Abstract: An ultrasonic atomizing burner for smaller heating apparatus particularly for mobile spaces, such as motor vehicles comprises an atomizer which has a fuel inlet and which is equipped with an atomizer discharge plate and a structure skirting the plate which defines a combustion air flow space for 1% at most of the combustion air amount. This structure includes a cylindrical combustion chamber having a forward discharge end with a flame baffle and with a heating gas outlet tube connected to the discharge end for the axial flow of the combustion gases. The combustion chamber has an ignition zone which is provided with wall bores for admitting primary air and it includes a spark plug in the ignition zone for igniting the combustion gases and the primary combustion air. The combustion chamber also has a burnout zone which is provided with wall slots for admitting secondary air downstream of the primary air.

Abstract: A burner for air heaters comprises a first wall structure defining an ignition chamber with an ultrasonic atomizer discharging into the ignition chamber and with means for delivering primary air into the ignition chamber for ignition by suitable ignition device to form an igniting gas mixture. The construction includes a second wall arrangement which is adjacent the ignition chamber and which defines a primary combustion chamber which has a passage for the ignited gas mixture from the ignition chamber and also for secondary air so as to complete the combustion in the main combustion chamber. The main combustion chamber in turn is connected downstream and into an exhaust diffuser in which the completely burnt gases are delivered to a place of use for heating an area such as a space in a motor vehicle.

Abstract: A combustion apparatus is fitted to the top of an oil burner having a single nozzle for the simultaneous introduction of oil and water by means of compressed air. The apparatus includes a combustion chamber defined by an inner vessel open at both ends with one end being fitted to the burner. An outer vessel is co-axially 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. The inner vessel is provided with a plurality of holes and a baffle is located within the pre-heating chamber in overlying relation with respect to the holes. Pressurized air is introduced into the heating chamber, around the baffle, and through the holes into the interior of the vessel to compress the flame of the water-oil fuel emulsion forcing it to swirl and remain in the vessel so that the combustion takes place at a temperature between 700.degree. and 1,000.degree. C.

Abstract: A combustion device, especially for slow-to-react pulverized coal or coal dust.

Abstract: NO.sub.x emissions are reduced in the combustion of fuels by carrying out the combustion in at least four serially connected combustion zones, including at least three fuel-rich zones followed by a fuel-lean zone. In accordance with another aspect of the present invention, SO.sub.x emissions are reduced in the burning of a normally solid fuel, containing significant amounts of SO.sub.x precursors, by adding a sulfur scavenger to the fuel and thereafter burning the fuel in at least four serially connected combustion zones, including at least three fuel-rich zones followed by a last fuel-lean zone, and carrying out the combustion of the fuel in at least four combustion zones.

Abstract: NO.sub.x emissions are reduced in the combustion of a fuel, containing significant amounts of NO.sub.x precursors, by carrying out the combustion in at least three, serially connected combustion zones in open communication with one another, including at least two fuel-rich zones and a last fuel-lean zone and in the presence of a combustion catalyst added to the fuel adjacent the upstream end of the first of the fuel-rich zones. SO.sub.x emissions are also reduced when burning a fuel, containing significant amounts of SO.sub.x precursors, by additionally adding a sulfur scavenger to the fuel adjacent the upstream end of the first fuel-rich zone.

Abstract: A device for gas jet cutting of materials, comprises a head (1), the case of which accommodates a primary and a secondary combustion chambers (3 and 4) interconnected by an axial passage (5), and injectors (9, 10, 11, 12) for supplying fuel and oxidizer into said combustion chambers (3 and 4). A nozzle (7) mating with the primary combustion chamber (3) ejects a cutting gas jet, and an igniter (8) is fitted to the secondary combustion chamber (4). The oxidizer supply injector (12) communicates with the primary combustion chamber (3) through the axial passage (5).

Abstract: A burner for heating air flowing in a passage in which the burner is disposed comprises a tube connected to the gas supply. The tube has mixing plates with flow apertures for the air secured to it to diverge from each other conically in the direction of air flow and is provided with gas outlet apertures between the mixing plates. The burner also comprises ignition means for the gas. The tube is in the form of a circular annulus and has gas outlet apertures in circumferential directions. The mixing plates consist of an outer conically diverging and an inner conically converging annular plate, the plates being at least partially bounded over their axial length by an air guide plate which converges conically in the direction of air flow and which is secured to the wall of the air passage for axial displacement. The ignition means are disposed in front of the gas outlet apertures which are arranged on a circle or a plurality of concentric circles.

Abstract: A staged, high efficiency burner for gaseous, liquid or pulverized solid fuels (including fuels having a high nitrogen content) in which NOX emissions are minimized. The burner includes a burner basket having a base including a throat and a concentric, tubular, frustroconically shaped wall that defines a primary combustion space. The fuel and primary air of about 75% of stoichiometric air are introduced into the basket which has a length so that the fuel has a residence time therein of between about 0.1 to 0.5 second. Secondary air is introduced into the flame downstream of the basket in the form of a multiplicity of individual air streams which are oriented to penetrate the flame and spin it about its axis so as to maintain a substantially cylindrical flame periphery.

Abstract: This relates to a method of operating a burner under conditions of stoichiometric combustion, wherein liquid fuel and combustion air are combined in a essentially constant ratio within a mixing and atomizing chamber, whereby a negative pressure is produced within said chamber owing to the guiding and metering of the air, said negative pressure serving to draw in fuel into said chamber. Furthermore, the invention relates to a burner assembly for carrying out the method.

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 atomizer nozzle for continuous fuel injection is provided. The nozzle can serve as a main injection nozzle or as an igniter for combustion chambers, and is provided with a single-hole fuel nozzle, and an annular gap for possible additional air supply located coaxially therebefore. The chamber or space between the nozzle opening and the annular gap is connected by pressure equalization openings with the combustion chamber behind or after the annular gap. The pressure equalization openings are represented and defined by individual spacers between the fuel nozzle body and the air nozzle ring.

Abstract: A multi-fuel industrial heating burner having an exhaust velocity of about 15,000 feet per minute. The fuel is first burned in a swirling toroidal recirculation zone and flows into the burner tile and shear mixes with a counter-swirling flow of combustion air flowing along the burner tile. As the flows shear mix, additional combustion air is provided to the central burning gases and the rotational momentum of the swirling flows is dissipated. The burner discharge gases flow axially without swirl.

Abstract: A method for substantially reducing emissions of nitrogenous compounds such as NO.sub.x formed during fuel combustion. The fuel is combusted with an oxygen-containing gas in an amount from about 45 to 75% of the total stoichiometric amount of oxygen required for complete combustion of the fuel. The resulting mixture of fuel and combustion products, including NO.sub.x, is maintained at a temperature of at least 1800.degree. K. for a time sufficient to reduce the NO.sub.x content of the mixture to a desired level. Thereafter, combustion may be completed in one or more additional zones at a temperature within the range of about 1600.degree. to 2000.degree. K. Alternatively, the mixture of combustion products and fuel having a reduced NO.sub.x content may be used for other applications without further combustion. For certain embodiments of the invention, various particulates may be added to the combustion zone so as to enhance the rate at which the NO.sub.x is destroyed.

Abstract: A ceramic combustion chamber having air inlet ports and a double wall formation in the region of each inlet port. The two walls of the formation have a cavity between them which communicates with the inlet port. The double wall formation may be formed by an annular slot in the wall of the part. Alternatively, the double wall formation may be formed by two nested but spaced apart shells joined together at one end of the combustion chamber. The combustion chamber may be made by compressing ceramic powder in two steps to create a compact having an internal lost core or cores which are burned out, after which the ports are formed. Alternatively, the combustion chamber may be made by die casting ceramic powder around cores having the shape of the desired air inlet ports, after which the cores are burned out.

Abstract: A burner for burning pulverized fuel, especially pulverized lignite or coal, comprises a combustion chamber 1, and an ignition chamber 2 having an ignition burner 9. A supply line 5 for powder and air for pneumatic conveyance debouches into the ignition chamber 2. Further combustion air may be fed through outflow means 8 into the combustion chamber. To achieve a short flame as well as an improved homogeneity of the distribution of the mixture, the burner includes a distribution pipe 3, the surface of which being provided with a large number of openings 11. The supply line 5 for powder and conveying air terminates into the distribution pipe 3, preferably a rotating movement being imparted to the mixture flowing along the wall of the distribution pipe 3.

Abstract: A method and apparatus for combustion of fuel wherein in two mutually perdicular air swirls are used. In the cylindrical section of the combustor, a horizontal swirl with respect to the combustor is set in motion. The conical section in conjunction with the cylindrical section forms a vertical swirl with respect to the combustor. Notably, the combustor is not dependent upon orientation in a gravity field.

Abstract: A burner construction for low emission burners in which the primary fuel is injected with air in an annulus into the upstream end of the burners so as to cause a significant recirculation of the fuel and air mixture adjacent to the end cap, the secondary fuel is injected into the burner in a small angle spray at a point substantially spaced from the end cap and large combustion and/or dilution holes in the burner wall a small distance upstream of the secondary nozzle are sized to produce an additional recirculation in the primary fuel and air around the secondary nozzle with this additional recirculation in the direction opposite to the first recirculation.

Abstract: A burner having a burner body in which combustion air is injected in an air flow pattern which establishes a relatively stagnant air region positioned within the flow of combustion air. A pilot flame injector is positioned to generate a pilot flame extending into the stagnant air region. The pilot flame can, thus, be maintained during the operation of the burner because the stable air conditions within the stagnant air region minimize disruption of the pilot flame by the flow of combustion air.A method for maintaining a uniform pilot flame within a burner operating over a range of combustion air flow rates by introducing combustion air into the burner and providing the combustion air with a flow configuration that establishes a stagnant air zone within the burner that is relatively independent of the flow rate of the combustion air. The pilot flame is then positioned within the stagnant air zone.An injector for feeding finely divided fuel to a burner.

Abstract: A burner having a burner body in which combustion air is injected in an air flow pattern which establishes a relatively stagnant air region positioned within the flow of combustion air. A pilot flame injector is positioned to generate a pilot flame extending into the stagnant air region. The pilot flame can, thus, be maintained during the operation of the burner because the stable air conditions within the stagnant air region minimize disruption of the pilot flame by the flow of combustion air.A method for maintaining a uniform pilot flame within a burner operating over a range of combustion air flow rates by introducing combustion air into the burner and providing the combustion air with a flow configuration that establishes a stagnant air zone within the burner that is relatively independent of the flow rate of the combustion air. The pilot flame is then positioned within the stagnant air zone.An injector for feeding finely divided fuel to a burner.

Abstract: In a liquid fuel combustion apparatus having a horizontal combustion cylinder including a peripheral wall provided with perforations through which air is supplied in the form of jets. A fuel supplying system includes a fuel reservoir provided at the lowermost portion of the combustion cylinder. Vaporized fuel is mixed with the air jets and is subsequently burnt as it is carried horizontally.

Abstract: A liquid fuel combustion apparatus comprises a combustion cylinder, a fuel reservoir, a housing, a blower and an electrical ignition heater. The reservoir is disposed inside the cylinder to store a liquid fuel supplied from outside of the cylinder. The housing is disposed outside the cylinder to create a space therebetween and has an end wall opposite to an end wall of the cylinder. The blower is disposed outside, and in a spaced apart relation to, the housing and supply air to the space. The heater is supported by the end walls and ignite liquid fuel stored in the reservoir.

Abstract: A combustor for a gas turbine engine includes a metal engine block including a wall portion defining a housing for a combustor having ceramic liner components. A ceramic outlet duct is supported by a compliant seal on the metal block and a reaction chamber liner is stacked thereon and partly closed at one end by a ceramic bypass swirl plate which is spring loaded by a plurality of circumferentially spaced, spring loaded guide rods and wherein each of the guide rods has one end thereof directed exteriorly of a metal cover plate on the engine block to react against externally located biasing springs cooled by ambient air and wherein the rod spring support arrangement maintains the stacked ceramic components together so that a normal force is maintained on the seal between the outlet duct and the engine block under all operating conditions.

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 device and process for the treatment of materials in different phases, one material being in a fluid phase and another in a gaseous phase, wherein the material in fluid phase is introduced as a stream within the axis of the gaseous phase in helicoidal flow for subsequent passage through a confined zone whereas a substance to be treated is introduced at the level of the smallest section of the confined zone.

Abstract: A thermal processing system and method which is directed to the controlled high rate of exchange of thermal energy between solid matter or liquids and a gas which functions simultaneously as the thermal energy transport medium and the physical transport medium. The system includes a primary processing device which is provided with means for introducing the solid or liquid matter in a finely divided state and a means for introducing the carrier gas so as to create a very high velocity stream together with means for supplying and/or controlling the thermal energy input(s) to the system by operating on such carrier gas. The system also includes means for continuously removing the resulting products (solids, liquids, gases and in some instances, energy) in such a way that a continuous stream process results. The system is also provided with any necessary or desirable auxiliary devices to ensure that all discharges from the process are substantially cleaner than required by any applicable environmental standards.

Abstract: A method of scrubbing reaction products resulting from flame burning of fuels containing impurities such as sulfur compounds, chlorine compounds, and fluorine compounds. The scrubbing is accomplished by the addition to the fire chamber of additives which bind the impurities. The additives are supplied to the burner flame by way of a gaseous and/or liquid carrier medium flow, accompanied by the formation of a veil surrounding the burner flame.

Abstract: A burner assembly for the smokeless flare burning of low calorific value gases, or diluted hydrocarbon gases, which comprises a plurality of separate burner heads arranged in a horizontal array, each of the burner heads being mounted on top of a vertical pipe through which the low calorific gases are supplied. A plurality of hollow radial arms are inserted into the wall of the head, arranged in equally-spaced array, each of the arms having a plurality of ports in the top surfaces, near the ends of the arms. These ports are of selected size and selected angle of their axes, which are tilted inwardly towards the central axis of the burner heads. Additionally, there is between each pair of arms at least one port drilled downwardly from the inside of the burner head, at a selected angle, so that jets of gas will impinge downwardly on an annular plate positioned beneath the arms, to close off the vertical flow to the space between the arms.

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: An oil burner including an oil atomizing nozzle to be mounted upstream of a ransverse wall in a cylindrical flame tube and to discharge oil through an aperture in the wall through which air also passes into a cylindrical mixing tube positioned co-axially within the flame tube and open at its downstream end. The flame tube has a length at least twice its diameter and a diameter between 2.0 and 2.5 times the diameter of the mixing tube. At least one passage adjacent the transverse wall communicates between the interior of the flame tube and the interior of the mixing tube to recirculate combustion gases from the downstream end of the mixing tube to the upstream end thereof. The peripheral wall of the mixing tube adjacent its downstream end is perforated.

Abstract: A pilot for a 1 to 2 million btu/hr. gas burning ignitor having a chamber for mixing gas and air in combustible proportions with an annular flame retaining and stabilizing device at its outlet. This device comprises two conical surfaces configured together in back-to-back relation within a cylindrical shroud, one a converging inlet to a restricted flow area and the other a diffusing outlet surface therefrom with a sharp circumferential lip inbetween. A distribution head at the inlet to the mixing chamber directs jets of gas at the lip of said cones which aspirate turbulent air through ports in the wall of the chamber. A high voltage elecrode ingites the gas/air mixture at the cone lip. A ported extension of the mixing chamber downstream of the stabilizing device contains the pilot flame and shrouds additional aspirated air for control of secondary combustion in the pilot.

Abstract: A burner having main air ports for issuing a secondary air at a relatively high flow velocity, and auxiliary air ports for issuing a secondary air at a relatively low flow velocity located upstream of the main air ports with respect to a stream of a gaseous fuel or a preformed mixture of fuel and primary air in which the fuel is enriched over and above a flammability limit. The secondary air issuing from auxiliary air ports may have its flow velocity reduced by utilizing speed reducting compartments formed in a combustion chamber or recesses formed in walls of the combustion chamber. Flame stabilizing plates may be provided near the auxiliary air ports to extend substantially perpendicularly to the stream of the gaseous fuel or the preformed mixture of fuel and primary air.

Abstract: An improved fuel burner particularly adapted for domestic use and capable of burning fuels such as fuel oil and the like with extremely high efficiency and low pollutant output is comprised of a pair of plenum type atomizers (26,26'), each having a convex surface onto which the fuel is flowed for atomization, the atomizers (26,26') being disposed at the end of a flame tube (3) which in turn is located within a blast tube (1), said atomizers (26,26') further being disposed symmetrically with respect to the axis of both the flame tube (3) and the blast tube (1) whereby the spray output from the atomizers is discharged into the flame tube (3) to create a stable flame front that can be readily ignited by a spark type of ignitor (18). The atomizers are provided with one or more apertures (29') through which atomizing gas is passed to generate the spray, and air access ports (12,12',13) are located along the flame tube to provide the necessary air to complete the combustion process.

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 sheet laminate is utilised in the manufacture of a combustion chamber for a gas turbine engine. The laminate has passages therethrough, which connect with ambient atmosphere via holes. The arrangement creates local relatively thick portions or lands which cause stress concentrations along the passages and lines of holes. Therefore pockets are machined in the rear face of each land, so as to reduce the differences in thickness of the laminate and thereby ensure the more even distribution of stresses.

Abstract: Air heater having an outer manifold and an inner combustion chamber with a common longitudinal axis, and a burner in the rear end of the chamber, of which the manifold has an air inlet in its rear end and a constricted air outlet in its front end, and the combustion chamber has in its peripheral wall a plurality of ports through which to divert part of the air from the manifold into the chamber for its heat-up by the burner flame therein and discharge through the open end of the chamber.

Abstract: An oil burner in which a liquid fuel oil is vaporized in a heated vaporizing chamber connected through an apertured partition to a multiple concentric shelled combustion chamber.

Abstract: A structure placed in the fire-box of a furnace to improve combustion comprises a plurality of stainless steel strips which are supported on a frame in position to be heated to incandescence by the flame of the burner. At least some of the strips are twisted in corkscrew manner. In one embodiment, twisted strips alternating with untwisted strips are hung on a cross piece of the frame on the side facing the burner. A perforated metal sheet is mounted on the back side of the frame. In another embodiment horizontally extending twisted strips are supported between spaced inner and outer arched supports which extend up from runners resting on the floor of the fire-box. A perforated metal sheet is applied over the outside of the outer supports.

Abstract: A mobile heater for aerospace ground equipment includes a diesel engine for continuously driving a centrifugal blower for introducing air into a plenum chamber so that the air is not contaminated by the diesel engine. The diesel fuel is utilized with a unique burner arrangement, which enables burning within a burner body or can without build up of carbon, having a portion of the air supplied to the plenum chamber supplied thereto. The hot products of combustion from the burner arrangement flow into a core of a heat exchanger where they are directed through longitudinal spiral slots which terminate inside of a shell of the heat exchanger from which they are vertically exhausted upwardly through an exhaust stack. Ventilating air from the plenum chamber is directed through a nest of formed arcuate tubes, which have common walls with the longitudinal spiral slots whereby heat is transferred through the common walls to heat the ventilating air.

Abstract: A multiple fuel burning system that may be employed in conjunction with a furnace includes a first annular tubular conduit connected to a source of pressurized fluid and a second annular conduit concentric with the first annular tubular conduit and coupled to a source of pressurized fuel. A third annular tubular conduit is also included that is concentric with the first and second tubular conduits but of a lesser diameter so as to be within the first and second annular tubular conduits. The third annular tubular conduit is connected to a source of heat retaining liquid such as water or the like. The first, second and third tubular conduits define an elongated combustion chamber with three nozzles mounted at one end. Two of the three nozzles are connected to a source of combustible fuel such as fuel oil. The third nozzle may be connected to a source of pulverized combustible fuel.

Abstract: A method of producing a hot gas flow by combustion of preferably liquid fuels, by the following steps:(a) atomizing the liquid fuel to form fine particles;(b) further atomizing the thus generated fuel particles with the aid of combustion air supplied as atomizing medium, and reducing the mean fuel particle diameter to less than one-half of the mean diameter obtained in step (a);(c) burning the fuel-air mixture within a flame cone extending on an axis A, under stoichiometric conditions or with an excess of oxygen within an air duct;(d) introducing a stream of cold air to be heated or of another medium, optionally including components adapted to be oxidized, in a plane E extending substantially perpendicularly to axis A.Further, the invention relates to a hot gas generator or incinerator for carrying out the method, comprising a straight air conducting pipe which has coaxially positioned therein a burner for liquid fuels, including a two-stage atomizing assembly for the liquid fuel.

Abstract: A burner body defines a combustion zone and a secondary dilution zone. A first inlet opening leads to the combustion zone to admit fuel and air while a second inlet opening leads to the secondary dilution zone. The burner body contains a tertiary dilution zone connected to a third inlet opening. The secondary dilution zone is positioned downstream from the combustion zone and the tertiary dilution zone is positioned downstream from the secondary dilution zone.The flow areas of the first inlet opening and the second inlet opening is arranged to have a constant ratio. An air passage supplies air to the first, second and third inlet openings and a flow controller is positioned to control the air flow through the third inlet opening. When the flow controller is closed, air flows from the passage through the first and second inlet openings, while, when the flow controller is open, air flows from the passage through the first, second and third inlet openings.

Abstract: Apparatus for burning combustible particles to heat circulated air. The apparatus includes an upright housing containing a removable liner which forms the combustion chamber of the burner, and a perforated, intermediate wall member which forms, with the walls of the housing and the liner, outer and inner gas-receiving spaces, respectively. Air injected into the housing passes from the outer, into the inner gas-receiving space, where the gas is directed, through tuyeres in the liner, into the chamber, substantially tangentially to the wall thereof, producing a gas vortex therein. Particles introduced into the chamber through an upper opening are combusted primarily in the chamber's upper core region with such combustion being supported by, and acting to heat, vortexing gas within the chamber prior to its discharge through a lower chamber opening.

Abstract: A gas burner system for providing a thin, flat flame for use in a long narrow combustion space, has a first air supply plenum which has a long narrow rectangular cross-section, which is placed above a second plenum or combustion chamber of substantially the same cross-section. At the junction between the first and second plena there are longitudinal projections inwardly from both long walls of the second plenum, forming a long narrow rectangular inlet to the second plenum. A burner assembly comprising an elongated flattened pipe having a plurality of short air baffles welded on each side is supported in this narrow inlet to the second plenum and substantially in the center thereof. The overall width of the burner assembly is less than that of the inlet so that there are two longitudinal gaps between the burner assembly and the projections for the passage of combustion air. There are two sets of ports in the lower edge of the flattened pipe.

Abstract: An oil burner for heating installations is provided, having a burner housing comprising a perforated evaporating tube which is equipped with a circular series of blades to impart a twisting motion to the air and a cone-shaped guiding piece to impart an injection effect to the air, and which has attached thereto and maintained at a fixed distance therefrom a perforated, disk-shaped baffle. The present burner arrangement provides for a complete and soot-free, stoichiometric combustion wherein a blue flame is generated with extremely low level of noise.

Abstract: A gas turbine combustor which may be of cylindrical or annular configuration has a concave inner surface at its upstream end, and means for directing combustion air along the concave surface towards the middle thereof so as to form a stable vortex pattern near the concave surface, the vortical flow being in an upstream direction in the region of the periphery of the concave surface. A fuel injector for directing fuel droplets into combustion air flowing over the surface may be located at the middle of the concave surface.

Abstract: A gas turbine engine combustor assembly of annular configuration has outer and inner walls made up of a plurality of axially extending multi-layered porous metal panels joined together at butt joints therebetween and each outer and inner wall including a transition panel of porous metal defining a combustor assembly outlet supported by a combustor mount assembly including a stiffener ring having a side undercut thereon fit over a transition panel end face; and wherein an annular weld joins the ring to the end face to transmit exhaust heat from the end face to the stiffener ring for dissipation from the combustor; a combustor pilot member is located in axially spaced, surrounding relationship to the end face and connector means support the stiffener ring in free floating relationship with the pilot member to compensate for both radial and axial thermal expansion of the transition panel; and said connector means includes a radial gap for maintaining a controlled flow of coolant from outside of the transition pa

Abstract: In a tank immersion heating system a conical casing surrounds the high intensity fuel burner with its narrower end communicating with the immersed tube to introduce combustion air with progressively increasing velocity so that although flame "lift-off" is avoided combustion takes place mainly within the tube.

Abstract: A fuel combustion apparatus comprising a double concentric combustion cylinder having an outer cylinder and an inner cylinder concentric with, and shorter than, the outer one, said inner cylinder being located in the upstream portion of the space and extending axially to form an annular space between itself and the outer cylinder, a plurality of fuel injection valves installed in a circular arrangement at the head of the annular space, combustion air swirlers mounted around the fuel injection valves, one for each, with the same angle of swirl in a given direction, another combustion air swirler installed at the inner end of the inner cylinder and having an angle of swirl in the direction reverse to that of the said swirlers, and a plurality of air holes formed confinedly in the wall portion of the outer cylinder surrounding the inner end of the inner cylinder and also in the wall portion of the outer cylinder at a distance of not less than the diameter of the outer cylinder downstream from the said first air

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.