METHODS AND APPARATUS FOR GAS COMBUSTION

Abstract: In a method of combustion designed to achieve a further reduction in harmful emissions, especially of NOx and CO, which is viable at advantageously reduced noise levels and lower cost with any burner of a type comprising a slotted or pierced diffuser of thin sheet metal in receipt of fully or partly mixed gas and air supplies, typically in appliances comprising a heat exchanger such as the boilers of central heating systems, the essential steps are: a) supplying a uniform flow of fuel-air mixture to the slots; b) discharging the mixture from a pierced surface of substantially doughnut geometry comprising a slotted peripheral area (Ap) and an essentially solid central area (Ac) of prescribed proportions; c) bringing combustion to completion in a slender lamellar flame; d) regulating the rate of aeration to a value between 0.9 and 1.4, or e) to values less than 1.6; f) effecting a recycle of post-combustion gases.

Description: METHODS AND APPARATUS FOR GAS COMBUSTION The invention relates to a method of bringing about the combustion of gases while controlling harmful emissions, and to the relative burner and system, that is, a new procedure by which to obtain thermal energy from gases such as methane, butane, propane or others, and blends thereof, whether by supplying the gas-air mixture to the burner partly premixed, i.e. with an aeration rate (the ratio between the effective quantity of air present in a given volume of the mixture and the quantity required to bring about stoichiometric combustion in the same volume) less than or equal to 1, or by supplying a mixture totally premixed, that is, with an aeration rate higher than 1, in such a way that harmful emissions (principall NOx and CO) are either eliminated completely or reduced to negligible levels; such a method is implemented by means of a burner and variable power fuel feed system also constituting subject matter of the disclosure. The prior art embraces a method of bringing about gas combustion at low NOx and CO emission levels as disclosed in application for international patent number PCT/IT 87/00079 filed 03/08/87 by the same applicant, which comprises the steps of: -aspirating -a quantity of primary air equal to at least 80* of the quantity stoichiometrically required; -directing a quantity of secondary air to the single flames, from the start of combustion, in excess of 100% of the stoichiometric value; -bringing combustion to completion internally of a thin flame of lamellar configuration, evidence of which, in the case of natural gas, is the emission of a violet colour of wavelength less than 0.42nm. For the implementation of such a method, the above application discloses exclusively an atmospheric burner, that is, a burner connected into a circuit through which fuel and air circulate naturally, in association with a horizontally disposed tubular diffuser affording groups of slots for the passage of the fuel and primary air mixture, distributed over the surface of the diffuser in successive sets extending transversely to its axis, which are set apart one from the next by an amount equal to nd/2, where d is the axial length of the group and n is the number of groups in each set, or the number of groups in two successive sets in the case of a chequered distribution pattern; the distance which separates the groups of slots of one set in the transverse direction is equivalent to at least 65_> of the length of the longest slot of one group. Each group generates a lamellar flame appearing as a pair of divergent wings, butterfly-like in form, of which the axis of symmetry coincides with the longitudinal median plane of each group. Whilst reflecting notable progress in the control of emissions, particularly NOx and CO, the method set forth in the aforementioned PCT application in effect neither envisages nor permits of feeding the diffuser with mixtures containing percentages of oxygen close to or exceeding stoichiometric values; neither can combustion be sustained in the presence of post-combustion gases, due to the instability of the flame and consequent impossibility of operation in these particular conditions, a fact attributable to the limitations of the method and of the design of th ' e burner, both separately and in combination. With regard to the control of output variations and feed, the prior art embraces devices as in patents DE 3010014 and DE 3018752, both filed in 1980. The former discloses regulation of the combustion assisting air by governing pressure upstream and downstream of the combustion chamber, which can be achieved by the installation of a diaphragm, in conjunction with control over the pressure of the gas supplied to the burner nozzles. The latter discloses a nozzle with two chambers in series, of which the outlet sections are controlled by respective obturators associated with a single stem, in conjunc ion with means by which to control both the flow of primary air and the flow of the fuel-air mixture. In both devices, there is the disadvantage that a high rate of aera ion cannot be achieved without specifying notably large dimensions both for the device itself and for the Venturi tube, hence for the body of the burner in the event that the tube is incorporated internally. As to the width of horizontally disposed tubular burners, the dimensions of the corresponding cross section are considered to be excessive in some instances. The prior art thus stands in need of considerable improvement with regard to overcoming the drawbacks mentioned above. Accordingly, the objects of the invention are to provide a method of combustion such as will ensure notable stability of a flame in any given condition under which gas is supplied to the relative burner, for example by varying the type of gas or its rate of flow at the nozzle outlet, and in any condition of operation, with fuel and air premixed totally or in part, or of installation of the burner, whether in atmospheric or forced circuits, in such a way that harmful emissions, NOx and CO especially, can be reduced either to zero or to negligible values (e.g. of the order of the standard error adopted for measuring instruments); and in implementing such a method to achieve a stable flame of lamellar configuration with the diffuser in receipt of fuel and air mixed either in hyperstoichiometric or near-stoichiometric proportions, notwithstanding combustion may occur in an environment wholly or partly occupied by combusted gases, with a diffuser disposed not only horizontal but also vertical, sub-vertical or howsoever, and in a burner of cylindrical, conical, parallelepiped or whatever embodiment whether as selected, or imposed by the geometry and location of the heat exchanger hence also of the combustion chamber; also to ensure combustion conditions such as will enable a smooth transition from ignition to steady burn, obtaining a stable flame and full combustion even with power in modulation and in extreme operating conditions, and to ensure that combustion occurs remotely from the diffuser, thereby contriving to prevent over-heating and avoid the need fo substitution of the relatively low cost sheet metal usuall employed with more expensive refractories, which are ofte fragile; and finally, to achieve all of the above at markedly reduced or restrained cost and with negligibl noise levels. The stated objects are achieved though the adoption of method consisting in a combination of the following steps: A) feeding the slots of the diffuser uniformly with a homogeneous mixture of air and combustible gas; B) efflux of the mixture from slots each exhibiting a width dimension that may be as much as equal to the depth, as considered in the direction of the efflux, or marginally greater, according to the type of gas, arranged in groups around relative central zones that are either unpierced or may be pierced over an area measuring no more than 20* of the overall area of the central zone itself; to advantage, the ratio between the area of the peripheral zone occupied by the slots and the area of the central zone is between 3 and 10, and the ratio between the area of the slots and the area of the peripheral zone between 1/2 and, 1/3.5, the central zone being of width up to 3 mm maximum, and of any given length; the groups of slots may be distributed in repeated rows orientated in any given direction, aligned or staggered; C) commencement and completion of combustion, brought about instantaneously and in a single stage at each group of slots in slender lamellar flames with a hyperstoichiometric mixture of fuel and air which, in the case of natural gas (methane) is reflected in the emission of violet radiation of wavelength less than 0.42 fm; the flames of each group combine to create the impression of butterfly wings, tulip corolla, trumpet, campanula or similar, regularly formed or otherwise, springing divergently from a level immediately above and at less than 2 mm from the surface of the diffuser, the axis or plane of symmetry disposed perpendicular to a tangential plane passing through the centre of each group, thereby obtaining a saturated volume of fully combusted gases, encompassed externally by the flames of each group and spreading with the increase in distance from the diffuser, in which the partial pressure of the oxygen is further reduced, and a slow recirculation of combusted gases occurring at the base of the volume such as will maintain temperatures sufficient to allow ignition; D) in operation at a variable rate of aeration, lower even than 1.1, with natural or forced circulation of combusted air and gases and with specific loading on the diffuser (ratio between thermal power output and the surface area of the flame outlets) of between 0.3 and 0.8 kW/σ , regulation of the aeration rate to within values of 0.9, related to opera ion at maximum output, and 1.4, related to operation at minimum output and starting; and with an aeration rate less than or equal to 1.1, induction of the quantity of air required to effect full combustion in a partial vacuum created by the jet of fuel-air mixture issuing from the slots to invest the external face of the lamellar flames; E) in operation with a rate of aeration permanently above 1.1, with natural or forced circulation of combusted air and gases, regulation of the rate to values no higher than 1.6 and advantageously between 1.1 and 1.3, whether at maximum output or in the starting or modulating modes, with specific loading on the diffuser of between 0.3 and 2 0.8 kW/σm j supply pressure of the gas fuel being, to advantage, between 100 and 450 mbar; F) diversion of the combusted gases by induction into a partial vacuum created with the jet of fuel-air mixture issuing from the slots to invest the external face of the lamellar flames, having been cooled and mixed with air at a rate of between 0 and 100*, with the result that the partial pressure of the oxygen is reduced during combustion by the gases, and the excess of air also limited, thus benefiting efficiency; G) diversion of the combusted gases by induction into a partial vacuum created with the jet of fuel-air mixture issuing from the slots to invest the external face of the lamellar flames, having been cooled and mixed with air at a rate of between 10 and 100*, with the result that the partial pressure of the oxygen is reduced during combustion by the gases, and the excess of air also limited, thus benefiting efficiency. The fol owing are preferred combinations of the steps of the method as recited above, related to possible fuel feed conditions: - A, B, C, D - A, B, C, E - A, B, C, D, G - A, B, C, E, F As to the preferred burner for implementa ion of such a method, the stated objects are realized by adopting a diffuser with slots distributed in groups, each group consisting in a peripheral zone encompassing a central zone either devoid of slots or pierced over an area limited to no more than 20* of the area of the central zone itself, occupying a surface, advantageousl , of between 5 and 40 mm3 such that the ratio between the area of the peripheral zone and the area of the central zone is advantageously between 3 and 10, and the ratio between the area of the slots and the area of the peripheral zone is between 1/2 and 1/3.5, whilst for a maximum width of the central zone measuring approximately 3 mm the corresponding length can assume any given value; the groups of slots can be distributed for example in longitudinally repeated transverse rows, and the width of a single slot can be equal to the thickness of the diffuser wall, or marginally greater, according to the type of gas. The burner may be provided with a Ven uri tube, disposed internally or externally of the body of the diffuser about a rectilinear axis or otherwise and vertical or horizontal, angled or skew, whilst the body of the diffuser itself may be of tubular section, cylindrical or prismatic and tapered, pyramidal, or rectangular and elongated, and embodied with groups of slots preferably of rectangular geometry, or of openings in general, occupying its surface entirely or in part. For installation in circuits where the circulation of poεt- combustion gas and air is forced, and advantage is gained from a maximum reduction in height, the preferred burner exhibits a body of cross section appearing bilobed at bottom to create a pair of lateral channels situated below a flat diffuser marginally arched in profile and outwardly convex, or indeed of any suitable profile and incorporating the slots or openings according to the invention, with central inlet ports at bottom distributed longitudinally between the two bilobed formations and directing the flow of mixture into two diverging branches of sinuous curvilinear axis and progressively increasing section, which are separated from the diffuser by a longitudinal baffle straddling the division of the branches and exhibiting a cross section of upturned minuscule omega profile extending the length of the burner. As to the fuel feed system, and the difficulties connected with regulating the power output while holding the rate of aeration steady between limits according to the method disclosed, where a natural current induced in the circuit carrying combusted air and gas is sufficient to sustain complete combustion, or where forced circulation is produced with a fan, these are overcome by adopting a gas nozzle of variable outlet section consisting in a proportioning element with a conical forward end, having a critical taper angle between 0 and 10C and capable of guided axial movement internally of an orifice formed in the body of the nozzle of which the taper angle is equal or approximatel equal to that of the proportioning element, thus obtaining a progressive reduction in gas pressure at the ou let through the reduction in section of the orifice in respect of the reduction in the rate of aeration with variation in flow, hence in output; the rear end of the proportioning element is fashioned as a plate biased into contact with the lateral surface of a manually or automatically operated cam by a spri g. Advantageously, operating with forced circulation of the combusted gas and air, use is made of a variable speed centrifugal compressor providing delivery pressures of between 100 and 450 mbar and enabling partial recycle of the mixture, of which the inlet circuit is equipped with alternating on/off valves installed on the air and gas lines. Advantages of the invention are: a reduction in the level of harmful emissions, especially NOx and CO, to values corresponding to the standard permissible errors adopted for measuring instruments; a further reduction in noise levels; an extension of the benefits of lower emissions and noise levels to all possible designs of burner with thin sheet metal diffusers (0.2 mm to thicknesses even in excess of 2 mm) in receipt of fuel and air mixed either fully or in part, installed in circuits through which combusted air and gas circulate either naturally or forcibly, also with outpu -modula ed circuits; increased specific thermal output; a lamellar flame of notable stability, even with fuel and air mixed in hyperstoichiometric proportions, and/or in the transition from ignition to steady burn, and/or when combustion occurs in an environment totally or partly occupied by combusted gases; the continued presence of a temperature at the base of the flame sufficiently high to sustain ignition though not so high as to damage the sheet metal by overheating or to necessitate the adoption of diffusers in ceramic material or other materials affording resistance to high temperatures; a notable reduction in costs; the provision of a functional, simple and economic device for regulating output; a reduction in burner height, where desirable; a further reduction in the distance separating heat exchanger and diffuser. The invention will now be described in detail, by way of example, with the aid of the twenty-one accompanying sheets of drawings, in which groups of slots are illustrated generically in shape and number as i occupying a flat surface, though the surface might in effect be curved or cuspidate : - fig 1 is the view from above of a tubular burner according to the invention, for installation in an appliance with forced circulation of combusted air and gas, disposed with axis horizontal and with groups of slots distributed over the entire surface of the diffuser; - fig 2 is the longitudinal and vertical section through II- II in fig 1; fig 3 shows the burner of fig 2 from the left, viewed along the longitudinal axis; fig 4 is the view from above of a tubular burner for installation in an appliance with natural circulation of combusted air and gas, and with groups of slots distributed over the top part of the topmost surface of the diffuser; ~ fi S 5 iε nβ side elevation of fig 4; fig 6 shows the burner of fig 4 from the left, viewed along the longitudinal axis; fig 7 is the view from above of a burner with a tubular cylindrical diffuser according to the invention, disposed with axis vertical and associated with an external and perpendicularly disposed Venturi tube, and with groups of slots distributed around the uppermost part of the lateral surface of the diffuser; - fig 8 iε a longitudinal and vertical section through VIII- VIII in fig 7; - fig 9 is the view from above of a burner with a vertically disposed tubular cylindrical diffuser according to the invention, similar to that shown in fig 7 but with the external Venturi tube located beneath and coaxial with the diffuser, and with groups of slots distributed over the lateral surface of the diffuser; - fig 10 is a longitudinal and vertical section through X-X in fig 9; - fig 10a is the side elevation of a slimline burner element for assembly in banked formation, with groups of slots distributed along the top of the diffuser, which exhibits a cuspidate profile with pitched surfaces mutually angled at 90° or more; - fig 10b is the plan of fig 10a; - fig 10c is an intermediate vertical cross section through three elements constituting a burner as in fig 10a; - figs 11, 12, 13, 14, 15, 16, 17, 18 are profiles of the right cross sections of diffusers as in the burners of figs 1, 2, 3, 4, 5 and 6, which exhibit a closed loop convex curvilinear outline; figs 19, 20, 21, 22, 23, 24 are profiles of the right cross sections of diffusers as in the burners of figs 1, 2, 3 » 4, 5 and 6, which exhibit a closed loop polygonal outline with radiused vertices, for example triangular, quadrangular, penta-, hexa- and octagonal; fig 25 illustrates one of the groups of slots of a diffuser according to the invention, enlarged and in detail and developed, of which the slots are disposed with their longitudinal axes mutually parallel and occupy a peripheral zone defined internally by a rhombus, constituting the central zone of the group, and -encompassed externally by an octagon; ~ fi S 2έ iε tne enlarged and detailed illustration of a group of diffuser slots as in fig 25, in this instance with the central zone occupied by three . longitudinally aligned holes serving to stabilize the flame; fig 27 is the enlarged and detailed illustration of a group of diffuser slots as in fig 25, in this instance with a single hole in the central zone serving to stabilize the flame and with the two central slots eliminated; fig 28 is the enlarged and detailed illustration of a group of slots as in fig 27, though without holes in the central zone for stabiliza ion of the flame; fig 29 is the enlarged and detailed illustration of a group of slots of a diffuser according to the invention, showing slots disposed with longitudinal axes mutually parallel and occupying a peripheral zone in the form of an annulus, and a central hole for stabilization of the flame; fig 30 iε the enlarged and detailed illustration of a group of slots as in fig 29, though without central holes for stabilization of the flame; fig 31 is the enlarged and detailed illustration of a group of slots of a diffuser according to the invention, showing slots arranged in a peripheral zone encompassed between two practically homothetic ovals, and a central hole for stabilization of the flame; fig 32 is the enlarged and detailed illustration of a group of slots as in fig 31, though with two holes in the central zone for stabilization of the flame; fig 33 is the enlarged and detailed illustration of a group of slots occupying an annular peripheral zone, angled singly between directions radial and tangential to the circular central zone of smaller radius, and intercalated with triangular openings; fig 34 is the enlarged and detailed illustration of a group of εlotε exhibiting a curved profile and occupying a peripheral zone encompassed between two concentric rectangles with curvilinear sides; fig 35 iε the enlarged and detailed illustration of a group of slots occupying an annular peripheral zone, distributed transversely and coinciding with the sides of a plurality of concentric pentagons inscribed within the annulus; fig 36 is the enlarged and detailed illustration of a group of slots arranged in two radiating sets of dissimilar dimensions internally of an annular peripheral zone; fig 37 iε the enlarged and detailed illustration of a group of εlotε arranged in oval tiers of increasing developable length; fig 38 is the enlarged and detailed illustration of a group of arcuate slots occupying concentric circumferences; fig 38a iε a plan εhowing groups of at least three elongated rectangular slots each, advantageously six in number and divided into two sub-groups in which the slotε are disposed parallel at a constant diεtance between centres and bordering a central zone of width less than or equal to 3 mm, by way of example, the distance between groups being between 1 and 4 mm, for example, and disposed along a rectilinear axis parallel to that of the εlots; - fig 38b is a plan showing groups of slots similar to those of fig 38a, in this instance bordering on a central zone exhibiting a zigzagging rectilinear axis; - fig 39 is the view from above of a flame appearing trumpet or funnel shaped; - fig 40 is a central vertical section through XL-XL in fig 39; - fig 41 is the central vertical section through XLI-XLI in fig 39, disposed perpendicular to that of fig 40; - fig 4-2 iε a view in perspective of the flame propagated from a group of εlotε as in figs 39, 40 and 41; fig 43 iε the view from above of an enlarged part of the topmost surface of the diffuser of a burner according to the invention, in which the groups of slots are aligned, at regular pitch, parallel with the axis of the burner; - figs 44, 45, 46 and 47 are developed views of part of the surface of a diffuser, showing groups of slots arranged and aligned respectively in two, three, four or five rows, parallel with the axis of the diffuser and staggered one from the next; - figs 48 and 49 are views showing part of the diffuser of a burner according to the invention,- with groups of slots distributed in alignment along two directions perpendicular one to another; - fig 50 iε a view similar to that of fig 43, with groups of slots arranged in square formation; figs 51, 52 and 53 are the developed views of diffusers exhibiting square frusto-pyramidal, triangular prismatic and frustoσonical geometry, respectively; - fig 54 is a longitudinal section through the variable outlet fuel nozzle according to the invention; fig 55 is the diagram of a system according to the invention for the mixture and forced feed of fuel and air; fig 56 is the longitudinal section through a low profile burner according to the invention; - fig 57 is the section through LVII-LVII in fig 56; - fig 58 shows the burner of fig 56 from above. With reference to the drawings, 1 denotes a burner of tubular embodiment, comprising a diffuser 2 of which the en ire operating surface is occupied by groups of slots 3, arranged in a given formation; 3a denotes the trumpet shaped flame issuing from each group of slots. 4 denotes a Venturi tube accommodated within and coaxial with the diffuser 2 of which the inlet is connected to a front flange 5 embodied with a peripheral internal lip 6 matched to the profile of the inner wall of the diffuser 2. 7 denotes one of a set of holes (fig 7) passing axially through the frontal surface of the flange 5 externally of the diffuser, by way of which to bolt the burner 1 to a gas manifold (not illustrated). 8 denotes a rear cover inserted into the end of the diffuser 2 positioned farthest from the flange 5. L1 denotes the length of the diffuser 2, which is between 10 cm and 1 metre or over, depending upon the length of the combustion chamber in which the burner is to be installed; L2 denotes the length of the Venturi tube, including the connection to the front section of the diffuser, which to advantage is equal to L1 less a quantity such that the mean velocity of the mixture in reverse flow will not exceed 2 m/s, to which end the tube may be fitted with suitable inversion baffles (not illustrated); L3 is the distance between the diffuser inlet and the farthest extremity of the farthest group of slots, and L4 the difference between L2 and L3, which to advantage is between 50 and 150* of the diameter of the outlet section of the Venturi tube. 9 denotes a tubular diffuser (fig 4) with groups of slots 3 distributed over the topmost part of the lateral surface; 10 denotes a nozzle mounted to a bracket 11 secured forward of the flange 5, from which the mixture of air and combustible gas is ejected. 12 denotes a burner (fig 7) comprising a vertically disposed tubular diffuser 12a of cylindrical shape, and an inlet and mixer duct 13, which might be a Venturi tube, located externally of and normal to the axis of the diffuser 12a and connected into the lower part of the diffuser side wall; 14 denotes a nozzle bracket rigidly associated with the top of the inlet and mixer duct 13 at the forward end, and affording a through hole 15 coaxial with the duct; the diffuser 1 a is enclosed by end covers 16 and exhibits groups of slots 3 ordered in successive bands around the uppermost part of the side wall. 17a denotes a burner (fig 9) comprising a tubular diffuser 18 of cylindrical embodiment disposed with axis vertical, and an externally located inlet and mixer duct 19 disposed coaxial with the diffuser 18 and connected centrally to the bottom end cover 20; 21 denotes a similar top end cover, and 22 a flange insertable into the end of the tube 19 farthest from the diffuser and carrying a nozzle bracket 23 with the usual axial hole; 24 denotes a formation of groups of slots 3 ordered in successive bands and occupying the entire available height of the diffuser side wall, with the axes of the single normal to the axis of the diffuser 18. 24a denotes a slimline burner (fig 10a) designed for assembly with others in banked forma ion, which comprises a Venturi type inlet duct 24b having a bent axis and emerging uppermost into a mixing and distribution chamber 24c of vertically elongated and parallelepiped embodiment, surmounted in turn by a diffuser 24d. of rounded or cuspidate profile; 24e denotes the part of the duct 24b connecting the rear end of the Venturi with the chamber 24σ above, and 24f a series of punched indentations extending longitudinally above the connecting duct 24e and serving to reduce the velocity of the air and gas mixture at the rear end of the burner element 24a. C denotes the combined height of the distribution chamber 24c and the diffuser 18; C1 is the height of the flame, effectively 10...15 mm or thereabouts in the case of natural gas, which iε propagated with little or no halo, thus liberating a potential heat of 2 kW approx per element 24a of the burner; C2 iε the corresponding width of the single flame, which for a diffuser 24d measuring 8 mm approx in width will be 13...20 mm; C3 denotes the distance between centres of adjacent elements 24a, typically 18...25mm; Z denotes the gas manifold, Z1 one of a plurality of nozzles disposed transversely to the manifold and in coaxial alignment with the inlet to the relative Venturi duct 24b, and Z2 a bracket supporting the element 24a, which is secured in its turn to a support Z3 located between the manifold and the Venturi inlet. Fig 11 shows the cross sectional profile 25 of a tubular diffuser as in the burner denoted 1, which is composed of parallel rectilinear stretches 26 interconnected at the top and bottom by tangential arcs 27; the groups of slots might be distributed over the topmost surface of such a diffuser or over the uppermost part of the lateral surface. Fig 12 shows a similar profile 28 which comprises convex curvilinear stretches 29 i terconnected in like manner. Fig 13 shows the cross sectional profile 30 of a diffuser that comprises curvilinear lateral stretches 31 converging downward and interconnected by a bottom arc 32, and with the top ends united by a substantially straight central stretch 33 and two respective circumferential arcs 34; fig 14 shows a profile 35 identical to that of fig 13 but with the vertical axis rotated through 180.°.. In like manner, any one of the profiles about to be described could be upturned. Fig 15 shows a profile 36 similar to that of fig 13 but with sides exhibiting a shorter radius of curvature; fig 16 shows the circular cross sectional profile 37 of a tubular diffuser; fig 17 shows an asymmetrically elliptical cross sectional profile 38 with a top curve of shorter radius than the corresponding bottom curve; fig 18 shows the profile 39 of a diffuser that appears triangular in section with curvilinear sides and rounded angles, and the vertex downwardly directed; fig 19 shows a further triangular profile 40 with straight sides, rounded angles and the vertex upwardly directed; fig 20 shows the profile 41 of a diffuser that appears in section as a square with rounded corners; fig 21 shows a profile 42 similar to that of the preceding figure, in this instance rectangular; fig 22 shows the profile of a diffuser appearing in section as a pentagon with rounded angles; figs 23 and 24 are cross sections 44 and 45 of hexagonal and octagonal profile, respec ively. 46 denotes a group of fourteen εlotε 46a (fig 25), each slot appearing as an elongated rectangle with rounded ends, disposed with axes parallel and lying transverεe or parallel to the axis of the diffuεer, or even angled in relation to the diffuεer axis, advantageously at approximately 45°; the slotε are arranged in nine rows, all encompassed within an octagonal profile, of which the five innermost comprise two εlotε aligned on either εide of and tangentially to an unpierced rhomboidal central zone Ac meaεuring 5...40 mm} in εurface area and with one diagonal diεpoεed parallel to the axes of the εlotε; Ap denotes the area of the εurface lying between the octagonal and rhomboidal profiles, in practice between 3 and 10 times the value of the central area Ac; P is the pitch or diεtance between centres of the adjacent slots of one group, which may be constant or variable and might be equal to or greater than 1.25 mm, for example, the length of each slot being, to advantage, between 2 and 15 mm, and the width between 0.4 and 0.7 mm approx, when fashioned in sheet metals of 0.4 to 0.65 mm gauge. 47 denotes a group of εlotε 46a identical to those of fig 25, in combination with additional central holes of diameter D between 0.6 mm and 1 mm approx, of which the purpose is to stabilize the flame; the central holes are disposed, advantageously, along one of the diagonals of the rhomboidal central zone and might be three in number, preferably, or indeed any number from 1 to 5, with a preferred distance H between centres of 1.4 mm approx. 48 denotes a group of slotε (fig 27) εimilar to that of fig 25, but in combination with a central hole 48a for εtabilization of the flame and without the middle pair of slots; 49 denotes a group of slotε (fig 28) identical to that of -Tig 27, but without the central hole for εtabiliza ion of the flame. 50 denotes a group of fourteen εlots 46a (fig 29) diεposed with axes parallel and lying transverse or parallel to the axis of the diffuεer or even angled in relation to the diffuser axis, advantageously, at 45° , each single slot appearing as an elongated rectangle with rounded ends; the slots are disposed tangential to one or both concentric circumferences of an annular peripheral zone; R1 is the radius of the inner circle of the annulus, measuring less than or equal to 3.5 mm approx., R2 is the radius of the outer circle, equal to or greater than 8 mm, whilst the width and the distance between centres of the slots are as described in respect of fig 25; 51 denotes the central stabilizing hole, which is of diameter D1 between 0.6 mm and 1 mm approx. 5 denotes a group of slots (fig 30) identical to that of fig 29, though without the central hole for stabilization of the flame. 53 denotes a group of twelve slotε (fig 31) either transversely or longitudinally disposed in relation to the axis of the diffuser, or angled in relation thereto advantageously at 45° or thereabouts, and lying externally tangential to an oval F of which the greater axis iε diεposed normal to the axes of the εlotε; G and G1 denote centres symmetrically located on either side of the greater axis of the oval F, from which radii R3 and R4 of identical length describe two relative arcs, two further arcε being described from respective centres N and N1 located symmetrically on either side of the lesser axis of the oval, with equal radii r and r1 : the radii R3 and R4 are equal to or greater than 5 mm, and the radii r and π equal to half the radii R3 and R4 or thereabouts. F1 denotes an internal oval tangential to the inner ends of the slots of the group, and substan ially homothetiσ in relation to the outer oval F; the dimensions and the distance between centres of the slots could be the same, for example, as those of the group of εlotε 46 shown in fig 25 and described above; 54 denotes a central hole for stabilization of the flame, of diameter between 0.6 mm and 1 mm or thereabouts. 55 denotes a group of εlotε (fig 32) εimilar to that εhown in fig 31, but in conjunction with two holes 54 for εtabi 1 ization of the flame; 56 denotes one of a group of skew elongated rectangular slots (fig 33), 57 one of a group of triangular slots, 58 one of a group of elongated arcuate slots (fig 34), and 59 one of a group of slots coinciding with the sides of a pentagon (fig 35); 60 and 61 denote dissimilar groups of radial slots (fig 36) ordered in two sets, 62 and 63 groups of slots (fig 37) ordered in radiating tiers, and 64 denotes a group of slots (fig 38) coinciding with concentric circles. In fig 43, P1 denotes the longitudinal pitch or distance between centres of groups of slots, which might be constant or variable from group to group, whilst P2 in fig 44 is the transverse pitch between groups of slots, which likewise might be variable from group to group; moreover, the groups of slots shown in figs 43 to 50 might be replaced with any of the types of group illustrated in figs 25 to 42. 65 denotes a formation of groups of slots (fig 50) of which the centres coincide with the corners and intermediately with each side of a square measuring length M per side, the groups at the corners being disposed with the longitudinal axes of the slots angled, advant geously, at 45° to the axis of tnθ diffuser; P3 denotes the pitch at the which the formations of the groups of slots are distributed. 66 denotes a square (fig 51) constituting the lesser base of a frustopyramidal diffuser, and 67 the relative trapezoidal faces; 68 denotes the top isosceles triangular face (fig 52) exhibited by a diffuser of three-sided prismatic embodiment, of which the squarer face of the form is denoted 69 and the two rectangular faces are denoted 70. 71 denotes a circle (fig 53) constituting the lesser base of a frustoσonical diffuser, and 72 the developed conical surface. Fig 54 illustrates a nozzle assembly comprising a cam 73 impinging on the end plate 74 of the stem 75 of a proportioning valve element 76 exhibiting a conical profile; 77 denotes a cylindrical coil spring encircling a sleeve 78 slidably βnsheathing the stem 75, by which the plate 74 is biased into engagement with the cam 73, and 79 the head of the sleeve which is breasted frontally with the end surface 80 of a coaxial chamber 81 formed in the rear part of a relative valve housing 82 of which the frustoσonical orifice 83 is disposed coaxial with the stem. U denotes the angle between the generators of the frustoconical orifice 83, which may be as much as 10° or more, and V denotes the angle between the generators of the conical end of the stem 75, which will approximate to the angle U. 84 denotes a plurality of radial slots set in the forward end of the sleeve 78, and 85 a plurality of notches in the body of the plate 74, both of which serve to allow the passage of fluid to the orfice. 86 denotes a compressor (fig 55) of which the outlet is branched into a recirculation duct 88 controlled by a valve element 89 biased toward the closed position by a spring 90, and into which air is directed from a pipeline 91 controlled by a first on-off valve 92 and connected with the inlet, denoted 93, into which gas is also directed by way of a relative valve 94 from a further pipeline 95; 96 denotes the body of the relative burner. 97 denotes the diffuser (fig 56) of a burner of which the cross section exhibits a pair of lateral lobes 98 (fig 57) flanking the inlet ports 99 to the burner longitudinally, and 100 a longitudinal baffle that exhibits an upturned minuscule omega profile when viewed in section and serves to create mixing ducts with sinuouε symmetrical axes. The diffuser 97 iε enclosed by covers 101 at each end. As regards the method disclosed, which can be implemented adopting two levels of premixture, with a rate of aeration equal to or less than 1.1 or continuously greater than 1-1, respectively, it will be obεerved that to obtain the one condition rather than the other depends not least on the manner in which the burner is installed in the relative appliance, and especially on temperature, and on the height of the column of gas and the aerodynamic reεiεtanceε offered by the circuit carrying post-co buεtion air and gaεeε; the two levels therefore are not dependent εolely upon the combuεtion type and construction specifications of the burner and the system. The following examples illustrate methods of planning the computa ion of specifications for burners in implementation of the method, designed for operation at the two levels in question- Example 1 Tubular burner for an appliance operating with natural circulation of combusted air and gas, and with any given rate of aeration: a1 ) Section of burner body with aspect ratio (height to width) advantageously greater than 1.5, to give mean velocity of the mixture no greater than 2 m/ε through the annular εection between Venturi tube and diffuser. b1 ) Venturi tube allowing mean velocity of mixture through the throat equal to or less than 4 m/ε; length of Venturi tube exceeding the pierced εurface of the diffuser at least by a quantity equal to 50...150$ of outlet εection; distance between outlet section of Venturi and end wall of diffuser such that velocity of the mixture at inverεion iε on average greater than 2 m/ε. o1 ) Groups of slots distributed at least over the topmost surface of a diffuser with horizontal axis, and occupying a total area εuch aε to determine a εpecific 2 loading on the diffuser of less than 0-7 kW/σm ; the single slots arranged around and extending transversely or tangential to a central zone, intercalated with smaller complementary holes or otherwise, and circular, rectangular, triangular, trapezoidal in shape or of other non geometrical shape; the central zone pierced with holes or otherwise, all according to the invention. d1 ) Distribution of the groups of slots in ranks (transverse to the diffuser axis) set apart one from the next by a diεtance at least equal to 65 _• of the maximum transverse dimension of the group, with an axial distance between the groups of two successive files equal at least to nd/2, where d is the axial dimension of one group and n iε the number of groups in one rank, or in two successive ranks in a chequered pat tern; e1 ) Fuel feed nozzles of variable outlet section, according to the invention. Example 2 Tubular burner for an appliance operating with forced circulation of combusted air and gas, and with a rate of aeration greater than 1.1: a2) Section of burner body with diffuser of tubular, circular, polygonal or any other profile. b2) Nixer device of embodiment alternative to Venturi tube. c2) Groups of slots distributed over the entire εurface of the diffuεer. d2) Arrangement of the groupε of εlotε in ranks with groups separated one from the next by a distance at least equal to 65SS of the maximum dimension of the group as measured along the direction of separation. e2) Nozzle outlet pressures between 100 and 450 bar at maximum output, according to the preεεure riεe overcome in effecting the circulation of poεt-combuεtion gaεeε (given, surpriεingly, that the value of the aeration rate remains constant with the diminishing pressure value), maintained advantageously through the use of a variable speed centrifugal compressor of which the outlet is branched to recirculate part of the delivery flow and the inlet iε connected to on-off valveε by which the gaε and air εupplieε are controlled and alternated to ensure a smooth transition from ignition to steady burn by flooding the combustion chamber initially with air. Example 3 Burner embodied in matching halves for installation preferably in banked elements, in appliances with natural or forced circulation of post-combustion gases and with any given rate of aeration. a3) Essentially tall mixing and distribution element of elongated rectangular cross εection, inεerted between the outlet section of a curvilinear axis Venturi tube and the diffuser. b3) Groups of slots according to the invention, aligned longitudinally along the topmost surface of the diffuser, and set apart one from the next at a distance calculable simply as less than half the longitudinal dimension of the group. Example 4 Burner with horizontal axis tubular diffuser, and coaxially disposed internal Venturi tube. - length of diffuεer 394.6 mm - length of Venturi tube 359 mm - diameter of Venturi throat εeσtion 26 mm - diameter of Venturi outlet εec ion 35 mm - diεtance between diffuser inlet and farthest group of slots 324 mm GEOMETRY OF DIFFUSER Cross section of profile appearing as a pair of opposed and upwardly convergent curvilinear lines interconnected uppermost by an arc and connected at bottom through further arcs to a curvilinear base (see fig 14): " height of diffuser 61.3 mm - width of diffuser 51.5 mm - radius of curvature of each of the two opposite sides 76 mm - radius of curvature of base 45.5 mm - radius of top interconnecting arc 23 mm - radius of arcs connecting sides and base 13 mm - centres to the base and top arc coinciding with the vertical axis of symmetry of the diffuser; - centres to the opposite sides coinciding with the horizontal axis on either side of the vertical axis of sym etry. TOPOGRAPHY OF SLOTS IN EACH GROUP - width of εingle slot 0.5 mm - diεtance between centres of slotε 1.25 mm - number of εlotε 14 - slots diεposed with axes mutually parallel and within a peripheral zone bordering internally on a rhombus wi h greater and lesser diagonals 6.1 mm and 5.5 mm respectively and encompassed by a regular octagon with apothem 5.75 mm"approx. DISTRIBUTION OF GROUPS OF SLOTS The groups are distributed along the top surface of the diffuser in four longitudinal files staggered one from the next by a distance of 13 mm, or a distance discernibly half the distance separating groups of the same file, and set apart transversely by a distance (pitch P2 in fig 46) of 13 mm, the distance separating groups of the same file (P1 ) being 26 mm. Example 5 Burner with horizontal axis tubular diffuser and coaxially diεpoεed internal Venturi tube. - length of diffuser 325.6 mm - length of Venturi tube 290 mm - diameter of Venturi throat εection 26 mm - diameter of Venturi outlet εection 35 mm - distance between diffuεer inlet and fartheεt group of slotε 290.6 mm GEOMETRY OF DIFFUSER Croεε εection of profile appearing aε a pair of opposed and downwardly convergent curvilinear lines interconnected at bottom by an arc and connected through further arcε to a curvilinear top εtretch (fig 13), of dimensions σorreεponding to those of Example 4 and obtained by rotation of the relative axis of εymmetry through 180°. TOPOGRAPHY OF SLOTS IN EACH GROUP aε in Example 4. DISTRIBUTION OF 6R0UPS OF SLOTS The groups are distributed along the top εurface of the diffuser in four longitudinal files staggered one from the next by a distance of 14.8 mm, or a diεtance discernibly half the distance separating groups of the same file, set apart at transverse pitch (P2) of 13 mm, and longitudinal pitch (P1 ) of 29.5 mm. Example 6 Burner with horizontal axis tubular diffuεer and coaxially disposed internal Venturi tube. - length of diffuser 336.5 mm - length of Venturi tube 302 mm - diameter of Venturi throat section 30 mm - diameter of Venturi outlet section 42 mm - distance between diffuser inlet and farthest group of slots 294.5 mm GEOMETRY OF DIFFUSER Cross εection of profile appearing as a pair of oppoεed and downwardly convergent curvilinear lines interconnected at bottom by an arc and connected through further arcs to a curvilinear top stretch (fig 13): - height of diffuser 82.9 mm - width of diffuser 54.5 mm - radius of curvature of each of the two opposite εideε 156 mm - radius of bottom interconnecting arc 23.7 mm - radius of curvature of top stretch 44.2 mm -radius of arcs connecting εideε and top 13 mm ~ centres to the top stretch and interconnecting bottom arc coinciding with the vertical axis of symmetry of the diffuser; - centres to the opposite sides situated at 13.5 mm from the horizontal axis on either side of the vertical axis of εymmetry. TOPOGRAPHY OF SLOTS IN EACH GROUP as in Example 4. DISTRIBUTION OF GROUPS OF SLOTS The groups are distributed along the top surface of the diffuser in four longitudinal files staggered one from the next by a distance of 13 mm, or by a distance discernibly half of that separating groups of the same file, set apart at a transverse pitch (P2) of 14 mm between the first and the second file and between the third and the fourth, and of 13 mm between the second and third, and at a longitudinal pitch (P1) of 26 mm. Example 7 Burner consisting in a bank of discrete slimline diffuser elements exhibiting elongated rectangular section, each liberating 2 kW approx, installed in an appliance with natural circulation of combusted air and gas: - length of slot approx 2 mm to approx 3 mm; - width of slot approx 0.5 mm to approx 0.7 mm; - pitch of slots equal to or greater than 1.3 mm; - diameter of central flame stabilizing holes approx 0.6 mm to approx 1 mm; - diεtance between centres of stabilizing holes approx 1.3 mm to approx 1.7 mm; - transverse pitch of slimline elements approx 18 mm to approx 25 mm; - pitch of groups of slotε approx 12 mm to approx 17 mm; - greater radiuε of outer oval profile approx 5 mm to approx 15 mm; - leεεer radiuε of outer oval profile approx 2.5 mm to approx 7.5 mm; - diεtance between the top εurface of the diffuser and the bottom surface of the heat exchanger approx 80 mm to approx 160 mm; - height of distribution chamber between a few mm and 50 mm. Example 8 Burner consisting in a bank of discrete slimline diffuεer elements exhibiting elongated rectangular section, for installation in an appliance with natural circulation of combusted air and gas: - type of diffuser: sheet metal, marginally convex; - width of diffuser - height of distribution chamber - number of εlotε per group on each of two sides - number of endmoεt εlotε per group - length of εingle slot - width of εingle slot - width of each group - length of each group (between axes of end ost slotε) - pitch of εlotε - pitch of groups 12.25 mm Example 9 Burner consisting in a bank of discrete slimline diffuser elements exhibiting elongated rectangular section, for installation in an appliance with natural circulation of combusted air and gas: - type of diffuser: sheet metal, marginally convex; - width of diffuser - height of distribution chamber ~ number of εlotε per group on each of two εideε - number of endmost slotε per group - length of εingle εlot - width of εingle slot - width of each group - length of each group (between axes of endmost slotε) - pitch of slotε - pitch of groups " diameter of central hole Example 10 Burner consisting in a bank of discrete slimline diffuser elements exhibiting elongated rectangular εection, for installation in an appliance with natural circulation of combusted air and gas: - type of diffuser: sheet metal, marginally convex; - width of diffuser - height of distribution chamber - number of slots per group on each of two sides - number of endmost slots per group - length of εingle εlot - width of εingle εlot - width of each group - length of each group (between axeε of end oεt εlotε) - pitch of slots - pitch of groups - diameter of 2 x central hole 0.8 mm -distance between centres of central holes 1.4 mm When carried into effect, the materials utilized, the dimensions and the constructional details of the invention might be other than disclosed whilst remaining equivalent in terms of the art and by no means straying from within the bounds of protection afforded by the appended claims. For example, the topographies of the holes and εlotε described and illustrated are applicable not only to conventional tubular and/or slimline diffusers and their derivatives, but also to diffusers of newly conceived geometry.

Claims: CLAIMS 1. A method of bringing about the combustion of gases while controlling the resultant harmful emissions, wherein combustion is brought to completion within a slender lamellar flame , characterized in that, assuming operation with an aeration rate of 1.1 and lower, natural or forced circulation of post-combustion gases and specific loading on the burner diffuser between 0.3 and 0-8 kW/σm 2, it comprises the following combination of steps: A) feeding the slots of the diffuser uniformly with a homogeneous mixture of gas fuel and air; B) efflux of the mixture from slots each exhibiting a width dimension that may be as much as equal to the depth, as considered in the direction of the efflux, or marginally greater, according to the type of gas, arranged in groups around relative central zones that are either unpierσed or may be pierced over an area measuring no more than 20fc of the overall area of the central zone itself; to advantage, the ratio between the area of the peripheral zone occupied by the slots and the area of the central zone being between 3 and 10, and the ratio between the area of the slots and the area of the peripheral zone between 1/2 and 1/3.5, the central zone being of width up to 3 mm maximum and of any given length, and the groups of slots distributed in repeated rows orientated in any given direction, aligned or staggered; C) commencement and completion of combustion, brought about instantaneously and in a εingle stage at each group of εlotε in εlender lamellar flameε with a hyperstoichiometric mixture of fuel and air; the flames of each group combining to create the impression of butterfly wings, tulip corolla, trumpet, campanula or similar shape, regularly formed or otherwise, springing divergently from a level immediately above and at a distance less than 2 mm from the surface of the diffuser, of which the axis or plane of symmetry lies perpendicular to a tangential plane passing through the - 27 - centre of each group, thereby obtaining a saturated volume of fully combusted gases, encompassed externally by the flames of each group and spreading with the increase in distance from the diffuser, in which the partial pressure of the oxygen is further reduced, and a slow recirculation of combusted gases occurring at the base of the volume such as will maintain temperatures sufficient to allow ignition; D) regulation of the aeration rate to within values of 0.9, related to operation at maximum output, and 1.4, related to operation at minimum output and starting; and with an aeration rate less than or equal to 1-1, induction of the quantity of air required to effect full combustion in a par ial vacuum created by the jet of fuel-air mixture issuing from the slots to invest the external face of the lamellar flames. 2- A method of bringing about the combustion of gases while controlling the resultant harmful emissions, wherein combus ion is brought to completion within a thin lamellar flame characterized in that, assuming operation with an aeration rate permanently greater than 1.1, with natural or forced circulation of combusted air and gases, it comprises the following combination of steps: A) feeding the slots of the diffuser uniformly with a homogeneous mixture of gas fuel and air; B) efflux of the mixture from slots each exhibiting a width dimension that may be as much as equal to the depth, as considered in the direction of the efflux, or marginally greater, according to the type of gas, arranged in groups around relative central zones that are either unpierσed or may be pierced over an area measuring no more than 20S5 of the overall area of the central zone itself; to advantage, the ra io between the area of the peripheral zone occupied by the slots and the area of the central zone being between 3 and 10, and the ra io between the area of the slots and the area of the peripheral zone between 1/2 and 1/3.5, the central zone being of width up to 3 mm maximum and of any given . - 30 length, and the groups of εlotε distributed in repeated rows orientated in any given direction, aligned or staggered; C) commencement and completion of combustion, brought about instantaneously and in a εingle stage at each group of slots in εlender lamellar flames with a hyperstoichiometric mixture of fuel and air " ; the flames of each group combining to create the impreεεiσn of butterfly wings, tulip corolla, trumpet, campanula or 10 similar shape, regularly formed or otherwiεe, εpringing divergently from a level immediately above and at a distance leεε than 2 mm from the surface of the diffuser, of which the axiε or plane of εymmetry lies perpendicular to a tangential plane passing through the 15 centre of each group, thereby obtaining a saturated volume of fully combusted gases, encompaεsed externally by the flames of each group and spreading with the increase in diεtance from the diffuser, in which the partial pressure of the oxygen is further reduced, and a 20 slow recirculation of combusted gases occurring at the base of the volume such as will maintain temperatures sufficient to allow ignition; E) regulation of the rate of aeration to values no higher than 1.6 and advantageously between 1.1 and 1.3, whether 25 at maximum output or in the starting or modulating modes, with specific loading on the diffuser of between 0.3 and 0-8 kW/σm * "; supply pressure of the gas fuel being advantageously between 100 and 450 bar. 30 3. A method a-s in claim 1 , comprising the further step of: G) diversion of the combusted gases by induction into a partial vacuum created with the jet of fuel-air mixture issuing from the slots to invest the external face of the lamellar flames, having been cooled and mixed with 35 air at a rate of between 10 and 1008s. 4. A method as in claim 2, comprising the further step of: F) diversion of the combusted gases by induction into a partial vacuum created with the jet of fuel-air mixture issuing from the slots to invest the external face Of the lamellar flames, having been cooled and mixed with air at a rate of between 0 and 1005,. 5. A burner suitable for implementation of the method of claim 1 or claim 2, comprising a diffuser with slots distributed in groups, characterized in that each group of slots occupies a peripheral zone encompassing a central zone either devoid of slots or pierced over an area limited to no more than 20% of the area of the central zone itself, preferably occupying a surface of between 5 and 40 m such that the ratio between the area of the peripheral zone and the area of the central zone iε between 3 and 10, advantageously, and the ratio between the area of the slσtε and the area of the peripheral zone iε between 1/2 and 1/3.5; in that the groupε of εlσtε can be diεtributed in longitudinally repeated tranεverεe rows or other εuitable formation, and the width of a εingle εlot iε equal to the thickneεε of the diffuεer wall, or marginally greater, according to the type of gas fuel; in that the burner may be provided with a Venturi tube, disposed internally or externally of the diffuεer about a rectilinear or non-rectilinear axis, vertical or horizontal, angled or εkew, whilεt the body of the diffuser may be of tubular εection, cylindrical or priεmatic and tapered, pyramidal, or rectangular and elongated, and the diffuεer itεelf embodied with groupε of εlotε preferably of rectangular geometry, or of openingε in general, occupying all or part of the relative surface. 6. A burner aε in claim 5, wherein a central zone of approximately 3 mm in width can be of any given length and extends along an axiε of rectilinear or curvilinear or zigzag or mixed geometry. 7. A burner aε in claim 5 or 6 affording the advantage of a maximum reduction in height while enεuring an optimum mixture of air and gas, particularly in forced circulation circuits, of which the body exhibits a croεε εection of bilobed profile with the two lobes (98) downwardly directed and creating two lateral channels at bottom, in combination with a substantially flat and slightly convex diffuser profile uppermost, wherein the fuel and air mixture enters by way of inlet ports (99) distributed longitudinally between the lobes and is directed along two diverging ducts of sinuous curvilinear axis and progressively increasing cross section, defined by a longitudinal baffle (100) of upturned minuscule omega profile extending the entire length °f the burner. 8. A burner as in claim 5, wherein the peripheral zone of the group of slots lies between concentric circles or ellipses and the radius of the inscribed central zone is equal to or less than 3.5 mm- 9. A burner as in claim 5, wherein the peripheral zone of the group of slotε iε annular, and the εlotε are elongated and rectangular, or triangular, and arranged in the annulus with axes mutually parallel or radially or transversely disposed, in one or more distinct rows. 10 - A burner aε in claim 5, wherein the peripheral zone of the group of slots is annular, and the elongated rectangular or triangular slotε are arranged in one or more tierε to coincide with the εides of regular polygonε such as pentagons, concentrically diεpoεed and either aligned or εtaggered mutually in the angular direction. 11. A burner as in claim 5, wherein the peripheral zone of the group of εlots iε annular, and occupied by elongated rectangular, triangular or arcuate εlots arranged in one or more tiers, identical or mixed, to coincide with concentric oblongated circles. 12. A system suitable for implementation of the method of claim 1 or 2, characterized in that, where a natural circulation through the combusted air and gas circuit is sufficient to sustain full combustion, or ■ 'where such circulation is fan-assisted, the rate of aeration is maintained within the limits envisaged according to the method by means of a gas nozzle affording an outlet of variable section. 13. A system as in claim 12, wherein the variable outlet gas nozzle (82) comprises a valve stem (75) exhibiting a conical proportioning element (76) with a taper angle of between 0° and 1C° capable of guided axial movement internally of an orifice (83) in the housing of the valve, of which the taper angle iε identical or approximate to that of the proportioning element, in such a way as to obtain a gradual reduction in gas pressure at the outlet commensurate with the reduction in section, in respect of the reduced variation in aeration rate occurring with variation in flow, hence in output, the rear end of the proportioning element being embodied as a plate (74) biased by a spring against the lateral surface of a manually or automatically operated cam (73) . 14. A εyεtem aε in claim 13, wherein the plate (74) is urged against the cam (73) by a spring wound around a sleeve (78), slidably and axially accommodating the proportioning element (75), of which the flat head (79) iε breasted with the end face of an axial chamber (81 ) formed in the rear part of the housing (82), the head (79) of the sleeve and the body of the plate (74) affording radial εlotε or notches to allow passage of the gas. 15. A system suitable for i plementation of the method of claim 1 or 2, characterized in that the circulation of combusted air and gas iε forced by meanε of a variable speed centrifugal compressor (86) operating at delivery presεures between 100 and 450 mbar, of which the outlet iε branched to effect a partial recirculation (88) of the delivery flow, and the inlet (93) iε connected to alternating on-off valves (92, 94) controlling the air and gaε supply lines. 16. A tubular burner suitable for implementation of the method of claim 1 or 2, characterized in that, being inserted in an appliance operating with natural circulation of combusted air and gas, and with any given rate of aeration, it is constituted by a1 ) a section of the burner body exhibiting a ratio between its height and width advantageously greater than 1.5 to give mean velocity of the mixture no greater than 2 m/s through the annular section between the Venturi tube and diffuser; b1 ) a Venturi tube allowing a mean velocity of mixture through the throat equal to or less than 4 m/s, the length of Venturi tube exceeding the pierced surface of the diffuεer at leaεt by a quantity equal to 50...150% of the outlet εection, and the diεtance between the outlet εection of the Venturi and the end wall of the diffuεer being such that velocity of the mixture at inverεion iε on average greater than 2 m/ε. d ) groupε of εlotε diεtributed at leaεt over the topmost surface of a diffuser with a horizontal axis, occupying a total area such aε to determine a specific loading on the diffuser of less than 0.7 kW/σm ; said slots being arranged around and extending transversely or tangential to a central zone, and intercalated with smaller complementary holes; said slots being circular, rectangular, triangular, trapezoidal in shape or of other even non geometrical shape, the central zone being pierced with holes or otherwise; d1 ) groups of slots distributed in ranks, transverse to the diffuser axis, set apart one from the next by a distance at least equal to 65*; of the maximum transverse dimension of the group, with an axial distance between the groups of two successive files equal at least to nd/2, where d is the axial dimension of the single group and n is the number of groups in one rank, or in two successive ranks of groups forming a chequered pattern. 17. A system as in claims 12, 13 and 14, incorporating a burner as in claim 16. 18. A tubular burner suitable for impl mentation of the method of claim 1 or 2, characterized in that, being the burner inserted in an appliance operating with forced circulation of combusted air and gas, and with a rate of aeration greater than 1.1, it is constituted by a2) a section of the burner body with a diffuser exhibiting a tubular, circular or polygonal or any other profile; b2) a mixer device instead of a Venturi tube; c2) groups of slots distributed over the entire surface of the diffuser; d2) groups of εlotε ordered in rankε with groups separated one from the next by a distance at least equal to 65% of the maximum dimension of the group as measured along the direction of separation; being provided that nozzle outlet pressures measure between 100 and 450 mbar at maximum output, according to the pressure rise accomplished in effecting the circulation of post-combuεtion gaεeε, the value of the aeration rate remaining conεtant with the diminiεhing pressure value, advantageously through the use of a variable speed centrifugal compressor of which the outlet is branched to recirculate part of the delivery and the inlet connected to on-off valves controlling the gas and air supply lines and operated in alternation in such a way aε to ensure a smooth transition from ignition to steady burn by flooding the combustion chamber initially with air. 19. A burner aε in claimε 8 to 11, embodied in matching halves, characterized in that, being installed in appliances operated with natural or forced circulation of post-combustion gaseε and with any given rate of aeration, comprises: a3) an essentially tall mixing and diεtribution chamber of elongated rectangular croεε section, inserted between the outlet εection of a Venturi tube of curvilinear axis, and the diffuser; b3) groups of slots aligned longitudinally along the topmost surface of the diffuser, set apart one from the next at a distance calculable simply as lesε than half the longitudinal di enεion of the group. 20. A tubular burner εuitable for i plementation of the method as in claim 1 or 2, characterized in that it comprises a coaxially disposed internal Venturi tube exhibiting the following eεεential dimensionε: - length of diffuser 394.6 mm - length of Venturi tube 359 mm - diameter of Venturi throat εection 26 mm - diameter of Venturi outlet section 35 mm - distance between diffuser inlet and farthest group of slots 324 mm in that the cross sectional profile of the diffuser consists in a pair of opposed and upwardly convergent curvilinear lines interconnected uppermost by an arc and connected at bottom through further arcs to a curvilinear base, with the following essential dimensions: - height of -diffuser 61.3 mm ~ width of diffuser 51.5 mm - radius of curvature of each of the two opposite sides 76 mm - radius of curvature of base 45.5 mm - radius of top interconnecting arc 23 mm - radius of arcs connecting sides and base 13 mm - centres to the base and top arc coinciding with the vertical axis of symmetry of the diffuser; - centres to the opposite sides coinciding with the horizontal axis on either side of the vertical axis of symmetry; in that the slotε of each group exhibit the following topography: - width of εingle εlot 0.5 mm - distance between centres of slotε 1.25 mm - number of εlotε 14 - slots disposed with axes mutually parallel and within a peripheral zone bordering internally on a rhombus with greater and lesser diagonals 6.1 mm and 5.5 respectively and encompassed by a regular octagon with apothem 5-75 mm approx. ; and in that the groups of slots are distributed along the top εurface of the diffuser in four longitudinal files staggered one from the next by a distance of 13 mm, or a distance discernibly half the distance separating groups of the same file, with transverse pitch (P2) and longitudinal pitch (P1 ) of 13 mm and 26 mm respectively. 21 - A tubular burner suitable for i plementa ion of the method of claim 1 or 2.characterized in that It comprises a σoaxial ' ly disposed internal Venturi tube exhibiting the following essential dimensions: - length of diffuser 325.6 mm - length of Venturi tube 290 mm - diameter of Venturi throat section 26 mm - diameter of Venturi outlet section 35 mm - distance between diffuser inlet and farthest group of slots 290.6 mm in that the cross sectional profile of the diffuser comprises a pair of opposed and downwardly convergent curvilinear lines interconnected at bottom by an arc and connected through further arcs to a curvilinear top stretch, with the following essential dimensions: - height of diffuser 61.3 mm - width of diffuser 51.5 mm - radius of curvature of each of the two opposite sides 76 mm - radius of curvature of top stretch 45.5 mm - radius of bottom interconnecting arc 23 mm ~ radius of arcs connecting sides and base 13 mm - centres to the base and top arc coinciding with the vertical axis of symmetry of the diffuser; - centres to the opposite sides coinciding with the horizontal axis on either side of the ver ical axis of symmetry; in that the εlots of each group exhibit the following topography: - width of εingle εlot 0-5 mm - diεtanσe between centres of slots 1.25 mm - number of εlots 14 - εlots diεpoεed with axes mutually parallel and within a peripheral zone bordering internally on a rhombus with greater and lesser diagonals 6.1 mm and 5.5 respectively and encompassed by a regular octagon with apothem 5.75 mm appro . ; and in that the groups of εlots are distributed along the top surface of the diffuser in four longitudinal files staggered one from the next by a diεtance of 14.8 mm, or a distance discernibly half the distance separating groups of the same file, set apart at transverse pitch (P2) and longitudinal pitch (P1 ) of 13 mm and 29.5 mm respectively. 22- A tubular burner suitable for implementation of the method of claim 1 or 2, characterized in that it comprises a coaxially disposed internal Venturi tube exhibiting the following essential dimensions: - length of diffuser 336.5 mm - length of Venturi tube 302 mm ~ diameter of Venturi throat section 30 mm - diameter of Venturi outlet section 42 mm - distance between diffuser inlet and farthest group of slots 294.5 mm in that the cross sectional profile of the diffuser comprises a pair of opposed and downwardly convergent curvilinear lines interconnected at bottom by an arc and connected through further arcs to a curvilinear top stretch, with the following essential dimensions: - height of diffuser 82.9 mm - width of diffuser 54.5 mm - radius of curvature of each of the two opposite sides 156 mm - radius of bottom interconnecting arc 23.7 mm - radius of curvature of top stretch 44.2 mm - radius of arcs connecting sides and top 13 mm - centres to the top stretch and interconnecting bottom arc coinciding with the vertical axis of symmetry of the diffuser; - centres to the opposite sides situated at 13.5 mm from the horizontal axis on either side of the vertical axis of symmetry; in that the slots of each group exhibit the following topography: - width of single slot 0.5 mm - distance between centres of slots 1.25 mm - number of slots 14 - slots disposed with axes mutually parallel and within a peripheral zone bordering internally on a rhombus with greater and lesser diagonals 6.1 mm and 5.5 respectively and encompassed by a regular octagon with apothβm 5.75 mm approx. ; and in that the groupε are diεtributed along the top surface of the diffuεer in four longitudinal files staggered one from the next by a distance of 13 mm, or by a distance discernibly half of that separating groups of the same file, set apart at a transverse pitch (P2) of 14 mm between the first and the second file and between the third and the fourth, and of 13 mm between the second and third, and at longitudinal pitch (P1 ) of 26 mm. 23. A burner suitable for implementation of the method of claim 1 or 2, characterized in that it conεiεtε in a bank of diεcrete slimline diffuser elements of elongated rectangular section, installed in an appliance with natural circulation of combusted air and gas, each liberating 2 W approx and exhibiting the following essential dimensions: - length of εlot approx 2 mm to approx 3 mm; " width of slot approx 0.5 mm to approx 0.7 mm; - pitch of slots equal to or greater than 1.3 mm; - diameter of central flame stabilizing holes approx 0-6 mm to approx 1 mm; - distance between centres of stabilizing holes approx 1.3 mm to approx 1.7 mm; - transverse pitch of elements approx 18 mm to approx 25 mm; - pitch of groups of slotε approx 12 mm to approx 17 mm; - greater radius of outer oval profile approx 5 mm to approx 15 mm; * lesser radius of outer oval profile approx 2.5 mm to approx 7.5 m ; - distance between the top surface of the diffuser and the bottom εurface of the heat exchanger approx 80 mm to approx 160 mm; - height of diεtribution chamber between a few mm and 50 mm. 24. A burner as in claim 23, comprising a diffuser embodied in sheet metal and of marginally convex profile and responding to the following parameters: - width of diffuser - height of distribution chamber - number of slots per group on each of two sides - number of endmost slots per group - length of single slot - width of single slot - width of each group - length of each group (between axes of endmost slots) - pitch of slots - pitch of groups 25. A burner as in claim 23, comprising a diffuser embodied in sheet metal and of marginally convex profile and responding to the following parameters: - width of diffuser - height of distribution chamber - number of slots per group on each of two sides "• number of endmost slots per group - length of single slot - width of single slot - width of each group - length of each group (between axes of endmost slots) - pitch of slots - pitch of groups - diameter of central hole 26. A burner as in claim 23, comprising a diffuser embodied in sheet metal and of marginally convex profile and responding to the following parameters: - width of diffuser 8 mm - height of distribution chamber 50 mm - number of slots per group on each of two sides 5 - number of endmost slots per group 2 - length of single slot 2.5 mm - width of single slot 0.65 mm - width of each group 7.75 mm - length of each group (between axes of endmost εlotε) 7.8 mm - pitch of εlotε 1.3 mm - pitch of groupε 12.25 mm - diameter of each of two central holes 0.8 mm - distance between centres of central holes 1.4 mm

Inventors: FOGLIANI GIUSEPPE, SEBASTIANI ENRICO, FOGLIANI, GIUSEPPE, SEBASTIANI, ENRICO
Applicants: WORGAS BRUCIATORI SRL, WORGAS BRUCIATORI S.R.L.
Application year: 1991
Main classification: F23D14
IPC codes: F23D14