Abstract: In a gasifying oil burner with an oil atomizing device, with combustion air upply means surrounding the atomizing device, with a shield having a shield opening, said shield being disposed downstream of the outlet of the atomizer, with a mixing tube disposed downstream of the outlet of the atomizer, with a mixing tube disposed downsteam of an co-axial with the shield opening, with a radial passage at an upstream portion of the mixing tube, with a generally cylindric flame tube whose upstream end is sealingly connected to the end wall of the combustion air supply means carrying the shield, and wherein it is proposed that the mixing tube be provided with a solid wall at a section thereof adjoining the shield, that the radial passage adjoin a part of the mixing tube provided with the solid wall, and that the axial length of the mixing tube portion with the solid wall extending between the shield and the radial passage be between the 0.1-multiple and the 0.

Abstract: A high velocity oxygen fuel burner (10) includes a combustor assembly (11) mounted in a graphite block (12), with the burner mounted in a water jacket (18) of a furnace. The combustor assembly includes a combustion chamber (48) that receives a stream of oxygen along its center axis (51). The fuel moves from fuel barrel (32) through fuel passages (50), with a portion of the fuel being diverted into the combustion chamber (48) by the annular fuel diverter ring (52) and with the rest of the fuel moving on through the fuel extension passages (50b) and through nozzle ring (34). The nozzle ring directs the fuel into the flame as it emerges from the combustion chamber, so that the fuel from the nozzle has a cooling effect at the exposed end of the burner and tends to develop the flame in an annular ring about the stream of high velocity oxygen that is directed toward the work product in the furnace.

Abstract: A burner for generating hot gases to be used for packaging purposes with thermal shrinkage of plastic foils has an elongate rectangular zone of transition between its pressure-distribution and combustion chambers, spanned by a flame-retaining tube forming narrow passages for the gas flow with the adjacent walls. A number of codirectionally curved sheet-metal baffles equispaced, and of equal radius of curvature, mounted on the downstream side of the tube and extending toward the opposite walls of the chamber, improve the combustion conditions of the gas mixture and lead to a higher velocity of the stream of hot gases leaving the burner, thus increasing the amount of ambient air entrained into the stream and thereby reducing the temperature of the combustion gases.

Abstract: The combustor comprises a single sheet of metal coated with catalyst and wound into a spiral. There is a single spiral passage leading into the core of the spiral. The fuel-air mixture burns on the catalyzed surface of the spiral, and heat is transferred through the metal wall of the spiral to the incoming fuel-air mixture. The incoming fuel-air mixture is preheated to a temperature sufficient to start the catalytic combustion. The fuel content in the mixture can be below the flammability limit. The combustor is compact so that it can be used as a catalytic air preheater in a downhole steam generator.

Abstract: A method of burning a fuel gas in a low NO.sub.x level in the exhaust gas is disclosed, wherein a radiant tube burner having concentrically arranged outer air flow nozzle, fuel gas nozzles arranged in a circle and inner air flow nozzle and having a particular structure is used and the fuel gas is burnt under a particularly limited condition.

Abstract: A fuel fired burner assembly comprises a fuel supply conduit (2) terminating in a nozzle (1) which extends with annular clearance (8a) into a combustion chamber (7) located within a tunnel (3). The nozzle (1) is provided with radially directed outlet passages (18) which convey the fuel from the conduit (2) to the clearance (8a) where the fuel mixes with air entering the clearance (8a) from passages (15), (16) and (8b). These passages formed between the tunnel body (3), an outer tunnel sleeve (11) and an intermediate sleeve (14) between the body (3) and the sleeve (11). The nozzle (1) is also provided with a through-going aperture (19) which is located between two adjacent fuel ports (18) and which is axially offset from the nozzle axis. Extending through the aperture (19) with annular clearance (20) is an electrically operated flame detection probe (21) whose electrode tip (22) is disposed within the central section (6) of the tunnel (3).

Abstract: The invention concerns a burner for producing a jet of hot gases, in particular to shrink plastic foils, with a pressure distribution chamber of a fan-like contour joined to a mixture feed means and merging at its wide end into a combustion chamber of an elongated cross-section, a flame holder being mounted in the transition zone between the pressure-distribution and the combustion chambers. In order that such a burner evince more reliable and constant properties while being of a simple design, the flame holder shall be a bar of shaped section extending across the entire width of the pressure-distribution and combustion chambers and together with the adjacent walls shall form passageway-gaps for the combustion gases.

Abstract: The object of the invention is to permit, for operation with coal by itself, easy adjustment of the flame length without varying the gas flow and with a relatively stable flame divergence. The burner according to the invention comprises a cylindrical tube (1) through which an air/fuel mixture is ejected into the flame, and inside which a coaxial cylindrical part (6) can move along the axis in order to permit adjustment of the output speed of the gas. Advantageously, this part (6) constitutes a means for injecting air and fuel-oil for mixed operation or operation with fuel-oil by itself.

Abstract: An apparatus and method for the combustion of water-in-oil emulsion fuels are described. The apparatus is fitted to the top of a burner and the fuel is burned in the apparatus whereby the rapid and complete combustion of the fuel is achieved. The apparatus includes an inner vessel open at both ends, with one end being fitted to the burner and a baffle coaxially attached to the inner vessel at the other end thereof which has a frusto-conical configuration with a plurality of holes therethrough. An outer vessel is coaxially mounted on the inner vessel with both ends being secured to the corresponding ends of the inner vessel to form a preheating chamber between the inner and outer vessels. Pressurized air is introduced into the preheating chamber, around the baffle and through the holes into the interior of the inner vessel to compress the flame of the water-fuel emulsion forcing it to swirl and remain in the inner vessel.

Abstract: An improved burner for attaining an improved combustion of a fuel-air mixe includes a plurality of vanes extending generally longitudinally of and disposed about an axis of the flow of the air-fuel mixture, each of the vanes having a first and a second end joined by first and second longitudinal edges. The first ends being contiguously arranged to extend along the circumference of a circle coaxial with the axis, the first edges defining a cylindrical surface coaxial with the main axis, and the second edges defining a conical surface coaxial with the axis. The vanes being interconnected at their first ends. The vane structure being confined in a cylindrical structure defining at the one end an annular opening through which compressed air is introduced, with a fuel nozzle being provided at the center of the same end. The nozzle being located at the end of the vane structure where the vanes substantially meet at the center of the structure.

Abstract: A burner system particularly useful for downhole deployment includes a tubular combustion chamber unit housed within a tubular coolant jacket assembly. The combustion chamber unit includes a monolithic tube of refractory material whose inner surface defines the combustion zone. A metal reinforcing sleeve surrounds and extends the length of the refractory tube.

Abstract: A flame-out-resistant portable torch for igniting gas-air blasts in industrial gas furnaces includes an inner pipe for receiving gas at one end, with the opposite end closed and a gas-expulsion slot along one side, surrounded in coaxial spacing by an outer pipe with an air-induction side slot 180.degree. from the slot in the inner pipe, the outer pipe has air-induction butt end opening, vents around portions of it near the slots, and a flame expulsion end with anti-back-pressure structure, and the coaxial space between the inner and outer pipes has special baffles along it for gas-air mixing for better flame-retention.

Abstract: An oil burner for installation in heating or steam-raising boilers. The ber has downstream of an oil atomization device a plate having a single opening or a plurality of openings arranged in a ring coaxially of the oil atomising device, the plate opening or openings being the only throughway for combustion air. A mixing tube is arranged coaxially at a distance downstream of the plate. The mixing tube has a diameter greater than the diameter of the single opening or of a circle which encloses the plurality of openings in the plate. A flame tube positioned coaxially around the mixing tube has a length such that the flow of combustion gases downstream of the mixing tube is applied against the internal wall of the flame tube. To enable the burner alternatively to be used for burning gaseous fuel at will, an annular chamber for the supply of a gaseous fuel and having gas outlet openings in the region of the plate opening or openings is also provided downstream of and close to the plate.

Abstract: A spray type combustion device comprises a fuel injection nozzle disposed inside an inner cylinder which is surrounded with an outer cylinder to form therebetween an annular air space, the inner cylinder being formed with an air introduction opening through which air is introduced to the inside of the inner cylinder, and a restrictor plate formed with a central opening and positioned to be close to the tip of the fuel injection nozzle so as to form therebetween a clearance for restricting air flow therethrough, thereby preventing the nozzle opening of the fuel injection nozzle from being clogged with carbon particles due to fuel incomplete combustion.

Abstract: A hydrogen gas burner for the mixture of hydrogen gas with ambient air and non-combustible gasses. The mixture of gasses when ignited provides a flame of extremely high, but controlled intensity and temperature. The structure comprises a housing and a hydrogen gas inlet directed to a combustion chamber positioned within the housing. Ambient air intake ports are provided for adding ambient air to the combustion chamber for ignition of the hydrogen gas by an ignitor therein. At the other end of the housing there is positioned adjacent to the outlet of the burner (flame) a barrier/heating element. The heating element uniformly disperses the flame and in turn absorbs the heat. The opposite side to the flame, the heating element uniformly disperses the extremely hot air. A non-combustible gas trap adjacent to the heating element captures a small portion of the non-combustible gas (burned air).

Abstract: A novel burner, e.g. for a gaseous fuel is provided herein. The burner is an improvement on the conventional hand-held blowpipe type of burner including a cylindrical housing, a nozzle body provided with a mixing chamber, an axial gas inlet port to the mixing chamber, a plurality of radial air inlet ports to the mixing chamber, and an axially extending burner tube connected to the mixing chamber. The mixed gas is substantially completely burned in the burner tube. The improvement is an add-on to the conventional burner and takes the form of a self-cooling shield. The shield includes a disc-like, centrally apertured baffle secured at the extreme forward end of the cylindrical housing with the axially extending burner tube projecting through the central aperture thereof. The shield also includes an outer tubular member, secured concentrically to the cylindrical housing by a disc-like centrally apertured rear wall, the central aperture surrounding the cylindrical housing and being secured thereto.

Abstract: A burner for the formation and combustion of an ignitable mixture of liquid uel and combustion air, which includes a closed combustion chamber for the infeed of the fuel with porous walls permeable to the fuel. The combustion chamber is arranged within a flow chamber which is streamed through by preheated combustion air flowing towards the combustion zone.

Abstract: A gas mixing line burner having a stoichiometric turndown ratio in the range of between twenty-five and thirty to one and capable of operating at a capacity of about 2,000,000 BTU/HR per lineal foot of burner. The burner includes an air/fuel manifold having a discharge face which causes combustion air jets to mix with fuel jets and form a main combustible mixture which is provided with a constant ignition source by virtue of stabilizing air jets interacting with the fuel jets and creating a secondary combustible mixture down the center of the main mixture. One embodiment of the burner includes a combustion chamber which is formed by refractory material while the combustion chamber of an alternative embodiment is formed by stainless steel sections connected by expansion joints which prevent warpage of the sections.

Abstract: A fuel, such as coal, is prepared by mixing with a petroleum product and possibly other materials to form a grease-like substance. In a motionless mixer the grease-like substance is combined with air to form a foam-like dispersion of fuel and air. Such foam-like dispersion is delivered substantially continuously to a combustion chamber for combustion thereat. The combustion chamber is relatively closed and has means cooperative with the foam-like dispersion and the pressure of expanding gases of the combustion process to impede flow of the foam-like dispersion therein; consequently the foam-like dispersion is maintained at a pressure head to maintain the air dispersion therein. The speed and heat of combustion may be controlled by controlling flow rate or pressure of the foam-like dispersion. Means are provided for reducing pollutants and for efficiently transferring heat out from the combustion chamber.

Abstract: A single-ended recuperative radiant tube assembly for increasing the efficiency of a combustion furnace system by using less fuel input per heat output than conventional systems. The single-ended recuperative radiant tube assembly has inner and outer recuperator tube assemblies positioned in a counterflow arrangement within a radiant tube assembly. Hot exhaust gases emitted from a burner within the single-ended radiant tube assembly are directed through a flame tube to an annular exhaust chamber located between the outer recuperator tube and radiant tube assemblies. Ambient air flowing towards the burner in an air chamber between the inner and outer recuperator tube assemblies is heated by the exhaust gases in the annular exhaust chamber.

Abstract: The tube-fired radiant heating system is of the type where an elongated tube is heated by hot gases of combustion which are passed. The heated tube radiates heat to the space to be heated therethrough.A burner is provided at one end of the tube to burn an air/fuel mixture. The products of combustion are forced through the tube by means of a blower provided at the tube inlet. Burning takes place within the tube. A tubular stream of air is constantly passed over the flame to protect the tube from the high heat of combustion.

Abstract: A porous ceramic heating reactor is positioned within a tubular casing to contain the flame and the end products of combustion. A flattened portion of the casing extends substantially past the reactor to provide for further transfer of heat through the casing wall from the hot exhaust gases and to carry those exhaust gases to a safe point of exhaustion. The unit is essentially modular so that any number can be selected for an installation. The casing configuration enhances turbulent flow of the hot gaseous products of combustion. Turbulent flow increases heat transfer to and through the walls of the casing to the boilder or other area to be heated. The size and shape of the tubular casing provides an explosion proof, leak proof, efficient heat transfer device. Each reactor has a spark plug one of whose elements is a bi-metallic strip. In a multi-unit installation the spark plugs are connected in parallel across a spark generator.

Abstract: An air-heating gas burner has a housing which includes a fuel gas supply passage and an air supply passage which open into a combustion zone defined between walls which extend downstream of outlets for the gas and air. Combustion products emerging from said combustion zone are confined between further walls which extend downstream to a location at which the combustion process is substantially complete. The burner is intended for mounting in an air conduit and the combustion products emerging from between the further walls have a particularly low content of oxides of nitrogen.

Abstract: A burner for pulverized coal such as in a rotary kiln includes three concentric cylindrical ducts. The outer duct carries an air supply which is directed in a generally axial direction into the kiln. The next innermost duct carries the pulverized coal-carrier gas mixture and is also generally directed in an axial direction. The next innermost duct carries air which is directed in a divergent radial direction in the kiln and includes a rotational air component. By controlling the quantities of air in the ducts which flank the coal duct, the resulting flame form can be controlled in the kiln without restoring to variations in the velocity or direction of the coal carrier gas stream. By eliminating such variations in regard to the coal carrier gas stream, the abrasive action of the pulverized coal is kept to a minimum.

Abstract: A blue-flame oil burner including a flame-tube, a wall extending transvery of the flame-tube and defining the upstream end thereof, the wall having therein a metering orifice through which air enters the flame-tube, the orifice being the only air inlet into the flame-tube, an oil atomizing nozzle positioned upstream of the wall and discharging an oil spray through the orifice into the flame-tube, and a mixing tube positioned within the flame-tube co-axially of the orifice and having its upstream end spaced axially from the wall by a distance such that the peripheral area of the space between the wall and the upstream end of the mixing tube and defined within an imaginary upstream extension of the peripheral wall of the mixing tube to the transverse wall is between one and three times the difference between the cross-sectional area at the upstream end of the mixing tube and that at the orifice, the mixing tube having a length, L, and a diameter, D, such that the ratio L/D is between 1.0 and 1.

Abstract: Unit for thermal incineration of non-explosive gases with minor amounts of organic pollutants and for production of hot air, and which can be adapted to various types of supplementary fuel. There is a combustion chamber which consists of a flame pipe inside an outer jacket. Through the space therebetween, incoming process gas is led as coolant. At its front end, the combustion chamber has a burner for supplementary fuel and a mixing-in zone for process gas. The process gas rapidly mixes with the hot combustion gases in the flame, the gas reaching its reaction temperature directly. Powerful turbulence in the mixing-in zone gas, film-layer cooling, convective cooling and even flow give highly efficient and pure combustion while keeping the flame pipe temperature low enough to prevent corrosion.

Abstract: A swirl burner of the two-stage combustion type with suppressed NO.sub.x generation which is so arranged that combustion air supplied into the burner is divided into primary and secondary combustion air, and the primary combustion air subjected to a powerful swirling motion by a primary combustion air nozzle having a frusto-conical shape and swirling vanes is supplied into a primary combustion chamber for drawing only primary combustion gas thereinto, while the secondary air is directed, in the form of a rectilinear flow, into a furnace through secondary combustion air nozzles provided around the primary combustion chamber, with oil and gas for fuel being supplied into the primary combustion chamber through a fuel injector nozzle. Part of the fuel is burned in the primary combustion chamber, while the remainder of the fuel is sequentially mixed with the secondary combustion air for combustion in the furnace.

Abstract: A portable space heater having a deep fuel tank in conjunction with a fuel pump for raising the fuel to a predetermined height to feed an aspirating type nozzle incorporated in the fuel system and an adjusting valve means to control the flow of fuel to the siphon line connected to the nozzle. The fuel pump feeds the fuel from the tank to a predetermined level at which the aspirating nozzle will operate efficiently. The fuel line system also has a return line to the tank which allows any excess fuel in the lines to be appropriately returned to the tank.

Abstract: The present invention provides an improved nozzle mixing line burner for automatically increasing available oxygen for combustion as the fuel gas flow rate increases. This improved nozzle mixing line burner includes a pair of fuel gas manifolds, each of which has a row of gas discharge ports discharging laterally and toward the opposite manifold to provide streams of fuel gas. An orifice plate extends between the fuel gas manifolds and includes a plurality of rows of air orifices extending along the line of the burner, with the air orifices closest to the gas manifolds being relatively smaller in size and the more internally disposed rows of air orifices increasing in orifice size toward the middle of the orifice plate, to increase the available air supply proportionately as the velocity of the fuel gas flow increases.

Abstract: A high velocity gas burner has a housing divided by a partition into an air plenum and a combustion zone. Air is introduced into the plenum with a swirl. A ring of gas jets penetrate the partition through clearance holes. Each jet has a collar tending to impede air flow through the respective hole and the partition is axially displaceable relative to the collars. The partition is preferably cup-shaped with a skirt extending along the housing into the combustion zone so that secondary or excess air can bypass the combustion proper and cool the combustion products to the desired usable temperature.

Abstract: A heater for burning particulate fuels in which a stream of air carrying combustible particles is injected upward into a combustion chamber (22) between two spaced perforated tubular members (33, 34), the outer member being taller. A deflector (55) located within the outer member and above the inner member causes the stream to flow outward and then upwardly, and helical vanes (139) may be provided between the members. A gun-type oil burner (61) is located below the members for initially heating them and igniting the particles. Particulate fuel is supplied through an auger 70 from a bin 71 which contains springs 77 rotated to prevent bridging or caking of the material. Rotation of the springs and drive of the auger are powered by a common motor 80.

Abstract: A burner apparatus for burning liquid fuels is equipped with a swirl atomizer nozzle (4), a flame holder (22) that is connected behind the nozzle mouth, and a combustion air delivery duct (8), in which the nozzle (4) is arranged coaxially. A thermally decoupled duct-like heat conductor (10) functions as a fuel vaporizer in the operation of the apparatus. In its main portion, which starts a small distance downstream from the nozzle, the heat conductor has an inside diameter such that droplets in the spray cone from the nozzle tend to impact evenly over the whole area of its inner surface. The heat conductor (10) is of silica nitride. It comprises at least partially a capillary inner layer.

Abstract: A process and apparatus for the combustion of liquid fuel provides an extremely intense blue/violet flame having a temperature in excess of 3000.degree. F. with combustion under near perfect stoichiometric conditions without the formation of soot. The liquid fuel is atomized and mixed with air within a nozzle and enters a flame tube surrounding the nozzle as a conical stream where it is further atomized by jets of air directed to converge on the stream and mixed with secondary combustion air to obtain the desired combustion mixture. Yet further atomization of the liquid fuel-air mixtures within the flame tube can be obtained as a consequence of at least partial vaporization of the liquid fuel therein through the heat of the flame tube. An advantageous relationship exists between the size, angle and point of convergence of the air jets with the atomized conical stream, the flame tube diameter and length and the location of the nozzle therein and the fuel feed.

Abstract: A fuel injection system for low emission burners in which the primary fuel is delivered in an annular spray into the primary combustion zone; at high power operation, secondary fuel is injected additionally in a low angle axial spray to penetrate beyond the primary zone and into the secondary combustion zone downstream of the primary zone.

Abstract: In a two stage burner construction in which primary fuel burns in an annulus in a primary combustion zone and secondary fuel is discharged through the primary zone to a secondary zone downstream of the primary zone, vortex generators are used in the passage through which the fuel and air entering the primary zone to enhance the mixing and to improve the toroidal flow in the combustion zone. Other vortex generators are used to improve the mixing of the secondary fuel and air to improve secondary combustion. The vortex generators may be used in conjunction with a trip on the secondary nozzle tube to further enhance primary combustion.

Abstract: In a jet torch of the type in which a venturi yields a high-velocity stream of air entrained with combustible gas released from a pressurized tank, the stream gases are mixed for reliable and efficient burning, while at the same time sidewall cooling and flashback-suppression are promoted, by thin crossed vanes edge-locked within the flame tube and bent without twist to deflect the stream gases about the cylindrical interior of the flame tube for resulting swirling motion.

Abstract: A flame cutting machine includes an ignition system for igniting the fuel gas which is connected by a transverse bore to a longitudinal bore parallel to the blend canal of the machine.

Abstract: A radiant heater in which the fuel is supplied at an inlet end of a combustion chamber, formed by an imperforate tubular shell, where combustion takes place, and the products of combustion are forced axially in one direction through the tubular shell, which is elongated to provide a substantial heat radiating wall, and out through an outlet end thereof. Surrounding the first shell, is a second tubular shell, which is concentric with the first shell to provide a second substantial heat radiating wall and an annular chamber which receives the products of combustion from the combustion chamber, directs them axially in a reverse direction, and permits them to discharge outwardly through radial outlets provided in said second radiating wall. Combustion is accomplished by a burner which is located at the inner end of the first shell to cooperate therewith and with the second shell in an effective manner to obtain maximum combustion and radiation.

Abstract: A low pressure burner capable of generating a relatively long narrow flame is disclosed. A rotationally symmetric chamber is open at each end. Air is forced through the chamber at low pressure, generally no greater than about 0.3 lbs. per square inch above ambient. An atomizer is located in the chamber and expels a combustible mixture out through the downstream end of the chamber. The mixture expelled by the atomizer of the present invention has a distribution which is not rotationally symmetric about the chamber axis. The atomizer utilizes low pressure air provided at no greater than about 4.5 lbs. per square inch above ambient. A flame throat is located at the downstream end of the chamber, and includes at least two axially spaced steps to induce and control eddy formation in the mixture. The nonsymmetric mixture distribution and the multistep chamber combine to provide a long, narrow, stable flame in the throat at relatively low inlet air pressures.

Abstract: A combustion head for a fluid fuel, particularly a liquid fuel, which is burnt particularly in the presence of a gas having an oxygen concentration substantially less than that of air, comprises, adjacent to the actual burner, a generally cylindrical box containing an inlet aperture designed to create a substantial pressure drop on injecting the oxygen-containing gas into the box, and a disc situated at the outlet of the box and dimensioned to create a second and lower pressure drop. The intense combustion produced in the box heats its walls to a temperature substantially above the final point of the distillation curve for the fuel, so preventing coke deposition.

Abstract: Large amounts of low boiling liquefied gases are evaporated by heat transfer in a cylindrical combustion chamber without a convection component and a passage for the gas to be evaporated surrounds the combustion chamber so that the liquefied gas is exposed to a burner flame upon entry into the passage.

Abstract: An oil burner for distillate fuel including a blower and air guiding elements producing a rapidly whirling pattern of combustion air close to the burner nozzles to produce an extremely hot fireball close to the nozzles. The fireball, once ignited, provides reliable continuous ignition of the entering fuel, obviating the usual requirement of continuous electrical ignition, and permitting the use of low voltage for the initial ignition. The blower produces an excess of air over that needed for combustion, and the excess air cools the combustion chamber externally to obviate any necessity of forming the chamber of stainless steel, cast iron or the like. When the burner includes a plurality of burner nozzles intended for use singly or simultaneously, automatic means are provided for supplying the necessary carefully regulated amounts of combustion air.

Abstract: A system for the transmission and conversion of the potential energy of hydrocarbon fuels to available heat, power and light. The system is particularly adapted for use with natural gas, artificial gases or any of the LPG fuels such as propane, butane, etc. According to the system of the invention, the fuel gas is mixed with air preferably in the amount providing the stoichiometric ratio to oxygen and is stored under pressure and ultimately transmitted to burner elements which are hermetically sealed except for the inlet and discharge ports, such as tubes, power sources, such as captive and free piston devices and gas turbines and light sources. The system includes special forms of equipment for mixing and pressurizing the gas and air in the correct ratio and special forms of equipment for establishing and controlling the combustion processes.

Abstract: A sleeve and damper to increase the efficiency of oil burner performance designed to substantially enclose the flame. The sleeve is heated by the flame to a temperature sufficiently high to assure automatic ignition of unburned hydrocarbons that may result from incomplete combustion of the fuel oil. By controlling the damper operation in conjunction with an adjustable induction air apparatus, unburned hydrocarbons which would ordinarily result are completely oxidized. The resulting completeness of combustion permits the use of oil as a fuel to heat ovens without imparting any odor or taste to the food products being processed therewithin.

Abstract: A burner for combustible fluids has a distribution opening adapted to feed a combustion chamber and supplied by a source of a comburant (combustion-sustaining gas such as air or a mixture of air and combustion products), a swirl generator between this source and the opening, an injection nozzle for the combustible fluid extending coaxially through this opening, and a constriction located immediately ahead of the discharge end of the nozzle and adjacent an outwardly diverging passage adapted to generate a toroidal vortex in the region of the end of the nozzle.

Abstract: A carbon black reactor which has a precombustion zone and reaction zone therein with inlet means communicating with the precombustion zone for the introduction of hot combustion gases thereinto. A conduit communicates with the interior of the reactor and has mounted one one end thereof a nozzle for the discharge of make hydrocarbon into either the precombustion zone or reaction zone. A tubular member has an open end and surrounds a free end of the nozzle with the tubular member extending downstream of the free end whereby the open end of the tubular member permits flow of make hydrocarbon from the nozzle through the tubular member and out into the reactor.

Abstract: Fuel is injected into a combustion chamber by a central burner. Combustion air is fed through an air supply passage provided in a plurality of air ejection holes on an annular plate surrounding the front end of said air supply passage.

Abstract: A fuel injection nozzle for a turbo engine is mounted at the base of a costion chamber, either tubular or annular, by means of an intermediate inwardly flared member having openings through its sides for admitting cooling air. An annular flange structure around the intermediate member supports the same and defines an annular space with the base of the chamber for a layer of cooling air admitted to that space through holes in the base. Several forms are disclosed in each of which the various holes and air inlets are dimensioned and positioned to provide a stoichiometric mixture of air and fuel under substantially all conditions of operation.

Abstract: A heating assembly for a heat treating furnace is disclosed which includes a heating tube from which heat is transferred to the furnace and a burner disposed in the heating tube. The burner is connected to a source of mixed fuel and air and is constructed to define a mixture inlet section, a throat section and a discharge section. A primary mixture flow passage is defined by the throat section and secondary mixture flow passages communicate with the discharge section to impinge secondary mixture flows into the primary flow and impart a vorticular motion to the mixture flowing from the burner.The burner is constructed from a first relatively easily machined member which defines the inlet and throat sections and in which the secondary passages are formed. A second tubular cylindrical heat resistive member defines the discharge section and the members are shrink fitted together to enable reconditioning of the burner by replacement of the second member.

Abstract: An improved premix gas burner design suitable for use in a metal melting furnace which has long service life, a low degree of maintenance, is easily cleared in case of burner blockage, allows inspection of the combustion chamber or furnace interior and still maintains the desired turndown capabilities of premix gas burners. These results are achieved by providing usual and/or physical access to the interior of the burner through a novel access tunnel and by providing a dual composition refractory combustion chamber.