Abstract: The present invention relates to an electromechanical system for automating the turning off of the knobs of a stove. The system can quickly identify the occurrence of a gas leak and turn off the knob corresponding to the burner that is leaking. The system is also connected to a user interface, providing real-time information about the status of the burners and allowing the user to turn off the knobs remotely. The system has an improved service life, does not considerably change the aesthetics of the stove and can be designed to fulfil different torque requirements. The invention also relates to cooktops comprising said system.

Abstract: A burner box assembly according to aspects of the disclosure includes an outer cover, the outer cover having a sloped bottom face that directs condensation away from a heat-exchange tube, a heat-resistant liner having a plurality of panel members, the heat-resistant liner being disposed within the outer cover, a shield disposed between the heat-resistant liner and the sloped bottom face of the outer cover such that an air gap is formed between the shield and the sloped bottom face, and a tubular member abutting at least one of the plurality of panel members and disposed within the heat-exchange tube.

Abstract: The invention relates to a method for starting up a gasifying reactor comprising a plurality of burners. Each burner is thereby charged with combustible dust from a metering vessel (1) via a dense flow conveyor line (51, 52, 53, 54), which is assigned thereto, and with fuel gas via a gas conveyor line (62, 63), wherein a fuel mixture of combustible dust and combustible gas is provided prior to a moment of ignition of a burner, wherein a first composition of combustible dust and combustible gas, with which a first burner is charged for ignition, is regulated as a function of the fuel quantity, which was supplied to the second burner for ignition, after the ignition of a second burner, which is charged with a second composition of combustible dust and combustible gas for ignition, following the ignition of the first burner, so that the starting up of each of the plurality of burners of the gasifying reactor takes place under a regulated supply of the fuel load.

Abstract: A rotary injector (95, 222) comprising one or more radially-extending arms (93) provides for injecting fuel (12, 12.1, 12.4) into a combustion chamber (16). The combustion chamber (16) receives air (14) from locations upstream and down-stream of the rotary injector (95, 222), and the arms (93) of the rotary injector (95, 222) are adapted so that a pressure (P2) in the combustion chamber (16) upstream of the rotary injector (95, 222) is less than a pressure (P0) in a plenum (212) supplying air (14) to the combustion chamber (16) upstream of the rotary injector (95, 222).

Abstract: A fuel reformer is provided that is capable of improving endurance and performance. The fuel reformer includes a first burner having a first-burner first end, a first-burner second end, and a first opening formed in the first-burner first end; a second burner surrounding the first burner and having a second-burner second end, a second-burner second end, and a second opening in the second-burner first end, wherein the second-burner second end is coupled to the first-burner second end to communicate a fluid. The reforming reactor is configured to generate heat from the first and second burners, and has a fuel supply including a nozzle unit in the first burner and supplies a second oxidation fuel from the outside to the first burner. A first oxidation fuel is introduced into the first opening and flows through the first burner in a first direction and flows through the second burner in a third direction opposite to the first direction.

Abstract: A combustor for a small gas turbine engine in which a compressor discharges a swirling air flow into the combustor, and a fuel impeller is rotatably connected to the compressor and slings atomized fuel into the combustor in a direction to produce a stagnation zone within the combustor. A plurality of fuel injectors delivers fuel to the inlet end of the fuel impeller. The combustor outlet is a nozzle shape that produces a high enough pressure level in the swirl air flow such that the cooler air flows along the inner combustor wall to form an insulation layer from the hot combustor gas flow within the combustor. The fuel impeller produces a very fine mist of fuel and the stagnation zone produced results in easy starting of the engine and stable combustor burning.

Abstract: A combustion burner device that includes a rotor chamber with a rotary element rotatably mounted therein. The rotor chamber has a cylindrical sidewall with an inlet port in communication with a source of pressurized gas and an outlet port in communication with a combustion chamber. The rotary element has at least two interrupters forming cavities therebetween within the rotor chamber. The cavities are configured for receiving pressurized gas from the chamber's inlet port and transferring the pressurized gas to the chamber's outlet port. The rotation of the rotary element is in response to and by way of reaction to the issuance of gas under pressure through the inlet port.

Abstract: Tertiary nozzle of port for gas injection into furnace includes a contracted flow producing channel provided obliquely toward central axis from the upstream side of gas flow so that the gas flow has a velocity component heading from the outer circumferential side of the port toward the central axis and a velocity component heading along the central axis toward the interior of the furnace, and including louver disposed for guiding so that the gas flows along the surface of throat wall of enlarged pipe configuration wherein the gas channel is enlarged at a furnace wall opening disposed at an outlet area of the contracted flow producing channel.

Abstract: An oil/slurry burner with injection atomization for the gasification of solids-containing liquid fuels under high pressures of e.g. 80 bar (8 MPa) and high temperatures of e.g. 1200 to 1900 degrees centigrade in reactors with liquid slag removal is proposed, wherein a plurality of feeding elements disposed outside the annular duct concentrically with respect to the burner axis are provided for introducing liquid fuel and atomizing agent, the individual feeding elements being implemented intrinsically straight in the burner, inclined to the burner axis in the direction of the burner mouth, and ending at the burner mouth adjacent to the oxidant outlet. By introducing the liquid fuel and atomizing agent in individual completely implemented tubes with a corresponding nozzle, different fuels can be supplied simultaneously via the individual feeds and converted in a flame reaction.

Abstract: A fuel manifold is provided for receiving a flow of fuel from a fuel source and delivering the flow of fuel to a rotary fuel slinger. The fuel manifold can include a housing having an end face and defining a cavity for receiving the flow of fuel; at least one exit orifice formed in the housing end face and in fluid communication with the cavity; and a fuel drip guide extending from the end face.

Abstract: A combustion system includes a fuel manifold adapted to receive a flow of fuel from a fuel source, the fuel manifold including at least one orifice from which the received fuel is discharged. The combustion system further includes a rotary fuel slinger disposed adjacent to the fuel manifold. The rotary fuel slinger includes a coupler shaft and a slinger disc coupled to the coupler shaft. The slinger disc includes a first portion disposed generally perpendicular to the coupler shaft and a second portion disposed at an angle to the first portion. The fuel manifold is positioned relative to the rotary fuel slinger such that the discharged fuel impinges on the second portion. The rotary fuel slinger is configured to rotate such that the flow of fuel is centrifuged radially outwardly from the second portion onto the first portion and subsequently off the rotary fuel slinger to atomize the received fuel.

Abstract: A radially-extending arm is adapted to rotate within a stream of first fluid flowing thereacross. In one embodiment, the arm comprises a plurality of lands located at different radial distances from the axis of rotation, and a port located on each land is operatively coupled to a source of a second fluid. The second fluid is sprayed from the rotating arm into the stream of first fluid that flows across the lands, and is thereby atomized. In another embodiment, the arm comprises a land stepped into the trailing edge thereof, and a port for injecting the second fluid is located on the land. In another embodiment, the land comprises a groove located between the port and an associated riser surface stepped into the trailing edge. In another embodiment, the arm comprises a port in the trailing edge thereof from which the second fluid is injected, and a groove is located on the trailing edge in a radially increasing direction from the port.

Abstract: A combustion heater comprising an induction chamber provided with an inlet, a combustion chamber in fluid communication with the inlet of the induction chamber, means for moving an oxydizer from the inlet of the induction chamber to the combustion chamber, a fuel reservoir, a frame defining a fuel passageway, means for moving a fuel from the fuel reservoir through the fuel passageway to the combustion chamber, means in fluid communication with the fuel passageway for shearing a fuel prior to combustion, means in fluid communication with the fuel passageway for heating the fuel prior to combustion, and means for combusting a fuel oxydizer mixture within the combustion chamber.

Abstract: An evaporative burner includes an evaporative medium for feeding fuel vapor into a combustion chamber, a first heating device, having at least one ignition heating element projecting with at least its heating region into the combustion chamber for igniting fuel vapor present in the combustion chamber, and a second heating device, with at least one evaporating heating element associated with the evaporative medium for affecting its evaporation characteristic.

Abstract: A TFT formed on an insulating substrate source, drain and channel regions, a gate insulating film formed on at least the channel region and a gate electrode formed on the gate insulating film. Between the channel region and the drain region, a region having a higher resistivity is provided in order to reduce an Ioff current. A method for forming this structure comprises the steps of anodizing the gate electrode to form a porous anodic oxide film on the side of the gate electrode; removing a portion of the gate insulating using the porous anodic oxide film as a mask so that the gate insulating film extends beyond the gate electrode but does not completely cover the source and drain regions. Thereafter, an ion doping of one conductivity element is performed. The high resistivity region is defined under the gate insulating film.

Abstract: A gas burner for cooking areas includes a lower part and an upper part. The upper part has gas repulsion ducts with gas outlet openings for gas flames. The upper part is rotatably mounted on the lower part by a compressed-air bearing configured to apply a compressed-air cushion to pneumatically lift the upper part off the lower part for allowing contactless turning of the upper part in relation to the lower part about an axis of rotation. The gas repulsion ducts are formed to drive the upper part in relation to the lower part about the axis of rotation by gas flowing through the gas repulsion ducts at positive pressure. Such a configuration makes it possible to evenly distribute the heat of the flames in the periphery of the burner and to minimize minimum gas burner output by using less flames.

Abstract: A gas burner for cooking areas includes a lower part and an upper part. The upper part has gas repulsion ducts with gas outlet openings for gas flames. The upper part is rotatably mounted on the lower part by a compressed-air bearing configured to apply a compressed-air cushion to pneumatically lift the upper part off the lower part for allowing contactless turning of the upper part in relation to the lower part about an axis of rotation. The gas repulsion ducts are formed to drive the upper part in relation to the lower part about the axis of rotation by gas flowing through the gas repulsion ducts at positive pressure. Such a configuration makes it possible to evenly distribute the heat of the flames in the periphery of the burner and to minimize minimum gas burner output by using less flames.

Abstract: A burner assembly includes a number of gas burners each utilizing a radiant ceramic plaque, the burners are disposed in confined combustion chambers where they direct heat towards a heat-receiving surface so that by this arrangement the plaque receives a substantial amount of back radiation.

Abstract: An auxiliary vehicle heater includes a combustion air fan, an intermittently rotating, absorbent wick, a glow plug for initiating combustion and a water jacket surrounding a combustion chamber. Fuel is supplied to the rotating wick by a metering pump and the hot combustion gases enter the combustion chamber and give up heat to the vehicle coolant surrounding it in the water jacket. The coolant is then pumped to the heater core of the vehicle heater. A thermocouple in the exhaust passage of the combustion chamber senses the exhaust temperature and three thermostats in the water jacket provide temperature data to a microprocessor which controls operation of the heater in response to sensed conditions and operator commands.

Abstract: An auxiliary vehicle heater includes a combustion air fan, an intermittently rotating, absorbent wick, a glow plug for initiating combustion and a water jacket surrounding a combustion chamber. Fuel is supplied to the rotating wick by a metering pump and the hot combustion gases enter the combustion chamber and give up heat to the vehicle coolant surrounding it in the water jacket. The coolant is then pumped to the heater core of the vehicle heater. A thermocouple in the exhaust passage of the combustion chamber senses the exhaust temperature and three thermostats in the water jacket provide temperature data to a microprocessor which controls operation of the heater in response to sensed conditions and operator commands.

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 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 gasifier (17) is located at a distance (49) from an air aperture plate (35). At the outlet (42) of the gasifier there is a stationary mixing head (29) having a deflector section (31) and lateral outlets (33). Fuel is supplied coaxially through an opening (55) of the air aperture plate. A flame tube (21) surrounds the gasifier (17) and an electric heater (39) leaving an annular space (40). When the burner is started up, the electric heater (39) is switched on until the gasifier has the necessary operating temperature. Fuel is then supplied. The fuel/air mixture is ignited by an electrode (65). The flame tube (21) extends to the end of the mixing head (29), or only a little therebeyond. A flame is formed at the outlets (33) that touches the flame tube after a short travel, then emerges from it and expands. Because the flame can immediately expand, only little NO.sub.x is formed.

Abstract: A stationary gasifier (17) is located at a distance (49) from an air aperture plate (35). At the outlet (42) of the gasifier there is a stationary mixing head (29) having a deflector section (31) and lateral outlets (33). Fuel is supplied coaxially through an opening (55) of the air aperture plate. A flame tube (21) surrounds the gasifier (17) and an electric heater (39) leaving an annular space (40). When the burner is started up, the electric heater (39) is switched on until the gasifier has the necessary operating temperature. Fuel is then supplied. The fuel/air mixture is ignited by an electrode (65). The flame tube (21) extends to the end of the mixing head (29), or only a little therebeyond. A flame is formed at the outlets (33) that touches the flame tube after a short travel, then emerges from it and expands. Because the flame can immediately expand, only little NO.sub.x is formed.

Abstract: The burner has a motor, a fuel pump and a fan. An easily replaceable component unit (27), the drive shaft (33) of which is coupled to the burner motor, is surrounded by the flame tube (21). The component unit (27) has a drive shaft (33), supported in an adaptor sleeve (37), for driving the gasifier (17). When the burner is started up, the rotatable gasifier (17) is heated by the heater (39). Once the gasifier has reached a predetermined temperature, the supply of fuel takes place through the line segment (19') and through the nozzle (71) to the immediate vicinity of the inner wall of the gasifier (17). Because of the rapid rotation, the fuel is distributed over the entire inner wall of the gasifier (17) and evaporates. Particularly in the mixing head (29), the evaporated fuel mixes with the combustion air flowing in through the opening (77) and is directed radially to the outside by a deflector (31, 31').

Abstract: A ferrofluid seal assembly for providing gas to a rotatable member includes a chamber between the bore of the magnet within the seal and a shaft passing through the bore. Fluid inlet means provides fluid to the chamber. The shaft is hollow from the chamber to one end and communicates with the chamber for providing fluid to a rotable member affixed to the end of the shaft.

Abstract: A fuel gasifying burner comprising a combustion plate having peripheral and bottom combustion surfaces provided with a plurality of gasified fuel blowing openings. The combustion plate is arranged within a combustion cylinder to define therebetween peripheral and bottom gas chambers communicating with each other. A partition plate is arranged within the bottom gas chamber to divide the same into first and second chamber sections. The first chamber section has an inner peripheral open end communicating with an axial open end of a fuel gasifying member rotatably arranged within the combustion cylinder. The partition plate forms an annular flow branching channel at a location where the peripheral and bottom gas chambers communicate with each other. Gasified fuel-air mixture entering the first chamber section is divided into two mixture streams at the annular flow branching channel.

Abstract: A fuel gasifying burner comprising a gas chamber defined between a bottom wall of a combustion cylinder and a combustion plate formed with gasified fuel blowing openings. A plurality of ventilation pipes extend through the gas chamber for communicating an air blowing chamber with an annular air ejection passage defined between the gas chamber and a fuel gasifying member rotatably arranged within the combustion cylinder. First and second mixing promotion cylinders arranged between the ventilation pipes and the gasified fuel blowing openings are spaced from each other to define therebetween a narrow and bent passage through which gasified fuel-air mixture from the fuel gasifying member flows into the gas chamber. A flat gas inflow chamber having a radially outward peripheral closed end is defined between the first mixing promotion cylinder and the bottom wall of the combustion cylinder.

Abstract: Burner for a suspension of fine-grained coal in a liquid, particularly water, which burner operates according to a combination of the rotary burner and toroidal burner principles. The fuel is supplied axially behind a transverse distribution baffle within a conical rotary body. At least the outer rim portion of the inner side of the rotary body forms an angle of 35.degree.-80.degree. with the axis of the burner. At the outer edge of the rotary body there is an annular air supply nozzle for supplying a conically diverging outwardly directed air stream. Outside the air supply nozzle and at a radial distance from it, there is a conical guide baffle (18, 48) which at its outer end may be curved inwardly and which, together with the diverging air stream, serves to produce a positive recirculation of combustion gases, non-combusted coal particles and ash particles in a direction back towards the rotary body in accordance with the toroidal burner principle.

Abstract: The burner has a motor (11), a fuel pump (13) and a fan (15). In the flame tube (81) is a gasification chamber having a gasification chamber housing (75) coaxially located to the flame tube (81), and a housing (75) located at a distance therefrom. The rotor (17) located in the housing (75) can be axially moved with respect to the bearing (29), thereby causing a slot between the axial bearing surfaces (51, 53). Through this slot fuel is ejected into the gasification chamber by the rotation of the rotor (17). The opening of the slot between the axial bearing surfaces (51, 53) depends on the oil pressure which is determined by signals of the heating control 24. The fuel throughput may be controlled in steps or continuously according to the heat requirements. The electric heating (77) is only used during the start phase. In operation of the burner the heat requirements for the gasifying chamber (25) are covered by the recirculation of hot combustion gases through the recirculation gas inlet (73).

Abstract: A coal-water mixture (CWM) burner includes a conically shaped rotating cup into which fuel comprised of coal particles suspended in a slurry is introduced via a first, elongated inner tube coupled to a narrow first end portion of the cup. A second, elongated outer tube is coaxially positioned about the first tube and delivers steam to the narrow first end of the cup. The fuel delivery end of the inner first tube is provided with a helical slot on its lateral surface for directing the CWM onto the inner surface of the rotating cup in the form of a uniform, thin sheet which, under the influence of the cup's centrifugal force, flows toward a second, open, expanded end portion of the rotating cup positioned immediately adjacent to a combustion chamber. The steam delivered to the rotating cup wets its inner surface and inhibits the coal within the CWM from adhering to the rotating cup.

Abstract: A fuel gasifying burner including a combustion cylinder, a rotary shaft extending into the combustion cylinder through its open base, a frustoconical rotary gasifying member connected to the rotary shaft and formed at a lower end of its wall with a bent portion extending outwardly and having at its peripheral end a liquid fuel scattering end, and an inner gasifying member located inside the rotary gasifying member to form a unit therewith and having connected to a lower end of its wall a fuel air-mixture gas diffusing wall extending outwardly a greater distance than the bent portion of the rotary gasifying member. The inner gasifying member is formed at its forward end with an air supply opening communicated through an air passage with an air blowing chamber. An annular flame ejecting upright wall is formed contiguous with a fuel-air mixture gas diffusing wall and provided at its end with a liquid fuel rescattering portion.

Abstract: In the construction of a liquid fuel burner in which liquid fuel is subjected to two-staged combustion, active and passive expedients are preferably combined for complete burning of the liquid fuel. The active expedient employs specified edge construction of a fuel scatter ring for production of ideally atomized fuel whereas the passive expedient employs a barrier construction arranged at the open front end of a combination cylinder for effective prevention of fuel drop causable of incomplete fuel burning.

Abstract: An improved fuel burning assembly particularly adapted for use with a boiler having a fire box situated below an array of boiler tubes. The assembly discharges a number of spaced rotating streams of minute droplets of a flowable fuel both laterally and longitudinally into the fire box to intermix with a stream of air that is moving rearwardly therein. The fuel air mixture when burning blankets substantially all the boiler tubes with a sheet of flame. Due to such flame contacts substantially all of the boiler tubes are heated uniformly thereby, rather than only a portion of the boiler tubes being contacted by the flame as occurs in a boiler when a conventional burner assembly is used. As a result of the flame distribution and uniform heating of the boiler tubes, an increased thermal efficiency is attained in the operation of the boiler on which the burner assembly of the present invention is used.

Abstract: A rotary burner has fuel discharge nozzles arranged exclusively in the high velocity zone of combustion air flow. The resulting annular flame pattern has a central region adjacent to the burner hub which is essentially combustion free.

Abstract: A burner (1,29) for the combustion of powdery fuels, in particular coal-dust, comprises a central duct (9,37) to supply a jet of core-air (13,41), a fuel channel (12,40) to supply the fuel and a casing channel (5,6; 31) to supply secondary air (7,8; 36).In order to make such a burner (1,29) also suitable for lesser power ranges, a widened range of regulation and less sensitive to a wide coal-dust band, the discharge means of the fuel channel (12,40) is designed as an annular nozzle (23,53) of which at least one of the two circumferential walls (19,47) is rotatable and driven, and the discharge means of the central duct (13,41) being so designed that the jet of core-air (13,41) is directed at least in part outwardly against the discharging fuel for the purpose of deflection into the region of the secondary air (7,8; 36).

Abstract: A rotary burner for liquid fuels includes a casing having a nozzle in which is rotatably mounted a fuel atomizer. The fuel atomizer is made in the form of a cup, which together with an outlet portion of the nozzle forms an annular convergent channel connected to a fuel supply means. On the external surface of the cup, near to an edge thereof, a circular row of vanes is mounted, the vanes being shaped as wedges whose bases face the edge of the atomizing cup.

Abstract: A liquid fuel gasifying burner including an inner gasifying member connected to a rotary gasifying member of the frustoconical shape so that the two members can rotate as a unit. The inner gasifying member is formed with an air port in the central portion of its upper end and open at its lower end, and the rotary gasifying member is closed at its upper end and open at its base and rotatably mounted in a combustion cylinder open at its upper end and formed with an air blowing chamber in the central portion of its bottom. A fuel-air mixture passage is defined between the outer circumferential surface of the inner gasifying member and the inner circumferential surface of the rotary gasifying member, and a liquid fuel spreading surface having a liquid fuel scattering portion at its outer periphery is formed on the upper end of the inner gasifying member. A liquid fuel feed line opens at its forward end close to the liquid fuel spreading surface.

Abstract: A liquid fuel burner for burning liquid fuel in gasified form including a cylindrical main body having a flame blowoff nozzle and an inner bottom wall at opposite ends, a gas chamber, a combustion plate formed with a multitude of gasified fuel blowing openings, a fuel gasifying member, a fuel diffusing member, an air supply duct, a fuel supply line, an air ejection chamber and a rotary shaft supporting the fuel gasifying member and fuel diffusing member for rotation within the cylindrical main body. An annular wall is secured to and extends inwardly from the inner wall surface of the combustion plate in a position nearer to the inner bottom wall than the gasified fuel blowing openings, and a liquefied fuel flow preventing plate is secured at one end to the inner wall surface of the cylindrical main body in a position near to the flame blowoff nozzle and free at the other end to define a liquefied fuel sump between the inner wall surface of the main body and the liquefied fuel flow preventing plate.

Abstract: An oil burner which operates on all grades of fuel oil, even dirty oil, has a rotating burner element spinning in a hollow container, with the fuel oil being fed to the burner element. Air is fed in from below. The burner element is of fan-like form with radially extending vanes, and causes forcible recirculation of the burning gases through the fire zone repeatedly, so as to ensure complete combustion.

Abstract: The disclosure relates to burners with a burner nozzle and a primary air nozzle, the nozzles being jointly axially offset in relation to a secondary air nozzle. The primary air nozzle is in the form of, or is mounted to, an elongate tube which, in its turn, is shiftably mounted on and extends through an openable scuttle and a coronal portion, located inside the scuttle, of a primary air supply duct. The tube is axially shiftable between an operative position and an inoperative position. The burner and its burner nozzle are mounted in the elongate tube and are disposed, together with the tube to move as a unit out from the coronal portion on opening of the scuttle. The elongate tube has at least one air passage which, in all adjustment positions of the tube, maintains communication between the primary air nozzle and the coronal portion of the primary air supply duct.

Abstract: A gasified liquid fuel burner having a combustion chamber in the form of a cylinder closed at the bottom, a hollow fuel gasifying member of a substantially conical shape located in the combustion chamber for rotation and having an open end formed therein with an obliquely outwardly turned portion, an air blast supply duct inserted in the fuel gasifying member, a fuel supply line for supplying a liquid fuel to the inner surface of the fuel gasifying member, a gas chamber formed in the combustion chamber in a manner to be juxtaposed against the open end of the fuel gasifying member to define a gasified fuel-air mixture ejection opening between the gas chamber and the obliquely outwardly turned portion of the fuel gasifying member, and a cylindrical gasified fuel-air mixing member provided in the gas chamber and spaced apart a small distance from the open end of the fuel gasifying member.

Abstract: Disclosed is a rotary burner of the type wherein the liquid fuel (to be referred to as "the oil" hereinafter in the specification) is atomized by uniform and stable ultrasonic waves and the oil particles are prevented from being sprayed outwardly so that the non-uniform distribution of concentrations of oil particles results, whereby the uniform combustion may be ensured.

Abstract: An improved embodiment of the rotary fuel-steam burner system described in copending application Ser. No. 664,214 filed Mar. 5, 1976, now U.S. Pat. No. 4,035,133.A fuel flow set point signal is delivered to a diaphragm motor valve to set a desired fuel flow-area therein; and, a differential pressure regulator maintains a correspondingly desired pressure drop thereacross.In a sonic flow embodiment regulator steam flow is controlled by a differential pressure regulator having its low pressure side connected to a ratio control device and its high pressure side connected to a downstream point in the steam line.

Abstract: An improved method and apparatus are described for burning gaseous or vaporizable fuels, such as kerosene or other light fuel oils or gases. The burner provides for an efficient and complete burning of the fuel in a small combustion space and at variable rates. The burner utilizes a rotating fan to form a spiral or helical air flow within the combustion chamber. An interconnected rotating fuel nozzle for spraying the fuel into the spiral air path may be used or a stationary nozzle directing the fuel toward the fan. This provides for a long residence time of the fuel and air mixture providing a complete combustion of the mixture within the relatively small volume of the combustion chamber.

Abstract: A system and method for controlling a rotary burner of the type in which attempts have been made to maintain predetermined differential pressures between steam and fuel delivered thereto. The fuel flow is adjusted to provide a given heat release; and without regard to pressure, the steam flow is adjusted in accordance with a predetermined ratio to correspond to the given fuel flow.

Abstract: A burner wherein a fuel gasifying member is rotatably mounted in a main body of the burner made of a thin metallic material and receiving an air supply duct inserted through one side, a gasified fuel-air mixing plate for scattering the liquid fuel in atomized particles into said main body is integrally mounted on said fuel gasifying member and a gas wall plate connected at one end to the air supply duct is provided, a swirlingly flowing air film of air blast in the main body of the burner is forcedly circulated to cool said main body from said air supply duct through an air supply opening and along the inner wall surface of said main body, an air shielding wall for preventing the stream of air blast from directly impinging on said main body is disposed in said main body, a combustion plate provided therein with a multitude of gasified fuel blowing openings is disposed in said main body so as to define an annular gasified fuel blowing passageway, an ignition facilitating device is disposed inside of said combu

Abstract: A power plant for producing heat. A frame is rotatably mounted within a container with an inertia wheel mounted to and rotatable with the frame. A fuel storage tank mounted within the frame is connected between and to an external source of fuel and a plurality of fuel injectors mounted to the inertia wheel. Cooling means within the container cover the frame and at least a portion of the inertia wheel with a combustion chamber provided within the container above the cooling means. Igniting means mounted to the container projects into the combustion chamber and is operable to ignite fuel intermittently injected into the combustion chamber by the injectors mounted to the inertia wheel. Pumping means provided on the frame is operable to pump fuel from the storage tank to the injectors in a timed relationship to the position of the injectors relative to the cooling means and combustion chamber. Heat is withdrawn from the container resulting from the combustion of the fuel.

Abstract: A burner wherein a fuel gasifying member is non-rotatably mounted in a main body of the burner and maintained in communication with a gas chamber formed in an outer marginal portion of the main body of the burner, and liquid fuel scattering means is rotatably mounted at an open end portion of the fuel gasifying member for scattering a liquid fuel in minuscule particles into the interior of the fuel gasifying member and the main body of the burner through a scattering gap. The liquid fuel thus scattered in the main body is ignited and burns to heat the fuel gasifying member in which the fuel supplied by the liquid fuel scattering means under the influence of an air blast supplied under pressure through an air supply duct is quickly gasified and forms a mixture of gasified fuel and air which is ejected through the gas chamber to sustain combustion of the liquid fuel in gasified form. A cooling chamber may be provided adjacent an inner wall plate of the main body of the burner.

Abstract: A generally cup-shaped fuel slinger concentrically secured by its base portion to a rotatable shaft located in a combustion chamber and having a radially inwardly extending lip at its open end provided with a plurality of circumferentially spaced notches opening toward the shaft and spaced at their bottommost portion from the inner annular surface of the slinger side wall. Fuel is delivered by a single tube through the open end of the slinger and is centrifuged outwardly against the inner annular surface of the slinger side wall, and thereafter delivered from the slinger to the combustion chamber through the notches. The slinger is located between a radial turbine and a compressor of a gas turbine engine. The fuel supply tube projects axially through a vane in the diffuser, radially along the diffuser, and then axially into the fuel slinger between the lip and the outer periphery of the adjacent shaft portion. In the disclosed embodiment the notches are generally V-shaped.