EP1845306A1 - Gas burner for cooking oven - Google Patents
Gas burner for cooking oven Download PDFInfo
- Publication number
- EP1845306A1 EP1845306A1 EP20070105609 EP07105609A EP1845306A1 EP 1845306 A1 EP1845306 A1 EP 1845306A1 EP 20070105609 EP20070105609 EP 20070105609 EP 07105609 A EP07105609 A EP 07105609A EP 1845306 A1 EP1845306 A1 EP 1845306A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- flame
- burner
- main
- air flow
- zone
- 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.)
- Granted
Links
- 238000010411 cooking Methods 0.000 title claims description 9
- 239000000203 mixture Substances 0.000 claims abstract description 19
- 230000002093 peripheral effect Effects 0.000 claims abstract description 16
- 239000008246 gaseous mixture Substances 0.000 claims abstract description 15
- 239000007789 gas Substances 0.000 claims description 48
- 238000002485 combustion reaction Methods 0.000 claims description 35
- 229910052751 metal Inorganic materials 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 11
- 125000006850 spacer group Chemical group 0.000 claims description 5
- 230000003068 static effect Effects 0.000 claims description 3
- 239000003546 flue gas Substances 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 description 10
- 239000000567 combustion gas Substances 0.000 description 4
- 239000004020 conductor Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000005273 aeration Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000009940 knitting Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000001052 transient effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24C—DOMESTIC STOVES OR RANGES ; DETAILS OF DOMESTIC STOVES OR RANGES, OF GENERAL APPLICATION
- F24C3/00—Stoves or ranges for gaseous fuels
- F24C3/08—Arrangement or mounting of burners
- F24C3/085—Arrangement or mounting of burners on ranges
- F24C3/087—Arrangement or mounting of burners on ranges in baking ovens
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
- F23C3/002—Combustion apparatus characterised by the shape of the combustion chamber the chamber having an elongated tubular form, e.g. for a radiant tube
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- 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
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
- F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
- F23D14/08—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with axial outlets at the burner head
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- 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
- F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/10—Flame diffusing means
- F23D2203/103—Flame diffusing means using screens
-
- 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
- F23D2900/00019—Outlet manufactured from knitted fibres
Definitions
- the invention relates to the field of gas burners for kitchen ovens, for example, ovens used in large commercial or institutional kitchens.
- the energy produced by combustion is recovered in thermal form.
- the products of the combustion of gas pass through, for example, heat exchanger tubes where they are cooled to extract thermal energy.
- the combustion gases from the burner are substantially at atmospheric pressure.
- the mechanical energy of the combustion gases from the burner is a disadvantage generating vibrations and noise in the kitchen oven.
- the patent application EP 698 768 (Electrolux, Zanussi) describes a gas stove equipped with hollow heating elements traversed by combustion products from a gas burner.
- a disadvantage of this type of burner is to be limited in thermal power. Indeed, when the rate of mixing of air and flammable gas increases, the propagation speed of the combustion of the flame in the gas mixture stream may be lower than the flow rate of the mixture and the flame is detached from the burner. If the phenomenon is not quickly corrected, the flame is blown and extinguished. Conversely, if the gas mixture flow rate is lower than the propagation of the flame, it can go upstream of the burner.
- Another disadvantage of this type of furnace is that under the effect of thermal variations and the mechanical effects of the flue gas flow, the heating elements, brought to high temperature, can come into vibration. This causes an unpleasant noise and shortens the life of the oven.
- the patent application FR 2 708 083 (Gaz de France) describes a flame attachment plate for a gas burner.
- This plate acts as a sieve for distributing gaseous mixture fillets. She comprises a compressed network of intertwined wires.
- This structure allows a passage distributed, substantially uniformly, gas streams on the entire surface of the plate and a regular spread of the flame created.
- this type of burner has the disadvantage of being limited in thermal power per cm 2 of attachment plate.
- this type of burner seeks to produce flames of relatively low height and where the thermal power is located close to the attachment plate. It seems that this type of burner is suitable for heating, from the outside, domestic boiler water coils, for example. However, for kitchen ovens, we want to heat from inside the heat exchanger tubes. It is advantageous to spread the flame to reduce hot spots.
- the patent application EP 840 061 discloses a flame attachment device comprising a plurality of identical rings composed of a compressed network of interwoven wires.
- the gaseous mixture passes radially through the rings.
- Each of the rings gives rise to a radial circular flame.
- the rings are coaxial and superimposed on each other and separated by solid spacers not traversed by the gas mixture.
- the outer diameter of the solid spacers is smaller than the outer diameter of the compressed network rings. Pilot flames are formed in the grooves corresponding to the spacers.
- Requirement US 2006/0 035 189 discloses a burner having porous body members of tubular form.
- the wall of the tube is in a compressed network of wires.
- Several tubular shapes are interlocked axially to form a larger burner.
- the stabilization of the flame is improved by a deflector plate.
- the thermal energy is disengaged radially with respect to the axis of the burner.
- the patent US 5,199,416 (Rational GmbH) describes a burner head where a closed combustion chamber opens onto several heat exchanger tubes through which the combustion gases pass. An enclosure surrounding the combustion chamber brings fresh air to the inlet of the heat exchanger tubes to reduce the transition temperature between the combustion chamber and the heat exchange tubes.
- the air contributing to the combustion of the flammable gas is entirely contained in the gas mixture upstream of the combustion chamber.
- the combustion products are evacuated through the exchanger tubes through an outlet manifold.
- the disadvantage of this type of burner is that in order to limit the non-oxidized combustion products by combustion, it is necessary to introduce into the gas mixture passing through the burner an excess of air relative to the stoichiometric proportions of the gas. For a given burner thermal power, the air supercharging can cause a detachment of the flame. Or, for the same limit of flame separation, the air supercharging reduces the thermal power of the flame.
- the invention proposes a burner for a kitchen gas oven that overcomes the above drawbacks and in particular that increases the thermal energy of the burner, avoiding detachment of the flame, and spreading said flame.
- the burner for a kitchen gas oven comprises a device for attaching the flame of the burner, separating a flame from a mixing chamber adapted to receive a main air flow and gas to constitute a gaseous mixture.
- the device for attaching the flame is provided with a lattice comprising metal wires, able to pass said gas mixture through the trellis, which trellis comprises at least one main zone and an adjacent pilot zone.
- the pilot zone has, in a main direction of the burner flame, a thickness greater than the thickness of the main zone, able to slow down the gaseous mixture passing through the pilot zone relative to the mixture crossing the main zone.
- the burner comprises at least one orifice adapted to receive a secondary air flow.
- pilot zone lattice zone is thicker in the direction of the burner flame, makes the gaseous mixture streams passing through the pilot zone are slowed down by a path traveled. in lattice longer than those crossing the main zone.
- the nets passing through the pilot zone have a lower speed than those crossing the main zone and can feed a small flame called "pilot flame” which is not likely to drop from said pilot zone.
- the flow rate of gaseous mixture in the main zone can be increased.
- the pilot flame initiates the start of combustion of the gas streams leaving the main zone.
- the thermal power of the burner is increased. This increase in power is accompanied by an increase in the length of the flame but not in its temperature. This can help prevent hot spots.
- the main zone of the lattice has a porosity of between 60% and 90%.
- the main zone of the compressed mesh has a thickness of between 3 and 8 mm.
- the thickness ratio of the pilot zone on the main zone is between 2 and 5.
- the burner comprises means for guiding the flow of secondary air towards the flame.
- the secondary air stream burns the combustion residues from the mixing chamber.
- the mixed gas flow rate can be increased, for example up to the stoichiometric proportion of the main air flow, with a low risk of flame takeoff.
- the thermal power of the burner is increased, and the flame increases in temperature.
- the secondary air flow also makes it possible to regulate the flows of the combustion products, in particular to control the conditions of ignition and development of the flame, the quality of the combustion and the operating stability, irrespective of the aeration rate, optimal for combustion, chosen for the burner mixing chamber.
- the flame attachment device comprises a main disk perpendicular to the direction of the burner flame and a coaxial pilot ring superimposed on the periphery and downstream of the main disk.
- the ring and the disc each comprise a wire mesh.
- the orifice adapted to receive the secondary air flow is located at the periphery of the device for attaching the flame.
- the two possibilities of increasing the thermal power of the burner due to the pilot zone and the secondary air flow accumulate.
- This variant has the additional advantage that the pilot ring helps the separation of the secondary air flow and the flame leaving the main zone. This separation prevents secondary air from blowing the flame.
- fresh air arrives at the edge of the flame. This avoids having a hot spot at the location of the flame attachment device. This also helps to spread the flame lengthwise.
- the pilot zone and the main zone are adjacent and the pilot zone is further downstream than the main zone.
- the burner comprises a sealed enclosure connected to a fan and surrounding the mixing chamber and the or the secondary air orifices.
- the fan is connected, inside the enclosure, to the mixing chamber by a leak connection means adapted to introduce into the mixing chamber the main air flow and to divert the flow of air towards the enclosure. secondary air.
- the metal wires of the lattice are arranged to constitute, in the direction of the flame, a succession deviating obstacles capable of deflecting the trajectory of a stream of the gas stream.
- This has the advantage that the gaseous mixture streams are distributed substantially uniformly over the entire surface of the mesh.
- the multiple deviating obstacles locally reduce the passage section of the gas nets. This locally increases the speed of the gas streams and prevents the flame from rising upstream of the trellis.
- the mixing chamber is provided with a static suction device intended to be traversed by a main air flow and adapted to suck up flammable gas.
- the burner for a kitchen gas oven comprises a device for attaching a flame of the burner separating the flame from a mixing chamber of the gas.
- the attachment device of the flame is provided with a lattice in the compressed state comprising metal son able to pass said gas mixture through the mesh.
- the trellis comprises at least one adjacent main area and an adjacent pilot area.
- the pilot zone has, in the direction of the burner flame, a thickness greater than the thickness of the main zone.
- the burner for a cooking gas oven comprises a device for attaching a flame of the burner separating the flame from a mixing chamber adapted to receive a main air flow and gas.
- the burner comprises at least one orifice adapted to receive a secondary air flow, and means for guiding the flow of secondary air towards the flame.
- the invention relates to a cooking oven equipped with a burner described above wherein the flame of the burner is located in a combustion pipe, extended by at least one heat exchanger tube capable of driving gases. combustion; the oven comprising a cooking air fan and means for guiding the cooking air from the fan to the heat exchanger tube or tubes and a cooking zone of the oven.
- the burner comprises a propulsion unit 1 fixed on a fixing plate 2 and surrounded by a box 3.
- the propulsion unit 1 comprises a fan 4, a venturi device 5, an upstream sleeve 6 and a device
- the fastening plate 2 also receives an ignition device 8 and an exchanger assembly 9.
- the exchanger assembly 9 successively comprises a combustion pipe 10 fixed to the fixing plate 2, at least one heat exchanger tube 11 and an outlet 12.
- the fan 4 is of the centrifugal type and propels air sucked through the venturi device 5.
- the venturi device 5 is fixed rigidly opposite and at a distance from the outlet orifice of the fan 4.
- the connection device to leakage 16 comprises spacers 13, for example in the form of columns or washers which are pressed between an inlet plate 14 of the venturi device 4 and an outlet plate of the fan 4.
- the mechanical connection between the venturi device 5 and the fan 4 is rigid but not waterproof.
- the air from the fan 4 separates between a main flow 17 and a secondary flow 18.
- the venturi device 5 has an axial cavity in the form of two opposite conical frustums, through which the main stream 17 passes.
- the cavity is of slow and continuous variation of its section and has a diameter restriction 19 situated between an upstream portion 5a and a downstream part 5b.
- the progressive expansion of the main air flow 17 in the downstream part 5b of the venturi device causes a depression on the wall of the cavity.
- a transverse channel 20 opens into the cavity where the main stream 17 has a depression.
- the venturi device 5 is a static suction device capable of sucking gas flammable through the transverse channel 20 connected to a gas supply.
- the space delimited by the downstream part 5b of the venturi device 5, the upstream sheath 6 and the flame attachment device 7 constitutes a mixing chamber 21.
- the connection of the venturi device 5 and the upstream sheath 6 is sealed.
- the main stream of air 17 is mixed with the gas from the transverse channel 20 to form a gaseous mixture 26 which flows through the mixing chamber 21, passes through the attachment device 7, and is then ignited by the injection device. ignition 8.
- the ignition device 8 is constituted by a central conductor 22 and an insulating sheath 23 surrounding the central conductor 22 and fixed on the fixing plate 2 and is of the incandescent or spark type.
- a plurality of peripheral orifices 24 are formed in the fixing plate 2 around the hooking device 7 of the flame and open into the combustion pipe 10.
- the box 3 surrounds the propulsion assembly 1 and is connected to The fixing plate 2 and the casing 3 together form a sealed enclosure 25 traversed by an end 6a of the upstream sheath 6 receiving the attachment device 7, via the transverse channel 20, by the 4 and the peripheral orifices 24.
- the secondary air flow 18 escaping from the leakage connection device 16 is trapped in the enclosure 25 and can escape through the peripheral orifices 24.
- the space separating the inlet plate 14 of the venturi 5 and the outlet plate 15 of the fan 4 is adjusted so that the secondary air flow 18, escaping from the leakage connection device 16, has a higher pressure e at atmospheric pressure and greater than the pressure inside the combustion pipe 10.
- a secondary air flow 39 passes through the peripheral orifices 24 in the direction of the flame 27.
- the combustion pipe 10 has an elongate shape surrounding the flame attachment device 27, the peripheral ports 24 and the ignition devices 8.
- the chemical reaction The flow direction of the gaseous mixture 26, downstream of the hooking device 7 of the flame 27, defines a main direction 28 of the flame 27 of the flame 27 of the flammable gas with the air. burner.
- the chemical reaction converts the gaseous mixture 26 into combustion products and releases thermal energy.
- the thermal energy heats the combustion products which come into contact with the combustion pipe 10 and then flow inside the heat exchanger 11.
- the heat exchanger assembly 9 is also heated by direct radiation from the heat exchanger. thermal energy of the flame 27.
- the orifices 24 are located near the flame 27, allows a reliable ignition and without noise. Indeed, when the ignition device 8 ignites the gas mixture 26, the pressure in the combustion pipe 10 increases sharply. The orifices 24 contribute to absorbing the transient effect of the ignition and avoid an explosion noise that is encountered in closed exchangers on the side of the device 7 for attaching the flame 27.
- the possibility of being able to adjust the secondary air flow rate 39 makes it possible to regulate the flow rate passing through the exchanger assembly 9, and in particular the tube 11. This allows, without modifying the thermal power of the burner, to avoid the heating regimes. resonance of the exchanger assembly 9 and the noise that would result.
- the attachment device 7 of the flame 27 is housed inside the end 6a of the sheath 6 and comprises a main disc 31 passing through the entire internal cross section of the sheath 6.
- pilot ring 32 coaxial with the main disk 31, is superimposed downstream of the main disk 31, and is in radial contact with the inner surface of the end 6a of the sheath 6.
- the main disk 31 and the pilot ring 32 are all both consist of a mesh of wire 35, interwoven or knitted, then compressed. During compression, the metal wires undergo plastic deformation. The lattice 35 in the free state retains the shape obtained during its compression. The remaining space between the deformed metal son allows the passage of gaseous mixture threads 26 after multiple deviations. This makes it possible to harmonize the speeds of the threads passing through the trellis 35. An embodiment of such trellis is described in the patent application. FR 2 708 083 to which we can usefully refer.
- a ring 33 is provided with ribs 33a in the form of braces and fixed upstream of the main disk 31.
- Lugs 34 extend radially inwardly of the sheath 6 and are arranged downstream and at the periphery of the pilot ring 32.
- the ring 33 and the lugs 34 enclose the main disk 31 and the pilot ring 32 to support them mechanically, despite the temperature rise of the attachment device 7 of the flame 27 which can reach 1000 ° C.
- the pilot ring 32 may be of rectangular section, and has a singing surface 32a, downstream and perpendicular to the main direction 28, and an inner cylindrical surface 32b.
- One end 22a of the central conductor 22 of the ignition device 8 is disposed in the immediate vicinity of the edge surface 32a.
- a spark spring s from the end 22a of the central conductor 22 to the metal wires 35a of the mesh 35, connected to the electrical ground.
- the main disc 31 comprises a central portion 31a and a peripheral portion 31b above which is superimposed the ring 32.
- the gas mixture 26 is shared, through the attachment device 7, between central threads 36 passing through the central portion 31a and peripheral threads 37 passing through the peripheral portion 31b and the ring 32.
- the central threads 36 have a homogeneous propagation speed over the entire surface of the central portion 31a.
- the peripheral threads 37 are distributed in a zone of slow propagation 38 located along the edge surface 32a and the inner surface 32b.
- the surface of the peripheral portion 31b is much smaller than the sum of the edge surface 32a and the inner surface 32b. This widening of the surface and the greater thickness of mesh 35 to be traversed by the peripheral threads 37, compared to the central threads 36, that the speed of the peripheral threads 37, downstream of the pilot ring 32, is greatly reduced with respect to the speed of the central threads 36 having passed through the central portion 31a.
- the spark initiates the combustion of the gas mixture 37 in said slow propagation zone 38 in which the pilot flame is formed, which in turn initiates the combustion of the central threads 36.
- the central threads 36 are in contact, over the entire axial distance, with the pilot flame to enter combustion.
- the propagation speed of the central threads 36 can be greatly increased without the main flame 27 picking up.
- Such an arrangement of the attachment device makes it possible to greatly increase the gas mixture flow rate 26 and the thermal power of the burner.
- the secondary air stream 39 from the orifices 24, has a pressure greater than the pressure of the combustion products and constitutes a thermally insulating layer. This limits the temperature rise of an upstream portion 10a of the combustion pipe 10 located opposite the end 6a of the sheath 6 and the flame 27. This thermal insulation makes it possible to avoid a hot spot of the combustion pipe.
- the secondary air flow 39 is guided in such a way that the connection zone between the fixing plate 2 and the burner is kept at a low temperature. This allows the use of common seals and improves the life of the entire burner.
- the secondary air 39 supplies oxygen to the flame 27 so as to reduce the proportion of unburned gases, or incompletely oxidized oxides such as carbon monoxides.
- the fact that the peripheral orifices 24 are located around the attachment device of the flame 27 allows the secondary air 39 to be naturally guided towards the flame 27.
- the flow 39 of secondary air contributes to the stabilization of the flame 27.
- the main disk 31 is constituted by a knitting of metal son.
- the metal wires may be stainless steel, for example type 304L and a diameter between 0.1 and 0.4 mm, preferably of the order of 0.2 mm.
- the disc 31 has an outer diameter of between 50 and 70 mm, preferably between 55 and 60 mm, and for example 57.8 mm.
- the thickness of the disk 31 is between 3 and 8 mm, preferably of the order of 5 mm.
- the ring 32 consists of a knit of stainless steel wires, for example of the type 309, and of a diameter that is thicker than the wire of the main disc 31, preferably between 0.2 and 0.35 mm, for example of the order of 0.28 mm.
- the ring 32 has an inside diameter smaller than the diameter of the main disc 31, preferably between 35 and 45 mm, for example of the order of 40 mm.
- the ring 32 has an outer diameter preferably identical to the diameter of the main disk 31 and a height of between 5 and 25 mm, preferably between 10 and 20 mm, in particular between twice and five times the thickness of the main disk. 31.
- the thickness of the ring 32 may be of the order of 15 mm.
- the mesh 35 constituted by the compressed knit has, for the ring, as for the disc, a porosity between 60% and 90% of the outer volume of the mesh, preferably between 70% and 80% and for example about 75%. .
- the thermal power of the burner can be adjusted over a range ranging for example from 8 to 40 kilowatts, including playing, in addition to flow rate variations, on the chemical composition of the flammable gas.
- a device 7 for hooking the flame 27 of the burner combining a pilot zone 32 associated with the orifices 24 gives the burner a great flexibility.
- a single burner can equip a wide variety of furnaces and accommodate the differences in pressure drop of the heat exchanger 9 according to the size of the furnaces equipped.
- the same device 7 with the associated orifices 24 can be used with the different types of gas usually encountered in kitchens.
- the same device 7, with the associated orifices 24 can equip burners whose nominal powers vary over a wide range, for example from single to double constant gas type, or more, including changing the type of gas.
- the fact that the same device 7 with the associated orifices 24 covers a wide range of applications makes it possible to reduce the costs of production and storage of the spare parts necessary for the after-sales services of the commercial networks.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Abstract
Description
L'invention concerne le domaine des brûleurs à gaz pour fours de cuisine, par exemple, des fours utilisés dans les grandes cuisines commerciales ou institutionnelles.The invention relates to the field of gas burners for kitchen ovens, for example, ovens used in large commercial or institutional kitchens.
L'énergie produite par la combustion est récupérée sous forme thermique. Les produits de la combustion du gaz traversent, par exemple, des tubes échangeurs de chaleur où ils sont refroidis pour en extraire l'énergie thermique. A part les éventuelles pertes de charge dans les tubes échangeurs de chaleur ou dans des conduits de cheminées, les gaz de combustion issus du brûleur sont sensiblement à la pression atmosphérique. L'énergie mécanique des gaz de combustion issus du brûleur est un inconvénient engendrant des vibrations et du bruit dans le four de cuisine.The energy produced by combustion is recovered in thermal form. The products of the combustion of gas pass through, for example, heat exchanger tubes where they are cooled to extract thermal energy. Apart from any pressure losses in the heat exchanger tubes or in chimney ducts, the combustion gases from the burner are substantially at atmospheric pressure. The mechanical energy of the combustion gases from the burner is a disadvantage generating vibrations and noise in the kitchen oven.
La demande de brevet
La demande de brevet
La demande de brevet
La demande
Le brevet
L'invention propose un brûleur pour four à gaz de cuisine qui remédie aux inconvénients précédents et notamment qui permet d'augmenter l'énergie thermique du brûleur, en évitant des décollements de la flamme, et en étalant ladite flamme.The invention proposes a burner for a kitchen gas oven that overcomes the above drawbacks and in particular that increases the thermal energy of the burner, avoiding detachment of the flame, and spreading said flame.
Selon un mode de réalisation, le brûleur pour four à gaz de cuisine comprend un dispositif d'accrochage de la flamme du brûleur, séparant une flamme d'une chambre de mélange apte à recevoir un flux d'air principal et du gaz pour constituer un mélange gazeux. Le dispositif d'accrochage de la flamme est muni d'un treillis comprenant des fils métalliques, apte à laisser passer ledit mélange gazeux à travers le treillis, lequel treillis comprend au moins une zone principale et une zone pilote adjacentes. La zone pilote présente, selon une direction principale de la flamme du brûleur, une épaisseur supérieure à l'épaisseur de la zone principale, apte à ralentir le mélange gazeux traversant la zone pilote par rapport au mélange traversant la zone principale. Le brûleur comprend au moins un orifice apte à recevoir un flux d'air secondaire.According to one embodiment, the burner for a kitchen gas oven comprises a device for attaching the flame of the burner, separating a flame from a mixing chamber adapted to receive a main air flow and gas to constitute a gaseous mixture. The device for attaching the flame is provided with a lattice comprising metal wires, able to pass said gas mixture through the trellis, which trellis comprises at least one main zone and an adjacent pilot zone. The pilot zone has, in a main direction of the burner flame, a thickness greater than the thickness of the main zone, able to slow down the gaseous mixture passing through the pilot zone relative to the mixture crossing the main zone. The burner comprises at least one orifice adapted to receive a secondary air flow.
On conçoit que dans un tel brûleur, le fait qu'une zone de treillis dite « zone pilote » soit plus épaisse dans la direction de la flamme du brûleur, fait que les filets de mélange gazeux traversant la zone pilote sont ralentis par un chemin parcouru dans le treillis de plus grande longueur que ceux traversant la zone principale. Les filets traversant la zone pilote présentent une vitesse inférieure à ceux traversant la zone principale et peuvent alimenter une flamme de petite dimension appelée « flamme pilote » qui ne risque pas de décrocher de ladite zone pilote. Le débit de mélange gazeux dans la zone principale peut être augmenté. La flamme pilote initie un début de combustion des filets de gaz sortant de la zone principale. La puissance thermique du brûleur est augmentée. Cette augmentation de la puissance s'accompagne d'une augmentation de la longueur de la flamme mais pas de sa température. Cela peut permettre d'éviter l'apparition de points chauds.It is understood that in such a burner, the fact that a so-called "pilot zone" lattice zone is thicker in the direction of the burner flame, makes the gaseous mixture streams passing through the pilot zone are slowed down by a path traveled. in lattice longer than those crossing the main zone. The nets passing through the pilot zone have a lower speed than those crossing the main zone and can feed a small flame called "pilot flame" which is not likely to drop from said pilot zone. The flow rate of gaseous mixture in the main zone can be increased. The pilot flame initiates the start of combustion of the gas streams leaving the main zone. The thermal power of the burner is increased. This increase in power is accompanied by an increase in the length of the flame but not in its temperature. This can help prevent hot spots.
Avantageusement, la zone principale du treillis présente un taux de porosité entre 60% et 90%.Advantageously, the main zone of the lattice has a porosity of between 60% and 90%.
Avantageusement, la zone principale du treillis comprimé présente une épaisseur comprise entre 3 et 8 mm.Advantageously, the main zone of the compressed mesh has a thickness of between 3 and 8 mm.
Avantageusement, le rapport d'épaisseur de la zone pilote sur la zone principale est compris entre 2 et 5.Advantageously, the thickness ratio of the pilot zone on the main zone is between 2 and 5.
Selon un autre mode de réalisation, le brûleur comprend un moyen pour guider le flux d'air secondaire vers la flamme. On conçoit que dans cet autre mode de réalisation, le flux d'air secondaire permet de brûler les résidus de combustion issus de la chambre de mélange. Le débit de gaz mélangés peut être augmenté, par exemple jusqu'à la proportion stoechiométrique du flux d'air principal, avec un faible risque de décollage de la flamme. La puissance thermique du brûleur est augmentée, et la flamme augmente en température. Le flux d'air secondaire permet en outre de régler les écoulements des produits de combustion, en particulier pour maîtriser les conditions d'allumage et de développement de la flamme, la qualité de la combustion et la stabilité de fonctionnement, indépendamment du taux d'aération, optimal pour la combustion, choisi pour la chambre de mélange du brûleur.According to another embodiment, the burner comprises means for guiding the flow of secondary air towards the flame. It is conceivable that in this other embodiment, the secondary air stream burns the combustion residues from the mixing chamber. The mixed gas flow rate can be increased, for example up to the stoichiometric proportion of the main air flow, with a low risk of flame takeoff. The thermal power of the burner is increased, and the flame increases in temperature. The secondary air flow also makes it possible to regulate the flows of the combustion products, in particular to control the conditions of ignition and development of the flame, the quality of the combustion and the operating stability, irrespective of the aeration rate, optimal for combustion, chosen for the burner mixing chamber.
Selon une variante, le dispositif d'accrochage de flamme comprend un disque principal perpendiculaire à la direction de la flamme du brûleur et un anneau pilote, coaxial, superposé en périphérie et en aval du disque principal. L'anneau et le disque comprennent chacun un treillis de fils métalliques.According to a variant, the flame attachment device comprises a main disk perpendicular to the direction of the burner flame and a coaxial pilot ring superimposed on the periphery and downstream of the main disk. The ring and the disc each comprise a wire mesh.
Avantageusement, l'orifice apte à recevoir le flux d'air secondaire est situé en périphérie du dispositif d'accrochage de la flamme.Advantageously, the orifice adapted to receive the secondary air flow is located at the periphery of the device for attaching the flame.
Dans cette variante, les deux possibilités d'augmentation de la puissance thermique du brûleur dues à la zone pilote et au flux d'air secondaire se cumulent. Cette variante présente un avantage supplémentaire du fait que l'anneau pilote aide à la séparation du flux d'air secondaire et de la flamme sortant de la zone principale. Cette séparation évite que l'air secondaire ne souffle la flamme. De plus, de l'air frais arrive en périphérie de la flamme. Cela évite d'avoir un point chaud à l'endroit du dispositif d'accrochage de la flamme. Cela contribue également à étaler en longueur la flamme. Par ailleurs, la zone pilote et la zone principale sont adjacentes et la zone pilote est plus en aval que la zone principale. Ces deux caractéristiques ont comme effet qu'une partie des filets sortant de la zone pilote peut rejoindre, à vitesse réduite, les filets sortant de la zone principale. Cela peut permettre une transition de débit du mélange entre la zone principale à haut débit et la zone pilote.In this variant, the two possibilities of increasing the thermal power of the burner due to the pilot zone and the secondary air flow accumulate. This variant has the additional advantage that the pilot ring helps the separation of the secondary air flow and the flame leaving the main zone. This separation prevents secondary air from blowing the flame. In addition, fresh air arrives at the edge of the flame. This avoids having a hot spot at the location of the flame attachment device. This also helps to spread the flame lengthwise. In addition, the pilot zone and the main zone are adjacent and the pilot zone is further downstream than the main zone. These two characteristics have the effect that part of the nets leaving the pilot zone can join, at reduced speed, the nets leaving the main zone. This can allow a flow transition of the mixture between the main broadband zone and the pilot zone.
Selon une autre variante, le brûleur comprend une enceinte étanche raccordée à un ventilateur et entourant la chambre de mélange ainsi que le ou les orifices d'air secondaire. Le ventilateur est relié, à l'intérieur de l'enceinte, à la chambre de mélange par un moyen de raccordement à fuite apte à introduire dans la chambre de mélange le flux d'air principal et à dévier vers l'enceinte le flux d'air secondaire.According to another variant, the burner comprises a sealed enclosure connected to a fan and surrounding the mixing chamber and the or the secondary air orifices. The fan is connected, inside the enclosure, to the mixing chamber by a leak connection means adapted to introduce into the mixing chamber the main air flow and to divert the flow of air towards the enclosure. secondary air.
Avantageusement, les fils métalliques du treillis sont agencés pour constituer, selon la direction de la flamme, une succession d'obstacles déviants apte à dévier la trajectoire d'un filet du flux gazeux. Cela présente l'avantage que les filets de mélange gazeux se répartissent de manière sensiblement uniforme sur toute la surface du treillis. De plus, les multiples obstacles déviants réduisent localement la section de passage des filets de gaz. Cela augmente localement la vitesse des filets de gaz et empêche que la flamme ne remonte en amont du treillis.Advantageously, the metal wires of the lattice are arranged to constitute, in the direction of the flame, a succession deviating obstacles capable of deflecting the trajectory of a stream of the gas stream. This has the advantage that the gaseous mixture streams are distributed substantially uniformly over the entire surface of the mesh. In addition, the multiple deviating obstacles locally reduce the passage section of the gas nets. This locally increases the speed of the gas streams and prevents the flame from rising upstream of the trellis.
Avantageusement, la chambre de mélange est munie d'un dispositif statique d'aspiration destiné à être traversé par un flux d'air principal et apte à aspirer du gaz inflammable.Advantageously, the mixing chamber is provided with a static suction device intended to be traversed by a main air flow and adapted to suck up flammable gas.
Selon un autre mode de réalisation, le brûleur pour four à gaz de cuisine comprend un dispositif d'accrochage d'une flamme du brûleur séparant la flamme d'une chambre de mélange du gaz. Le dispositif d'accrochage de la flamme est muni d'un treillis à l'état comprimé comprenant des fils métalliques, apte à laisser passer ledit mélange gazeux à travers le treillis. Le treillis comprend au moins une zone principale et une zone pilote adjacentes. La zone pilote présente, selon la direction de la flamme du brûleur, une épaisseur supérieure à l'épaisseur de la zone principale.According to another embodiment, the burner for a kitchen gas oven comprises a device for attaching a flame of the burner separating the flame from a mixing chamber of the gas. The attachment device of the flame is provided with a lattice in the compressed state comprising metal son able to pass said gas mixture through the mesh. The trellis comprises at least one adjacent main area and an adjacent pilot area. The pilot zone has, in the direction of the burner flame, a thickness greater than the thickness of the main zone.
Selon un autre mode de réalisation, le brûleur pour four à gaz de cuisine comprend un dispositif d'accrochage d'une flamme du brûleur séparant la flamme d'une chambre de mélange apte à recevoir un flux d'air principal et du gaz. Le brûleur comprend au moins un orifice apte à recevoir un flux d'air secondaire, et un moyen pour guider le flux d'air secondaire vers la flamme.According to another embodiment, the burner for a cooking gas oven comprises a device for attaching a flame of the burner separating the flame from a mixing chamber adapted to receive a main air flow and gas. The burner comprises at least one orifice adapted to receive a secondary air flow, and means for guiding the flow of secondary air towards the flame.
Selon un autre aspect, l'invention concerne un four de cuisine équipé d'un brûleur décrit ci-dessus dans lequel la flamme du brûleur est située dans un tuyau de combustion, prolongé par au moins un tube échangeur de chaleur apte à conduire des gaz de combustion ; le four comprenant un ventilateur d'air de cuisson et des moyens de guidage de l'air de cuisson depuis le ventilateur vers le ou les tubes échangeurs thermiques et une zone de cuisson du four.According to another aspect, the invention relates to a cooking oven equipped with a burner described above wherein the flame of the burner is located in a combustion pipe, extended by at least one heat exchanger tube capable of driving gases. combustion; the oven comprising a cooking air fan and means for guiding the cooking air from the fan to the heat exchanger tube or tubes and a cooking zone of the oven.
D'autres caractéristiques et avantages apparaîtront à la lecture de la description détaillée de quelques modes de réalisation pris à titre d'exemples non limitatifs et illustrés par les dessins annexés, selon lesquels :
- la figure 1 est une représentation schématique en coupe du brûleur; et
- la figure 2 est une vue de détail du dispositif d'accrochage du brûleur.
- Figure 1 is a schematic sectional view of the burner; and
- Figure 2 is a detail view of the attachment device of the burner.
Comme illustré en figure 1, le brûleur comprend un ensemble propulseur 1 fixé sur une plaque de fixation 2 et entouré d'un caisson 3. L'ensemble propulseur 1 comprend un ventilateur 4, un dispositif venturi 5, une gaine amont 6 et un dispositif d'accrochage 7 d'une flamme 27. La plaque de fixation 2 reçoit également un dispositif d'allumage 8 et un ensemble échangeur 9. L'ensemble échangeur 9 comprend successivement un tuyau de combustion 10 fixé sur la plaque de fixation 2, au moins un tube échangeur de chaleur 11 et une sortie 12.As illustrated in FIG. 1, the burner comprises a propulsion unit 1 fixed on a fixing
Le ventilateur 4 est du type centrifuge et propulse de l'air aspiré à travers le dispositif venturi 5. Le dispositif venturi 5 est fixé rigidement en regard, et à distance, de l'orifice de sortie du ventilateur 4. Le dispositif de raccordement à fuite 16 comprend des entretoises 13, par exemple en forme de colonnettes ou de rondelles qui sont pressées entre une platine 14 d'entrée du dispositif venturi 4 et une platine 15 de sortie du ventilateur 4. La liaison mécanique, entre le dispositif venturi 5 et le ventilateur 4, est rigide mais non étanche. L'air issu du ventilateur 4 se sépare entre un flux principal 17 et un flux secondaire 18.The
Le dispositif venturi 5 présente une cavité axiale en forme de deux troncs de cône opposés, traversés par le flux principal 17. La cavité est à variation lente et continue de sa section et présente une restriction de diamètre 19 située entre une partie amont 5a et une partie aval 5b. La dilatation progressive du flux d'air principal 17 dans la partie aval 5b du dispositif venturi provoque une dépression sur la paroi de la cavité. Un canal transversal 20 débouche dans la cavité à l'endroit où le flux principal 17 présente une dépression. Le dispositif venturi 5 est un dispositif statique d'aspiration apte à aspirer du gaz inflammable à travers le canal transversal 20 relié à une alimentation en gaz.The
L'espace délimité par la partie aval 5b du dispositif venturi 5, la gaine amont 6 et le dispositif d'accrochage de flamme 7 constitue une chambre de mélange 21. Le raccordement du dispositif venturi 5 et de la gaine amont 6 est étanche. Le flux principal d'air 17 est mélangé au gaz en provenance du canal transversal 20 pour former un mélange gazeux 26 qui s'écoule à travers la chambre de mélange 21, traverse le dispositif d'accrochage 7, puis est enflammé par le dispositif d'allumage 8.The space delimited by the
Le dispositif d'allumage 8 est constitué par un conducteur central 22 et une gaine isolante 23 entourant le conducteur central 22 et fixée sur la plaque de fixation 2 et est de type à incandescence ou à étincelles.The
Une pluralité d'orifices périphériques 24 sont ménagés dans la plaque de fixation 2 autour du dispositif d'accrochage 7 de la flamme et débouchent à l'intérieur du tuyau de combustion 10. Le caisson 3 entoure l'ensemble propulseur 1 et est raccordé de manière étanche à la plaque de fixation 2. La plaque de fixation 2 et le caisson 3 forment ensemble une enceinte 25 étanche traversée par une extrémité 6a de la gaine amont 6 recevant le dispositif d'accrochage 7, par le canal transversal 20, par la sortie du ventilateur 4 et par les orifices périphériques 24. Le flux d'air secondaire 18 s'échappant du dispositif 16 de raccordement à fuite est prisonnier de l'enceinte 25 et peut s'échapper par les orifices périphériques 24. L'espace séparant la platine d'entrée 14 du venturi 5 et la platine de sortie 15 du ventilateur 4 est réglé de manière que le flux d'air secondaire 18, s'échappant du dispositif de raccordement à fuite 16, présente une pression supérieure à la pression atmosphérique et supérieure à la pression à l'intérieur du tuyau de combustion 10. Un flux d'air secondaire 39 traverse les orifices périphériques 24 en direction de la flamme 27.A plurality of
Le tuyau de combustion 10 présente une forme allongée entourant le dispositif d'accrochage de la flamme 27, les orifices périphériques 24 et les dispositifs d'allumage 8. La réaction chimique d'oxydation du gaz inflammable avec l'air a lieu dans la flamme 27. La direction d'écoulement du mélange gazeux 26, en aval du dispositif d'accrochage 7 de la flamme 27, définit une direction principale 28 de la flamme 27 du brûleur.The
La réaction chimique transforme le mélange gazeux 26 en produits de combustion et dégage de l'énergie thermique. L'énergie thermique échauffe les produits de combustion qui entrent en contact avec le tuyau de combustion 10 puis s'écoulent à l'intérieur de l'échangeur de chaleur 11. L'ensemble échangeur de chaleur 9 est également échauffé par radiation directe de l'énergie thermique de la flamme 27.The chemical reaction converts the
Le fait que les orifices 24 soient situés à proximité de la flamme 27, permet un allumage fiable et sans bruit. En effet, lorsque le dispositif d'allumage 8 enflamme le mélange gazeux 26, la pression dans le tuyau de combustion 10 augmente brusquement. Les orifices 24 contribuent à absorber l'effet transitoire de l'allumage et évitent un bruit d'explosion que l'on rencontre dans des échangeurs clos du côté du dispositif 7 d'accrochage de la flamme 27.The fact that the
De plus, la possibilité de pouvoir régler le débit d'air secondaire 39 permet de régler le débit traversant l'ensemble échangeur 9, et notamment le tube 11. Cela permet, sans modifier la puissance thermique du brûleur, d'éviter les régimes de résonance de l'ensemble échangeur 9 et le bruit qui en résulterait.In addition, the possibility of being able to adjust the secondary
Comme illustré sur la figure 2, le dispositif d'accrochage 7 de la flamme 27 est logé à l'intérieur de l'extrémité 6a de la gaine 6 et comprend un disque principal 31 traversant toute la section transversale intérieure de la gaine 6. Un anneau pilote 32, coaxial au disque principal 31, est superposé en aval du disque principal 31, et est en contact radialement avec la surface intérieure de l'extrémité 6a de la gaine 6. Le disque principal 31 et l'anneau pilote 32 sont tous les deux constitués par un treillis 35 de fils métalliques, entrelacés ou tricotés, puis comprimés. Lors de la compression, les fils métalliques subissent une déformation plastique. Le treillis 35 à l'état libre conserve la forme obtenue lors de sa compression. L'espace restant entre les fils métalliques déformés permet le passage des filets de mélange gazeux 26 après de multiples déviations. Cela permet d'harmoniser les vitesses des filets traversant le treillis 35. Un mode de réalisation de tels treillis est décrit dans la demande de brevet
Une bague 33 est munie de nervures 33a en forme de croisillons, et fixée en amont du disque principal 31. Des ergots 34 s'étendent radialement vers l'intérieur de la gaine 6 et sont disposés en aval et en périphérie de l'anneau pilote 32. La bague 33 et les ergots 34 enserrent le disque principal 31 et l'anneau pilote 32 pour les soutenir mécaniquement, malgré l'élévation de température du dispositif d'accrochage 7 de la flamme 27 qui peut atteindre 1000 °C.A
L'anneau pilote 32 peut être à section rectangulaire, et présente une surface de chant 32a, en aval et perpendiculaire à la direction principale 28, ainsi qu'une surface cylindrique intérieure 32b. Une extrémité 22a du conducteur central 22 du dispositif d'allumage 8 est disposée à proximité immédiate de la surface de chant 32a. Lors de l'allumage, une étincelle jaillit de l'extrémité 22a du conducteur central 22 vers les fils métalliques 35a du treillis 35, reliés à la masse électrique.The
Le disque principal 31 comprend une partie centrale 31a et une partie périphérique 31b au dessus de laquelle est superposé l'anneau 32. Le mélange gazeux 26 se partage, en traversant le dispositif d'accrochage 7, entre des filets centraux 36 traversant la partie centrale 31a et des filets périphériques 37 traversant la partie périphérique 31b et l'anneau 32. Les filets centraux 36 présentent une vitesse de propagation homogène sur toute la surface de la partie centrale 31a. Les filets périphériques 37 se répartissent dans une zone de propagation ralentie 38 située le long de la surface de chant 32a et de la surface intérieure 32b.The
La surface de la partie périphérique 31b est bien inférieure à la somme de la surface de chant 32a et de la surface intérieure 32b. Cet élargissement de surface et l'épaisseur plus importante de treillis 35 à traverser par les filets périphériques 37, par rapport aux filets centraux 36, font que la vitesse des filets périphériques 37, en aval de l'anneau pilote 32, est fortement réduite par rapport à la vitesse des filets centraux 36 ayant traversé la partie centrale 31a.The surface of the
L'étincelle initie la combustion du mélange gazeux 37 dans ladite zone de propagation ralentie 38 dans laquelle se forme la flamme pilote, qui initie à son tour la combustion des filets centraux 36. Le fait que l'anneau pilote 32 présente une surface intérieure 32b s'étendant sur une certaine distance axiale contribue à l'efficacité de la flamme pilote. Les filets centraux 36 sont en contact, sur toute cette distance axiale, avec la flamme pilote pour entrer en combustion. La vitesse de propagation des filets centraux 36 peut être fortement augmentée sans que la flamme principale 27 ne décroche. Une telle disposition du dispositif d'accrochage permet d'augmenter fortement le débit de mélange gazeux 26 et la puissance thermique du brûleur.The spark initiates the combustion of the
Le flux d'air secondaire 39, provenant des orifices 24, présente une pression supérieure à la pression des produits de combustion et constitue une couche isolante thermiquement. Cela limite l'élévation de température d'une partie amont 10a du tuyau de combustion 10 située en regard de l'extrémité 6a de la gaine 6 et de la flamme 27. Cette isolation thermique permet d'éviter un point chaud du tuyau de combustion 10. En particulier, le flux d'air secondaire 39 est guidé de manière que la zone de liaison entre la plaque de fixation 2 et le brûleur est maintenue à basse température. Cela permet d'utiliser des joints d'étanchéité courants, et d'améliorer la durée de vie de l'ensemble du brûleur. De plus, l'air secondaire 39 apporte de l'oxygène à la flamme 27 de façon à réduire la proportion de gaz imbrûlés, ou d'oxydes incomplètement oxydés tels que des monoxydes de carbone. Le fait que les orifices périphériques 24 soient situés autour du dispositif d'accrochage de la flamme 27 permet à l'air secondaire 39 d'être naturellement guidé vers la flamme 27. Le flux 39 d'air secondaire contribue à la stabilisation de la flamme 27.The
Dans un mode particulier de réalisation, le disque principal 31 est constitué par un tricotage de fils métalliques. Les fils métalliques peuvent être en inox, par exemple de type 304L et d'un diamètre compris entre 0,1 et 0,4 mm, de préférence de l'ordre de 0,2 mm. Le disque 31 présente un diamètre extérieur compris entre 50 et 70 mm, de préférence entre 55 et 60 mm, et par exemple de 57,8 mm. L'épaisseur du disque 31 est comprise entre 3 et 8 mm, de préférence de l'ordre de 5 mm.In a particular embodiment, the
L'anneau 32 est constitué par un tricot de fils métalliques en inox, par exemple de type 309 et d'un diamètre plus épais que le fil du disque principal 31, de préférence compris entre 0,2 et 0,35 mm, par exemple de l'ordre de 0,28 mm. L'anneau 32 présente un diamètre intérieur inférieur au diamètre du disque principal 31, de préférence compris entre 35 et 45 mm, par exemple de l'ordre de 40 mm. L'anneau 32 présente un diamètre extérieur de préférence identique au diamètre du disque principal 31 et une hauteur comprise entre 5 et 25 mm, de préférence comprise entre 10 et 20 mm, en particulier entre deux fois et cinq fois l'épaisseur du disque principal 31. L'épaisseur de l'anneau 32 peut être de l'ordre de 15 mm. Le treillis 35 constitué par le tricot comprimé présente, pour l'anneau, comme pour le disque, une porosité comprise entre 60 % et 90 % du volume extérieur du treillis, de préférence entre 70 % et 80 % et par exemple de 75 % environ.The
La puissance thermique du brûleur peut être ajustée sur une plage allant par exemple de 8 à 40 kilowatts, en jouant notamment, en plus des variations de débit, sur la composition chimique du gaz inflammable.The thermal power of the burner can be adjusted over a range ranging for example from 8 to 40 kilowatts, including playing, in addition to flow rate variations, on the chemical composition of the flammable gas.
D'autres types de matériaux pourraient convenir pour le treillis 35 dès lors qu'ils présentent une succession aléatoire d'obstacles déviants, répartis aléatoirement sur tout le volume du treillis 35, de manière que les filets de gaz, traversant ledit matériau, soient déviés et répartis de manière homogène sur toute la surface du treillis 35.Other types of material could be suitable for the
Un dispositif 7 d'accrochage de la flamme 27 du brûleur combinant une zone pilote 32, associé aux orifices 24 confère une grande souplesse au brûleur. Un brûleur unique peut équiper une grande variété de four et s'accommoder des différences de pertes de charge de l'échangeur thermique 9 selon la taille des fours équipés. Le même dispositif 7 avec les orifices 24 associés peut être utilisé avec les différents types de gaz habituellement rencontrés dans des cuisines. Le même dispositif 7, avec les orifices 24 associés peut équiper des brûleurs dont les puissances nominales varient sur une grande plage, par exemple du simple au double à type de gaz constant, ou plus, notamment en changeant le type de gaz. Le fait que le même dispositif 7 avec les orifices 24 associés couvre une grande plage d'applications, permet de réduire les coûts de production et de stockage des pièces détachées nécessaires aux services après-vente des réseaux commerciaux.A
Claims (12)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR0603332A FR2899956B1 (en) | 2006-04-14 | 2006-04-14 | GAS BURNER FOR KITCHEN OVEN |
Publications (2)
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EP1845306A1 true EP1845306A1 (en) | 2007-10-17 |
EP1845306B1 EP1845306B1 (en) | 2019-03-27 |
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EP07105609.7A Active EP1845306B1 (en) | 2006-04-14 | 2007-04-04 | Gas burner for cooking oven |
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US (1) | US7665987B2 (en) |
EP (1) | EP1845306B1 (en) |
CA (1) | CA2584063A1 (en) |
ES (1) | ES2730006T3 (en) |
FR (1) | FR2899956B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104154537A (en) * | 2014-08-07 | 2014-11-19 | 湖南省特种设备检验检测研究院娄底分院 | Fuel gas vortex combustion device with oxygen supplied for front end |
BE1024169B1 (en) * | 2016-04-27 | 2017-11-27 | Termico Sprl | Heating device |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100119984A1 (en) * | 2008-11-10 | 2010-05-13 | Fox Allen G | Abatement system |
KR101308928B1 (en) | 2012-02-28 | 2013-09-23 | 주식회사 경동나비엔 | Dual venturi for water heater |
US9739483B2 (en) * | 2013-09-26 | 2017-08-22 | Rheem Manufacturing Company | Fuel/air mixture and combustion apparatus and associated methods for use in a fuel-fired heating apparatus |
US20170082286A1 (en) * | 2015-09-18 | 2017-03-23 | Robert R. Trimble | High efficiency burner |
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0698768A1 (en) * | 1994-06-22 | 1996-02-28 | ZANUSSI GRANDI IMPIANTI S.p.A. | Combined gas-microwave cooking oven with steam cooking facility |
US5496171A (en) * | 1991-12-24 | 1996-03-05 | Tokyo Gas Co., Ltd. | Surface combustion burner |
US5562440A (en) * | 1995-02-21 | 1996-10-08 | Burner Systems International, Inc. | Gas burner with radiant retention head |
EP0809078A2 (en) * | 1996-05-22 | 1997-11-26 | ZANUSSI GRANDI IMPIANTI S.p.A. | Cooking apparatus with forced-draft burner |
US6227451B1 (en) * | 1999-08-06 | 2001-05-08 | Pat Caruso | Radiant heater system |
EP1217294A2 (en) * | 2000-12-13 | 2002-06-26 | Ambi-Rad Limited | A radiant tube burner |
US20050175944A1 (en) * | 2004-02-06 | 2005-08-11 | Farshid Ahmady | Variable low intensity infrared heater |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1606390A (en) * | 1922-06-22 | 1926-11-09 | Firm Of Pharos Feuerstatten Ge | Gas heater |
US2201385A (en) * | 1938-11-03 | 1940-05-21 | Lee Wilson Sales Corp | Fuel supply and ignition system |
US2424765A (en) * | 1942-10-06 | 1947-07-29 | Stewart Warner Corp | Hot-air heater having means to recirculate cooled gases |
US3188366A (en) * | 1962-01-17 | 1965-06-08 | Charles S Flynn | Heating process |
US3213919A (en) * | 1962-05-14 | 1965-10-26 | Calzolari Roberto | Nozzle apparatus for burning fuel |
US4231735A (en) * | 1978-03-13 | 1980-11-04 | Downs Edgar S | Radiant heater |
US4541796A (en) * | 1980-04-10 | 1985-09-17 | Union Carbide Corporation | Oxygen aspirator burner for firing a furnace |
JPH0743100B2 (en) * | 1985-09-13 | 1995-05-15 | 三浦工業株式会社 | High load combustion burner |
KR950012777B1 (en) * | 1989-03-31 | 1995-10-21 | 신닛본 세이데쓰 가부시기가이샤 | Method and apparatus for burning liquid fuel |
NL9001366A (en) * | 1990-06-15 | 1992-01-02 | Veg Gasinstituut Nv | PREMIX GAS BURNER WITH WIDE CONTROL RANGE. |
JP3171703B2 (en) * | 1992-11-26 | 2001-06-04 | 大阪瓦斯株式会社 | Burner |
DE4330130C1 (en) * | 1993-09-06 | 1994-10-20 | Fraunhofer Ges Forschung | Catalytic burner |
US5431557A (en) * | 1993-12-16 | 1995-07-11 | Teledyne Industries, Inc. | Low NOX gas combustion systems |
US5839890A (en) * | 1996-09-19 | 1998-11-24 | Praxair Technology, Inc. | Condensation free nozzle |
EP0931979A1 (en) * | 1998-01-23 | 1999-07-28 | DVGW Deutscher Verein des Gas- und Wasserfaches -Technisch-wissenschaftliche Vereinigung- | Method and apparatus for supressing flame and pressure fluctuations in a furnace |
WO2002016833A1 (en) * | 2000-08-22 | 2002-02-28 | Sang Nam Kim | Heating apparatus using thermonuclear reaction of brown gas |
DE10061526A1 (en) * | 2000-12-11 | 2002-06-20 | Alstom Switzerland Ltd | Premix burner arrangement for operating a combustion chamber |
FR2817946B1 (en) * | 2000-12-11 | 2003-03-21 | Inst Francais Du Petrole | CATALYTIC COMBUSTION DEVICE WITH SPRAYING LIQUID FUEL ON HOT WALLS |
US6896512B2 (en) * | 2001-09-19 | 2005-05-24 | Aztec Machinery Company | Radiator element |
JP3881985B2 (en) * | 2001-12-04 | 2007-02-14 | 株式会社アトック | Quartz glass fluid single-hole nozzle and quartz glass fluid multi-hole burner head |
US7250151B2 (en) * | 2002-08-15 | 2007-07-31 | Velocys | Methods of conducting simultaneous endothermic and exothermic reactions |
US6854457B2 (en) * | 2003-04-15 | 2005-02-15 | Premark Feg L.L.C. | Convection oven and related cooking air flow system |
US7214055B2 (en) * | 2003-11-10 | 2007-05-08 | Zippo Manufacturing Company | Colinear burner |
-
2006
- 2006-04-14 FR FR0603332A patent/FR2899956B1/en not_active Expired - Fee Related
-
2007
- 2007-04-04 EP EP07105609.7A patent/EP1845306B1/en active Active
- 2007-04-04 ES ES07105609T patent/ES2730006T3/en active Active
- 2007-04-06 US US11/784,169 patent/US7665987B2/en not_active Expired - Fee Related
- 2007-04-10 CA CA 2584063 patent/CA2584063A1/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5496171A (en) * | 1991-12-24 | 1996-03-05 | Tokyo Gas Co., Ltd. | Surface combustion burner |
EP0698768A1 (en) * | 1994-06-22 | 1996-02-28 | ZANUSSI GRANDI IMPIANTI S.p.A. | Combined gas-microwave cooking oven with steam cooking facility |
US5562440A (en) * | 1995-02-21 | 1996-10-08 | Burner Systems International, Inc. | Gas burner with radiant retention head |
EP0809078A2 (en) * | 1996-05-22 | 1997-11-26 | ZANUSSI GRANDI IMPIANTI S.p.A. | Cooking apparatus with forced-draft burner |
US6227451B1 (en) * | 1999-08-06 | 2001-05-08 | Pat Caruso | Radiant heater system |
EP1217294A2 (en) * | 2000-12-13 | 2002-06-26 | Ambi-Rad Limited | A radiant tube burner |
US20050175944A1 (en) * | 2004-02-06 | 2005-08-11 | Farshid Ahmady | Variable low intensity infrared heater |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104154537A (en) * | 2014-08-07 | 2014-11-19 | 湖南省特种设备检验检测研究院娄底分院 | Fuel gas vortex combustion device with oxygen supplied for front end |
BE1024169B1 (en) * | 2016-04-27 | 2017-11-27 | Termico Sprl | Heating device |
Also Published As
Publication number | Publication date |
---|---|
ES2730006T3 (en) | 2019-11-07 |
FR2899956B1 (en) | 2008-07-25 |
FR2899956A1 (en) | 2007-10-19 |
EP1845306B1 (en) | 2019-03-27 |
CA2584063A1 (en) | 2007-10-14 |
US20080318174A1 (en) | 2008-12-25 |
US7665987B2 (en) | 2010-02-23 |
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