EP0334736A1 - Gas burners - Google Patents

Gas burners Download PDF

Info

Publication number
EP0334736A1
EP0334736A1 EP89400765A EP89400765A EP0334736A1 EP 0334736 A1 EP0334736 A1 EP 0334736A1 EP 89400765 A EP89400765 A EP 89400765A EP 89400765 A EP89400765 A EP 89400765A EP 0334736 A1 EP0334736 A1 EP 0334736A1
Authority
EP
European Patent Office
Prior art keywords
wall
air
burner according
perforated
orifice
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
Application number
EP89400765A
Other languages
German (de)
French (fr)
Other versions
EP0334736B1 (en
Inventor
Joseph Le Mer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chaffoteaux et Maury SAS
Original Assignee
Chaffoteaux et Maury SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chaffoteaux et Maury SAS filed Critical Chaffoteaux et Maury SAS
Priority to AT89400765T priority Critical patent/ATE86371T1/en
Publication of EP0334736A1 publication Critical patent/EP0334736A1/en
Application granted granted Critical
Publication of EP0334736B1 publication Critical patent/EP0334736B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/34Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/70Baffles or like flow-disturbing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/72Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/74Preventing flame lift-off
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00012Liquid or gas fuel burners with flames spread over a flat surface, either premix or non-premix type, e.g. "Flächenbrenner"

Definitions

  • the invention relates to gas burners of the type distributing, through multiple nozzles, the flames generated by the combustion of a combustible gas under pressure in the air, this gas being able to be, for example, one or the other of the following: natural gas, butane, propane.
  • Such burners are used, for example, in water heaters, bath heaters, domestic or industrial central heating boilers, stoves, etc.
  • the invention relates more particularly, among these burners, those which include an air box of which an outer wall is perforated by a large number of close orifices, a gas manifold connected to a source of pressurized combustible gas, this manifold being arranged so as to present opposite the perforated wall of the air box a perforated partition sufficiently spaced from this perforated wall so that air can circulate freely between said wall and said partition and a plurality of hollow needles each connected in a manner watertight at the edge of a hole in the partition and each opening into the central zone of the entrance to an orifice in the perforated wall so as to define with the latter a nozzle for distributing the fuel air-gas mixture forming a site for flame production.
  • the air box communicates with the atmosphere and the air used for the formation of the flame-generating combustible mixture is entrained in the orifices by the stream of pressurized gas leaving the needles, said orifices having for this purpose a profile converging downstream.
  • the flame-generating combustible mixture is not homogeneous, the relative proportion of the gas with respect to the air being higher in the area near the outlet axis of each needle, area in which the gas stream flows without being obstructed by any obstacle, only in the peripheral regions of each distribution nozzle: this results in imperfect combustion of said mixture and the production of undesirable toxic gases, in particular carbon monoxide and nitrogen oxides, in the products of combustion.
  • the object of the invention is, above all, to remedy these drawbacks.
  • the burners of the type in question according to the invention are essentially characterized in that the air box is connected to a source of pressurized air, in that each orifice is constituted by at least one cylindrical hole, and in that a mechanical obstacle is placed across the central zone of the outlet of each orifice, in the axial extension of the corresponding needle, so as to deflect the jet of gas leaving this needle towards the air stream surrounding this jet.
  • the mechanical obstacles are bridges dividing the corresponding orifices into two identical halves, the perforated area of the perforated wall of the box is delimited laterally by at least one series of small holes passing through this wall from side to side and opening outwardly at the foot of a rim projecting outwardly from the wall, - additional orifices are made in the perforated wall of the air box, regularly distributed between the above orifices and of cross section smaller than that of these orifices, the orifices hollowed out in the perforated wall of the air box are circular and delimited by counterbores on the outside of this wall, the orifices hollowed out in the perforated wall of the air box are joined together by grooves hollowed out in the external face of this wall, the bridges constituting the mechanical obstacles consist of thin wires housed in the above grooves, the perforated wall of the air box and the perforated partition of the
  • the invention includes, apart from these main provisions, certain other provisions which are preferably used at the same time and which will be more explicitly discussed below.
  • the burner which is the subject of FIGS. 1 to 5 comprises an air box 1 in the form of a thick wafer, that is to say bounded by a cylindrical side wall of revolution 2 and by two transverse plane walls 3 and 4.
  • planar walls 3 is perforated by a multitude of close orifices 5 whose inner face is cylindrical of revolution.
  • the other flat wall 4 is crossed by a pipe 6 connecting the box to an external source of pressurized air such as a fan (not shown).
  • a gas manifold 7 which, like the box 1, has the shape of a cylindrical wafer, but smaller than the said box and hollowed out in the center by a fireplace 8.
  • This manifold is arranged coaxially with the box 1, it is connected by a pipe 9 to a source of pressurized combustible gas and its flat wall 10 parallel to the perforated wall 3 is bristling with a multitude of hollow needles 11 each connecting the inside the nurse 7 at the central area of an orifice 5.
  • the distance D between the opposite faces of the wall 3 and of the partition 10 is large enough for the air to circulate freely in the space Z created between these elements and, for the same reason, the spacings E between the different needles are large enough and the outside diameter d e thereof, small enough.
  • the air pressure occupying space Z is then the same at all points in this space.
  • the internal volume of the annular manifold 7 is large enough for the gas admitted into it through the pipe 9 to be subjected to the same pressure at all points in this volume.
  • pressurized gas flows distributed respectively to the outlets of the different needles 11 are all identical to each other and that the pressurized air flows projected towards the outside of the box 1, around the outlets of needles, at through the holes 5, are also identical to each other.
  • compositions of the air-gas mixture to be burned which are distributed on the combustion sites themselves through the various nozzles 12 formed by the orifices 5 and the outlets of the needles 11 are identical to each other and very easy to adjust by acting on the air inlet pressure in the box 1 and / or on the gas inlet pressure in the manifold 7.
  • This obstacle deflects the jet of gas leaving the needle, creating a certain turbulence therein, which ensures its intimate mixing with the stream of pressurized air which surrounds it just before the distribution of the mixture obtained at the outlet of the corresponding nozzle.
  • the obstacles in question are thin wires 16 made in particular of stainless steel, wires attached to the external face of the perforated wall 3 of the air box, diametrically across the orifices 5.
  • the quality and homogeneity of the combustion can be further improved by fitting the perforated wall 3 of the air box as follows: - the orifices 5 are delimited, on the side of the external face of said wall, by counterbores 14, - These counterbores 14 are joined together by grooves 15 hollowed out in said face and constituting a network of small channels facilitating the interignition as well as the attachment of the flames 13, some of these grooves 15 receiving the wires 16 above, which also serve as flame catchers, -
  • the perforated annular zone of the wall 3 is delimited laterally, both internally and externally, by a ring of small holes 17 passing through this wall right through and opening outwardly at the foot of a rim 18 which projects outwardly from said wall, a plurality of small circular orifices 24 are regularly hollowed out in the perforated zone of the wall 3 regularly distributed between the orifices 5 and of diameter smaller than that of these orifices 5, - At least one air inlet 19 (see FIGS.
  • the various dimensions of the components of the circular nozzles 12 are advantageously given the following values: distance D, which corresponds substantially to the length of each needle 11 protruding from the partition 10: 8 to 10 mm, preferably 9 mm, - spacing E between the axes of the neighboring needles: 5 to 9 mm, preferably 6 to 8 mm, - internal diameter d i of each needle: 0.4 to 0.8 mm, preferably 0.6 mm to 0.7 mm, - outside diameter d e of each needle: 1 to 1.5 mm, preferably 1.2 to 1.4 mm, - thickness e of the perforated wall 3: 2 to 5 mm, - diameter T of each orifice 5: 3 to 5 mm, preferably 4 mm, - diameter L of each counterbore 14: 5 to 7 mm, preferably 6 mm and depth thereof: approximately 1 mm.
  • the diameter of the holes 17 and that of the orifices 24, if provided, are advantageously of the order of 2 to 3 mm.
  • the number of needles is generally several tens, or even several hundreds.
  • the transverse plane into which each needle 11 opens is generally located axially a little below the level of the interior surface of the perforated wall 3 of the box 1, that is to say inside the box, but it can be located a little beyond this level towards the outside, without however exceeding that of the outside surface of the wall 3.
  • the air box 1 is generally formed by stamped metal sheets, for example stainless steel or aluminum, including its perforated wall 3, which could however be made of a molded or sintered ceramic, while the manifold 7 is made of a metal part, for example made of molded aluminum alloy.
  • the burner which is the subject of Figures 6 to 8 is of the same type as the previous one and differs only in the perforated outer wall of the air box.
  • This wall also has the general shape of a circular plate, but this plate is here composed of two flat discs 25, 26 joined against one another, one of these discs 25, arranged on the inside. of the box, preferably being thicker than the other disc 26, outside, the thickness of each disc being in particular of the order of 1 to 2 mm.
  • the orifices hollowed out in said wall are no longer here circular holes but radial slots each composed of a first slot 27 cut out in the inner disc 25 and by two radial slots 28 radially aligned with the outer disc 26, the inner lateral faces of said slots being all cylindrical.
  • the two radial slots 28 are separated by a bridge 29 located opposite the center of the corresponding slot 27, that is to say in the axial extension of the corresponding needle 11.
  • the bridges 29 play here the role of a deflecting obstacle and creator of turbulence, or even of flame catching device, which was played by the wires 16 in the previous embodiment.
  • the slots 27 are, in turn, separated by bridges 30 against which abut the streams of pressurized air tending to escape from the air box.
  • these perforations are all narrow radial slots and aligned radially, the width of the slots 27 hollowed out in the disc 25 being slightly greater than that of the slots 28 which is typically of the order of 2 mm- and the bridges 30 mutually separating the slots 27 are wider as they are closer to the common axis of the two discs.
  • the slots 27 and 28 could also have forms other than rectilinear and radial, extending for example according to rectilinear segments inclined on the corresponding radii, or according to concentric arcs of a circle, or even according to spiral arcs or even according to crosses.
  • these slots are delimited laterally by cylindrical walls, which allows them to be produced by simple stamping of sheets.
  • an obstacle is provided opposite the center of each slot, and this obstacle is bordered by voids large enough to allow through them an unimpeded distribution of the mixture of the flame-generating fuel to the outside of the box 1 .
  • the obstacle in question is generally, as before, a trigger guard crossing, at its exit, the associated dispensing orifice, which it divides into two identical halves.
  • the flow rate of the air-gas mixture can be adjusted once and for all by giving predetermined values to the flow rates of its two components, the ratio between these two flow rates corresponding to the stoichiometric formula. of the perfect combustion increased by the minimum excess air imposed by the standards, taking into account the possible contributions of air carried through the holes (17, 24) not associated with needles (11).
  • the flow rates or pressures of the two components can be adjusted as desired, taking care of course that the composition of the mixture remains close to its optimal value.
  • the burner described above can deliver at will a calorific power varying from 2 to 30 kW and even beyond, that is to say starting from an extremely low minimum value for which each flame is reduced to a tiny blue pearl visible only in the dark up to the maximum value corresponding to the pressure of the network or other source of gas and that of the blown air, taking into account the dimensions of the distribution orifices.
  • burners have many advantages over those previously known, in particular: - in that they allow excellent combustion over the entire "surface" of the burner, defined by the perforated area of its air box, which reduces, or even cancels, the proportion of unwanted toxic gases (such as carbon monoxide or nitrogen oxides) in the products of combustion, - and in that they lend themselves to a very simple power adjustment in an extremely wide range which can exceed the ratio of 1 to 20 between its extreme values.
  • unwanted toxic gases such as carbon monoxide or nitrogen oxides
  • the invention is in no way limited to those of its modes of application and embodiments which have been more especially envisaged; on the contrary, it embraces all variants, in particular: - those or the flames 13 would have an orientation other than ascending vertical, for example descending vertical, or horizontal, - And those where the perforated wall from which the flame mat comes out would have a shape other than that illustrated with a flat washer, for example that of a flat disc, or that of at least one flat and elongated rectangle forming a kind of "lit ramp", or even that of at least the lateral surface of a cylinder, of revolution or not, or that of a hemisphere or a sphere excluding a portion of this sphere reserved for the necessary radial admissions of the gaseous components.

Abstract

A gas burner is provided of the type distributing, through multiple nozzles (12), the flames (13) generated by the combustion of a pressurized fuel gas in air, comprising an air-fox (1) one wall (3) of which is perforated with a large number of closely spaced orifices (5), a gas feed-tank (7) connected to a pressurized fuel gas source and a plurality of hollow needles (11) each connecting the inside of the feed-tank (7) to the central zone of the inlet of an orifice (5) in the perforated wall (3) so as to define with this orifice one of the flame production sites (12). The air-box is connected to a pressurized air source, the orifices are cylindrical and a mechanical obstacle (16) is provided in the centre of the outlet of each orifice, for deflecting the gas jet leaving the needle and mixing it with the air stream which surrounds it.

Description

L'invention est relative aux brûleurs à gaz du type distribuant à travers des ajutages multiples les flammes engendrées par la combustion d'un gaz combus­tible sous pression dans l'air, ce gaz pouvant être par exemple à volonté l'un ou l'autre des suivants : gaz naturel, butane, propane.The invention relates to gas burners of the type distributing, through multiple nozzles, the flames generated by the combustion of a combustible gas under pressure in the air, this gas being able to be, for example, one or the other of the following: natural gas, butane, propane.

De tels brûleurs équipent par exemple les chauffe-eau, les chauffe-bains, les chaudières de chauf­fage central domestiques ou industrielles, les cuisiniè­res, ...Such burners are used, for example, in water heaters, bath heaters, domestic or industrial central heating boilers, stoves, etc.

L'invention vise plus particulièrement, parmi ces brûleurs, ceux qui comprennent une boîte à air dont une paroi extérieure est perforée par un grand nombre d'orifices rapprochés, une nourrice à gaz connectée à une source de gaz combustible sous pression, cette nour­rice étant agencée de façon à présenter en regard de la paroi perforée de la boîte à air une cloison perforée suffisamment écartée de cette paroi perforée pour que l'air puisse circuler librement entre ladite paroi et ladite cloison et une pluralité d'aiguilles creuses rac­cordées chacune de façon étanche au bord d'un trou de la cloison et débouchant chacune dans la zone centrale de l'entrée d'un orifice de la paroi perforée de façon à définir avec ce dernier un ajutage de distribution de mélange combustible air-gaz formant un site de produc­tion de flamme.The invention relates more particularly, among these burners, those which include an air box of which an outer wall is perforated by a large number of close orifices, a gas manifold connected to a source of pressurized combustible gas, this manifold being arranged so as to present opposite the perforated wall of the air box a perforated partition sufficiently spaced from this perforated wall so that air can circulate freely between said wall and said partition and a plurality of hollow needles each connected in a manner watertight at the edge of a hole in the partition and each opening into the central zone of the entrance to an orifice in the perforated wall so as to define with the latter a nozzle for distributing the fuel air-gas mixture forming a site for flame production.

Dans les modes de réalisation connus de ces brû­leurs, dits "atmosphériques", la boîte à air communique avec l'atmosphère et l'air utilisé pour la formation du mélange combustible générateur de flammes est entraîné dans les orifices par le courant du gaz sous pression sortant des aiguilles, lesdits orifices présentant à cet effet un profil convergent vers l'aval.In the known embodiments of these burners, called "atmospheric", the air box communicates with the atmosphere and the air used for the formation of the flame-generating combustible mixture is entrained in the orifices by the stream of pressurized gas leaving the needles, said orifices having for this purpose a profile converging downstream.

Il est alors difficile de régler dans une large gamme la puissance calorifique du brûleur, vu notamment la nécessité d'éviter, pour les faibles puissances, l'extinction de certaines flammes par rentrée de celles-­ci vers l'amont des ajutages de distribution et, pour les puissances élevées, l'extinction de certaines flam­mes par décollement de celles-ci vers l'aval.It is therefore difficult to settle in a wide range the calorific power of the burner, in particular given the need to avoid, for low powers, the extinction of certain flames by re-entry of these upstream of the distribution nozzles and, for high powers, the extinction of certain flames by detachment of these downstream.

De plus, le mélange combustible générateur de flammes n'est pas homogène, la proportion relative du gaz par rapport à l'air étant plus élevée dans la zone voisine de l'axe de sortie de chaque aiguille, zone dans laquelle le courant gazeux circule sans être entravé par aucun obstacle, que dans les régions périphériques de chaque ajutage de distribution : il en résulte une com­bustion imparfaite dudit mélange et la production de gaz toxiques indésirables, notamment de monoxyde de carbone et d'oxydes d'azote, dans les produits de la combustion.In addition, the flame-generating combustible mixture is not homogeneous, the relative proportion of the gas with respect to the air being higher in the area near the outlet axis of each needle, area in which the gas stream flows without being obstructed by any obstacle, only in the peripheral regions of each distribution nozzle: this results in imperfect combustion of said mixture and the production of undesirable toxic gases, in particular carbon monoxide and nitrogen oxides, in the products of combustion.

L'invention a pour but, surtout, de remédier à ces inconvénients.The object of the invention is, above all, to remedy these drawbacks.

A cet effet, les brûleurs du genre en question selon l'invention sont essentiellement caractérisés en ce que la boîte à air est raccordée à une source d'air sous pression, en ce que chaque orifice est constitué par au moins un trou cylindrique, et en ce qu'un obsta­cle mécanique est disposé en travers de la zone centrale de la sortie de chaque orifice, dans le prolongement axial de l'aiguille correspondante, de façon à dévier le jet de gaz sortant de cette aiguille vers le courant d'air entourant ce jet.To this end, the burners of the type in question according to the invention are essentially characterized in that the air box is connected to a source of pressurized air, in that each orifice is constituted by at least one cylindrical hole, and in that a mechanical obstacle is placed across the central zone of the outlet of each orifice, in the axial extension of the corresponding needle, so as to deflect the jet of gas leaving this needle towards the air stream surrounding this jet.

Dans des modes de réalisation préférés, on a re­cours en outre à l'une et/ou à l'autre des dispositions suivantes :
- les obstacles mécaniques sont des pontets divisant les orifices correspondants en deux moitiés identiques,
- la zone trouée de la paroi perforée de la boîte est délimitée latéralement par au moins une suite de pe­tits trous traversant cette paroi de part en part et débouchant extérieurement au pied d'un rebord faisant saillie extérieurement sur la paroi,
- des orifices complémentaires sont pratiqués dans la paroi perforée de la boîte à air, régulièrement répar­tis entre les orifices ci-dessus et de section droite inférieure à celle de ces orifices,
- les orifices évidés dans la paroi perforée de la boîte à air sont circulaires et délimités par des lamages du côté extérieur de cette paroi,
- les orifices évidés dans la paroi perforée de la boîte à air sont réunis entre eux par des rainures creusées dans la face extérieure de cette paroi,
- les pontets constitutifs des obstacles mécaniques sont constitués par des fils minces logés dans les rainures ci-dessus,
- la paroi perforée de la boîte à air et la cloison per­forée de la nourrice sont écartées entre elles d'une distance de l'ordre du cm, le diamètre de chaque ori­fice évidé dans la paroi perforée est de l'ordre de 4 mm, le diamètre intérieur de chaque aiguille est de l'ordre de 0,6 mm à 0,7 mm, son diamètre extérieur est de l'ordre de 1,2 à 1,4 mm, la distance entre les axes des aiguilles voisines est de l'ordre de 6 à 8 mm, le diamètre de chaque orifice complémentaire, s'il en est prévu, est de l'ordre de 2 à 3 mm et celui des petits trous de bordure, s'il en est prévu, est de l'ordre de 2 à 3 mm,
- la paroi perforée de la boîte à air est composée de deux parois accolées, l'une intérieure et l'autre extérieure, présentant des perforations décalées mu­tuellement de façon telle que la paroi extérieure forme en regard des zones centrales des perforations de la paroi intérieure des pontets constitutifs des obstacles mécaniques,
- les perforations évidées dans les parois ci-dessus présentent des formes allongées à bords parallèles et sont mutuellement alignées selon la direction de leur allongement,
- les deux parois accolées sont circulaires et leurs perforations sont allongées radialement,
- les pontets formés entre les perforations évidées dans la paroi intérieure sont plus larges dans les zones des parois accolées, les plus proches de l'axe de ces parois,
- la paroi intérieure est plus épaisse que la paroi ex­térieure,
- la face, de la paroi perforée de la boîte à air, inté­rieure à cette boîte, est évidée à proximité immédiate de chaque orifice par au moins une entrée d'air propre à imprimer un mouvement rotatif à l'air admis dans cet orifice,
- la boîte à air présente la forme générale d'une galet­te cylindrique et la nourrice, celle d'un anneau creux coaxial à la boîte et contenu dans celle-ci.
In preferred embodiments, use is also made of one and / or the other of the following arrangements:
- the mechanical obstacles are bridges dividing the corresponding orifices into two identical halves,
the perforated area of the perforated wall of the box is delimited laterally by at least one series of small holes passing through this wall from side to side and opening outwardly at the foot of a rim projecting outwardly from the wall,
- additional orifices are made in the perforated wall of the air box, regularly distributed between the above orifices and of cross section smaller than that of these orifices,
the orifices hollowed out in the perforated wall of the air box are circular and delimited by counterbores on the outside of this wall,
the orifices hollowed out in the perforated wall of the air box are joined together by grooves hollowed out in the external face of this wall,
the bridges constituting the mechanical obstacles consist of thin wires housed in the above grooves,
the perforated wall of the air box and the perforated partition of the manifold are spaced apart by a distance of the order of cm, the diameter of each orifice hollowed out in the perforated wall is of the order of 4 mm, the internal diameter of each needle is of the order of 0.6 mm to 0.7 mm, its external diameter is of the order of 1.2 to 1.4 mm, the distance between the axes of the neighboring needles is of the order of 6 to 8 mm, the diameter of each additional orifice, if provided, is of the order of 2 to 3 mm and that of the small border holes, if provided, is in the order of 2 to 3 mm,
- the perforated wall of the air box is composed of two adjoining walls, one interior and the other exterior, having perforations offset mutually so that the exterior wall forms opposite the central areas of the perforations of the interior wall bridges constituting mechanical obstacles,
the perforations hollowed out in the above walls have elongated shapes with parallel edges and are mutually aligned according to the direction of their elongation,
- the two adjoining walls are circular and their perforations are elongated radially,
the bridges formed between the perforations hollowed out in the inner wall are wider in the areas of the adjoining walls, the closest to the axis of these walls,
- the inner wall is thicker than the outer wall,
the face of the perforated wall of the air box, inside this box, is hollowed out in the immediate vicinity of each orifice by at least one air inlet capable of imparting a rotary movement to the air admitted into this orifice,
- The air box has the general shape of a cylindrical wafer and the nurse, that of a hollow ring coaxial with the box and contained in it.

L'invention comprend, mises à part ces disposi­tions principales, certaines autres dispositions qui s'utilisent de préférence en même temps et dont il sera plus explicitement question ci-après.The invention includes, apart from these main provisions, certain other provisions which are preferably used at the same time and which will be more explicitly discussed below.

Dans ce qui suit, l'on va décrire deux modes de réalisation préférés de l'invention en se référant aux dessins ci-annexés d'une manière bien entendu non limi­tative.

  • Les figures 1 et 2, de ces dessins, montrent respectivement en coupe axiale selon I-I, figure 2 et en demie vue en plan, un brûleur à gaz établi selon l'in­vention.
  • La figure 3 est un détail agrandi de la figure 1.
  • Les figures 4 et 5 montrent à plus grande échel­le, respectivement, un morceau de la face extérieure de la paroi perforée comprise par ledit brûleur et un mor­ceau de la face intérieure de cette paroi.
  • La figure 6 montre en vue en plan une variante de brûleur à gaz établi selon l'invention.
  • Les figures 7 et 8 montrent à échelle agrandie une portion de ce brûleur en coupe axiale selon VII-VII figure 8 et en vue en plan.
In what follows, two preferred embodiments of the invention will be described with reference to the accompanying drawings, of course in a non-limiting manner.
  • Figures 1 and 2 of these drawings show respectively in axial section along II, Figure 2 and in half plan view, a gas burner established according to the invention.
  • Figure 3 is an enlarged detail of Figure 1.
  • Figures 4 and 5 show on a larger scale, respectively, a piece of the outer face of the perforated wall included by said burner and a piece of the inner face of this wall.
  • Figure 6 shows in plan view a variant of gas burner established according to the invention.
  • Figures 7 and 8 show on an enlarged scale a portion of this burner in axial section along VII-VII Figure 8 and in plan view.

Le brûleur faisant l'objet des figures 1 à 5 comprend une boîte à air 1 en forme de galette épaisse, c'est-à-dire délimitée par une paroi latérale cylindri­que de révolution 2 et par deux parois planes transver­sales 3 et 4.The burner which is the subject of FIGS. 1 to 5 comprises an air box 1 in the form of a thick wafer, that is to say bounded by a cylindrical side wall of revolution 2 and by two transverse plane walls 3 and 4.

L'une de ces parois planes 3 est perforée par une multitude d'orifices 5 rapprochés dont la face inté­rieure est cylindrique de révolution.One of these planar walls 3 is perforated by a multitude of close orifices 5 whose inner face is cylindrical of revolution.

L'autre paroi plane 4 est traversée par une con­duite 6 reliant la boîte à une source extérieure d'air sous pression telle qu'un ventilateur (non représenté).The other flat wall 4 is crossed by a pipe 6 connecting the box to an external source of pressurized air such as a fan (not shown).

A l'intérieur de la boîte 1 est logée, avec jeu dans toutes les directions, une nourrice à gaz 7 qui présente comme la boîte 1 la forme d'une galette cylin­drique, mais plus petite que ladite boîte et évidée en son centre par une cheminée 8.Inside the box 1 is housed, with play in all directions, a gas manifold 7 which, like the box 1, has the shape of a cylindrical wafer, but smaller than the said box and hollowed out in the center by a fireplace 8.

Cette nourrice est disposée coaxialement à la boîte 1, elle est reliée par une conduite 9 à une source de gaz combustible sous pression et sa paroi plane 10 parallèle à la paroi perforée 3 est hérissée d'une mul­titude d'aiguilles creuses 11 reliant chacune l'inté­rieur de la nourrice 7 à la zone centrale d'un orifice 5.This manifold is arranged coaxially with the box 1, it is connected by a pipe 9 to a source of pressurized combustible gas and its flat wall 10 parallel to the perforated wall 3 is bristling with a multitude of hollow needles 11 each connecting the inside the nurse 7 at the central area of an orifice 5.

La distance D entre les faces en regard de la paroi 3 et de la cloison 10 est assez grande pour que l'air circule librement dans l'espace Z créé entre ces éléments et, pour la même raison, les écartements E en­tre les différentes aiguilles sont suffisamment grands et le diamètre extérieur de de celles-ci, suffisamment petit.The distance D between the opposite faces of the wall 3 and of the partition 10 is large enough for the air to circulate freely in the space Z created between these elements and, for the same reason, the spacings E between the different needles are large enough and the outside diameter d e thereof, small enough.

La pression de l'air qui occupe l'espace Z est alors la même en tous les points de cet espace.The air pressure occupying space Z is then the same at all points in this space.

De même le volume intérieur de la nourrice annu­laire 7 est suffisamment grand pour que le gaz admis dans celle-ci par la conduite 9 soit soumis à la même pression en tous les points de ce volume.Likewise, the internal volume of the annular manifold 7 is large enough for the gas admitted into it through the pipe 9 to be subjected to the same pressure at all points in this volume.

Il en résulte que les débits de gaz sous pres­sion distribués respectivement aux sorties des diffé­rentes aiguilles 11 sont tous identiques entre eux et que les débits d'air sous pression projetés vers l'ex­térieur de la boîte 1, autour des sorties d'aiguilles, à travers les orifices 5, sont également identiques entre eux.It follows that the pressurized gas flows distributed respectively to the outlets of the different needles 11 are all identical to each other and that the pressurized air flows projected towards the outside of the box 1, around the outlets of needles, at through the holes 5, are also identical to each other.

Par conséquent, les compositions des mélanges air-gaz à brûler qui sont distribués sur les sites mêmes de la combustion à travers les différents ajutages 12 constitués par les orifices 5 et les sorties des aiguil­les 11 sont identiques entre elles et très faciles à ajuster en agissant sur la pression d'admission de l'air dans la boîte 1 et/ou sur celle d'admission du gaz dans la nourrice 7.Consequently, the compositions of the air-gas mixture to be burned which are distributed on the combustion sites themselves through the various nozzles 12 formed by the orifices 5 and the outlets of the needles 11 are identical to each other and very easy to adjust by acting on the air inlet pressure in the box 1 and / or on the gas inlet pressure in the manifold 7.

Si donc les deux composants air et gaz du mélan­ge combustible sont intimement mélangés aux sites indi­qués, on obtient automatiquement en ces sites une com­bustion excellente et homogène lors de la formation des multiples flammes 13 dues à l'allumage dudit mélange en lesdits sites.If therefore the two air and gas components of the combustible mixture are intimately mixed at the sites indicated, an excellent and homogeneous combustion is automatically obtained at these sites during the formation of the multiple flames 13 due to the ignition of said mixture at said sites.

Pour assurer ce mélange intime, on prévoit un obstacle mécanique dans la zone centrale de chaque ori­fice 5, c'est-à-dire dans le prolongement axial de cha­que aiguille 11.To ensure this intimate mixing, a mechanical obstacle is provided in the central zone of each orifice 5, that is to say in the axial extension of each needle 11.

Cet obstacle dévie le jet de gaz sortant de l'aiguille en y créant une certaine turbulence, ce qui assure son mélange intime avec le courant d'air sous pression qui l'entoure juste avant la distribution du mélange obtenu à la sortie de l'ajutage correspondant.This obstacle deflects the jet of gas leaving the needle, creating a certain turbulence therein, which ensures its intimate mixing with the stream of pressurized air which surrounds it just before the distribution of the mixture obtained at the outlet of the corresponding nozzle.

Dans le mode de réalisation des figures 1 à 5, les obstacles en question sont des fils minces 16 cons­titués notamment en acier inoxydable, fils rapportés sur la face extérieure de la paroi perforée 3 de la boîte à air, diamètralement en travers des orifices 5.In the embodiment of FIGS. 1 to 5, the obstacles in question are thin wires 16 made in particular of stainless steel, wires attached to the external face of the perforated wall 3 of the air box, diametrically across the orifices 5.

La qualité et l'homogénéité de la combustion peuvent être encore améliorées en aménageant comme suit la paroi perforée 3 de la boîte à air :
- on délimite les orifices 5, du côté de la face exté­rieure de ladite paroi, par des lamages 14,
- on réunit entre eux ces lamages 14 par des rainures 15 creusées dans ladite face et constituant un réseau de petits canaux facilitant l'interallumage ainsi que l'accrochage des flammes 13, certaines de ces rainures 15 recevant les fils 16 ci-dessus, qui servent égale­ment d'accroche-flammes,
- on délimite latéralement la zone annulaire perforée de la paroi 3, aussi bien intérieurement qu'extérieure­ment, par une couronne de petits trous 17 traversant cette paroi de part en part et débouchant extérieure­ment au pied d'un rebord 18 qui fait saillie exté­rieurement sur ladite paroi,
- on évide dans la zone perforée de la paroi 3 une plu­ralité de petits orifices circulaires 24 régulièrement répartis entre les orifices 5 et de diamètre inférieur à celui de ces orifices 5,
- on évide dans la face intérieure de la paroi 3, à pro­ximité immédiate de chaque orifice 5, au moins une entrée d'air 19 (voir figures 3 à 5) propre à imprimer un mouvement rotatif à l'air sous pression admis dans cet orifice, ce qui améliore son mélange avec le gaz combustible sortant de l'aiguille centrale 11, avan­tage particulièrement précieux lorsque ce gaz est du butane ou du propane.
The quality and homogeneity of the combustion can be further improved by fitting the perforated wall 3 of the air box as follows:
- the orifices 5 are delimited, on the side of the external face of said wall, by counterbores 14,
- These counterbores 14 are joined together by grooves 15 hollowed out in said face and constituting a network of small channels facilitating the interignition as well as the attachment of the flames 13, some of these grooves 15 receiving the wires 16 above, which also serve as flame catchers,
- The perforated annular zone of the wall 3 is delimited laterally, both internally and externally, by a ring of small holes 17 passing through this wall right through and opening outwardly at the foot of a rim 18 which projects outwardly from said wall,
a plurality of small circular orifices 24 are regularly hollowed out in the perforated zone of the wall 3 regularly distributed between the orifices 5 and of diameter smaller than that of these orifices 5,
- At least one air inlet 19 (see FIGS. 3 to 5) is hollowed out in the inner face of the wall 3, in the immediate vicinity of each orifice 5, capable of imparting a rotary movement with the pressurized air admitted into this orifice, which improves its mixture with the combustible gas leaving the central needle 11, a particularly valuable advantage when this gas is butane or propane.

Dans la pratique, on donne avantageusement aux différentes cotes des composants des ajutages circulai­res 12 les valeurs suivantes :
- distance D, qui correspond sensiblement à la longueur de chaque aiguille 11 faisant saillie hors de la cloi­son 10 : 8 à 10 mm, de préférence 9 mm,
- écartement E entre les axes des aiguilles voisines : 5 à 9 mm, de préférence 6 à 8 mm,
- diamètre intérieur di de chaque aiguille : 0,4 à 0,8 mm, de préférence 0,6 mm à 0,7 mm,
- diamètre extérieur de de chaque aiguille : 1 à 1,5 mm, de préférence 1,2 à 1,4 mm,
- épaisseur e de la paroi perforée 3 : 2 à 5 mm,
- diamètre T de chaque orifice 5 : 3 à 5 mm, de préfé­rence 4 mm,
- diamètre L de chaque lamage 14 : 5 à 7 mm, de préfé­rence 6 mm et profondeur de celui-ci : environ 1 mm.
In practice, the various dimensions of the components of the circular nozzles 12 are advantageously given the following values:
distance D, which corresponds substantially to the length of each needle 11 protruding from the partition 10: 8 to 10 mm, preferably 9 mm,
- spacing E between the axes of the neighboring needles: 5 to 9 mm, preferably 6 to 8 mm,
- internal diameter d i of each needle: 0.4 to 0.8 mm, preferably 0.6 mm to 0.7 mm,
- outside diameter d e of each needle: 1 to 1.5 mm, preferably 1.2 to 1.4 mm,
- thickness e of the perforated wall 3: 2 to 5 mm,
- diameter T of each orifice 5: 3 to 5 mm, preferably 4 mm,
- diameter L of each counterbore 14: 5 to 7 mm, preferably 6 mm and depth thereof: approximately 1 mm.

Le diamètre des trous 17 et celui des orifices 24, s'il en est prévu, sont avantageusement de l'ordre de 2 à 3 mm.The diameter of the holes 17 and that of the orifices 24, if provided, are advantageously of the order of 2 to 3 mm.

Le nombre des aiguilles est en général de plu­sieurs dizaines, voire de plusieurs centaines.The number of needles is generally several tens, or even several hundreds.

Le plan transversal en lequel débouche chaque aiguille 11 est en général situé axialement un peu en deçà du niveau de la surface intérieure de la paroi per­forée 3 de la boîte 1, c'est-à-dire à l'intérieur de la boîte, mais il peut être situé un peu au-delà de ce ni­veau vers l'extérieur, sans pour autant dépasser celui de la surface extérieure de la paroi 3.The transverse plane into which each needle 11 opens is generally located axially a little below the level of the interior surface of the perforated wall 3 of the box 1, that is to say inside the box, but it can be located a little beyond this level towards the outside, without however exceeding that of the outside surface of the wall 3.

On voit encore sur le dessin :
- des vis 20 (figure 1) permettant de fixer la nourrice 7 à l'intérieur de la boîte 1 et coopérant avec des alésages filetés complémentaires 21 évidés dans des surépaisseurs 22 de cette nourrice,
- et un allumeur 23 (figure 2), par exemple du type piezoélectrique à étincelles.
We can still see on the drawing:
screws 20 (FIG. 1) making it possible to fix the manifold 7 inside the box 1 and cooperating with complementary threaded bores 21 hollowed out in extra thicknesses 22 of this manifold,
- And an igniter 23 (Figure 2), for example of the piezoelectric spark type.

La boîte à air 1 est généralement constituée par des tôles métalliques embouties, par exemple en acier inoxydable ou en aluminium, y compris sa paroi perforée 3, laquelle pourrait toutefois être constituée en une céramique moulée ou frittée, alors que la nourrice 7 est constituée par une pièce métallique, par exemple en al­liage d'aluminium moulé.The air box 1 is generally formed by stamped metal sheets, for example stainless steel or aluminum, including its perforated wall 3, which could however be made of a molded or sintered ceramic, while the manifold 7 is made of a metal part, for example made of molded aluminum alloy.

Le brûleur faisant l'objet des figures 6 à 8 est du même type que le précédent et ne diffère que par la paroi extérieure perforée de la boîte à air.The burner which is the subject of Figures 6 to 8 is of the same type as the previous one and differs only in the perforated outer wall of the air box.

Cette paroi présente encore la forme générale d'une plaque circulaire, mais cette plaque est ici com­posée de deux disques plats 25, 26 accolés l'un contre l'autre, l'un de ces disques 25, disposé du côté de l'intérieur de la boîte, étant de préférence plus épais que l'autre disque 26, extérieur, l'épaisseur de chaque disque étant notamment de l'ordre de 1 à 2 mm.This wall also has the general shape of a circular plate, but this plate is here composed of two flat discs 25, 26 joined against one another, one of these discs 25, arranged on the inside. of the box, preferably being thicker than the other disc 26, outside, the thickness of each disc being in particular of the order of 1 to 2 mm.

Les orifices évidés dans ladite paroi ne sont plus ici des trous circulaires mais des fentes radiales composées chacune par une première fente 27 évidée dans le disque intérieur 25 et par deux fentes radiales 28 radialement alignées du disque extérieur 26, les faces latérales intérieures desdites fentes étant toutes cylindiques.The orifices hollowed out in said wall are no longer here circular holes but radial slots each composed of a first slot 27 cut out in the inner disc 25 and by two radial slots 28 radially aligned with the outer disc 26, the inner lateral faces of said slots being all cylindrical.

Les deux fentes radiales 28 sont séparées par un pontet 29 situé en regard du centre de la fente 27 cor­respondante, c'est-à-dire dans le prolongement axial de l'aiguille 11 correspondante.The two radial slots 28 are separated by a bridge 29 located opposite the center of the corresponding slot 27, that is to say in the axial extension of the corresponding needle 11.

Les pontets 29 jouent ici le rôle d'obstacle déviateur et créateur de turbulence, voire d'accroche-­flammes, qui était joué par les fils 16 dans le mode de réalisation précédent.The bridges 29 play here the role of a deflecting obstacle and creator of turbulence, or even of flame catching device, which was played by the wires 16 in the previous embodiment.

Les fentes 27 sont, quant à elles, séparées par des pontets 30 contre lesquels viennent buter les cou­rants d'air sous pression tendant à s'échapper de la boîte à air.The slots 27 are, in turn, separated by bridges 30 against which abut the streams of pressurized air tending to escape from the air box.

Les différentes perforations des deux disques sont dessinées de façon telle que la simple juxtaposi­tion axiale de ces deux disques, en des positions angu­laires relatives bien déterminées, se traduit par la présence d'un pontet 29 en regard du centre de chaque fente 27.The different perforations of the two discs are drawn in such a way that the simple axial juxtaposition of these two discs, in well defined relative angular positions, results in the presence of a trigger guard 29 opposite the center of each slot 27.

Dans le mode de réalisation illustré sur les figures 6 à 8, ces perforations sont toutes des fentes radiales étroites et alignées radialement, la largeur des fentes 27 évidées dans le disque 25 étant légèrement supérieure à celle des fentes 28 -qui est typiquement de l'ordre de 2 mm- et les pontets 30 séparant mutuellement les fentes 27 sont d'autant plus larges qu'ils sont plus rapprochés de l'axe commun des deux disques.In the embodiment illustrated in FIGS. 6 to 8, these perforations are all narrow radial slots and aligned radially, the width of the slots 27 hollowed out in the disc 25 being slightly greater than that of the slots 28 which is typically of the order of 2 mm- and the bridges 30 mutually separating the slots 27 are wider as they are closer to the common axis of the two discs.

Les fentes 27 et 28 pourraient également présen­ter d'autres formes que rectilignes et radiales en s'é­tendant par exemple selon des segments rectilignes in­clinés sur les rayons correspondants, ou selon des arcs de cercle concentriques, ou encore selon des arcs de spirale ou même selon des croix.The slots 27 and 28 could also have forms other than rectilinear and radial, extending for example according to rectilinear segments inclined on the corresponding radii, or according to concentric arcs of a circle, or even according to spiral arcs or even according to crosses.

Dans chaque cas, ces fentes sont délimitées la­téralement par des parois cylindriques, ce qui permet de les réaliser par simple estampage de tôles.In each case, these slots are delimited laterally by cylindrical walls, which allows them to be produced by simple stamping of sheets.

Dans chaque cas, un obstable est prévu en regard du centre de chaque fente, et cet obstacle est bordé par des vides suffisamment larges pour permettre à travers eux une distribution sans entrave du mélange du combus­tible générateur des flammes vers l'extérieur de la boî­te 1.In each case, an obstacle is provided opposite the center of each slot, and this obstacle is bordered by voids large enough to allow through them an unimpeded distribution of the mixture of the flame-generating fuel to the outside of the box 1 .

L'obstacle en question est en général, comme précédemment, un pontet traversant, au niveau de sa sortie, l'orifice de distribution associé, qu'il divise en deux moitiés identiques.The obstacle in question is generally, as before, a trigger guard crossing, at its exit, the associated dispensing orifice, which it divides into two identical halves.

Ici encore des trous supplémentaires affectés uniquement au passage de l'air sous pression pourraient être évidés dans les disques.Here again, additional holes allocated solely for the passage of pressurized air could be hollowed out in the discs.

Le débit du mélange air-gaz peut être réglé une fois pour toutes en donnant des valeurs prédéterminées aux débits de ses deux composants, le rapport entre ces deux débits correspondant à la formule stoechiométrique de la combustion parfaite augmenté de l'excès d'air minimum imposé par les normes, compte tenu des apports éventuels d'air effectués à travers les trous (17, 24) non associés à des aiguilles (11).The flow rate of the air-gas mixture can be adjusted once and for all by giving predetermined values to the flow rates of its two components, the ratio between these two flow rates corresponding to the stoichiometric formula. of the perfect combustion increased by the minimum excess air imposed by the standards, taking into account the possible contributions of air carried through the holes (17, 24) not associated with needles (11).

Selon une variante avantageuse, on peut régler à volonté les débits ou pressions des deux composants en prenant soin bien entendu que la composition du mélange demeure voisine de sa valeur optimale.According to an advantageous variant, the flow rates or pressures of the two components can be adjusted as desired, taking care of course that the composition of the mixture remains close to its optimal value.

On peut ainsi "moduler" la puissance calorifique du brûleur.We can thus "modulate" the calorific power of the burner.

Cette modulation est ici possible dans une gamme extrêmement large puisqu'elle peut aller de 1 à 20 et même davantage alors qu'avec les réalisations antérieu­rement connues à brûleurs "atmosphériques" il était dif­ficile de dépasser un rapport de 4 entre les deux va­leurs extrêmes de la puissance calorifique susceptible d'être engendrée par le brûleur.This modulation is possible here in an extremely wide range since it can go from 1 to 20 and even more whereas with the previously known embodiments with "atmospheric" burners it was difficult to exceed a ratio of 4 between the two extreme values of the calorific power likely to be generated by the burner.

C'est ainsi que le brûleur décrit ci-dessus peut délivrer à volonté une puissance calorifique variant de 2 à 30 kW et même au-delà, c'est-à-dire partant d'une valeur minimum extrêmement faible pour laquelle chaque flamme est réduite à une minuscule perle bleue visible seulement dans l'obscurité jusqu'à la valeur maximum correspondant à la pression du réseau ou autre source de gaz et à celle de l'air soufflé, compte tenu des cotes des orifices de distribution.Thus the burner described above can deliver at will a calorific power varying from 2 to 30 kW and even beyond, that is to say starting from an extremely low minimum value for which each flame is reduced to a tiny blue pearl visible only in the dark up to the maximum value corresponding to the pressure of the network or other source of gas and that of the blown air, taking into account the dimensions of the distribution orifices.

En suite de quoi, et quel que soit le mode de réalisation adopté, on dispose finalement de brûleurs dont la constitution et le fonctionnement résultent suf­fisamment de ce qui précède.As a result of this, and whatever the embodiment adopted, there are finally burners whose constitution and operation result sufficiently from the above.

Ces brûleurs présentent de nombreux avantages par rapport à ceux antérieurement connus, notamment :
- en ce qu'ils permettent une excellente combustion sur la totalité de la "surface" du brûleur, définie par la zone perforée de sa boîte à air, ce qui réduit, voire annule, la proportion de gaz toxiques indésirables (tel que le monoxyde de carbone ou les oxydes d'azote) dans les produits de la combustion,
- et en ce qu'ils se prêtent à un réglage très simple de puissance dans une gamme extrêmement large pouvant dé­passer le rapport de 1 à 20 entre ses valeurs extrê­mes.
These burners have many advantages over those previously known, in particular:
- in that they allow excellent combustion over the entire "surface" of the burner, defined by the perforated area of its air box, which reduces, or even cancels, the proportion of unwanted toxic gases (such as carbon monoxide or nitrogen oxides) in the products of combustion,
- and in that they lend themselves to a very simple power adjustment in an extremely wide range which can exceed the ratio of 1 to 20 between its extreme values.

Comme il va de soi, et comme il résulte d'ail­leurs déjà de ce qui précède, l'invention ne se limite nullement à ceux de ses modes d'application et de réali­sation qui ont été plus spécialement envisagés ; elle en embrasse, au contraire, toutes les variantes, notam­ment :
- celles ou les flammes 13 auraient une orientation autre que verticale ascendante, par exemple verticale descendante, ou horizontale,
- et celles où la paroi perforée d'où sort le tapis de flammes présenterait une forme autre que celle illus­trée d'une rondelle plane, par exemple celle d'un disque plan, ou encore celle d'au moins un rectangle plan et allongé formant une sorte de "rampe allumée", ou même celle d'au moins la surface latérale d'un cy­lindre, de révolution ou non, ou encore celle d'une demi-sphère ou d'une sphère à l'exclusion d'une por­tion de cette sphère réservée aux admissions radiales nécessaires des composants gazeux.
As is obvious, and as already follows from the foregoing, the invention is in no way limited to those of its modes of application and embodiments which have been more especially envisaged; on the contrary, it embraces all variants, in particular:
- those or the flames 13 would have an orientation other than ascending vertical, for example descending vertical, or horizontal,
- And those where the perforated wall from which the flame mat comes out would have a shape other than that illustrated with a flat washer, for example that of a flat disc, or that of at least one flat and elongated rectangle forming a kind of "lit ramp", or even that of at least the lateral surface of a cylinder, of revolution or not, or that of a hemisphere or a sphere excluding a portion of this sphere reserved for the necessary radial admissions of the gaseous components.

Claims (16)

1. Brûleur à gaz comprenant une boîte à air (1) dont une paroi extérieure (3 ; 25,26) est perforée par un grand nombre d'orifices rapprochés, une nourrice à gaz (7) connectée à une source de gaz combustible sous pression, cette nourrice étant agencée de façon à pré­senter en regard de la paroi perforée de la boîte à air une cloison perforée (10) suffisamment écartée de cette paroi perforée pour que l'air puisse circuler librement entre ladite paroi et ladite cloison et une pluralité d'aiguilles creuses (11) raccordées chacune de façon étanche au bord d'un trou de la cloison et débouchant chacune dans la zone centrale de l'entrée d'un orifice (5 ; 27,28) de la paroi perforée de façon à définir avec ce dernier un ajutage (12) de distribution de mélange combustible air-gaz formant un site de production de flamme (13), caractérisé en ce que la boîte à air (1) est raccordée à une source d'air sous pression, en ce que chaque orifice (5 ; 27,28) est constitué par au moins un trou cylindrique et en ce qu'un obstacle méca­nique (16 ; 29) est disposé en travers de la zone cen­trale de la sortie de chaque orifice, dans le prolonge­ment axial de l'aiguille correspondante (11), de façon à dévier le jet de gaz sortant de cette aiguille vers le courant d'air entourant ce jet.1. Gas burner comprising an air box (1) of which an outer wall (3; 25,26) is perforated by a large number of close orifices, a gas manifold (7) connected to a source of combustible gas under pressure, this manifold being arranged so as to present opposite the perforated wall of the air box a perforated partition (10) sufficiently spaced from this perforated wall so that the air can circulate freely between said wall and said partition and a plurality hollow needles (11) each sealingly connected to the edge of a hole in the partition and each opening into the central zone of the inlet of an orifice (5; 27,28) of the perforated wall so as to define with the latter a nozzle (12) for distributing the fuel air-gas mixture forming a flame production site (13), characterized in that the air box (1) is connected to a source of pressurized air, in that each orifice (5; 27,28) is constituted by at least one cylindrical hole and in that a mechanical obstacle (16; 29) is arranged across the central zone of the outlet of each orifice, in the axial extension of the corresponding needle (11), so as to deflect the jet of gas leaving this needle towards the air stream surrounding this jet. 2. Brûleur selon la revendication 1, caracté­risé en ce que les obstacles mécaniques (16 ; 29) sont des pontets divisant les orifices correspondants (5 ; 27, 28) en deux moitiés identiques.2. Burner according to claim 1, characterized in that the mechanical obstacles (16; 29) are bridges dividing the corresponding orifices (5; 27, 28) into two identical halves. 3. Brûleur selon l'une quelconque des précé­dentes revendications, caractérisé en ce que la zone trouée de la paroi perforée (3 ; 25,26) de la boîte (1) est délimitée latéralement par au moins une suite de pe­tits trous (17) traversant cette paroi de part en part et débouchant extérieurement au pied d'un rebord (18) faisant saillie extérieurement sur la paroi.3. Burner according to any one of the preceding claims, characterized in that the perforated area of the perforated wall (3; 25,26) of the box (1) is delimited laterally by at least one series of small holes (17) crossing this wall right through and opening outwardly at the foot of a ledge (18) projecting outwardly from the wall. 4. Brûleur selon l'une quelconque des précé­dentes revendications, caractérisé en ce que des ori­fices complémentaires (24) sont pratiqués dans la paroi perforée de la boîte à air, régulièrement répartis entre les orifices ci-dessus et de section droite inférieure à celle de ces orifices.4. Burner according to any one of the preceding claims, characterized in that complementary orifices (24) are formed in the perforated wall of the air box, regularly distributed between the above orifices and of cross section smaller than that of these holes. 5. Brûleur selon l'une quelconque des précé­dentes revendications, caractérisé en ce que les orifi­ces (5) évidés dans la paroi perforée (3) de la boîte à air sont circulaires et délimités par des lamages (14) du côté extérieur de cette paroi.5. Burner according to any one of the preceding claims, characterized in that the orifices (5) hollowed out in the perforated wall (3) of the air box are circular and delimited by countersinks (14) on the outside of this wall . 6. Brûleur selon la revendication 5, caracté­risé en ce que les orifices (5) sont réunis entre eux par des rainures (15) creusées dans la face extérieure de la paroi (3).6. Burner according to claim 5, characterized in that the orifices (5) are joined together by grooves (15) hollowed out in the outer face of the wall (3). 7. Brûleur selon la revendication 6, caracté­risé en ce que les pontets constitutifs des obstacles mécaniques sont constitués par des fils minces (16) logés dans les rainures (15).7. Burner according to claim 6, characterized in that the bridges constituting the mechanical obstacles consist of thin wires (16) housed in the grooves (15). 8. Brûleur selon l'une quelconque des précé­dentes revendications, caractérisé en ce que la paroi perforée de la boîte à air (1) et la cloison perforée de la nourrice (7) sont écartées entre elles d'une distance (D) de l'ordre du cm, en ce que le diamètre (T) de cha­que orifice (5) évidé dans la paroi perforée est de l'ordre de 4 mm, en ce que le diamètre intérieur (di) de chaque aiguille (11) est de l'ordre de 0,6 mm à 0,7 mm, en ce que son diamètre extérieur (de) est de l'ordre de 1,2 à 1,4 mm, en ce que la distance (E) entre les axes des aiguilles voisines est de l'ordre de 6 à 8 mm, en ce que le diamètre de chaque orifice complémentaire (24), s'il en est prévu, est de l'ordre de 2 à 3 mm et en ce que celui des petits trous de bordure (17), s'il en est prévu, est de l'ordre de 2 à 3 mm.8. Burner according to any one of the preceding claims, characterized in that the perforated wall of the air box (1) and the perforated partition of the manifold (7) are spaced apart by a distance (D) of l order of cm, in that the diameter (T) of each orifice (5) hollowed out in the perforated wall is of the order of 4 mm, in that the internal diameter (di) of each needle (11) is of the order of 0.6 mm to 0.7 mm, in that its external diameter (of) is of the order of 1.2 to 1.4 mm, in that the distance (E) between the axes of the neighboring needles is of the order of 6 to 8 mm, in that the diameter of each complementary orifice (24), if provided, is of the order of 2 to 3 mm and in that of the small border holes (17), if provided, is of the order of 2 to 3 mm. 9. Brûleur selon l'une quelconque des revendi­cations 1 à 4, caractérisé en ce que la paroi perforée de la boîte à air est composée de deux parois accolées (25,26), l'une intérieure et l'autre extérieure, pré­sentant des perforations (27,28) décalées mutuellement de façon telle que la paroi extérieure forme en regard des zones centrales des perforations de la paroi inté­rieure des pontets (29) constitutifs des obstacles mécaniques.9. Burner according to any one of claims 1 to 4, characterized in that the perforated wall of the air box is composed of two adjoining walls (25, 26), one inside and the other outside, having perforations (27,28) mutually offset so that the outer wall forms, opposite the central zones, perforations of the inner wall of the bridges (29) constituting the mechanical obstacles. 10. Brûleur selon la revendication 9, caracté­risé en ce que les perforations (27,28) présentent des formes allongées à bords parallèles et sont mutuellement alignées selon la direction de leur allongement.10. Burner according to claim 9, characterized in that the perforations (27,28) have elongated shapes with parallel edges and are mutually aligned in the direction of their elongation. 11. Brûleur selon la revendication 10, caracté­risé en ce que les deux parois accolées (25,26) sont circulaires et en ce que leurs perforations (27,28) sont allongées radialement,11. Burner according to claim 10, characterized in that the two adjoining walls (25, 26) are circular and in that their perforations (27, 28) are elongated radially, 12. Brûleur selon la revendication 11, caracté­risé en ce que les pontets (30) formés entre les perfo­rations (27) évidées dans la paroi intérieure (25) sont plus larges dans les zones, des parois accolées, les plus proches de l'axe de ces parois.12. Burner according to claim 11, characterized in that the bridges (30) formed between the perforations (27) hollowed out in the inner wall (25) are wider in the areas, of the adjoining walls, closest to the axis of these walls. 13. Brûleur selon l'une quelconque des revendi­cations 9 à 12, caractérisé en ce que la paroi intérieu­re (25) est plus épaisse que la paroi extérieure (26).13. Burner according to any one of claims 9 to 12, characterized in that the inner wall (25) is thicker than the outer wall (26). 14. Brûleur selon l'une quelconque des revendi­cations 9 à 13, caractérisé en ce que les parois acco­lée< (25,26) ont des épaisseurs de l'ordre de 1 à 2 mm et en ce que les perforations (27,28) évidées dans ces parois sont des fentes estampées dont la largeur est de l'ordre de 2 mm.14. Burner according to any one of claims 9 to 13, characterized in that the adjoining walls <(25,26) have thicknesses of the order of 1 to 2 mm and in that the perforations (27,28) hollowed out in these walls are stamped slots whose width is of the order of 2 mm. 15. Brûleur selon l'une quelconque des précé­dentes revendications, caractérisé en ce que la face, de la paroi perforée de la boîte à air, intérieure à cette boîte, est évidée à proximité immédiate de chaque ori­fice par au moins une entrée d'air (19) propre à impri­mer un mouvement rotatif à l'air admis dans cet orifice.15. Burner according to any one of the preceding claims, characterized in that the face of the perforated wall of the air box, internal to this box, is hollowed out in the immediate vicinity of each orifice by at least one air inlet (19) suitable for imparting a rotary movement to the air admitted into this orifice. 16. Brûleur selon l'une quelconque des précéden­tes revendications, caractérisé en ce que la boîte à air (1) présente la forme générale d'une galette cylindrique et la nourrice (7), celle d'un anneau creux coaxial à la boîte et contenu dans celle-ci.16. Burner according to any one of the preceding claims, characterized in that the air box (1) has the general shape of a cylindrical wafer and the feeder (7), that of a hollow ring coaxial with the box and contained in it.
EP89400765A 1988-03-21 1989-03-17 Gas burners Expired - Lifetime EP0334736B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT89400765T ATE86371T1 (en) 1988-03-21 1989-03-17 GAS BURNER.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8803618 1988-03-21
FR8803618A FR2628826B1 (en) 1988-03-21 1988-03-21 IMPROVEMENTS ON GAS BURNERS

Publications (2)

Publication Number Publication Date
EP0334736A1 true EP0334736A1 (en) 1989-09-27
EP0334736B1 EP0334736B1 (en) 1993-03-03

Family

ID=9364438

Family Applications (1)

Application Number Title Priority Date Filing Date
EP89400765A Expired - Lifetime EP0334736B1 (en) 1988-03-21 1989-03-17 Gas burners

Country Status (18)

Country Link
US (1) US4887963A (en)
EP (1) EP0334736B1 (en)
JP (1) JPH01318805A (en)
KR (1) KR950013965B1 (en)
CN (1) CN1036822A (en)
AT (1) ATE86371T1 (en)
AU (1) AU621093B2 (en)
BR (1) BR8901313A (en)
CA (1) CA1300485C (en)
DE (1) DE68905056T2 (en)
DK (1) DK169632B1 (en)
ES (1) ES2037973T3 (en)
FR (1) FR2628826B1 (en)
GR (1) GR3007212T3 (en)
MA (1) MA21518A1 (en)
PT (1) PT90045B (en)
TN (1) TNSN89038A1 (en)
ZA (1) ZA892011B (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0350388B1 (en) * 1988-07-05 1992-03-25 Chaffoteaux & Maury Hot water generator
EP0580500A1 (en) * 1992-07-23 1994-01-26 Chaffoteaux Et Maury Gas burner
US5441402A (en) * 1993-10-28 1995-08-15 Gas Research Institute Emission reduction
EP0780631A3 (en) * 1995-12-19 1998-09-30 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Method and burner for combustion of hydrogen
WO1999019669A1 (en) * 1997-10-09 1999-04-22 Leonid Nikolaevich Parfenov Method for the radiation-convection heating of heat-exchange surfaces
DE102008019854A1 (en) * 2008-04-23 2009-10-29 J. Eberspächer GmbH & Co. KG Wall structure and burner as well as system
CN102777902A (en) * 2011-05-10 2012-11-14 程敏 Six-ring-fire energy-saving burner
CN105823043A (en) * 2016-03-21 2016-08-03 广东工业大学 Energy-saving gas combustion system
DE102019121922B3 (en) * 2019-08-14 2020-11-26 Alfons Krapf External mixing gas series burner

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8900030A (en) * 1989-01-06 1990-08-01 Remeha Fabrieken Bv NOX-POOR ATMOSPHERIC GAS BURNER.
US5102329A (en) * 1991-04-15 1992-04-07 Coen Company, Inc. High intensity burner
US5133657A (en) * 1991-06-17 1992-07-28 Harmony Thermal Co. Inc. High turndown sheet metal atmospheric gas burner
US5161379A (en) * 1991-12-23 1992-11-10 United Technologies Corporation Combustor injector face plate cooling scheme
AT399561B (en) * 1992-08-03 1995-06-26 Vaillant Gmbh ATMOSPHERIC BURNER
US5397234A (en) * 1993-11-15 1995-03-14 Harper-Wyman Company Gas stove top burner assembly
DE29512231U1 (en) * 1995-07-28 1996-11-28 Aga Ab External mixing burner
US6267585B1 (en) * 1995-12-19 2001-07-31 Daimlerchrysler Aerospace Airbus Gmbh Method and combustor for combusting hydrogen
US5881756A (en) * 1995-12-22 1999-03-16 Institute Of Gas Technology Process and apparatus for homogeneous mixing of gaseous fluids
US6813889B2 (en) * 2001-08-29 2004-11-09 Hitachi, Ltd. Gas turbine combustor and operating method thereof
US6928823B2 (en) * 2001-08-29 2005-08-16 Hitachi, Ltd. Gas turbine combustor and operating method thereof
US6702571B2 (en) 2001-09-05 2004-03-09 Gas Technology Institute Flex-flame burner and self-optimizing combustion system
DE102004037689A1 (en) * 2004-08-02 2006-03-16 Behr Gmbh & Co. Kg Surface burner, in particular for a fuel cell system
CN100464120C (en) * 2005-08-26 2009-02-25 浙江帅康电气股份有限公司 Gas burner
US20070059657A1 (en) * 2005-09-15 2007-03-15 Chia-Hsi Yen Gas burner
CN100410586C (en) * 2006-03-13 2008-08-13 郑宗标 High-pressure blowing-in and combustion-supporting gas cooker
JP4934696B2 (en) * 2009-03-26 2012-05-16 株式会社日立製作所 Burner and combustor
EP2246619B1 (en) * 2009-04-30 2015-08-19 Electrolux Home Products Corporation N.V. Vertical flame burner
US8707672B2 (en) * 2010-09-10 2014-04-29 General Electric Company Apparatus and method for cooling a combustor cap
US8939759B2 (en) * 2011-10-21 2015-01-27 Rinnai Corporation Tubular burner
JP5723327B2 (en) * 2012-07-03 2015-05-27 リンナイ株式会社 Tubular burner
DE112014002809T5 (en) * 2013-06-14 2016-04-28 Beneq Oy Burner nozzle, burner and a surface treatment device
KR20160124203A (en) * 2014-03-18 2016-10-26 쳉퉁 찬 Stove core structure of infrared gas stove
CN104132341B (en) * 2014-07-07 2017-01-18 宁波多贝机械实业有限公司 Gas boiler burner
CN105387463B (en) * 2015-12-02 2019-04-12 芜湖美的厨卫电器制造有限公司 Burner and water heater with it
CN105423298B (en) * 2015-12-14 2017-09-26 丹东太智厨房设备有限公司 Blowed premixed gas burner
CN105423299A (en) * 2015-12-28 2016-03-23 广东海信家电有限公司 Gas distributing disk, combustor and gas stove
CN106895401A (en) * 2016-03-20 2017-06-27 孙瑜 A kind of flame core oxygen enriching burning-aid formula gas burner
US11226092B2 (en) 2016-09-22 2022-01-18 Utilization Technology Development, Nfp Low NOx combustion devices and methods
IT201800005589A1 (en) * 2018-05-22 2019-11-22 Modular burner

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR639438A (en) * 1927-01-24 1928-06-21 Gas burner
FR1284906A (en) * 1961-03-24 1962-02-16 Cie Belgo Luxembourgeoise Du C Gas burner
US3061001A (en) * 1958-09-12 1962-10-30 Zink Co John Gaseous fuel burner
US3203769A (en) * 1961-12-06 1965-08-31 Res Ass Of Polymer Raw Materia Furnace for cracking hydrocarbons having a flame-adjustable burner
US3204682A (en) * 1963-08-26 1965-09-07 American Gas Furnace Co Oxy-gas blowpipe
FR1520464A (en) * 1967-01-12 1968-04-12 Air Liquide Improvement in ramp burners
FR1580006A (en) * 1967-09-29 1969-08-29
US3574507A (en) * 1969-07-31 1971-04-13 Gen Electric Air/fuel mixing and flame-stabilizing device for fluid fuel burners
US4169700A (en) * 1976-09-10 1979-10-02 Nippon Steel Corporation Burner for a regenerative hot blast stove
EP0069245A2 (en) * 1981-07-03 1983-01-12 Messer Griesheim Gmbh Nozzle mixing gas-oxygen burner

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1518577A (en) * 1922-09-07 1924-12-09 Stephen P Enright Gas heater
US1697002A (en) * 1928-02-01 1929-01-01 Evanko John George Gas-saving appliance
US2594914A (en) * 1949-02-12 1952-04-29 Grosskloss John Frederick Burner
DE1529197B1 (en) * 1966-04-06 1970-04-30 Kurt Krieger Radiant burner
GB1227347A (en) * 1967-10-26 1971-04-07
US3695818A (en) * 1969-10-31 1972-10-03 Rinnai Kk Radiant burner
FR2157328A5 (en) * 1971-10-18 1973-06-01 Mitsubishi Electric Corp
US4848313A (en) * 1987-03-23 1989-07-18 Scheu Manufacturing Company Compact forced air heater

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR639438A (en) * 1927-01-24 1928-06-21 Gas burner
US3061001A (en) * 1958-09-12 1962-10-30 Zink Co John Gaseous fuel burner
FR1284906A (en) * 1961-03-24 1962-02-16 Cie Belgo Luxembourgeoise Du C Gas burner
US3203769A (en) * 1961-12-06 1965-08-31 Res Ass Of Polymer Raw Materia Furnace for cracking hydrocarbons having a flame-adjustable burner
US3204682A (en) * 1963-08-26 1965-09-07 American Gas Furnace Co Oxy-gas blowpipe
FR1520464A (en) * 1967-01-12 1968-04-12 Air Liquide Improvement in ramp burners
FR1580006A (en) * 1967-09-29 1969-08-29
US3574507A (en) * 1969-07-31 1971-04-13 Gen Electric Air/fuel mixing and flame-stabilizing device for fluid fuel burners
US4169700A (en) * 1976-09-10 1979-10-02 Nippon Steel Corporation Burner for a regenerative hot blast stove
EP0069245A2 (en) * 1981-07-03 1983-01-12 Messer Griesheim Gmbh Nozzle mixing gas-oxygen burner

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0350388B1 (en) * 1988-07-05 1992-03-25 Chaffoteaux & Maury Hot water generator
EP0580500A1 (en) * 1992-07-23 1994-01-26 Chaffoteaux Et Maury Gas burner
FR2694072A1 (en) * 1992-07-23 1994-01-28 Chaffoteaux Et Maury Improvements to gas burners.
US5441402A (en) * 1993-10-28 1995-08-15 Gas Research Institute Emission reduction
EP0780631A3 (en) * 1995-12-19 1998-09-30 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Method and burner for combustion of hydrogen
WO1999019669A1 (en) * 1997-10-09 1999-04-22 Leonid Nikolaevich Parfenov Method for the radiation-convection heating of heat-exchange surfaces
US8573968B2 (en) 2008-04-21 2013-11-05 Eberspächer Climate Control Systems GmbH & Co. KG Wall structure and burner as well as system
DE102008019854A1 (en) * 2008-04-23 2009-10-29 J. Eberspächer GmbH & Co. KG Wall structure and burner as well as system
CN102777902A (en) * 2011-05-10 2012-11-14 程敏 Six-ring-fire energy-saving burner
CN105823043A (en) * 2016-03-21 2016-08-03 广东工业大学 Energy-saving gas combustion system
CN105823043B (en) * 2016-03-21 2018-05-29 广东工业大学 Economical gas combustion system
DE102019121922B3 (en) * 2019-08-14 2020-11-26 Alfons Krapf External mixing gas series burner

Also Published As

Publication number Publication date
DE68905056T2 (en) 1993-08-19
EP0334736B1 (en) 1993-03-03
BR8901313A (en) 1989-11-07
MA21518A1 (en) 1989-10-01
US4887963A (en) 1989-12-19
KR890014961A (en) 1989-10-25
DK134689A (en) 1989-09-22
CN1036822A (en) 1989-11-01
JPH0565766B2 (en) 1993-09-20
PT90045A (en) 1989-11-10
DK169632B1 (en) 1994-12-27
AU3148189A (en) 1989-09-21
CA1300485C (en) 1992-05-12
FR2628826A1 (en) 1989-09-22
KR950013965B1 (en) 1995-11-18
DE68905056D1 (en) 1993-04-08
ATE86371T1 (en) 1993-03-15
PT90045B (en) 1994-03-31
AU621093B2 (en) 1992-03-05
DK134689D0 (en) 1989-03-20
TNSN89038A1 (en) 1991-02-04
JPH01318805A (en) 1989-12-25
GR3007212T3 (en) 1993-07-30
FR2628826B1 (en) 1992-04-24
ES2037973T3 (en) 1993-07-01
ZA892011B (en) 1990-05-30

Similar Documents

Publication Publication Date Title
EP0334736B1 (en) Gas burners
EP1306616B1 (en) Gas burner of the atmospheric type
EP1195556B1 (en) Gas burner and cooking appliance using such burner
FR2586453A1 (en) CARBURETOR FOR GAS TURBINE ENGINE
FR2601756A1 (en) BURNER ASSEMBLY OPERATING AT HIGH TEMPERATURE
CA2925737A1 (en) Lean gas burner
FR2511478A1 (en) BURNER WITH GAS MIX
FR2481415A1 (en) Burner for pressurised gas - has powered air induction and divergent passage for delivery of mixture
EP0222654A1 (en) Gas turbine engine with an afterburner having radially disposed individual atomizers
EP0967434B1 (en) Burner with concentric air ducts and central stabilizer
CA3146685A1 (en) Modular burner and furnace comprising this burner
FR2695457A1 (en) Gas burners for heating and heating water supplies - has venturi tubes each having injectors and supplying common parallel rectangular burners with perforated burner ramps
FR2772887A1 (en) LOW-EMISSION NITROGEN OXIDE BURNER WITH RECYCLED GAS CIRCUIT
EP0178198A2 (en) Burner with a priorily mixture and an integrated pilot-flame
FR2694072A1 (en) Improvements to gas burners.
FR2766557A1 (en) LIQUID AND GASEOUS FUEL BURNERS WITH LOW EMISSION OF NITROGEN OXIDES
FR2570473A1 (en) Improvements to gas boilers with parallel flow comprising a rose and a flame retention baffle (hub) relating to gas boilers and independent supply of combustion air
FR2686397A1 (en) FLAME TUBE FOR A BURNER, IN PARTICULAR FOR LIQUID FUELS.
WO2023213820A1 (en) Flame-proof and explosion-proof surface combustion gas burner
EP0162761B1 (en) Burner with vanes and a well-balanced secondary air supply
EP0631091A1 (en) Low NOx gas burner
CH631004A5 (en) APPARATUS FOR COMBUSTING A MIXTURE OF AIR AND FUEL.
CA1264437A (en) Gas burner
FR2714455A1 (en) Improved combustion head for gas burner, burner equipped with such a head and combustion method.
FR2719361A1 (en) Improvements to gas burners.

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE ES FR GB GR IT LI LU NL SE

17P Request for examination filed

Effective date: 19900306

17Q First examination report despatched

Effective date: 19910528

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE ES FR GB GR IT LI LU NL SE

REF Corresponds to:

Ref document number: 86371

Country of ref document: AT

Date of ref document: 19930315

Kind code of ref document: T

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19930302

REF Corresponds to:

Ref document number: 68905056

Country of ref document: DE

Date of ref document: 19930408

ITF It: translation for a ep patent filed

Owner name: UFFICIO TECNICO ING. A. MANNUCCI

REG Reference to a national code

Ref country code: GR

Ref legal event code: FG4A

Free format text: 3007212

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2037973

Country of ref document: ES

Kind code of ref document: T3

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 19940221

Year of fee payment: 6

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GR

Payment date: 19940223

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19940311

Year of fee payment: 6

Ref country code: ES

Payment date: 19940311

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 19940316

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 19940317

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LU

Payment date: 19940430

Year of fee payment: 6

EPTA Lu: last paid annual fee
EAL Se: european patent in force in sweden

Ref document number: 89400765.7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19950317

Ref country code: GB

Effective date: 19950317

Ref country code: AT

Effective date: 19950317

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19950318

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19950318

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19950324

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19950331

Ref country code: CH

Effective date: 19950331

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19950331

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 19950413

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

Effective date: 19950930

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19950317

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

Ref country code: GR

Ref legal event code: MM2A

Free format text: 3007212

EUG Se: european patent has lapsed

Ref document number: 89400765.7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Effective date: 19960331

BERE Be: lapsed

Owner name: CHAFFOTEAUX & MAURY

Effective date: 19960331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19961001

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 19961001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19961203

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 19990301

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20040323

Year of fee payment: 16

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050317

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20051130

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20051130