Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
  • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
  • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
• • C—CHEMISTRY; METALLURGY
  • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
  • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
  • C10J3/00—Production of combustible gases containing carbon monoxide from solid carbonaceous fuels
  • C10J3/72—Other features
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
  • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
  • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
  • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
  • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
  • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
  • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
  • F23D14/46—Details, e.g. noise reduction means
  • F23D14/48—Nozzles
  • F23D14/58—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
  • F23D14/46—Details, e.g. noise reduction means
  • F23D14/62—Mixing devices; Mixing tubes
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23N—REGULATING OR CONTROLLING COMBUSTION
  • F23N1/00—Regulating fuel supply
  • F23N1/002—Regulating fuel supply using electronic means
• • C—CHEMISTRY; METALLURGY
  • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
  • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
  • C10J2300/00—Details of gasification processes
  • C10J2300/09—Details of the feed, e.g. feeding of spent catalyst, inert gas or halogens
  • C10J2300/0913—Carbonaceous raw material
  • C10J2300/0916—Biomass
• • C—CHEMISTRY; METALLURGY
  • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
  • C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
  • C10J2300/00—Details of gasification processes
  • C10J2300/16—Integration of gasification processes with another plant or parts within the plant
  • C10J2300/164—Integration of gasification processes with another plant or parts within the plant with conversion of synthesis gas
  • C10J2300/1643—Conversion of synthesis gas to energy
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
  • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
  • F23C2900/03004—Tubular combustion chambers with swirling fuel/air flow
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
  • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
  • F23C2900/06041—Staged supply of oxidant
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D2204/00—Burners adapted for simultaneous or alternative combustion having more than one fuel supply
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23D—BURNERS
  • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
  • F23D2900/14—Special features of gas burners
  • F23D2900/14002—Special features of gas burners of premix or non premix types, specially adapted for the combustion of low heating value [LHV] gas
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23N—REGULATING OR CONTROLLING COMBUSTION
  • F23N2237/00—Controlling
  • F23N2237/08—Controlling two or more different types of fuel simultaneously

Definitions

• the invention belongs to the field of industrial gas burners, more particularly gas burners adapted to the combustion of poor gases.
• a "synthesis gas” (or “syngas”) is a CO / H 2 mixture resulting from the gasification of carbonaceous products in the presence of steam and / or air, optionally enriched with oxygen.
• the synthesis gas obtained from the conversion of biomass in a gasifier without oxygen enrichment has a lower heating value than that of fossil fuels (in particular propane and butane gases); it is a "low calorific gas”.
• lean gas or "low calorific gas” means a gas with a heating value (LHV) of less than 3000 Kcal / m 3 .
• Particularly patent FR 2 889 292 discloses a burner for lean fuel gas of the type comprising a combustion nose on a central axis and means for feeding a mixture of combustible gas and combustion air in rotation around the central axis of the burner.
• the burner is distinguished by being configured to eject a non-flammable premix stream in front of the combustion nose containing a mixture of premix air and fuel gas, a complementary flow of reaching a flammability threshold of the mixture in front of the combustion nose, said flow being ejected at the center of the premix flow through a central complementary air flow and / or around the pre-mixing flow by through an additional peripheral air flow.
• This configuration has a complexity of mounting and adjustment of the means implemented with the additional disadvantage if the lean gas is loaded with tars and particles progressive fouling equipment, especially in the premix zone before ignition of the fuel.
• EP 1 800 062 discloses a burner for the combustion of a low calorific gas, comprising a channel extending along an axis of the burner, for the supply of combustion air, and a channel for the fuel gas, which is designed for a large volume stream of low calorific fuel gas, the gas channel and the air channel opening into a mixing zone.
• the air channel has an immediately adjacent mouth area (flow technique) of the mixing zone and a swirl element for the production of turbulent combustion air is provided in the mouth zone. and swirl fins are disposed in the air channel upstream of the swirl element. Because of its configuration, this burner does not minimize the production of nitrogen oxides, and there are risks of pulsations of the flame. In addition, it is not suitable for poor gases containing tar because the tars are likely to condense on the cold wall of the duct and the lean gas introduction duct is sensitive to fouling (annular zone). The air-gas mixture is probably not very uniform.
• US Pat. No. 7,003,957 relates to a synthesis gas burner.
• the fuel gas is injected through radially inclined holes to the center of the combustion chamber, having a diameter D and an angle of injection alpha. These holes are placed at the exit of the burner, namely at the end of the swirl space.
• Diameter D and angle alpha are specific parameters that are appropriately selected by those skilled in the art based on different variables (specific gas composition, emissions, etc.).
• This burner is very sensitive to fouling because the injection of the lean gas is through holes, so the burner is not suitable for the presence of tars in the lean gas. It is a burner without pilot flame, which poses a problem to ensure the stability of combustion. Because of its configuration, this burner certainly produces a lot of nitrogen oxides, and there are risks of pulsations of the flame.
• patent EP 0 008 842 describes a burner capable of simultaneously burning several gaseous fuels of different heat capacities.
• the multi-burner Gaseous fuel utilizes pre-heated forced draft air, and comprises a cylindrical inner burner tube, means being provided for injecting through the upstream end of combustion air preheated to a selected temperature and compressed to a selected pressure.
• the downstream end of the inner burner tube is closed, and a plurality of longitudinal slots are circumferentially spaced in the wall of the tube at the closed end.
• Means are provided for injecting a rich fuel gas under a selected pressure into the inner burner tube along its axis.
• An outer burner tube axially surrounds the inner burner tube and forms an annular passage.
• Means are also provided for passing lean fuel gas at low pressure into the annular passage and out through a peripheral slot at the end of the outer burner tube into the furnace.
• This burner is very sensitive to fouling because the injection of lean gas is through holes, the burner is not suitable for the presence of tars in the lean gas. It is a burner without pilot flame, which poses a problem to ensure the stability of combustion. Because of its configuration, this burner certainly produces a lot of nitrogen oxides, and there are risks of pulsations of the flame. This burner produces a flat flame, without the possibility of extending it, which destines it to specific furnaces.
• EP 0 780 630 B1 (Alstom) describes a burner comprising a whirlpool followed by a tube, this tube itself being followed by the actual combustion chamber (in the direction of the gas flow).
• the junction zone between the tube and the combustion chamber (called “A” in the patent description) has a particular shape that allows the formation of a "detachment edge" whose role is to stabilize a reflux zone.
• This ebb area plays the role of a "flame catchper”.
• This burner is very sensitive to fouling because the injection of the lean gas is through holes, the burner is not suitable for the presence of tars in the lean gas. It is a burner without pilot flame, which poses a problem to ensure the stability of combustion. Because of its configuration, this burner certainly produces a lot of nitrogen oxides, and there are risks of pulsations of the flame.
• a first object of the invention is to provide an industrial burner adapted to the combustion of lean gas, that is to say having a low PCI (low calorific value) and whose PCI may be variable depending on the composition of the supply gas.
• this lean gas is also available at a high temperature (up to 600 ° C).
• the lean gas can also be loaded with tars and solid particles, it is therefore necessary to have a burner in which a good air-fuel mixture can be made without hindrance to the flow to prevent fouling of said obstacles.
• Another object of the invention is to provide a lean gas burner, and in particular synthesis gas obtained from the gasification of biomass air, which can replace an existing burner in an installation.
• the synthesis gas burner must have a design such that one can adjust the length and / or the flame diameter according to the geometry of the existing combustion chamber with which it is associated.
• a gas burner for burning a gas with a low calorific value, such as synthesis gas resulting from biomass gasification
• the burner being of substantially cylindrical shape, and comprising a first annular zone formed between the wall external burner and an inner wall of the burner substantially parallel to the outer wall, a second annular zone formed between the outer wall of the burner and the inner wall downstream of the first zone, and the burner further comprising a feed duct gas with a low calorific value substantially parallel to the burner axis, a primary air supply duct formed in the outer wall and opening into the first annular zone, a secondary air supply duct formed in the outer wall and opening in the second annular zone, an annular slot for introducing the primary air of the first annular zone into the zone of combi utilization, said annular gap being formed between the outer wall and the upstream end of the inner wall, secondary air introduction orifices of the second annular zone in the combustion zone, said orifices being pierced in the inner wall; said burner being further distinguished by the fact that the
• the annular slot is formed by means of a so-called "air introduction” piece located at the upstream end of the internal wall of the burner.
• This air introduction piece has a lip shape; more precisely, it has a conical portion diverging from the upstream downstream forming with the inner wall of the burner an angle of between 20 ° and 45 °, and a so-called “extrados” portion terminating on a trailing edge which allows to direct said annular air sheet become conical in the desired profile to form a compression zone located on the axis of the burner.
• the compression zone comes into contact with the flow of lean gas to allow a good air-fuel mixture.
• the air introduction piece has a flat upstream edge perpendicular to the burner axis and substantially parallel to a flat surface of the outer wall of the burner, thereby creating a rectified air flow perpendicular to the axis. burner.
• the conical part of the air introduction piece is followed by a rounded portion along a radius of curvature r1, itself followed by a plane upstream edge, and the extrados portion follows the upstream plane edge, and is constituted by a first rounded portion with a radius of curvature r2 followed by a second portion consisting of three successive flat profiles forming respective angles ⁇ 1, ⁇ 2 and ⁇ 3 with the plane of the upstream edge, the angles ⁇ 1, ⁇ 2 and ⁇ 3 being respectively between 30 and 80 °.
• the secondary air inlet orifices are of cylindrical or oblong section, and are distributed in the part of the internal wall of the burner facing the zone of secondary air introduction and have a unit diameter of between 3 and 15 mm, so as to allow the introduction of secondary air at a speed between 10 and 50 m / s.
• the axes of the secondary air inlet orifices are inclined at angles between 15 and 40 °, and preferably substantially equal to 25 ° with respect to the plane perpendicular to the axis of the burner.
• the axes of the orifices are further inclined at angles between 10 and 25 ° and preferably substantially equal to 15 °, with respect to the radius of the cylinder formed by the burner and passing through the orifice, so as to allow optimal swirling of the secondary air.
• Yet another object of the invention is to be able to supply the burner with a supplement of fossil fuel to increase the PCI if necessary, or to increase the total power supplied, and / or to be able to have a pilot flame powered with a fossil fuel.
• Yet another object of the invention is to allow operation with a fossil fuel substitution at 100% of the nominal power.
• the burner can only work with a fossil fuel supply. This mode of operation can be useful in case of rupture of the supply of lean gas.
• the burner according to the invention comprises a control means comprising a memory and regulating the flow rate of air introduced for each rate and ratio of lean gas / fossil fuel, as a function of operating points parameterized and set in memory.
• Another object of the invention is to reduce the temperature of the internal wall of the burner so as to limit its thermal fatigue. Yet another object of the invention is to reduce the temperature of the outer wall of the burner so as to limit the need for thermal insulation. Yet another object of the invention is to preheat the primary air and secondary combustion air, so as to improve the quality of combustion.
• Another object of the invention is the use of the burner according to the invention in ovens, boilers or dryers.
• Yet another object of the invention is an installation comprising a burner according to the invention, associated with a biomass gasifier.
• the burner according to the invention was developed for the combustion of lean gas, and in particular synthesis gas (or syngas) resulting from the gasification of biomass.
• the burner according to the invention combines two air flows for a staged combustion.
• Staged combustion involves introducing either combustion air or fuel into the flame at different stages.
• a portion of the combustion air typically of the order of 5 to 50%, is supplied to a zone primary combustion with all the fuel. This results in a fuel-rich zone and the formation of nitrogen oxides is reduced.
• the rest of the air is injected further downstream, forming a secondary flame zone, where combustion is complete.
• the primary and secondary air flows are formed as follows:
• the stability of the flame in the burner according to the invention is effective at all stages of combustion by combining the axial and rotary modes of the primary and secondary oxidizing air streams respectively.
• this mode of combustion allows to vary the relative contribution of different fuels, including synthesis gas, natural gas and propane, depending on the desired power and the availability of said fuels.
• the burner can support a mixed lean gas / fossil fuel input in varying proportions from 100% lean gas to 100% fossil fuel.
• the quality of combustion depends on the quality of the air-fuel mixture. More specifically, it is important to achieve the air-fuel mixture as uniform as possible to limit hot spots and thus minimize the formation of nitrogen oxides.
• the staged combustion used in the burner according to the invention also requires rapid mixing of fuel and air.
• Various devices are used in existing burners to improve the quality of the mixture, such as baffles, fins, perforated plates or impact plates ("impact plate” means a screen placed perpendicular to the flow in its axial part). All these devices have the disadvantage of creating an obstacle to the flow and are therefore sensitive to fouling.
• An advantage of the burner according to the invention is that it allows an optimal air-fuel mixture while presenting no obstacle to the flow.
• the quality of mixing is ensured in particular by the particular shape of the primary air flow.
• the annular slot has a shape such that the primary air is brought into the combustion zone in the form of a conical air space that supports or drives the fuel streams (lean gas and fossil fuel).
• the burner according to the invention was designed to be able to burn mainly a lean gas and more particularly the synthesis gas resulting from the gasification of the biomass.
• the burner according to the invention is also capable of burning a traditional fuel such as natural gas, propane, or even domestic fuel.
• the burner according to the invention is a mixed burner that can operate indifferently to synthesis gas, natural gas or propane or with a mixture of these different fuels (especially with a mixture of synthesis gas and fossil fuels).
• its particular design gives it a great flexibility of use, with a possible modulation of a 100% operation of fossil fuel to an operation with 100% of lean gas, in particular gas resulting from the conversion of biomass .
• the amount of combustion air is adjusted to the fuel mixture that is supported by the burner.
• this adjustment is achieved by means of a control means, such as a control automaton, which makes it possible to supply an air flow calculated for each rate and for each ratio of lean gas / fossil fuel, as a function of operating points. set and stored.
• a lambda probe also measures the oxygen content of the combustion fumes, which makes it possible to refine the control of the combustion air flow rate.
• the adjustment of the air flow is generally (total flow of primary air and secondary air).
• the burner according to the invention is equipped with a pilot burner for ignition and flame safety. The pilot flame is mandatory in some cases for safety reasons (EN 746-2 standard).
• FIGS 1, 2 and 3 illustrate an embodiment of the burner according to the invention.
• Figure 1 is a front view of the burner according to the invention.
• Figure 2 is a view of the burner according to the invention in section along the plane A - Figure 1.
• FIG. 3 is an enlarged view of detail B of FIG.
• the burner according to the invention has a substantially cylindrical shape. It has an outer wall 16, and an inner wall 17 separated from the wall 16 to form annular zones 5 and 8. These zones 5 and 8 are separated from each other by a partition 20.
• the first annular zone 5 is used for the introduction of the primary air into the combustion zone 7.
• the second annular zone 8 is used for the introduction of secondary air into the combustion zone 7.
• a conduit 1 allows the introduction of lean gas into the burner.
• the lean gas introduction duct 1 is cylindrical, and its diameter is calculated as a function of the amount of lean gas to be supported.
• the rate of introduction of the lean gas into the burner is generally between 5 and 30 m / s, and preferably between 15 and 25 m / s.
• a conduit 2 allows the introduction of fossil fuel (natural gas, propane or domestic fuel oil in particular).
• the fossil fuel introduction pipe 2 is cylindrical preference. Its diameter is calculated according to the amount of fuel gas to be supported.
• the rate of introduction of the fossil fuel into the burner is between 5 and 30 m / s (preferably between 15 and 25 m / s).
• a liquid fuel domestic fuel
• it is sprayed by a specific injector (not shown).
• a duct 3 allows the introduction of primary air into the annular zone 5.
• the primary air introduced into the annular zone 5 through the duct 3 is then directed towards an annular slot 6 which is shaped to create a blade cone air and a compression zone in zone 7. It is this specific configuration of the burner according to the invention which allows a good mixture of the primary air with the fuel.
• the primary air velocity is 20 to 200 m / s at the lip or the annular gap 6.
• the flow of primary air is in laminar flow.
• the air introduction piece 14 has a flat upstream edge 19 perpendicular to the axis of the burner and substantially parallel to a flat surface of the outer wall 16 of the burner, thereby creating a rectified air flow perpendicular to the axis of the burner.
• the profile of the air introduction part 14 supports the flow of air to direct it, without modification of its laminar flow, to an area located substantially on the axis of the burner.
• the conical air knife is intended primarily to achieve a good air-fuel mixture, but it also allows to protect the inner wall of the burner, especially in the case where the lean gas is loaded with tars and particles.
• a duct 4 allows the introduction of secondary air into the annular zone 8.
• the secondary air introduced into the annular zone 8 via the duct 4 is directed towards a set of injection orifices 9 making it possible to put the secondary air in rotation or swirl.
• the rotation of the secondary air makes it possible to avoid the stall of the high-power flame. It also helps to avoid the pulsations of the flame responsible for vibration phenomena that might otherwise occur at certain powers and for certain air / fuel ratios.
• the orifices 9 are orifices of cylindrical or oblong section.
• the secondary air introduction orifices 9 pierced in the internal wall 17 of the burner preferably have a unit diameter of 3 to 15 mm, thus allowing the injection of secondary air at speeds of between 10 and 50 m / s. and preferably between 20 and 40 m / s.
• the inner wall 17 of the burner has a divergent conical shape (ie widening downstream) in its downstream portion, at the level of the secondary air introduction zone.
• the orifices 9 are distributed in the conical portion of the inner wall 17 of the burner.
• the axes of the orifices 9 are inclined at angles between 15 and 40 °, and preferably substantially equal to 25 ° relative to the plane perpendicular to the burner axis.
• the axes of the orifices 9 are further inclined at angles between 10 and 25 ° and preferably substantially equal to 15 °, relative to the "radius of the cylinder formed by the burner and passing through the orifice", of in order to allow optimal swirling of the secondary air.
• the compression zone is generally constituted by a line segment located substantially on the axis of the burner.
• the compression zone is obtained by the flow of air in laminar flow whose trajectory is rectified by the profile of the lip ("in extrados").
• the rectified annular air knife forms a cone whose thickness increases as it approaches the vertex.
• the passages 10, 11 and 12 shown in Figure 2 allow the implantation of a conventional ignition member such as an ionization probe or a burner creating a pilot flame (not shown) or a flame detector.
• the passages 10, 11 and 12 can also be used to implant one or more additional fossil fuel feedstocks to allow operation of the burner according to the invention with this type of fuel over a wide range of power. These passages are not limited in number. Depending on the power of the burner, one can imagine more passages for the supply of fossil fuels, a pilot flame and / or a flame detector.
• Detail B of Figure 1 is shown in detail in Figure 3. It shows a particular form of the annular slot 6 for introducing the primary air into the combustion zone in the form of a conical blade.
• the shape of the annular slot 6 shown in FIG. 3 has been designed to minimize pressure drops.
• the annular slot 6 itself is formed by the space between a part 14 called “primary air introduction” into the burner, and the "bottom" of the outer wall 16 burner.
• the primary air introduction part 14 is positioned at the upstream end 25 of the inner wall 17 of the burner.
• the primary air introduction piece 14 is preferably formed in one piece with the inner wall 17.
• the primary air introduction part 14 has a conical portion diverging from downstream upstream 15 forming with the inner wall 17 of the burner an angle ⁇ , the part conical 15 to create a blade of air.
• the angle a is between 20 and 45 °.
• the conical part 15 makes it possible to avoid a large recirculation of the air in the annular zone and thus to limit the pressure drop.
• the conical portion 15 is followed by a rounded portion 18 with a radius of curvature r1, preferably between 3 and 15 mm.
• the rounded portion 18 also makes it possible to limit the recirculations of the air inside the annular zone 5.
• the sharp angles disturb the air circulation by creating micro-zones of turbulence which increase the air flow. loss of load, that is why it is preferred to use a rounded portion 18 rather than a right angle.
• the rounded portion 18 is itself followed by a plane upstream edge 19 substantially parallel to the "bottom" of the outer wall 16 of the burner.
• This upstream plane edge is then followed by a portion 13 having a shape called “extrados" which allows to direct the air gap in the desired profile, to form a compression zone on the burner axis.
• the upper portion 13 is constituted by a first portion 21 rounded with a radius of curvature r2, preferably between 8 and 30 mm, followed by a second portion consisting of three successive flat profiles 22, 23, 24 forming respective angles. ⁇ 1, ⁇ 2 and ⁇ 3 with the plane of the upstream plane plane 19, the angles ⁇ 1, ⁇ 2 and ⁇ 3 preferably being respectively between 30 and 80 °.
• the burner according to the invention in combination with a gasifier and especially in combination with a biomass gasifier, allows the total or partial substitution of a fossil fuel (fuel oil, natural gas, propane) with solid biomass for the production of heat.
• a fossil fuel fuel oil, natural gas, propane
• Usable biomass fuels include wood chips, crushed pallets, wood pellets and agricultural co-products.
• the co-current fixed bed gasifier described in the patent application WO 2013/098525 in the name of Cogebio is particularly suitable for operating in association with the burner according to the invention.
• This co-current fixed bed gasifier comprises a reactor body, said reactor body comprising an upper portion and a lower portion, and the biomass is introduced through an inlet conduit located at the top of the upper part of the body of the reactor.
• said gasifier comprises, from top to bottom: a pyrolysis zone of the biomass, an oxidation zone of the biomass, a reduction zone, a grid comprising a plurality of openings through which the ashes to be evacuated, and said gasifier also comprises means for introducing a gasification agent, such as air or oxygen, and said gasifier being characterized in that said means for introducing the gasification agent comprise: a cone of diffusion of the gasification agent situated at the top of the oxidation zone of the gasifier or above said oxidation zone, and means of injection of the gasification agent located in the oxidation zone of the gasifier.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Oil, Petroleum & Natural Gas (AREA)
• Organic Chemistry (AREA)
• Pre-Mixing And Non-Premixing Gas Burner (AREA)

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• 2013
  • 2013-10-14 FR FR1359968A patent/FR3011911B1/fr not_active Expired - Fee Related
• 2014
  • 2014-10-06 EP EP14799187.1A patent/EP3058275A1/fr not_active Withdrawn
  • 2014-10-06 CA CA2925737A patent/CA2925737A1/fr not_active Abandoned
  • 2014-10-06 US US15/024,877 patent/US10378760B2/en not_active Expired - Fee Related
  • 2014-10-06 WO PCT/FR2014/052523 patent/WO2015055916A1/fr active Application Filing
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