de leur partie supérieure 11 par rapport à l'axe AA est sensiblement égal à l'angle d'inclinaison du divergent 8 par rapport à ce même axe AA.Preferably, at least the tubes 10 so arranged substantially annular around the axis AA of the venturi 5 and located furthest from this axis inject the motive fluid in the venturi at an angle α, formed with the axis AA of the venturi 5, greater than 3 °, and preference substantially equal to that formed by the divergent 8 with said axis. Their lower part 12 can be cylindrical and substantially parallel to the axis AA of the venturi 5, while, as can be seen in FIG. 2, the angle of inclination α of their upper part 11 by relation to the axis AA is substantially equal to the angle of inclination of the diverging 8 with respect to this same axis AA.

    Dans une variante de l'invention non représentée sur les figures, les axes des tubes 10 peuvent former avec l'axe AA du venturi 5 un angle sensiblement égal à celui que forme le divergent avec l'axe dudit venturi.In a variant of the invention not shown in the figures, the axes of the tubes 10 can form with the axis AA of the venturi 5 an angle substantially equal to that that forms the divergent with the axis of said venturi.

    Les tubes 10 pénètrent tous généralement dans le venturi 5 d'une même profondeur, qui peut être identique ou inférieure à la profondeur de pénétration du tube central 9 dans le venturi 5. The tubes 10 all generally enter the venturi 5 of the same depth, which can be the same or less than the penetration depth of the central tube 9 in the venturi 5.

    Selon une variante (non représentée sur les figures), le tube central 9 est remplacé par une seconde pluralité de tubes disposés de façon annulaire autour de l'axe AA, de telle sorte qu'ils soient entourés par les tubes 10.According to a variant (not shown in the figures), the central tube 9 is replaced by a second plurality of tubes arranged annularly around the axis AA, of so that they are surrounded by the tubes 10.

    Comme indiqué ci-dessus, dans un même dispositif, les tubes 10 ainsi que le tube central 9 (ou la pluralité de tubes qui le remplacent) peuvent être identiques les uns aux autres, présentent une section transversale globalement circulaire et sont de préférence tous reliés au tube d'alimentation 13, lui-même étant relié à une source de fluide moteur. Ils sont dimensionnés de telle sorte qu'ils transportent entre 1% et 33% du fluide moteur et, de préférence, entre 5% et 33% dudit fluide.As indicated above, in the same device, the tubes 10 as well as the central tube 9 (or the plurality of tubes which replace it) may be identical others have a cross section overall circular and are preferably all connected to the tube power supply 13, itself being connected to a source of motor fluid. They are sized so that they transport between 1% and 33% of the working fluid and, from preferably between 5% and 33% of said fluid.

    Avantageusement, les dispositifs 3 disposés de façon annulaire autour de l'extrémité du tube 2 d'arrivée du gaz à brûler sont tous identiques.Advantageously, the devices 3 arranged so annular around the end of the gas inlet tube 2 to burn are all identical.

    Une variante de l'invention peut également être utilisée, comme indiqué sur cette figure 3, pour le brûlage des gaz nécessitant une forte température de combustion, par exemple l'hydrogène sulfuré, dont la température d'oxydation est supérieure à 700°C.A variant of the invention can also be used, as shown in this figure 3, for burning gases requiring a high combustion temperature, for example hydrogen sulfide, whose temperature oxidation is greater than 700 ° C.

    Comme on peut le voir sur la figure 3, la zone de combustion 1 est couverte par un corps formant venturi 15, dans lequel est injecté le gaz à brûler par l'intermédiaire du tube 2, ledit corps permettant de maintenir une température et un temps de résidence plus élevés tout en préservant la flamme des perturbations extérieures. Conformément à l'invention, une pluralité de dispositifs est disposée de façon annulaire autour de l'extrémité du tube 2 d'arrivée du gaz à brûler, de façon telle que le fluide moteur sortant de chacun des divergents de la pluralité de dispositifs est injecté dans le corps formant venturi 15, améliorant ainsi la combustion du gaz à brûler.As can be seen in Figure 3, the area of combustion 1 is covered by a venturi body 15, into which the gas to be burned is injected via of tube 2, said body making it possible to maintain a higher temperature and residence time while preserving the flame from external disturbances. According to the invention, a plurality of devices is arranged annularly around the end of the tube 2 for supplying the gas to be burned, so that the motor fluid exiting from each of the diverging the plurality of devices is injected into the body forming venturi 15, thereby improving the combustion of the gas to be burned.

    Procédé selon l'inventionMethod according to the invention

    Selon l'invention, pour améliorer la combustion des gaz par apport supplémentaire de comburant, on alimente au moyen d'un fluide l'arrivée de fluide moteur 4 de chacun des dispositifs 3.According to the invention, to improve the combustion of gases by additional supply of oxidizer, medium of fluid the arrival of motor fluid 4 of each devices 3.

    Comme fluide moteur, on utilise généralement de l'air, de l'air enrichi avec de l'oxygène, un gaz lui-même combustible ou de la vapeur d'eau. La pression du fluide moteur est habituellement comprise entre 0,5 et 6.105 Pa (0,5 à 6 bars) et, de préférence, entre 1 et 3.105 Pa (1 à 3 bars).As the working fluid, air, air enriched with oxygen, a gas which is itself combustible or steam is generally used. The pressure of the working fluid is usually between 0.5 and 6.10 5 Pa (0.5 to 6 bars) and, preferably, between 1 and 3.10 5 Pa (1 to 3 bars).

    Il ne se produit donc aucune combustion à l'intérieur des dispositifs 3, car ces derniers ont simplement pour rôle d'améliorer la combustion des gaz combustibles, en provoquant une augmentation de l'induction du comburant (l'air) et une turbulence favorisant le mélange entre le carburant et le comburant.There is therefore no combustion inside 3 devices, because these simply have role of improving the combustion of combustible gases, by causing increased oxidant induction (air) and turbulence favoring the mixing between the fuel and oxidizer.

    Lors du fonctionnement de l'appareil selon l'invention (voir figure 1), le gaz combustible est introduit coaxialement dans la zone de combustion 1 suivant les flèches G. La combustion se produit dans la zone de combustion 1. Elle est favorisée par les dispositifs 3, qui, grâce à l'introduction d'un fluide moteur, seul ou en mélange, suivant les flèches H, entraínent de l'air à travers le venturi 5, suivant les flèches I. Cet air entraíné ressort par le divergent 8 du dispositif concerné et vient alors améliorer la combustion des gaz.During the operation of the apparatus according to the invention (see figure 1), the combustible gas is introduced coaxially in combustion zone 1 according to the arrows G. Combustion occurs in the area of combustion 1. It is favored by devices 3, which, thanks to the introduction of a working fluid, alone or in mixture, following the arrows H, cause air to through the venturi 5, following the arrows I. This air driven spring by the divergent 8 of the device concerned and then comes to improve the combustion of gases.

    Ainsi, l'utilisation des dispositifs 3 permet donc une combustion complète d'un gaz contenant un hydrocarbure, un mélange d'hydrocarbures, un gaz acide ou un mélange de ces gaz, grâce à un entraínement d'air élevé avec une faible quantité de fluide moteur. Ceci se traduit par une réduction du bruit, par rapport aux torches existantes, où est réalisée une induction d'air à l'aide de tubes classiques alimentés en vapeur d'eau au niveau de la zone de combustion. En effet, comme le bruit est dû à la détente du fluide moteur dans les tubes, l'utilisation d'une quantité moindre de fluide moteur entraíne une réduction du bruit. Thus, the use of the devices 3 therefore allows a complete combustion of a gas containing a hydrocarbon, a mixture of hydrocarbons, an acid gas or a mixture of these gas, thanks to a high air entrainment with low amount of working fluid. This results in a noise reduction, compared to existing torches, where air induction is carried out using tubes classics supplied with water vapor in the area combustion. Indeed, as the noise is due to the trigger of the working fluid in the tubes, the use of a less amount of working fluid leads to a reduction in noise.

    La Demanderesse a constaté, au cours d'essais qu'elle a effectués, que l'utilisation de l'appareil selon l'invention requiert un débit de la vapeur nécessaire pour assurer une combustion sans fumées, qui est 14 fois inférieur au débit exigé par les torches classiques pour l'obtention du même résultat.The Applicant has found, during tests it has that the use of the device according to the invention requires a flow rate of the steam necessary for ensure smoke-free combustion, which is 14 times lower than the flow required by conventional torches for obtaining the same result.

    L'appareil selon l'invention a en outre l'avantage de pouvoir être réalisable facilement sur une plateforme, en peu de temps, en aménageant simplement une torche classique, ce qui n'occasionne qu'un arrêt de faible durée du fonctionnement de l'unité de raffinage, ou sur un site de production d'huile ou de gaz. Les pertes d'exploitation sont donc minimes.The apparatus according to the invention also has the advantage of be easily achievable on a platform, shortly, by simply fitting out a torch classic, which only causes a short stop the operation of the refining unit, or on a site oil or gas production. Operating losses are therefore minimal.

    Claims (11)

    1. An apparatus of gas-flare stack type, to facilitate the combustion of combustible gases in the atmosphere, comprising a combustion zone (1) supplied with at least one combustible gas through at least one inlet tube (2) for gas to be burnt, the end of said tube being surrounded by a plurality of devices (3) arranged around said end, each of said devices comprising a venturi tube (5) and a supply of motive fluid (4);
      characterised in that each of the devices (3) comprises a plurality of tubes (10) arranged in a substantially annular manner around the axis AA of the venturi tube (5);
      and in that all the tubes (10) of each device (3), which inject motive fluid into the venturi tube (5), diverge from one another to form an angle α with the axis A-A of the venturi tube (5) which is greater than 3° and, preferably, substantially equal to that which the divergent section (8) of said venturi tube forms with said axis.
    2. An apparatus according to claim 1, characterised in that the devices (3) are arranged in a substantially symmetrical manner and preferably annularly around the end of the inlet tube (2) for the gas to be burnt.
    3. An apparatus according to either one of claims 1 and 2, characterised in that the axis AA of the venturi tube (5) of each device (3) forms with the axis BB of the inlet tube (2) for the gas to be burnt an angle β of between 1° and 70° and, preferably, between 5° and 60°.
    4. An apparatus according to any one of the preceding claims, characterised in that the supply tubes (13) for all the devices (3) are connected to the same source of motive fluid under pressure.
    5. An apparatus according to any one of the preceding claims, characterised in that each of the tubes (10) of each device (3) disposed in a substantially annular manner around the end of the inlet tube (2) for the gas to be burnt is of such a size that it can convey between 1 % and 33 % and, preferably, between 5 % and 33 % of the motive fluid.
    6. An apparatus according to any one of the preceding claims, characterised in that the inlet of motive fluid (4) for each device (3) comprises a central tube (9) and a plurality of tubes (10) disposed in an annular manner around the axis AA of the venturi (5).
    7. An apparatus according to any one of the preceding claims, characterised in that the inlet of motive fluid (4) comprises two sets of tubes arranged respectively in an annular manner around the axis AA of the venturi tube (5).
    8. An apparatus according to any one of the preceding claims, characterised in that the tubes (10) of one device (3) are all identical to one another and are overall of circular cross-section.
    9. An apparatus according to any one of the preceding claims, characterised in that the tubes (10) are arranged in an annular manner along at least one ring, the centre of which is situated on the axis AA of the venturi tube (5).
    10. An apparatus according to any one of the preceding claims, characterised in that the combustion zone (1) is surrounded by a venturi tube (15) disposed downstream of the devices (3).
    11. Use of an apparatus according to any one of claims 1 to 10 to facilitate the combustion in the atmosphere of a combustible gas supplying the gas-inlet tube (2), while the tubes (13) of the devices (3) for the inlet of motive fluid are supplied with a fluid chosen from the group comprising air, oxygen-enriched air, steam or a combustible gas, characterised in that the pressure of the motive fluid is between 0.5 and 6.105 Pa and, preferably, between 1 and 3.105 Pa, and in that each tube (10) conveys between 1 % and 33 % and, preferably, between 5 % and 33 % of this motive fluid.
    EP99961180A 1998-12-30 1999-12-28 Burner-type apparatus and fuel combustion method Expired - Lifetime EP1144915B1 (en)

    Applications Claiming Priority (3)

    Application Number Priority Date Filing Date Title
    FR9816622A FR2788112B1 (en) 1998-12-30 1998-12-30 TORCHERE-TYPE APPARATUS AND METHOD FOR THE COMBUSTION OF GAS
    FR9816622 1998-12-30
    PCT/FR1999/003300 WO2000040902A1 (en) 1998-12-30 1999-12-28 Burner-type apparatus and fuel combustion method

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    EP1144915A1 EP1144915A1 (en) 2001-10-17
    EP1144915B1 true EP1144915B1 (en) 2004-05-06

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    EP (1) EP1144915B1 (en)
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    Families Citing this family (27)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    FR2788109B1 (en) * 1998-12-30 2001-06-08 Total Raffinage Distribution DEVICE FOR IMPROVING THE BURNING OF GASEOUS FUELS
    SE528808C2 (en) * 2004-09-15 2007-02-20 Aga Ab Combustion process and burner
    US7354265B2 (en) * 2004-12-02 2008-04-08 Saudi Arabian Oil Company Flare stack combustion method and apparatus
    DE102006005386B4 (en) * 2006-02-03 2009-04-09 Uhde Gmbh Gas burner with optimized nozzle arrangement
    CN101384670B (en) * 2006-02-10 2013-06-05 日本化药株式会社 Novel porphyrazine dye, ink, ink set, and colored material
    US7967600B2 (en) * 2006-03-27 2011-06-28 John Zink Company, Llc Flare apparatus
    US7677882B2 (en) * 2006-04-04 2010-03-16 Expro Americas, Llc Smokeless liquid dual-phase burner system
    US7677883B2 (en) * 2006-04-04 2010-03-16 Expro Americas, Llc Trailer mounted smokeless dual-phase burner system
    JP5404031B2 (en) * 2008-12-26 2014-01-29 三菱重工業株式会社 Grand Flare
    US20100291492A1 (en) * 2009-05-12 2010-11-18 John Zink Company, Llc Air flare apparatus and method
    DE102009041167B4 (en) * 2009-09-11 2021-08-12 Erbe Elektromedizin Gmbh Multifunctional instrument and method for preventing the carbonization of tissue by means of a multifunctional instrument
    DE102009044512B4 (en) * 2009-09-11 2021-08-12 Erbe Elektromedizin Gmbh Anti-carbonization device
    US8629313B2 (en) 2010-07-15 2014-01-14 John Zink Company, Llc Hybrid flare apparatus and method
    DE102010035153A1 (en) 2010-08-23 2012-02-23 Thyssenkrupp Uhde Gmbh Crude gas flare with adjustable opening cross-section for flaring flammable gases and combustion of raw gases
    CN102297437A (en) * 2011-07-30 2011-12-28 山西亚乐士环保技术股份有限公司 Automatic smoke-eliminating flare tip
    CN104566379A (en) * 2013-10-14 2015-04-29 陈凤利 Laminar gas intake way after fuel gas lagging
    CN103968383A (en) * 2014-06-02 2014-08-06 魏伯卿 Combined adjustable oxygen-enriched combustor
    US9416966B2 (en) 2014-07-25 2016-08-16 Flame Commander Corp. Venturi nozzle for a gas combustor
    EP2995858A1 (en) * 2014-09-11 2016-03-16 Linde Aktiengesellschaft Method for burning exhaust gas with oxygen injection
    DE102014013474A1 (en) * 2014-09-11 2016-03-17 Linde Aktiengesellschaft Process for combustion of exhaust gas with oxygen supply
    KR102498930B1 (en) * 2015-03-09 2023-02-10 데이코 아이피 홀딩스 엘엘시 Vacuum generating device using the Venturi effect
    US9982885B2 (en) * 2015-06-16 2018-05-29 Honeywell International Inc. Burner with combustion air driven jet pump
    NL2015096B1 (en) * 2015-07-06 2017-01-31 Johannus Theodorus Maria Taris Hermanus Burner configuration and application thereof.
    JP2017096615A (en) * 2015-11-18 2017-06-01 Jfeスチール株式会社 Diffusion breeder
    CN106969354A (en) * 2017-04-03 2017-07-21 山东宇丰商用厨具有限公司 A kind of burner cooked for steamed rice in clay pot
    CN114198746B (en) * 2021-12-03 2024-02-09 北京航化节能环保技术有限公司 Accurate air distribution method for non-premixed flame smoke abatement
    JPWO2023145219A1 (en) 2022-01-28 2023-08-03

    Family Cites Families (25)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US315187A (en) * 1885-04-07 Device for feeding air to furnaces
    FR387475A (en) * 1908-01-25 1908-07-10 Alexis Nograbat Blower device producing smoke
    FR412314A (en) * 1910-02-04 1910-07-09 Procedes Westinghouse Leblanc Jet device
    US1421840A (en) * 1914-09-14 1922-07-04 Westinghouse Electric & Mfg Co Fluid translating device
    US1181125A (en) * 1915-05-03 1916-05-02 Henry L Erlewine Steam-blower.
    US1264116A (en) * 1915-07-19 1918-04-23 Gen Electric Pump.
    US1449504A (en) * 1919-04-03 1923-03-27 Elliott Co Method of and apparatus for compressing elastic fluids
    US1443315A (en) * 1920-05-19 1923-01-23 Elliott Co Ejector
    FR573059A (en) * 1923-11-12 1924-06-18 Morgan Construction Co Blowing device
    US2072599A (en) * 1935-02-26 1937-03-02 Lemaitre Maurice Device for covering the steam exhaust pipe of locomotives
    US2111266A (en) * 1936-12-28 1938-03-15 Thomas S Hopkins Draft inducer
    US2164263A (en) * 1938-03-25 1939-06-27 John J Wall Jet air pump
    US2506972A (en) * 1947-03-08 1950-05-09 Standard Oil Co Flare stack tip
    US3101773A (en) * 1960-03-22 1963-08-27 Selas Corp Of America Air preheating burner
    GB1218189A (en) * 1967-10-09 1971-01-06 Albert Edward Proctor Improvements in or relating to flare stack tips
    GB1323674A (en) * 1969-06-24 1973-07-18 Ici Ltd Flare stacks and steam/air mixing devices therefor
    US3659962A (en) * 1970-06-02 1972-05-02 Zink Co John Aspirator
    US4445464A (en) * 1980-05-14 1984-05-01 Advanced Mechanical Technology, Inc. High efficiency water heating system
    FR2526525A1 (en) * 1982-05-06 1983-11-10 Chaudot Gerard SAFETY SYSTEM INTENDED IN PARTICULAR TO ELIMINATE COATED OR CONDENSED LIQUIDS WHEN BURNING OR DISPERSION OF HYDROCARBON GASES
    FR2530317B1 (en) * 1982-07-15 1987-05-29 Raffinage Cie Francaise METHOD AND DEVICE FOR THE COMBUSTION OF FUEL GASES WITH ATMOSPHERIC AIR INDUCTION
    SU1236253A1 (en) * 1983-11-25 1986-06-07 Производственно-Техническое Предприятие Треста "Укрэнергочермет" Low-pressure gas burner
    EP0215864B1 (en) * 1985-03-16 1989-10-18 Saarbergwerke Aktiengesellschaft Smoke gas exhaust by way of a cooling tower
    DE4418014A1 (en) * 1994-05-24 1995-11-30 E E T Umwelt Und Gastechnik Gm Method of conveying and mixing a first fluid with a second fluid under pressure
    US5865613A (en) * 1996-11-05 1999-02-02 Rajewski; Robert Carl Steam over air flare tip
    US6010329A (en) * 1996-11-08 2000-01-04 Shrinkfast Corporation Heat gun with high performance jet pump and quick change attachments

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    AR024851A1 (en) 2002-10-30
    DE69917073T2 (en) 2005-04-21
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    DE69917073D1 (en) 2004-06-09
    FR2788112A1 (en) 2000-07-07
    PT1144915E (en) 2004-09-30
    AU1787500A (en) 2000-07-24
    CN1332838A (en) 2002-01-23
    ES2221468T3 (en) 2004-12-16
    KR100678775B1 (en) 2007-02-05
    WO2000040902A1 (en) 2000-07-13
    FR2788112B1 (en) 2001-06-08
    KR20010101345A (en) 2001-11-14
    US6638059B1 (en) 2003-10-28
    ATE266177T1 (en) 2004-05-15
    CN1165708C (en) 2004-09-08
    EP1144915A1 (en) 2001-10-17

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