Abstract: A fuel lance for liquid and/or gaseous fuels for use in a combustion chamber includes a liquid fuel pipe extending along a lance center line and defining a liquid fuel passage, a gas pipe surrounding the liquid fuel pipe and forming therebetween a gas passage, and a lance outer shell surrounding the gas pipe and forming an air passage around the gas pipe for cooling air and atomizer air. At least one air/fuel nozzle is provided in a peripheral side of the lance outer shell at a downstream end of the fuel lance for air flow out of the air passage into the combustion chamber. At least one gas nozzle is provided in the gas pipe for gas flow out of the gas passage into the air passage, the gas nozzle is positioned relative to the air/fuel nozzle so that gas from the gas nozzle flows with air from the air passage through the at least one air/fuel nozzle into the combustion chamber.

Abstract: An apparatus for the automatic combustion of gas produced from oil and natural gas wells at remote locations is described as including an inner conduit having a first and second end that is disposed within a larger dimension outer conduit, each of which share a parallel longitudinal axis. The inner conduit first end is attached to a source of escaping gas and the second end is disposed within the outer conduit. At least one fin is included in the inner conduit for deflecting a portion of the escaping gas through at least one hole that is provided in the inner conduit. The gas thus deflected passes into the area disposed between the outside of the inner conduit and the inside of the outer conduit where it produces a partial vacuum as it continues to travel in the same general direction out of the outer conduit. The partial vacuum draws ambient air into the outer conduit where at least one slow roll fin is present to agitate the ambient air being drawn therein.

Abstract: A two stage rapid mix burner provides apparatus and method which significantly reduce the burner size of a rapid mix burner, and/or the burner pressure drop, while maintaining the rapid mix feature and stability of the basic rapid mix design. The burner can also be easily altered to fit in non-circular geometries, such as a corner or tangential fired boiler. The invention uses a circular basic rapid mix burner located internally of a larger burner which can be non-circular. The inner burner provides the flow of hot gases which stabilizes the outer burner. In effect, the combustion gases produced in the inner burner replace the strong internal recirculation flow generated by the basic RMB as an ignition source for the outer burner flow.

Abstract: Combustion air is supplied being divided into inner and outer cylinders of a main burner body, and liquid fuel is injected and burnt by a liquid fuel injection nozzle provided in the inner cylinder, wherein a tip end injection hole of the nozzle faces outside of the nozzle through a fore end opening of the inner cylinder. An annular flame piloting baffle plate for the inner cylinder is provided in front of the injection hole of the tip end opening of the inner cylinder, a swirler is provided inside of a tip end portion of the outer cylinder, and an annular flame piloting baffle plate is provided at a tip end opening portion of a cylindrical space formed between the outer and inner cylinders. Due to the foregoing construction, flames of the burner for burning liquid fuel are stabilized and an amount of generated NOx gas is reduced.

Abstract: A burner configuration includes approximately concentrically disposed annular conduits for delivering various operating media. A plurality of outlet nozzles admix a gaseous medium or a liquid medium in finely distributed form with an air flow flowing in an approximately conically tapering outer annular-conduit air delivery system. A further annular conduit on an inflow side discharges into the annular-conduit air delivery system above the outlet nozzles.

Abstract: A combustion method wherein high velocity fuel is injected into a cavity recessed from a furnace zone for flow into the furnace zone, low velocity oxidant fluid is injected into the cavity for coaxial flow with the fuel, and the resulting combusting fuel and oxygen has imparted to it an angular component by operation of swirling oxygen flow and/or outwardly angled fuel flow, enabling control of the high velocity flame length.

Abstract: A gas burner system in which a turbulator disk is arranged between a burner and an opening in a combustion chamber aligned with the burner. The turbulator disk defines a central port and a plurality of peripheral voids adjacent to the central port. A burner flame, produced by ignition of a gas-primary air mixture, together with a quantity of secondary air, may be directed through the central port of the turbulator disk into the combustion chamber. A additional quantity of secondary air may be directed through the voids into the combustion chamber for combustion of the uncombusted gas from the gas-primary air mixture.

Abstract: A burner having a primary flame zone and a secondary flame zone. The throat of the quarl in the center of the primary flame zone is provided with a gas nozzle supported by a swirl element. The orifices of the nozzle are radially and obliquely distributed so that the gas introduced via the frustoconical chamber mixed with the primary air to form a swirl current. The frustoconical chamber extends to the inner surface of the burner to form a circular extended section to restrain the width of the flame; the extended section is parallel to the secondary air inlets distributed on the burner body around the periphery of the frustoconical chamber to effectively control the formation of NOx during combustion.

Abstract: A burner unit has a fuel dispersion arrangement at a burner head leading to a flame region which distributed fuel from longitudinal slots extending along trailing edges of spinner vanes of a spinner vane assembly. The spinner vane assembly is disposed transversely across a flow channel of combustion air past the burner head and has a function of deflecting the axial flow of the combustion air radially outward into a conical flow. The deflective air flow pressure distribution over the spinner vanes contributes to induction and mixing of the fuel with the combustion air as the combustion air enters the flame region of the burner. Combustion gases resulting from a combustible mixture achieved in this manner have resulted in emission products with pollutant levels within currently specified limits.

Abstract: A forced draft burner apparatus and method providing extremely low NO.sub.x, CO and hydrocarbon emissions, while maintaining the desirable features of a nozzle mix burner. This is accomplished by injecting the fuel gas in a position that would be typical for a nozzle mix burner, while generating such rapid mixing that, effectively, premixed conditions are created upstream of the ignition point.

Abstract: A flame retaining nozzle tip for a burner for a pulverized fuel fired furnace receiving a primary stream of pulverized fuel and primary transport and combustion air for discharge into the combustion zone of the furnace comprises a hollow, open-ended, choke or body having an inlet end of generally polygonal flow cross-section for receiving the stream and an outlet end of generally rounded cross-section for accelerating and discharging the stream into the furnace. The outlet end of the choke has a flow cross-sectional area that is less than that of the inlet end to provide choking action. An elongated center element is mounted in coaxial alignment with a central axis of the choke body extending between the inlet and outlet ends.

Abstract: A low-nox burner for use in industrial furnaces and/or boilers which burn pulverized coal. The burner includes a burner tip which divides an annular pulverized coal stream into alternating fuel-rich and fuel-lean streams. The tip includes a plurality of alternating main and secondary blade members which are skewed to produce rotational movement in the streams. The main blade has a leading edge that is aligned with a radial vector extending through a center axis of the burner and a trailing edge that is tilted with respect to the radial vector in order to define a substantially planar surface between the leading and trailing edges. The secondary blade includes leading and trailing edges that are both aligned with radial vectors and defines a twisted surfaces between the edges. The secondary blade is skewed with respect to the longitudinal direction by an angle that is substantially greater than the angle at which the main blade is skewed.

Abstract: A heating devices for complete intermixing of gaseous fuel and air to allow complete combustion of the gas and air mixture in a mushroom shaped flame. The device includes an element for supplying an axial flow of air and a swirling device in fluid communication with the air supply to turbulently swirl and radially inward direct the air entering from the air supply. The heating device also includes an nozzle element located within a mixing chamber formed by the swirling device. The nozzle forms a plurality of bores to emit the fuel as generally radially outward directed streams into the swirling stream of air exiting from the swirling device to intermixes the fuel and air. A disk connected to the nozzle restrains the gas streams within the mixing chamber to facilitate the mixing of the fuel and air. The intermixed fuel and air is then ignited by an ignition device. A combustion chamber is disposed about an upper first end of the swirling device to contain the generated flame.

Abstract: A flame stabilizer for a burner of solid fuel, such as pulverized coal or sander wood dust, is described whereby the swirl number is varied radially to enhance swirl inducement towards the periphery of the flame stabilizer while more axial flow occurs near the central conduit through which fuel is supplied. The amount of swirl and the amount of combustion air being selected so as to provide an integrated swirl number for the flame stabilizer in the range from about 0.6 to about 2.0. A pressure control ring is described with which the static pressure in the windbox is increased to a level where flame pulsations attributable to low static pressure in the windbox are reduced while the vortex is maintained. An enhanced axial combustion air flow around the discharge end of the fuel supply conduit is described to modify the position of the adverse pressure gradient boundary in a downstream direction.

Abstract: Disclosed is a burner register assembly having an air register assembly for imparting a controlled vortex swirl to secondary combustion air of a furnace in order to entrain the fuel and primary air of the furnace and carry them into the furnace interior. The assembly may comprise a series of arcuate vanes circumferentially spaced about the fuel and primary air nozzle, the vanes being designed to induce both turbulence and a well defined vortex to the secondary air flow. A separate air valve, such as a butterfly valve, is provided upstream of the air register assembly to regulate the volume of secondary air flow. Shadow vanes may also be provided in the vicinity of the air register assembly outlet, and positioned adjacent the furnace walls in order to protect the air register assembly from furnace heat, particularly when the burner associated with the air register assembly is idle and the secondary air flow is lowered.

Abstract: A combustor includes inner and outer arrays of generally Vee-shaped, radially extending, circumferentially spaced gutters canted in a circumferential direction relative to one another to produce isolated concentric counter-rotating circumferentially directed flows downstream of the gutters. A lean premixed combustion mode is used at baseload operations. At non-baseload operations, particularly low-load operating conditions, a diffusion combustion mode is employed by direct fuel injection into air supplied to one of the isolated flow fields, preferably the radially inner flow field, to produce a stabilized, locally hotter flame, resulting in higher combustion efficiency and lower emissions than otherwise using a lean premixed combustion mode at the non-baseload operating conditions.

Abstract: A low-nox burner for use in industrial furnaces and/or boilers which burn pulverized coal. The burner includes a burner tip which divides an annular pulverized coal stream into alternating fuel-rich and fuel-lean streams. The tip includes a plurality of alternating main and secondary blade members which are skewed to produce rotational movement in the streams. The main blade has a leading edge that is aligned with a radial vector extending through a center axis of the burner and a trailing edge that is tilted with respect to the radial vector in order to define a substantially planar surface between the leading and trailing edges. The secondary blade includes leading and trailing edges that are both aligned with radial vectors and defines a twisted surfaces between the edges. The secondary blade is skewed with respect to the longitudinal direction by an angle that is substantially greater than the angle at which the main blade is skewed.

Abstract: Disclosed is a structure of a burner which can be fueled with gas fuel or oil fuel. The main features includes: a specially designed swirl generator; an annular hollow gas gun; an oil gun received in the gas gun where the gas jets of the gas gun and the oil jets of the oil gun have an predetermined angle with respect to the centerline. Under designed operating conditions, a swirling air flow can be generated with a low pressure drop and low turbulences, which is beneficial to flame stability, reducing flame temperature, and delaying the mixing of air and fuel, thus inhibiting the formation of NO.sub.x. Staging air and flue gas recirculation are available for further reduction of nitrogen oxides.

Abstract: In direct fired fluid burner heater of the type where fuel is continuously injected and burned at one end of a cylindrical combustion chamber and combustion gases discharged at an opposite open end pass through a heat exchanger for heating a circulating medium, and where high heat capacity is achieved for a given chamber size by swirling the flame in the combustion chamber, acoustical low frequency buzzing is controlled by restricting the discharge area through which exhaust gases flow downstream of the heat exchanger.

Abstract: A burner for the combustion of a fuel plus air mixture comprises a central nozzle pipe having an inner surface with a portion which diverges outwardly. An axially moveable plug is positioned within the nozzle pipe and includes an outer wall with a diverging section extending within the diverging section of the nozzle pipe. By axially moving the plug, the cross sectional area of the space between the diverging surfaces increases and decreases for respectively decreasing and increasing the velocity of the fuel plus air mixture passing through the nozzle space. This reduces the formation of NO.sub.x and the length of the flame produced by the burner.

Abstract: A turbo burner assembly provides for dispersion of liquid fuel into a flame region adjacent a burner head of the assembly by using compressed air to force a fine spray through apertures in an atomizing assembly. The dispersed fuel is supplied at a variable rate that corresponds to the combustion settings of the burner over the entire operating range of the burner. The dispersed fuel becomes entrained into a low quantity flow of high velocity turbo air. The quantity or rate of flow of the high velocity turbo air corresponds to the combustion air required for the correct air to fuel mixture at the lowest fuel flow rate. At increasing fuel flow rates for increased combustion settings a second low velocity stream of turbo air is introduced at a variable volume flow rate to provide together with the first stream of turbo air a correct combustion mixture with the introduced fuel over the entire range of combustion settings of the burner assembly. A gaseous fuel can be substituted for the liquid fuel.

Abstract: A parallel flow liquid fuel burner is disclosed which has a device for injecting fuel in a central flame stabilizer; the stabilizer comprises a blade-containing rose situated around a central hub itself situated around the injection device and the injection device comprises several fuel injection orifices adapted to provide separate elementary flames.

Abstract: A burner for a hearth including a gun for introducing a primary comburant and a gun for supplying a secondary comburant, with a device for supplying a gaseous fuel and a deflector stabilizer arranged substantially at an extremity of the gun introducing the primary comburant. The fuel supply device includes a first fuel injector arrangement adapted to produce a first jet of fuel substantially axially or slightly divergent with respect to a longitudinal center axis of the burner, and a second fuel injector arrangement adapted to produce a second jet of fuel divergent with respect to the longitudinal center axis of the burner.

Abstract: A flame stabilizer for a burner of solid fuel, such as pulverized coal or sander wood dust, is described whereby the swirl number is varied radially to enhance swirl inducement towards the periphery of the flame stabilizer while more axial flow occurs near the central conduit through which fuel is supplied. The amount of swirl and the amount of combustion air being selected so as to provide an integrated swirl number for the flame stabilizer in the range from about 0.6 to about 2.0. A pressure control ring is described with which the static pressure in the windbox is increased to a level where flame pulsations attributable to low static pressure in the windbox are reduced while the vortex is maintained. An enhanced axial combustion air flow around the discharge end of the fuel supply conduit is described to modify the position of the adverse pressure gradient boundary in a downstream direction.

Abstract: In a premixing burner, which consists of two hollow partial conical bodies (1, 2), which are positioned on one another and have a cone inclination increasing in the direction of flow, the fuel feed takes place via central fuel nozzle (3) and/or via a plurality of fuel nozzles (17), which are placed along the inflow of the combustion air (15) into the interior (14) of the burner. The combustion air (15) itself is a mixture of fresh air and exhaust gas. The fresh air is led up via a first flow funnel (23a, 23b ) and exhaust gas recirculation takes place via a second flow funnel (22a, 22b). These two gases mix with one another before flowing tangentially into the interior (14). An optimum, homogenous fuel concentration over the cross-section arises in the region of the return flow zone (6).

Abstract: This burner arrangement has a main feed channel (2) for a fuel-air mixture, which channel discharges into a combustion chamber (1). A swirler, which is provided with swirl vanes (5), is penetrated by a burner lance (3), and into which exit openings for the fuel feed discharge, is provided in this main feed channel (2). The aim is to create a burner arrangement in which it is impossible for undesired instances of ignition of the fuel-air mixture to occur outside the combustion chamber (1). This is achieved in that the exit openings are constructed as nozzles (9) which discharge into a region between the swirl vanes (5). In this regard, at least one nozzle is provided between two neighboring swirl vanes (5).

Abstract: A burner apparatus which comprises a pilot burner including a nozzle and swirlers disposed around the nozzle, and a plurality of main burners which are arranged around the pilot burner and each of which comprises a nozzle and swirlers disposed around the nozzle; and the angle of the swirlers for the pilot burner is set larger than the angle of the swirlers for the main burner so that the angles of the two types of swirlers cross. NOx production can be considerably reduced with a very simple structure based on the present invention for combustion in boilers and gas turbines.

Abstract: The invention relates to the improved combustion of fuel in a combustion chamber of a stirling engine and the like by dividing combustion into primary and secondary combustion zones through the use of a diverter plate.

Abstract: A burner assembly for gaseous fuels having an outer housing, a blower and a unitized combustion cartridge. The combustion cartridge comprises an elongated cylinder having a flame holder at a downstream end thereof. The flame holder is provided with a plurality of spatially disposed diffusion plates attached to the cylindrical body of the combustion cartridge such that the center lines of the diffusion plates extend radially and perpendicularly from the cylindrical body. Each plate extends from the cylindrical body at an acute positive angle from the plane of their center lines. A plurality of orifices are disposed in the cylindrical body substantially adjacent the flame holder and a portion of the orifices communicate with orifice extender tubes so that gaseous fuel can be distributed over the upstream surface of the flame holder.

Abstract: A burner is of generally tubular configuration, and comprises an inner shell and an outer shell. The inner shell has therein a nozzle, an ignition electrode, and a sight tube. An annular gap is provided between the two shells, through which a comburant-gas flows to an annular, inwardly directed and constricted discharge opening, with swirl blades upstream of the discharge opening. A comburant-gas supply passes through openings in the inner shell upstream of a baffle which is positioned transversely of the inner shell, and which has radial slots therein inclined to the plane of the baffle to cause swirling of comburant-gas passing through the slots in the baffle. A toroidal-cyclone combustion zone is created due to the slots in the baffle creating a swirling downstream flow downstream of the baffle, and the inwardly directed annular and constricted opening, which aspirates comburant-gas which has passed through the baffle.

Abstract: A burner for operation with gas and/or includes a central pilot burner system selectively operable with gas and/or oil as a diffusion burner or as a separate pre-mixing burner and an annular main burner system surrounding the pilot burner system and carrying a primary air flow. The main burner system includes a multiplicity of first nozzles admixing gas with the primary air flow for pre-mixing operation and second inlet nozzles pre-mixing oil into the primary air flow.

Abstract: A cyclone combustion apparatus includes a combustion chamber having a substantially cylindrical wall, a substantially cylindrical exit throat at the rear end of the combustion chamber, means for supplying fuel into the combustion chamber at a front end thereof, means for supplying air into the combustion chamber and for forming a cyclonic flow pattern of hot gases for combustion within the chamber, and heat exchange means surrounding and extending throughout the axial length of the combustion chamber. The means for supplying air includes a plenum chamber having an air inlet and an annular air supply opening in communication with and coaxial with the combustion chamber. The annular air supply opening has spaced radial vanes tilted at a selected angle from the axis of the combustion chamber. The means for supplying fuel includes a fuel plenum chamber having a fuel inlet and a plurality of radially spaced fuel holes for supplying fuel in the annular air supply opening between the spaced radial vanes.

Abstract: In order to avoid carbon buildup and to assist fuel atomization, a fuel injection system (40) includes a fuel injector (42) associated with the upstream portion (44) of a combustor (10). The fuel injector (42) has a fuel flow passage (46) in communication with a source of fuel (14) and terminating in the upstream portion (44) of the combustor (10). The fuel injection system (40) also includes a primary oxidant delivery tube (20) associated with the upstream portion (44) of the combustor (10). The primary oxidant delivery tube (20) defines a primary oxidant flow passage (48) in communication with a source of oxidant (12) and terminating in the upstream portion (44) of the combustor (10). The fuel injection system (40) further includes a secondary oxidant delivery tube (50) associated with the upstream portion (44) of the conbustor (10).

Abstract: A burner register assembly is provided for controlling a supply of secondary air to a furnace having a fuel and primary air supply and a secondary air supply. The burner register assembly includes a body and a pair of air valves in the body for communication with the secondary air supply to control the admission of secondary air to the register assembly. Each air valve communicates with a scroll section in the burner register body, which scroll section has a scroll passageway which spirals inwardly in the direction of secondary air flow to provide a controlled flow pattern of secondary air into the furnace. The air valve is disposed upstream of the scroll section with which it communicates and thus is well removed from the extreme environment of the opening or throat to the furnace. The burner register assembly also includes a shadow vane assembly positioned proximate to the outlet of the register, i.e., proximate to the furnace throat, to provide protection form radiant heat from the furnance.

Abstract: A burner assembly (75) for the combustion of liquid fuels in furnaces (12) and the like. The assembly comprises fuel gun means (78) for creating a mixture of combustible fuel and an atomizing medium and injecting a stream of the mixture into the interior of a furnace; housing means (76) supporting the fuel gun means, attachable to the furnace, so that the combustible fuel mixture is delivered to the interior of the furnace for combustion and for supplying a first flow of air (B) into the furnace separate from the air mixed with the fuel to encompass the injected fuel mixture; and sirler means (79) having a plurality of blades (94) interposed within the housing means so that the first flow moves around and through the blades for imparting a rotation to the first flow of air to break up the stream of fuel mixture.

Abstract: High flame stability and good starting qualities are obtained in a relatively smoke free hot gas generator including a housing 10 having an interior combustion chamber 12 with a diverging interior wall 20 that is generally a surface of revolution. An axially directed opening 18 is centered in the wall 20 and an outer, oxidant inlet 48, 52 is provided and includes swirler vanes 50 for introducing into the chamber 12 at the interior wall 20 a swirling, hollow body of oxidant such that centrifugal force will create a diverging hollow body of swirling oxidant on the interior wall 20. A central fuel inlet 52, 58 is located within the opening 18 and within the oxidant inlet 48, 52 and is generally concentric therewith.

Abstract: A low NOx burner comprises a pulverized coal nozzle for injecting a flow of a mixture of pulverized coal with primary air, a secondary air nozzle arranged externally of and coaxially with the pulverized coal nozzle, a tertiary air nozzle arranged externally of the secondary air nozzle and disposed coaxially with the pulverized coal nozzle, and a swirl flow generator for injecting secondary air and tertiary air as a respective swirl flow. Between the secondary air nozzle and the tertiary air nozzle, there is provided a spacer having such a thickness as to delay the mixing of the secondary air and the tertiary air and to form a swirl flow between the secondary air and the tertiary air.

Abstract: A burner assembly (10) for the combustion of pulverized coal in furnaces (12) and the like. The assembly comprises wind box means (23) for providing a primary source of air to the interior (13) of the furnace; feeding means (30) for delivering pulverized coal through a wall (11) of the furnace and into the interior thereof; means for supplying (31) a secondary flow of air through the feeding means and into the furnace separate from the primary flow of air; and swirler means (32) having a plurality of blades around the feeding means so that the first flow moves around and through the blades for imparting a rotation to the primary flow of air to penetrate the pulverized coal funnel. A method for supplying pulverized coal to furnaces and the like through burner assemblies is also provided and results in increased combustion efficiency.

Abstract: A fuel or coal-water slurry burner with oxygen supply to the primary air through the vanes of a diffuser plate that swirls primary air is described.

Abstract: An improved high efficiency swirl combustor type gas burner for use in residential or commercial water heaters is provided having a swirl cone to induce turbulence in the combustion air and a mixing zone where turbulent gas is mixed with the combustion air and then combusted at a distance away from the burner face.

Abstract: The emission of NOx, soot and particulates is minimized by combusting fuel in two sequential steps, viz. a first combustion step wherein a number of fuel jets and a substoichiometric amount of combustion air in the form of an equal number of high-velocity air jets are injected into a combustion chamber in such a manner that(a) each fuel jet merges into one high velocity air jet,(b) the characteristic mixing time of each fuel jet is less than about 10.sup.-4 sec, and(c) a plurality of separate fuel/air jets is generated forming at ignition a plurality of primary flames in which a residence time for the fuel of substantially at least 100 ms is maintained;and a second combustion step comprising introducing further combustion air into said combustion chamber for complete combustion of the fuel.

Abstract: An air register apparatus, method, and arrangement is disclosed in which each air register includes two portions, one of which feeds combustion air to an inner, ignition zone where fuel is first ignited, the other of which feeds combustion air to an outer, supplemental zone where the main combustion takes place. These two register portions provide separate and discrete air streams having measurable characteristics which accurately reflect the characteristics of the overall flow through each register portion and which characteristics govern combustion characteristics in the associated zone. Each air stream passes through an inwardly spiralling scroll passageway having a simple upstream air valve at the entrance to the passageway for controlling the flow of air through the passageway. This upstream air valve is remote from the hostile environment of the furnace or other combustion device.

Abstract: A fuel burner assembly for providing a stable, non-pulsating flame wall proximate to a burner duct outlet thereof including structure which causes a combustion air stream to flow radially outwardly and then inwardly across a fuel supply outlet and spaced igniter centrally positioned adjacent the duct outlet, the stream then being divided into three flow paths, one path being axial, another being centrally rotated and a third being annularly compacted to stabilize the produced flame wall proximate the duct outlet.

Abstract: A device for improved combustion of gaseous fuel and air includes a tubular housing and has a combustion chamber disposed about the tubular housing. A first conduit extends from one end of the tubular housing for the passage of air therethrough. A second conduit extends coaxially through the first conduit and tubular housing and has a circular baffle cooperative therewith so as to retard the passage of air. A circular opening in the second end of the tubular housing has an annular baffle disposed therein to assist in retarding flow of air. A series of curvilinear fins are disposed in a spiral configuration between the circular baffle and the annular baffle so as to effect a swirling motion of air passing therethrough. An end cap is attached to the end of the second conduit with a circular baffle at one end of the end cap, an annular baffle at the other end and fins disposed therebetween. Gaseous fuel passes through the second conduit and the end cap.

Abstract: In a combustion chamber having a flame tube therein at an annular gap from a housing of the chamber, a burner apparatus including at least one pilot burner near an end face of the flame tube for generating a pilot flame from natural gas and/or heating oil, an air supply channel surrounding the head of the pilot burner, a premixing device for natural gas in the form of a ring channel system surrounding the head including flow conduction walls defining an inflow cross section at an air inflow side of the ring channel system open toward the annular gap for conducting a majority of combustion air from the annular gap to a combustion zone developing downstream of the burner head in the flame tube, the combustion air having flow vectors with components entering the combustion zone in directions from parallel to the burner axis to an acute angle to the burner axis, the combustion air components having swirl components superimposed thereon tangentially relative to the burner axis acting as a swirl center, a multiplic

Abstract: An ignition and combustion supporting burner for pulverized solid fossil fuel comprises an axial conduit for feeding the pulverized fuel in a primary combustion supporting gas. The shape of a refractory tap-hole enables the initial part of the flame to be confined. A conduit for feeding tertiary combustion supporting gas is concentric with the tap-hole and partially or totally surrounds it. The burner also incorporates a flame detector device and an igniter in the refractory tap-hole or in the axial conduit. The axial conduit is provided with translation means providing for adjustment of the length of a chamber for preliminary mixing of the fuel and part of the combustion supporting gas comprised between the end of this conduit and the inlet of the tap-hole.

Abstract: An air register is provided for admitting to and regulating combustion air in industrial open flame heated boilers and furnaces. The register comprises an outer member to impart rotation, balancing and blending of opposed incoming air streams; an inner member to impart a spiral motion to a resultant single air stream in the direction of the boiler or furnace entrance; and a third member to form the air stream into a flame encompassing envelope.

Abstract: The invention relates to method and apparatus for the combustion of fluidal fuels. The fuel is dispersed in combustion air and, in order to improve the combustion rate and efficiency, is exposed to a high particle velocity of a sound produced by a low frequency sound generator. The frequency of the sound is determined by the sound generator, the maximum frequency being 30 Hz. A reciprocating movement of combustion air and fuel particles entrained therein is obtained. The sound generator is a quarter wave type sound generator with a tubular resonator forming a diffuser at the open end thereof.

Abstract: A flame retention head assembly for use in a fuel burner having a fuel nozzle mounted coaxially within an air pipe. This assembly comprises a continuously contoured, outwardly diverging flame retention head mounted concentrically within the air pipe in front of the fuel nozzle. This head successively defines, starting from its inlet end: an air-and-fuel mixture chamber; a first expansion chamber; a throttle and a second expansion chamber. A spinner plate is mounted transversely across the inlet end of the head. This plate comprises a central ring provided with a central hole having a diameter substantially identical to the one of the fuel nozzle, and a plurality of blades regularly distributed around the ring to cause air to enter and swirl into the mixture chamber. A round-shaped deflector is also mounted concentrically transversely within the retention head, to cause the air and fuel entering the head through its inlet end to stay longer within the first or second expansion chamber.

Abstract: In a combustion chamber having a substantially cylindrical housing and a flame tube .[.therein at an annular gap from a housing of the chamber,.]. .Iadd.with an end face, the flame tube being thermally movable and disposed in the combustion chamber and the flame tube being spaced from the cylindrical housing defining an annular gap therebetween, the improvement includes .Iaddend.a burner apparatus .Iadd.having a burner axis and .Iaddend.including at least one pilot burner .[.near an.]. .Iadd.having a head and being disposed in the vicinity of the .Iaddend.end face of the flame tube for generating a pilot flame .[.from.]. .Iadd., the pilot burner operating with at least one fuel from the group consisting of .Iaddend.natural gas .[.and/or.]. .Iadd.and .Iaddend.heating oil, an air supply channel surrounding the head .[.of the pilot burner.]., a premixing device for .[.natural gas.]. .Iadd.mixing gas and air .Iaddend.in the form of a ring channel system surrounding the head.Iadd., the ring channel system .