Abstract: In a fluent fuel burner using a flame anchor plate, secondary air from a plenum leaves the plenum through a restricted passage so that the secondary air is at high velocity and correspondingly low pressure and this low pressure is used to suck the flame to the rim of the anchor plate. Two dual fuel burners are described in which a gaseous fuel introduction means has an enlarged end portion which extends from within the air plenum into a combustion space, the said portion having slots in it to allow primary air to enter the said portion to serve as primary air for combustion, and which has associated with it a flame anchor plate. The plenum has a wall on the combustion side with a hole in it. In one embodiment, the anchor plate overlies the rim of the hole so that a narrow annular passage defined between the plate and the wall directs the secondary air in a radial blast.

Abstract: A diesel fueled engine coolant heater for vehicles powered by a liquid cooled diesel engine. The heater is adapted to burn diesel fuel ordinarily carried by the vehicle. All electrical components of the system are powered by the vehicle electrical system. The heater supplies a source of thermal energy for engine coolant fluid in order to provide for rapid starting of the vehicle engine in cold temperatures and, if needed, to provide heat for the passenger compartment of the vehicle while the vehicle engine is stopped.

Abstract: A radiant tube burner mixes liquid fuel and/or gaseous fuel with air for combustion in a radiant tube to produce a quiet and stable luminous flame through the entire length of the radiant tube. A flame holding plate is positioned within the radiant tube to define a feed zone and a combustion zone. A liquid fuel nozzle positioned centrally in the plate directs fuel through the plate and into the combustion zone. The plate defines a series of apertures circumscribing the nozzle and another passage outward from the series of openings and concentric therewith. Combustion air is proportioned and admitted to the combustion zone through the series of openings and the passage. Gaseous fuel may be admitted to the combustion zone through the series of openings.

Abstract: A high capacity, quiet burner for a hot air heating system for use in heating the top and bottom ends of a plastic coated carton, or the like, and which has a tubular burner body provided with a chamber therein which is open at an outlet end and enclosed at an inlet end. A burner nozzle is mounted in the burner body chamber adjacent the inlet end, and a mixture of primary air and fuel is conveyed into the burner nozzle and ignited by a spark plug. Secondary air under pressure is conveyed into the burner body chamber, for flow around the burner nozzle for heating the secondary air and for mixing the secondary air with combustion gases formed by the combustion of the mixture of primary air and fuel in the burner nozzle, and for subsequent discharge through the outlet end of the burner body chamber onto a carton end to be heated. The burner nozzle is provided with a screen pack for dividing the primary air and gas mixture into fine segments, and with a fiberglass filter means for reducing fluid flow noises.

Abstract: A gas cooking range of the smooth top type has four burners positioned under a single plate of heat-resistant glass/ceramic material; and a single igniter and safety control assembly is centrally positioned between the burners. The supply of gas to each of the burners flows through an ignition chamber where it is ignited, and it then flows through a combustion tube to a combustion chamber, where combustion is completed. Some air is mixed with the gas at the fuel supply control valve, and additional air is supplied through the ignition chamber. The burning gas mixture then flows through the combustion tube to the combustion chamber at the entrance of which an additional quantity of air is added to provide the remainder of air necessary for complete combustion.

Abstract: A burner which is capable of burning a very lean mixture of flammable vapors and air, and which preferably also can burn a mixture of varying richness and B.T.U. content, with the burner desirably including a structure forming an upwardly facing recess and an inlet for introducing the vapor-air mixture into a lower portion of that recess in a relation enabling the mixture, when lean, to burn at least partially in the recess in isolation from external air, and when richer to burn at an upper elevation at which external air can mix with the basic vapor-air mixture.

Abstract: The hot flue gas expelled from a furnace is used to heat air which is supplied to the burners that fire the furnace. The heated air is delivered to each burner through its ceramic burner block rather than through its cast iron burner body so as to avoid the need of making the body out of expensive alloys capable of withstanding high temperatures.

Abstract: A method and apparatus for burning oil or gas mixed with air to produce a long stable flame in which the fuel is atomized in a chamber by a primary atomizing medium introduced tangentially into the chamber to form a confined stream, secondary air moving parallel to the confined streams mixed with the stream which is then expanded and tertiary air supplied to the stream in a helical swirling path about the stream periphery.

Abstract: Fuel is burned in a primary combustion chamber with less than the air required for stoichiometric combustion so that the combustion gases have a high carbon monoxide (CO) and hydrocarbon content and the temperature of the gases is held below that at which significant nitrogen oxides (NO.sub.2) would be produced. The combustion gases are then passed through a secondary combustion zone in which more air is injected into the gas stream to oxidize the CO and hydrocarbons to carbon dioxide (CO.sub.2). The secondary burner comprises a plurality of foraminous tubes through which secondary air is emitted. Combustion in the secondary zone is maintained at a temperature below that at which nitrogen oxides (NO.sub.x) will be produced in significant quantities.

Abstract: A combustor for a gas turbine engine has a prevaporization chamber wall having a plurality of air passages therethrough and wherein a variable geometry air flow control element is located in overlying relationship with the air passages to control air flow therethrough. A fuel injector is located concentrically within the chamber for supplying fuel for combustion with air supplied thereto and a hydraulic control actuator is located in surrounding relationship with the injector immediately outboard of the chamber including the hydraulic actuator having pressure supplied thereto from the fuel flow through the nozzle and including means for coupling the actuator directly to the control element for increasing primary air flow in accordance with increased fuel flow to the prevaporization chamber.

Abstract: A tube-fired radiant energy heating system comprising a burner of high rated capability and having a combustion chamber which is connected to an elongate radiant energy emitter tube typically carring a directing reflector, and connected at the output end to a power exhaust fan. Fixed primary and adjustable excess air inlet means are provided at the burner unit to permit excess air to be continuously drawn around the combustion chamber and into the radiant energy heater tube to be mixed with the ignited primary fuel/air mixture at the inlet to the heater tube. This method of firing permits the construction of the apparatus using lower cost materials which, if used in a burner system fired at Stoichiometric fuel/air ratios, would be thermally oxidized and weakened. The excess air flow results in the control of the emitted air temperature to safe levels, minimizing oxidation and maintaining the high tensile strength with high BTU inputs.

Abstract: A burner unit is provided for receiving gaseous and liquid fuels and generating heat therefrom. The burner unit is formed with a plurality of orifices for introducing combustion air into the burner chamber.

Abstract: Fuel and less than the amount of air for stoichiometric combustion are injected into a combustion chamber so that the fuel rich mixture burns as a core in the combustion chamber. The balance of the air for substantially stoichiometric combustion is injected coaxially and rotationally as a sheath or vortex which surrounds the core. Where the core is hot and rich, there is little mixing of the sheath air and core gases and the available oxygen combines preferentially with fuel components other than nitrogen so that little nitrogen oxides are produced. After some heat is extracted from the gases in the core, more complete mixing of the sheath air and core gases occurs. Under these lean and cool combustion conditions, production of nitrogen oxides is also unsubstantial. Means for mixing the gas streams may be disposed adjacent the exit end of the combustion chamber when necessary to promote turbulence and further mixing of the air and hot gases for bringing about complete combustion of any residual combustibles.

Abstract: A nozzle employed as a burner within a fluidized bed is coaxially enclosed within a tubular shroud that extends beyond the nozzle length into the fluidized bed. The open-ended shroud portion beyond the nozzle end provides an antechamber for mixture and combustion of atomized fuel with an oxygen-containing gas. The arrangement provides improved combustion efficiency and excludes bed particles from the high-velocity, high-temperature portions of the flame to reduce particle attrition.

Abstract: A system for the direct firing of immersion tubes for heating of liquids in vats or tanks, including a gas burner, of the postmixer nozzle type comprising a gas supply tube having a blanked off downstream end provided with a series of peripheral gas ports, the gas tube being concentrically disposed within an air tube and having a perforated cone attached thereto slightly rearwardly of the gas ports, the arrangement being such that gas and air is entrained above atmospheric pressure and thoroughly mixed at the burner head by the turbulent flow of air through the perforated cone and around its periphery so as to create regions of gas rich and weak mixtures whereby to obtain flame stability. The system also includes a combustion chamber communicating the burner with the immersion tube.

Abstract: Fuel is burned in a primary combustion chamber with less than the air required for stoichiometric combustion so that the combustion gases have a high carbon monoxide (CO) and hydrocarbon content and the temperature of the gases is held below that at which significant nitrogen oxides (NO.sub.x) would be produced. The combustion gases are then passed through a secondary combustion zone in which more air is injected into the gas stream to oxidize the CO and hydrocarbons to carbon dioxide (CO.sub. 2). The secondary burner comprises a plurality of foraminous tubes through which secondary air is emitted. Combustion in the secondary zone is maintained at a temperature below that at which nitrogen oxides (NO.sub.x) will be produced in significant quantities.

Abstract: A flare stack gas burner for waste combustible gas from oil refineries, chemical plants, oil production rigs, LPG and other marketing terminals, pipe lines and the like is disclosed which includes a stack with a centrally disposed combustible gas delivery pipe having a divider at the top with arms for upward delivery of the combustible waste gas through a plurality of radial slots to a mixing space, air under pressure being supplied to the stack and between the arms to the mixing space, a rotary diffuser being provided above the mixing space for directing the combustible gas-air mixture for combustion thereabove in a cylindrical or flaring frusto-conical vortex for smokeless combustion. Suitable gas pilots and igniters are employed. An optional flaring frusto-conical shield may be provided for a portion of the burning vortex where required.

Abstract: A crude oil burner is provided particularly suited for oil well testing in Arctic and sub-Arctic regions having a plurality of aligned and spaced air cones to the rear end of which crude oil is delivered, and into which air is induced. Air is also available at the space between the cones and at the front of the front cone. Gas assist heads are provided connected to a ring at the space between the cones and connected to a ring at the front of the front cone for inducing air and aiding in the combustion of the crude oil to provide smokeless combustion. The burner can be mounted for turning in accordance with the wind direction to avoid undesired deflection of the flame by the wind.

Abstract: A method and an apparatus for increasing the combustion flame temperature of a partially-aerated atmospheric gas burner heater and the heat transfer therefrom by the injection of jets of preheated secondary air into the combusting chamber transiting the flow of burning gases thereof.

Abstract: A wall burner is described for firing a flame laterally into a duct of the type generally known as a waste heat recovery duct wherein hot exhaust gases are passed in a heat exchange relationship with a second fluid downstream from the wall burner. The wall burner may be used as an igniter for a grid burner system disposed within the duct or the wall burner may itself be used to reheat the hot exhaust gases. The wall burner includes a combustion chamber pipe and ignition means located outside the duct so that ignition occurs outside the duct thereby obviating instabilities inherent in trying to ignite a combustible mixture within the hot exhaust gas path.

Abstract: Carbonaceous fuel is thermally combusted with an amount of air substantially less than that needed for complete combustion to carbon dioxide and water of all the combustible components in the fuel to produce a gaseous first effluent containing a substantial proportion of carbon monoxide but little or no nitrogen oxides. The first effluent is mixed with additional air and at least a portion of the resulting mixture is passed into the presence of a solid oxidation catalyst for combustion at a temperature above the instantaneous auto-ignition temperature of the mixture but below nitrogen-oxide-forming temperatures. Heat is withdrawn from the initial thermal combustion stage and from the gases downstream of the catalyst for the purpose for which the furnace is being operated.

Abstract: A burner construction especially for gas turbine engines in which the combustion takes place in a plurality of small porous ceramic burner cans that are mounted on a flame tube and extend substantially at right angles to the tube with fuel nozzles at the end remote from the flame tube.

Abstract: An apparatus for passing a portion of a cooling fluid, flowing in a plenum in a predetermined direction, in a protective film upon a liner defining a hot gas passage. The apparatus is comprised of a first liner portion or segment partially defining the plenum and a second liner portion or segment partially defining the hot gas passage and cooperating with the first liner segment to form a pocket. A first lip is located at the downstream end of the second liner segment and is radially adjacent a second lip located at the upstream end of the first liner segment. The first lip is spaced from the first liner segment to form an exit from the pocket for directing cooling air along the first liner segment in the predetermined direction. The apparatus further comprises a plurality of apertures in the first liner to pass cooling fluid in a plurality of streams into the pocket and along the second lip in a direction substantially opposite from said predetermined direction.

Abstract: The invention discloses a low NO.sub.x emission burner for use with an apparatus in which the material or materials are heated by the heat radiated from the radiation surface which is heated by the combustion by the burners. The secondary air injection ports or outlets are so arranged as to inject the secondary air upon the radiation surface to control the combustion, thereby reducing the release of NO.sub.x without producing CO and soot.

Abstract: Fuel is burned in a primary combustion chamber with less than the air required for stoichiometric combustion so that the combustion gases have a high carbon monoxide (CO) and hydrocarbon content and the temperature of the gases is held below that at which significant nitrogen oxides (NO.sub.x) would be produced. The combustion gases are then passed through a secondary combustion zone in which more air is injected into the gas stream to oxidize the CO and hydrocarbons to carbon dioxide (CO.sub.2). The secondary burner comprises a plurality of foraminous tubes through which secondary air is emitted. Combustion in the secondary zone is maintained at a temperature below that at which nitorgen oxides (NO.sub.x) will be produced in significant quantities.

Abstract: A method and an apparatus for the combustion of liquid sulphur in a combustion chamber. The injection device for the liquid sulphur and the primary air comprises a double spraying arrangement : a simple mechanical spraying device in which the liquid sulphur is driven through a spray nozzle without the aid of an auxiliary driving fluid and a pneumatic spraying device in which a turbulent rotational primary air stream mixes with the relatively coarse spray produced by the spray nozzle through a constriction zone and into the combustion chamber, transforming the relatively coarse spray into a relatively fine spray. The fine spray enters the combustion chamber at the apex of a conical end wall of the combustion chamber and is driven into contact with the conical end wall due to the whirling action of the primary air. Secondary air is introduced along the lateral walls of the combustion chamber, in order to protect these walls of refractory material from the radiation heat produced during combustion.