Abstract: A burner is provided for heating a stream of combustion supporting gas, like air. The burner has a main feed pipe extending across the stream of combustion supporting gas. The main feed pipe has an inlet for receiving a fuel gas from a fuel gas source, and at least one outlet for producing a main jet of fuel gas substantially in the direction of the stream. The burner also has two parallel auxiliary feed pipes extending across the stream of combustion supporting gas, at a predetermined distance downstream from the main pipe and on each side of the main jet. Each of the auxiliary feed pipes has an inlet for receiving fuel gas from the fuel gas source, and at least one outlet for producing an auxiliary jet of fuel gas in the direction of the stream. The burner further has two bluff-body devices in front of the outlets of both the auxiliary feed pipes respectively.

Abstract: A fuel fired, forced air, draft induced heating furnace is provided with NOx reduction apparatus associated with a plurality of combustor tubes forming a portion of its heat exchanger structure. In-shot type fuel burners are spaced apart from and face the open inlet ends of horizontal combustion sections of the combustor tubes. The NOx reduction apparatus includes a plurality of insert members received in inlet end portions of the combustor tubes. Each insert member is formed from a single sheet of metal mesh material and has a hollow, open-ended body portion coaxially received in its associated combustor tube and spaced laterally inwardly from its interior side surface, and a circumferentially spaced plurality of integral, laterally outwardly projecting support rib portions that slidably engage the interior side surface of the combustor tube, thereby automatically maintaining the insert member in a coaxial relationship with the combustor tube regardless of the positional orientation of the tube.

Abstract: Method and apparatus for generating oxy-liquid fuel with lowered NO.sub.x products using low pressure oxygen to atomize liquid fuel and produce an oxy-liquid fuel flame and surrounding the oxy-liquid fuel flame by an oxidizer, confining the oxy-liquid fuel flame and oxidizer in a precombustor for a distance determined by the rate of flame propagation and the diameter of the pre-combustor.

Abstract: A kerosene heater (1) having a pump assembly (106) which includes a piston (113) having a hollow bore (121) through which fuel (98) is routed to the hollow shaft of a fuel atomizer (27). The piston (113) is operated by a cam (117) machined into the shaft (114) of the heater motor (22). Mounted on the motor shaft (114) between the atomizer (27) and the pump assembly (106) is a novel fan (26) combining both low pitched outer blade portions (143) and high pitched vanes (146) near the hub (136) of the fan (26). The air flow near the periphery of the fan tends to be axial while the flow near the hub (136) tends to be turbulent and of lower velocity. A series of rear heads (32,33) downstream of the atomizer (27) tends to separate cooling and combustion air while preheating a portion of the air in the region of the atomizer (27).

Abstract: A supersonic flame jet device includes a body having an entry portion of relatively small cross-sectional area, an expanding supersonic nozzle section and a cylindrical duct of extended length connected in series with each other. In using the device, an oxidant at high pressure is introduced into the entry passage wherein the flow is increased to sonic velocity. The sonic velocity flow of oxidant is then introduced into the passage of expanding cross-section in the direction of the gas flow while introducing a fuel to be burned into the flow of the oxidant. The velocity of flow of the oxidant or the oxidant and the fuel is then increased to supersonic velocity prior to entry into the extended duct of constant cross-sectional area where a shock is produced to stabilize flame reactions along the extended duct length whereby a supersonic flame jet will exit the extended duct.

Abstract: A premixed gas burner has a hollow body including a closed end and an entry end into which a combustible gas and air mixture may flow. The body has a multiplicity of apertures through which the mixture may pass from the hollow interior. A burner portal deck is positioned in superposed relationship over the apertures for permitting the gas air mixture to form a controlled flame. A porous woven fabric formed from ceramic fiber having high thermal insulation properties is located above the deck and separates the deck from the flame front formed when the mixture is ignited. The fabric insulates the deck from excessive temperatures, prevents flash back, allows use of conventional stainless steel for the deck and body components and makes possible the manufacture of long burner sections. A long burner section has a number of decks in side-by-side relationship with an insulating fabric mat over the decks for not only providing insulation, but also forms a gasket between the adjacent decks.

Abstract: A burner apparatus comprising: a liquid fuel discharge means for discharging a liquid fuel; an ignition chamber wherein an ignitable gaseous composition can be ignited to yield an ignited composition; and a gas delivery means for delivering a gaseous, free oxygen source and a combustible gas to the ignition chamber such that the ignitable gaseous composition is provided in the combustion chamber. The ignition chamber is positioned with respect to the liquid fuel discharge means such that, upon leaving the ignition chamber, the ignited gaseous composition will ignite the liquid fuel as the liquid fuel is discharged from the discharge means. Preferably, the gas delivery means includes a conduit through which the free oxygen source is conducted into the ignition chamber. The gas delivery means also preferably includes a passageway, adjacent the exterior of the conduit, through which the combustible gas is conducted into the ignition chamber.

Abstract: A burner assembly combines air and fuel to produce a burn firing into a downstream tube. The assembly includes a funnel formed to include an inlet, an outlet, and an air and fuel mixing region therebetween. The funnel also includes a cylindrical intake end at the inlet and a conical side wall mating with the cylindrical intake end and converging from the cylindrical intake end toward the outlet to fire a burn initiated in the mixing region into a tube coupled to the outlet of the funnel. The assembly also includes a system for supplying a gaseous fuel to the mixing region in the funnel and a system for introducing combustion air into the mixing region through the inlet of the funnel. The combustion air mixes with the gaseous fuel in the mixing region to produce a combustible mixture.

Abstract: A gas burner comprising a housing with a front exit, a back surface, and an outer surface. The housing has a closed back surface at one end and an open exit at the other end. The housing is separated into a fuel-oxygen mixing chamber and a second chamber by a support plate. A multiplicity of jets passing through the support plate such that the fuel-oxygen mixing chamber is in communication with the second chamber through the jets. The fuel-oxygen mixing chamber has an inlet for a first-gas, usually a fuel gas, and an exit. The second chamber has an inlet for a second-gas, usually oxygen. The jets arranged such that each jet centerline is unique with respect to all other jet centerlines and each jet centerline is directed from the support plate to the housing exit.

Abstract: A burner for an industrial furnace has a plurality of lines passing through a furnace wall for fuel gas, burner air, and waste gas. Arranged in the furnace space is a combustion chamber (66) in which a mixture of fuel gas and burner air is combusted, and from which a flame (89) is directed into the furnace space. The combustion chamber (66) is delimited by walls (32, 65). The walls (32, 65) are arranged to be movable with respect to one another (65', 65"), so that the volume of the combustion chamber (66) is adjustable (FIG. 2).

Abstract: Space heating appliance of the radiant tube type has sheet metal or other shield formations mounted in the tube to extend downstream of fan induced gas flow from side edges of the mouth of a fluid fueled burner head which projects into the tube to feed hot gases into the flow so as initially to separate that infeed from the general flow along the tube.

Abstract: A burner for burning a combustible gas comprising fuel gas and air that has been mixed before being supplied to the burner. The burner has a flame holder concavely recessed into a flame outlet. The concave configuration of the flame holder focuses the individual flames on the combustion surface toward a central location where the individual flames interact with and reinforce one another in a direction axial to the burner. Thus very little heat is transmitted directly from the burner in a direction normal to the burner axis. This characteristic of the burner allows it to be used to fire a flue type heat exchangers where the walls of the heat exchanger are very close to the burner without excessive temperatures being produced in the heat exchanger walls adjacent the burner.

Abstract: A burner assembly is provided for combining oxygen and fuel to produce a flame. The burner assembly includes a burner block including a combustion chamber and a nozzle discharging an oxygen and fuel mixture into a first stage region formed in the combustion chamber. First stage oxygen is supplied to the first stage region in the combustion chamber to combine with the oxygen and fuel mixture discharged into the first stage region by the nozzle. Second stage oxygen is also delivered to a downstream second stage region in the combustion chamber in sequence through an oxygen delivery tube, a flow regulator plate, and then an oxygen-conducting passage formed in the burner block. The flow regulator plate has a fixed-diameter oxygen-flow orifice having an internal diameter that is less than the internal diameter of the oxygen delivery tube to meter the flow of second stage oxygen discharged into the second stage region so as to apportion oxygen flow between the first and second stage regions.

Abstract: A kinetic dissociator is formed by a primary combustion chamber and a secondary combustion chamber. The primary and secondary combustion chambers are connected by at least one flow stabilization tube. A source of high temperature, high velocity gas is provided by at least one high speed combustion jet axially aligned with the flow stabilization tube such that the jet gas mixes with a process gas passes through the tube and impinges against a conically shaped wall forming a portion of the secondary combustion chamber.

Abstract: A burner is disclosed having a burner chamber with heavily insulated heat retaining walls and a series of off center mixer tubes located at one end thereof. A uniform concentration gas/air mixture to 50% additional fuel above the lean flammability limit coming from the mixer tubes is ignited in the burner chamber due to the recirculation of combusting gas and air back to the end of the burner chamber above auto the ignition temperature for the mixture. The particular mixture disclosed utilizes 0.55-0.7 equivalence ratio.

Abstract: An improved two-stage combustion chamber for burning waste hydrocarbons such as crank case oil, spent motor oil, transmission fluid, lubrication dopes, and heavy bodied gear lubes. The combustion chamber is formed from a plurality of spaced apart, stacked annular rings that form a flame containment housing having superheated surfaces. The flame containment housing contains the flame of an atomizing oil burner suitable for burning the variable viscosity waste hydrocarbons. The annular rings include outer walls and inwardly extending flanges that intercept unburned fuel droplets and combustion byproducts, vaporizing the droplets and/or stimulating secondary combustion. The annular rings are removable and replaceable, and are supported in spaced-apart relation by spacers on a plurality of support rods.

Abstract: A burner assembly combines air and fuel to produce a burn firing into a downstream tube. The assembly includes a funnel formed to include an inlet, an outlet, and an air and fuel mixing region therebetween. The funnel also includes a cylindrical intake end at the inlet and a conical side wall mating with the cylindrical intake end and converging from the cylindrical intake end toward the outlet to fire a burn initiated in the mixing region into a tube coupled to the outlet of the funnel. The assembly also includes a system for supplying a gaseous fuel to the mixing region in the funnel and a system for introducing combustion air into the mixing region through the inlet of the funnel. The combustion air mixes with the gaseous fuel in the mixing region to produce a combustible mixture.

Abstract: A combustor assembly having a preestablished rate of thermal expansion is mounted within a gas turbine engine having a preestablished rate of thermal expansion being greater than the preestablished rate of thermal expansion of the combustor assembly. The combustor assembly is constructed of a inlet end portion, a outlet end portion and a plurality of combustor ring segments positioned between the end portions. A retaining ring is positioned radially adjacent the combustor ring segments to allow for thermal radial expansion of the combustor ring segments while maintaining radially compressive force on the combustor ring segments and distributing force evenly along the combustor ring.

Abstract: A Stirling engine having a cooler, regenerator and heat exchanger stacked end to end along with a working cylinder position adjacent to the heat transfer stack and connected thereto by several connecting ducts. By using more than one hot connecting duct, their bending stiffness is less as compared with a single duct being the same area as the multiple ducts, allowing thermally induced relative displacement between the elements to occur. The heat exchanger includes a plurality of axially extending tubes spaced apart from one another with a combustor positioned adjacent to the tubes such that the combustion gases flow between the tubes. The tubes are preferably flattened in the direction of the gas flow between them to increase the surface area for heat transfer. Furthermore, wire is coiled around and brazed to the tubes creating a fin for additional heat transfer.

Abstract: A jet burner construction, heating apparatus utilizing the jet burner construction and methods of making the same are provided, the jet burner construction having opposed ends and having a fluted portion disposed spaced from and intermediate the inlet and the outlet of the burner body and having opposed ends, the fluted portion defining a central opening part and radiating portions of the outlet opening of the burner body which is generally located in the middle of the fluted portion, the fluted portion expanding and extending axially beyond the central opening part at one of the opposed ends thereof and comprising part of a flame retainer unit that also comprises a generally ring-like structure between the one of the opposed ends of the fluted portion and the one of the opposed ends of the burner body, the one of the opposed ends of the fluted portion expanding outwardly substantially at a right angle to the longitudinal axis of the burner construction.

Abstract: A fuel-fired, forced air draft induced heating furnace is provided with NO.sub.x reduction apparatus associated with a plurality of combustor tubes forming a portion of its heat exchanger structure. In-shot type fuel burners are spaced apart from and face the open inlet ends of horizontal combustion sections of the combustor tubes. The NO.sub.x reduction apparatus includes a plurality of metal mesh tubes having diameters substantially less than the internal diameters of the combustion tubes. The mesh tubes are coaxially supported within the combustor tubes, adjacent their inlet ends, by elongated support members longitudinally passing through the mesh tubes and having first ends anchored to the combustor tube inlet ends, and second ends slidably resting on internal side surface portions of the combustor tubes.

Abstract: A fuel-air combustion chamber with improved mounting and thermal distribution features. The combustion chamber is formed with a flange adapted for receiving a plurality of retainer rings therearound for direct securement of the flange to a burner mounting plate adjacent a fuel-air nozzle for generating heat within the combustion chamber. The combustion chamber is also temporarily supported within the furnace housing by a combustible support leg affixed thereto. In this manner, the combustion chamber is supported during shipping and handling by a support leg which is automatically disintegrated during use of the combustion chamber.

Abstract: The gasification burner of this invention capable of maintaining a high combustion rate for a long period of time comprises a combustion chamber having a ceiling with a small hole in its center, a pre-mixing pipe fitted into the small hole and having a nozzle at its top, wherein the pre-mixing pipe and the combustion chamber are concentric, and the spread angle of the gas flow sprayed from the end of the pre-mixing pipe is between 10 and 40 degrees, so that the relationship between the bottom of the combustion chamber and the conical gas flow is regulated by keeping a good balance between the gasification rate of the powdered coke and the life of the combustion chamber.

Abstract: The invention concerns a fiber burner-brick 5, 13, 24, 34 with a fiber part 7, 15, 25, 35, 46, 54 made of refractory fibers. In order that the said brick be of low eight, insensitive to mechanical and thermal stresses and be characterized by fine and uniform porosity, the fiber part 7, 15, 25, 35, 46, 54 is composed of individual fiber strips 9, 10, 18, 19, 20, 21, 26, 36, 47, 55 each consisting of mutually displaceable fibers intrinsically cohesive and only by themselves, the fiber strips 9, 10, 18, 19, 20, 21, 26, 36, 47, 55 being compressed against each other by a compression system 8, 16, 27, 28, 29, 30, 31, 38, 39, 44, 45, 51.

Abstract: A hot air burner in which a nozzle assembly is comprised of an inlet port housing (8) incorporating an internal plenum chamber (18) into which is introduced a flow of compressed air via an inlet port (4) in the inlet housing (8). The flow of compressed air is controlled by the width of an adjustable gap created between a frusto-conical exterior surface (20) of the internal annular chamber (18) and the internally chamfered wall (22) of a mixing tube (12). Turbulence in the compressed airflow is created as the air enters the mixing tube (12) and this swirling effect promotes efficient mixing of subsequently introduced combustible gases to tile mixing tube (12) via an inlet port (6) in the inlet housing (8). The combustible mixture is ignited and the resultant combustion contained within the confines of an outer burner tube (10). The flame front is contained within the burner tube (10) and extends approximately six inches into the length of the tube (10).

Abstract: A tube assembly, such as a flame tube for a gas turbine plant, includes a tube segment having an inner region for guiding a hot gas in one flow direction. A heat shield faces toward the inner region and includes a plurality of bricks being disposed side by side. At least one metal support frame supports the heat shield. The support frame has a plurality of conduits for supplying a cooling gas and a lip encompassing the tube segment and substantially covering the conduits toward the inner region leaving a slit for conducting the cooling gas from the conduits past the lip to the inner region.

Abstract: A liquid fuel power plant (100) including an open-ended combustion chamber (102) and a first mechanism (112) for delivering a combustible liquid fuel to the open-ended combustion chamber (102). A second mechanism (136) is included for igniting the fuel in the open-ended combustion chamber (102). A coiled tube-shaped mechanism (140) located external to the combustion chamber (102) is provided for extending the length of the combustion chamber (102) to decompose the ignited fuel and to provide an exhaust gas comprised of fundamental elements. Finally, a third mechanism (160) is provided for using the exhaust gas to perform useful work. The air input line (120) delivers compressed air, which can be preheated, in an air passageway (130) and thereafter is mixed with the combustible fuel in the open-ended combustion chamber (102).

Abstract: A liquid fuel power plant (100) including an open-ended combustion chamber (102) and a first mechanism (110) for delivering a combustible fuel to the open-ended combustion chamber (102). A second mechanism (136) is included for igniting the fuel in the open-ended combustion chamber (102). A folded tubular mechanism (140) is provided for extending the length of the combustion chamber (102) to decompose the ignited fuel and to provide an exhaust gas comprised of fundamental elements. Finally, a third mechanism (160) is provided for using the exhaust gas to perform useful work. In a preferred embodiment the liquid fuel power plant (100) includes separate fuel and air inlet lines (110, 120). The air inlet line (120) delivers compressed air, which can be preheated, in an air passageway (130) and thereafter is mixed with the combustible fuel in the open-ended combustion chamber (102). An igniter (136) causes combustion of a compressed air-fuel mixture in an ignition region (118) of the combustion chamber (102).

Abstract: A self contained catalytic heating device within which a fuel/oxidizer mixture and combustion products are held out of physical contact with a heated medium, allowing the temperature of the catalytic material to be maintained at a level that is independent of the temperature at the surface in contact with the heated medium; materials and geometric dimensions can be chosen to achieve required temperatures for catalytically coated surfaces and heating surfaces, for example in a tubular construction.

Abstract: A jet burner construction, heating apparatus utilizing the jet burner construction and methods of making the same are provided, the jet burner construction having opposed ends and having a fluted portion disposed spaced from and intermediate the inlet and the outlet of the burner body and having opposed ends, the fluted portion defining a central opening part and radiating portions of the outlet opening of the burner body which is generally located in the middle of the fluted portion, the fluted portion expanding and extending axially beyond the central opening part at one of the opposed ends thereof and comprising part of a flame retainer unit that also comprises a generally ring-like structure between the one of the opposed ends of the fluted portion and the one of the opposed ends of the burner body, the one of the opposed ends of the fluted portion expanding outwardly substantially at a right angle to the longitudinal axis of the burner construction.

Abstract: A burner for heating a gas stream is disclosed having a primary combustor mounted coaxially within a main combustor to form an assembly. The assembly is coaxially mounted within a burner housing and defines a gas flow space between the assembly and the housing. Gas enters the housing upstream of a substantial portion of the assembly and flows axially over the exterior thereof, picking up heat rejected from the assembly as it travels axially through the housing to an outlet area of a reduced diameter which defines a mixing zone. In the mixing zone, burner output and excess air are introduced to the gas stream in a manner so that the inputs are injected into the exhaust stream in a direction which has a normal component to the direction of gas flow thereby assuring adequate mixing and a resultant even distribution of heat in the flow.

Abstract: The invention relates to a process and an apparatus for the treatment of moist, explosive gas-dust mixtures, particularly coal dust mixtures in mill drying plants. To avoid a condensing out of residual moisture from intermediately stored dust, heated inert gas is supplied to the conveying system for the coal dust or the intermediate storage points.

Abstract: A pulse combustor ignitor comprising a small combustion chamber located external to the pulse combustion chamber. A spark ignition source such as a spark plug is associated with the chamber and separate inlets for fuel and air are provided. The fuel/air mixture is ignited by the spark plug and the ignited mixture is directed into the combustion chamber of the pulse combustor until a steady state operation of the pulse combustor is achieved. An air preheater may be used for the air delivered to the ignitor combustion chamber. The flow pattern of the fuel/air mixture and the flame may be controlled by an adjustable passage element located between the respective ignitor and pulse combustor combustion chambers. A flame scanner positioned external to the pulse combustor may be used to sense the entrance of the ignited mixture from the ignitor into the pulse combustor.

Abstract: A liquid fuel power plant (100) including an open-ended combustion chamber (102) and a first mechanism (110) for delivering a combustible liquid fuel to the combustion chamber (102). A second mechanism (118) is included for delivering compressed air to the combustion chamber (102) to provide a pressurized air-fuel mixture. A third mechanism (130) ignites the pressurized air-fuel mixture in the combustion chamber (102) and a fourth mechanism (134) is provided for extending the length of the combustion chamber (102) for decomposing the pressurized air-fuel mixture to provide an exhaust gas comprised of fundamental elements. Finally, a fifth mechanism (142) is provided for using the exhaust gas to perform useful work. The air inlet line (116) delivers compressed air from a turbocharger (118) which is preheated in an air passageway (128) and thereafter mixed with the fuel in the combustion chamber (102).

Abstract: A rotary fluid bed gasifier which comprises: a rotatable drum having a circumferentially extending wall which is permeable to gases; a means for feeding a fluidizing gas through the wall into the drum; a bed of particles which, at least when the gasifier is in use, is supported on an internal face of the wall and is fluidized by the fluidizing gas; an outlet means for receiving an oil-in-water emulsion from outside the gasifier and delivering the oil-in-water emulsion to the drum; a means for introducing steam into the drum; a de-NO.sub.x boiler having a quench zone and a nitrogen fixing zone; a means for introducing secondary air disposed between the quench zone and the nitrogen fixing zone; and a means for introducing tertiary air disposed between the de-NO.sub.x boiler and a main boiler or furnace.

Abstract: A liquid fuel power plant (100) including an open-ended combustion chamber (102) and a first mechanism (114) for delivering a combustible fuel to the open-ended combustion chamber (102). A second mechanism (124) is included for igniting the fuel in the open-ended combustion chamber (102) and a concentric cylinder-shaped mechanism (130) is provided for extending the length of the combustion chamber (102) for decomposing the fuel to provide an exhaust gas comprised of fundamental elements. Finally, a third mechanism (202) is provided for using the exhaust gas to perform useful work. The air inlet line (122) delivers compressed air which is preheated in an air inlet passageway (194) and thereafter mixed with the combustible fuel in the open-ended combustion chamber (102). The residue of the combusted air-fuel mixture is thereafter forced by the compressed air into the concentric cylinder-shaped extension (130) which forms the reaction region (180) of the combustion chamber (102).

Abstract: A jacketed jet radiant heater for an industrial process furnace as a frame tube composed of axially aligned pipe pieces abutted on one another that are held together by clasps on the outside of the flame tube that have studs which protrude into holes in adjacent pipe pieces and have a head portion which serves to center the flame tube within the jacket tube. The clasps make it possible to provide exhaust gas releasing slots between some of the pipe pieces of the flame tube and thereby avoiding local overheating of the jacket tube.

Abstract: A jet burner construction, a heating apparatus utilizing the jet burner construction and methods of making the same are provided, the jet burner construction comrpising a burner body having a chamber therein and having an inlet leading to the chamber for directing fuel from a fuel source therein and an outlet leading from the chamber and defining an outlet opening through which the fuel is adapted to issue from the chamber to burn externally to the burner body, the outlet opening having a central opening part and a plurality of spaced apart opening portions interconnected thereto and radiating outwardly therefrom whereby flows of fuel respectively issuing out of the portions and the central part of the outlet opening merge together in a turbulent manner externally of the outlet opening.

Abstract: An exhaust gas burner reactor which comprises a burner apparatus having a combustor tube which extends axially in a spaced relationship to an exhaust gas conduit. The combustor tube has a first, base end having fuel and air inlets and a mixing chamber therein, and a second combustor end having a combustor chamber and outlets for ejecting burning fuel and air into the exhaust gas conduit. The combustor assembly is oriented so as to locate the burner outlets upstream of the first end so that heated exhaust gas/burner output mixture passes through an exhaust reactor defined between the combustor tube and the exhaust gas conduit. The reactor aids in the combustion of unreacted fuel components in the exhaust gas.

Abstract: An improved liquid fuel combustion device comprising a combustion chamber, a fuel inlet nozzle communicating with said combustion chamber, means for delivering a stream of turbulent air into said combustion chamber in a manner to cause liquid fuel to flow into an mix with said air stream, and means for igniting the mixture. If desired, additional air may be provided to promote more complete burning of the fuel.

Abstract: Method and apparatus for generating an oxy-fuel flame with lowered NOX products by confining the oxy-fuel flame produced in a concentric orifice burner along a path defined by the rate of flame propagation and the diameter of the burner.

Abstract: An apparatus for producing an emulsion by agitatedly mixing liquid fuel and water. Low pollutant level emissions and an efficient combustion system are realized by burning this emulsion. An agitator chamber supplies liquid fuel and water from a liquid fuel tank and a water tank and agitating blades are arranged inside agitator chamber to agitatedly mix liquid fuel and water. Movable permanent magnets are fixed on agitator disks and an agitating blade driving motor rotates agitating blades to produce an ionized emulsion. A pump pressurizes the emulsion and a burner sprays it for burning.

Abstract: A burner head for a recuperative radiant tube burner system is constructed so as to effect clean burning of a gaseous fuel such as butane having a relatively high heat value. The burner head includes a sleeve having a frustoconical section formed with combustion air ports which cause combustion air to spin and mix thoroughly with butane discharged from a gas nozzle having a discharge orifice located downstream of certain ones of the combustion air ports.

Abstract: A burner structure and a method of operating a burner to reduce the pollutant emissions produced thereby are disclosed. Air and gas are premixed in a manner such that a substantially homogeneous mixture containing excess combustion air results. The velocity of the substantially homogeneous mixture is increased as it passes through the burner causing the "residence time" associated with the formation of the flame to be decreased, i.e., the combustion gases are in the reaction zone of the flame for a significantly shorter period of time, reducing the production of NO.sub.x. In order to prevent the flame from "lifting-off" the burner because of the high velocity of the substantially homogeneous air/gas mixture, flame stabilizing devices and/or a burner structure which provides flame stabilization are utilized resulting in the production of a high heat flux and low pollutant emissions.

Abstract: A cooling system including a cooling duct adjacent to the hot air duct of an air heater. The cooling duct includes a first wall and a second wall spaced from the first wall such that a passageway is formed therebetween. A wire mesh sheet is arranged in the duct passageway. The wire mesh sheet comprises a plurality of layers of wire mesh and has an undulate configuration which together with its density prevents substantial heat radiation from the first wall of the cooling duct to the second wall without significantly impeding airflow through the cooling duct. Cooling air introduced into the cooling duct flows through the duct, removes heat, radiated by the first wall and absorbed by the wire mesh sheet, and carries that heat away from the duct as it exits through the outlet opening. In this way, the system cools the first wall and prevents any significant heat transfer to the second wall of the cooling duct and elements in the vicinity thereof.

Abstract: A combustion apparatus comprises: a large-diameter sleeve-like element forming an incoming passage through which an air/fuel mixture gas flows in a predetermined direction; at least one small-diameter sleeve-like element disposed in the incoming passage, which small-diameter sleeve-like element forms an outgoing passage through which a combustion gas having been issued from the incoming passage flows in a direction counter to the above predetermined direction; an air/fuel mixing unit for issuing the air/fuel mixture gas under a predetermined pressure to a main incoming port located in an upstream side of the incoming passage; an auxiliary incoming unit for issuing a combustion gas produced by a pilot burner to the upstream side of the incoming passage prior to supplying the air/fuel mixture gas to the incoming passage; and a combustion-gas outlet port for discharging the combustion gas having passed through the outgoing passage, which combustion-gas outlet port communicates with an outlet opening of the outgo

Abstract: An oxy-fuel system for reducing NO.sub.x formation in corrosive high temperature environments including a self-cooled adjustable oxy-fuel burner that generally produces a luminous flame having a concentric fuel rich phase and an outer surrounding oxidizer rich phase the flame directed through a precombustor mounted on the flame end of the burner the precombustor having a length to diameter (L/d) ratio fixed by the firing rate of the burner.

Abstract: In a pilot light igniter for a burner, an inner tube for receiving fuel gas is concentrically positioned within an outer tube for receiving air in the annular space between the inner tube and the outer tube. Apertures are formed in the inner tube to impart angular momentum to the fuel gas as it flows from the inner tube into the annular space so that the mixture of air and gas swirls as it flows to the open distal end of the outer tube. A spark disk is provided on the end of the inner tube and a flame rod extends axially from the spark disk. The air and fuel mixture is ignited by a spark produced by high voltage applied between the spark disk and the outer tube. A low voltage source applied between the flame rod and the outer tube causing current pulses provides an indication of the presence of a flame.

Abstract: A jet burner construction, a heating apparatus utilizing the jet burner construction and methods of making the same are provided, the jet burner construction comprising a burner body having a chamber therein and having an inlet leading to the chamber for directing fuel from a fuel source therein and an outlet leading from the chamber and defining an outlet opening through which the fuel is adapted to issue from the chamber to burn externally to the burner body, the outlet opening having a central opening part and a plurality of spaced apart opening portions interconnected thereto and radiating outwardly therefrom whereby flows of fuel respectively issuing out of the portions and the central part of the outlet opening merge together in a turbulent manner externally of the outlet opening.

Abstract: A gun-type oil burner is disclosed having a motor axially aligned with a fuel pump and a blower at opposite ends. The blower draws air into the burner, the amount of which is controlled by an adjustable air gate. The blower inlet is covered by a removable, protective air scoop. Upon removal of the air scoop, an outside air boot is easily connected to the burner without burner modification. The air in the burner travels along a serpentine path which contains smooth curves and perimetrally disposed protrusions for reducing the velocity of the air flow and maintaining its static pressure. The air flows through an air tube in a helical pattern, mixes with oil and is ignited at the air tube outlet. A fuel nozzle, ignitors and a fuel supply conduit are supported as a burner sub-assembly within the tube by a spider. A preselected stop of a number of removable stops of differing sizes is located on the spider and properly positions the burner sub-assembly within the air tube.