Abstract: An air to gas mixing valve is provided for fireplaces especially those having sealed combustion chambers as employed in direct vent fireplaces. The novel mixing valve comprises a channel shaped shutter which mounts on and is linearly slidable over a window or windows made a part of the gas mixing pipe which connects to the fireplace burner. An adjustment rod is rotatably coupled to an actuating arm on the channel shaped shutter and extends through at least one sealed panel and has a rotatable nut or screw for linearly moving the shutters over the windows from a remote position.

Abstract: A gas burner assembly is provided for use with a gas stove top. The gas burner assembly includes a burner base with an inlet receiving a mixture of gas and primary air. A burner cap is supported by the burner base. The burner base and the burner cap together define a burner fuel chamber. The burner cap includes a plurality of main burner ports where the air and gas mixture exits and burns in the presence of secondary air. A spark ignition assembly is operatively associated with the burner base for igniting the mixture. The burner cap includes an ignition pocket for capturing gas for reignition for drafts or door slam conditions. A venturi assembly communicates with the burner base inlet providing the air and gas mixture. The venturi assembly includes mounting features for mounting the gas burner assembly to the gas stove, thereby eliminating the need for fasteners to secure the burner base to the gas stove.

Abstract: In a burner for operating a combustion chamber with a liquid and/or gaseous fuel (12, 16), the combustion air (7) required for this purpose is directed through tangential air-inlet ducts (5, 6) into an interior space of the burner. This directing of the flow results in a swirl flow in the interior space, which swirl flow induces a backflow zone at the outlet of the burner. In order to stabilize the flame front forming there, at least one zone (27) is provided at each sectional body (1, 2) forming the burner, within which zone (27) inlet openings (29) are provided for the injection of supplementary air (32) into the swirl flow (7a). Due to this injection, a film forms at the inner wall of the sectional bodies (1, 2), which film prevents the flame from being able to flashback along the inner wall of the sectional bodies (1, 2) into the interior space of the burner.

Abstract: In a burner of the double-cone design for burning liquid (12) and gaseous fuels (16), the at least two sectional cone bodies (1, 2) overlap at least partly, the overlap angle (.delta.) increasing in the direction of flow of the burner, and the distance between the fuel injectors (15) and the air-inlet plane (21) into the burner increasing simultaneously with the increase in the overlap angle (.delta.). As a result, the air-inlet plane (21) and the fuel-injection plane (22) no longer coincide. Improved premixing of the gaseous fuel (16) with the combustion air is achieved by the invention, which leads to lower NOx emissions of the burner and to lower thermal loading of the burner front.

Abstract: A cast aluminum burner base has a tubular inlet communicating with a cavity formed in an enlarged diameter flange remote from the inlet. The cavity is closed by a cast aluminum cap registered against the base. The base and cap are each castellated along the parting line such that the castellations are interdigitated. Grooves having semi-circular cross sections and formed radially across the castellations and the spaces between and close on the parting line to form circular cross section primary flame-generating ports. The castellations on the cap are truncated and tapered to provide flame stabilizing passages adjacent alternate flame-generating ports. The grooves forming the primary flame generating ports are configured to preferably form a converging-diverging nozzle; and, the flame stabilizing passages are formed as a diverging nozzle, both for reducing flow velocity to pressurize flame separation.

Abstract: A gas burner for a cooking device. The gas burner includes a burner head connected to a mixing pipe. An impeller disk is disposed above the burner head and below a cover. The impeller disk is operable to swirl a gas stream and defines a generally circular inner opening. The impeller disk includes a body and a plurality of paddle-shaped flame guidance members formed by a plurality of evenly-spaced and radially-directed cuts in the body. The flame guidance members are bent such that edges of the flame guidance members form oblique angles with the body. The edges each have an end disposed above the body and another end disposed below the body.

Abstract: The present invention concerns a low nitrogen oxides generating combustion apparatus and a low nitrogen oxides generating combustion method. The apparatus and method of the present invention, the effect of self-induced exhaust gas recirculation can be obtained to the maximum extent, and the lower flame temperature and the lower oxygen concentration assure remarkably low NOx generation.

Abstract: A gaseous fuel (B) is fed to a a premixing burner which has a main line (10) for the feed of oxygenous gas (G) into at least one mixing zone and/or a combustion zone (VMZ, EMZ, VZ). In the process, at least a first portion of the fuel is fed to the main line (10), in which it is mixed with oxygenous primary gas (PG) inside at least one premixing zone (VMZ) and forms a premixture. The concentration of the fuel in the premixture (VM), under the respective operating conditions of the burner, is selected in such a way that the premixture lies outside the ignition limit. The premixture (VM) is fed to a final mixing zone (EMZ) and is mixed therein with the residual fuel (RB) likewise supplied and/or with oxygenous secondary gas (SG). The resulting final mixture (EM) is fed to a following combustion zone (VZ).

Abstract: Disclosed is a mechanical swirler for generating diverging flow in lean premixed fuel burners. The swirler of the present invention includes a central passage with an entrance for accepting a feed gas, a flow balancing insert that introduces additional pressure drop beyond that occurring in the central passage in the absence of the flow balancing insert, and an exit aligned to direct the feed gas into a combustor. The swirler also has an annular passage about the central passage and including one or more vanes oriented to impart angular momentum to feed gas exiting the annular passage. The diverging flow generated by the swirler stabilizes lean combustion thus allowing for lower production of pollutants, particularly oxides of nitrogen.

Abstract: In a burner for a heat generator, which consists essentially of a swirl generator (100a) for a combustion air stream (115) and of means for injecting a fuel into this combustion air stream, a mixing stage (220) is arranged downstream of said swirl generator. This mixing stage has, within a first stage part (200), a number of transition channels (201) running in the direction of flow, which ensure the continuous transfer of the flow (40), formed in the swirl generator (100a), into a tube (20) located downstream. A nozzle (103), arranged on the head side and on the burner axis (60), for the injection of a fuel is offset upstream at a distance relative to the start of the swirl generator.

Abstract: A pair of spaced tubular half-shells are stamped in each of two separate sheets of metal which are then joined at their margins to form two mixer tubes each having an inlet end with a venturi for connection to a fuel gas supply and an outlet end adapted for connection to a burner. The space between the mixer tubes is stamped to form a pair of grooves which lock and seal the sheets together to prevent the fuel/air mixture from leaking from one mixer tube to the other.

Abstract: An object of the present invention is to achieve lower NOx combustion in response to the increasingly intensified NOx regulations for burners. The present invention provides a low nitrogen oxides generating combustion method and apparatus which utilizes effective self-induced exhaust gas recirculation before the initiation of the combustion of diffusion flames, or allows part of the combustion gas to be entrained by auxiliary fuel flow, air flow and fuel flow before the formation of the diffusion flames to further intensify the recirculation flow of the combustion gas by the diffusion flames or, in addition, which can achieve rich and lean combustion in the diffusion flames for decreasing the generation of NOx by a combination of these measures, and which are excellent in flame stability even in a low temperature atmosphere.

Abstract: A portable forced air heater includes a base, an outer tubular housing mounted on the base which includes front and rear ends, and a burner assembly mounted within the outer housing. The burner assembly includes an inner housing, and support brackets on the inner housing include tabs which extend through slots in the outer housing. A fan is mounted within the outer housing behind the inner housing. The outer housing is provided with an air opening rearwardly of the inner housing, and an air scoop below the air opening guides air from the fan toward the front of the outer housing for cooling the support surface of the heater. An air diffuser plate on the rear end-of the inner housing is provided with radially extending tapered slots which include radially outwardly diverging side edges. The diffuser plate includes a vane for each slot which partially obstructs the slot. A fuel valve is mounted on the base, and a fuel tube extends between the fuel valve and the burner assembly.

Abstract: A radiant heating system 30 comprising a tube 34 for radiating heat having a vacuum pump 40 coupled to an upstream end 35 for introducing negative pressure therein, a plurality of burner assemblies 32 mounted in series along a length thereof for igniting a combustible gas within the tube 34, and a metering element 90 for controlling the firing rate of the burner assemblies 32 under variable negative pressure conditions.

Abstract: A gas burner produces a homogeneous mixture of gas and air in a short mixing zone by creating turbulence to promote thorough mixing. The burner includes a burner housing supporting a gas distribution tube and an air blower, the distribution tube emitting jets of gas in a radial direction and supporting a baffle plate having a plurality of openings. Air from the blower impinges on the jets of gas to form streams of gas and air that pass through the openings in the baffle plate. A diffuser ring is disposed downstream from the baffle plate and extends radially inward to form a flow constriction. The streams of gas and air contact the diffuser ring and undergo turbulence and the resulting mixture of gas and air passes through the diffuser ring and expands within the interior of a perforated combustion head. The mixture passes through the perforations and when ignited obtains combustion of nearly 100% of the gas and produces a very even flame profile.

Abstract: A multiple inshot-type gas burner structure is formed from a pair of facing, intersecured stamper sheet metal plates. A spaced plurality of parallel, rectangularly cross-sectioned burner bodies are defined by facing triangular indentation pairs in the plates and have, at front outlet end portions thereof, side indentations which serve to mix air and gaseous fuel received at rear end portions of the burner bodies, and to divert a portion of the fuel/air mixture into crossover channels intercommunicating front interior portions of the burner bodies. The crossover channels have central arcuate closed portions that cooperate with progressively sized standoff dimples extending between opposite wall portions of the channels to provide an even crossover flame pattern along the outlet slot section of each channel.

Abstract: A device for injecting fuels (4) into compressed gaseous media essentially comprises a cylindrical hollow body (24) with at least one fuel feed passage (2) and means for the introduction of compressed atomization air (5). A swirl chamber (1) is arranged in the interior of the hollow body (24), this swirl chamber being connected via at least one inlet opening (6) to the fuel feed passage (2). The cross-section of the swirl chamber (1) narrows in the direction of flow of the atomization air passed through the interior of the hollow body (24), thereby forming a cone (8). A dividing wall (20), which extends downstream at least as far as the center of the inlet openings (6), is arranged upstream of the swirl chamber (1), between the fuel in the swirl chamber (1) and the atomization air (5). A method for operating the device is furthermore described.

Abstract: A heating apparatus for delivering heated air to an enclosure comprising a casing with at least two compartments separated by a panel. A burner with an arcuate profile is located within a first compartment of the casing for burning a combustible fuel-air mixture delivered thereto and producing products of combustion. A heat exchanger is located within a second compartment of the casing and has an opposed inlet and outlet. The inlet is in fluid communication with the burner through an aperture in the panel. The heat exchanger receives the products of combustion. A blower is located within the casing for directing a flow of air across the heat exchanger into the enclosure. Through the heat exchanger heat is transferred from the products of combustion to the air. An exhaust system is in fluid communication with the outlet and includes a vent for exhausting the products of combustion from the casing. The vent is contained within the casing.

Abstract: A gas burner assembly for connection to a gas source includes a burner body having a sidewall and a main gas conduit. The burner body further includes a number of primary burner ports disposed within the sidewall, each for supporting a respective main flame, and a simmer flame port disposed within the sidewall adjacent to the primary burner ports for supporting a simmer flame. Additionally, a main fuel chamber is disposed within the burner body to provide fuel to the primary burner ports, and a stability chamber is disposed within the burner body to channel fuel to the simmer flame port. In one configuration, the stability chamber has one or more stability inlets proximate the burner throat which provide the stability chamber with fuel by utilizing the static pressure associated with each stability inlet. In another configuration, the stability chamber has a small feed hole located proximate the burner throat of the main gas conduit.

Abstract: In a premix burner (100) for a heat generator, which essentially comprises at least two hollow, conical sectional bodies (101, 102) nested one inside the other in the direction of flow, the longitudinal symmetry axes (101b, 102b) of the sectional bodies are offset from one another in such a way that the adjacent walls of these sectional bodies form air-inlet slots (119, 120), tangential in their longitudinal extent, for the throughflow of combustion air (115). On the head side, the premix burner (100) has a fuel nozzle (103) which is shifted upstream by a distance (126) relative to the cone start (125) induced by the sectional bodies. Thus the fuel injection is caught by the combustion air only when the fuel spray cone can be penetrated more effectively, which leads to better mixture formation.

Abstract: In a premix burner for the combustion of gaseous and/or liquid fuel, in which the fuel is injected as secondary flow into a gaseous, ducted main flow, the premix duct (20) through which flow occurs being annular and being defined by an inner (21a) and an outer cylinder wall (21b), and the main flow being guided via vortex generators (9, 9a) which generate longitudinal vortices without a recirculation area and of which a plurality are arranged next to one another over the periphery of the annular duct (20) on at least one duct wall (21), and means for injecting fuel being arranged directly downstream of the vortex generators (9, 9a) on the inner and/or outer duct wall (21a, 21b), the vortex generators (9, 9a) generate such vortices which leave behind a residual vortex after the complete mixing of the fuel with the air of the fuel/air mixture flow.

Abstract: A premixed gas burner for use in a boiler or the like has a burner body including a distribution tube into which air under pressure and a gas fuel are received. The gas is supplied to the distribution tube through a gas supply orifice tube having a flange in the form of a disk disposed about the periphery of the gas supply tube and positioned a short distance within the distribution tube. The gas supply tube has a number of orifices located about the tube adjacent to the downstream facing surface of the flange. The distribution tube is located within a pressurized air chamber and gas supplied from a manifold to the supply tube is mixed turbulently adjacent the downstream face of the flange. The invention extends the operating range of premixed gas burners and reduces the carbon monoxide and NO.sub.x output of the burner.

Abstract: A burner for a gas fireplace wherein a plurality of apertures are provided along the length of an enclosure and gas inlets are provided for introducing gas into both ends of the enclosure. Movable members are disposed over air inlet holes at each end for selectively restricting the inlet of combustion air into the enclosure thereby allowing control over the longitudinal position of maximum flame from the burner.

Abstract: A premixed gas burner has an elongated hollow burner body including a burner deck formed by a multiplicity of burner ports about a small sector of the body. The burner body is closed at one end and an elongated distribution tube is received within the body through and extending out the other end. The end of the distribution tube extending out of the burner body has an inlet into which a mixture of gas and air may enter, the opposite end of the distribution tube being closed. A series of directional ports formed between louvered slats adjacent the closed end and spaced from the inlet are formed along a small sector of the distribution tube and directs the mixture of gas and air back toward the inlet end. The sector of the distribution tube in which the ports are formed is substantially 180.degree. from the sector of the burner body in which the deck ports are formed.

Abstract: In a burner (1) for heat generation, the inflowing air (4) is first of all directed into a hollow conical swirl generator (3) which is surrounded by a mixing tube (2). This swirl generator (3) tapers in the direction of flow in such a way that a hollow cone results therefrom. Furthermore, the swirl generator (3) has tangential openings (6, 7) in the direction of flow, which are preferably designed as ducts through which the combustion air (5) flows out of the hollow space (16) into the mixing tube (2). In the region of the tangential openings (6, 7), nozzles (12, 13) are provided through which a fuel (14) is injected into the combustion air (5) flowing past there. A fuel, whether liquid or gaseous, may be supplied by further means in operative connection with the burner (1).

Abstract: In a burner which essentially comprises a swirl generator (100) for a combustion-air flow (115) and means for injecting a fuel into the combustion-air flow (115), a mixing section (220) is arranged downstream of the abovementioned swirl generator. This mixing section (220) has inside a first part (200) of the section a number of transition passages (201) which run in the direction of flow and ensure the smooth passing of the flow (40) formed in the swirl generator (100) into a tube (20) arranged downstream. The outlet plane of this tube (20) to the combustion chamber (30) is formed with a breakaway edge which serves to stabilize and enlarge a backflow zone (50) forming downstream.

Abstract: A method of operating a pre-mix power burner assembly. The method comprises the steps of: using a fan to supply and control combustion; mixing fuel gas and primary air together; introducing the mixture into secondary air in a combustion zone; and relieving pressure on the exterior of the fan near the fan shaft to the interior of the fan.

Abstract: The present invention is referred to a gas injector for a stove burner and its method of manufacture. The injector includes: a gas pipe located at the body of a domestic gas stove burner which itself includes: an area that is externally deformed with a semi-flattened out flange, near the end of the stated pipe which itself is attached to the burner; a threaded section on the internal part of the stated pipe, on top of the first area of the said deformed pipe; and, an upper flange which extends to the end of the pipe and does so angularly towards a greater diameter, preferably about a 45 degree angle relative to its axial shaft.

Abstract: In a premix burner which essentially comprises at least two hollow conical sectional bodies (1, 2) which are nested one inside the other in the direction of flow and form an interior space (14), tangential air-inlet slots (21, 22) are formed by offsetting the center axes (1b, 2b) of these sectional bodies from one another. Feed ducts (25, 26) extend upstream of these tangential air-inlet slots, which feed ducts (25, 26) each end with an injector system (200) for the provision of combustion air (15) consisting of fresh air (19) and flue gas (20). A perforated plate (23, 24) belonging to the injector system runs parallel to the inflow planes (30, 40) of the feed ducts and is provided with injector nozzles (23a, 24a) whose inflow angle varies continuously in the longitudinal direction of the premix burner relative to the burner axis.

Abstract: A flashback resistant burner for lean fuel/air mixtures includes apparatus for mixing a primary fuel and combustion air to form a noncombustible fuel/air mixture. Means are provided for accelerating the noncombustible fuel/air mixture to a velocity higher than the flame speed of a combustible mixture of the primary fuel and air. Means are further provided for mixing a secondary fuel with the accelerated noncombustible fuel/air mixture to form a combustible fuel/air mixture that has an equivalence ratio less than 1. Means are then provided for burning the combustible fuel/air mixture.

Abstract: A gas burner, specifically a gas burner for cooking grills. The burner comprises and elongated conduit member having an upper portion of a generally inverted V-shape, a lower portion defining burner ports angled such that the flame caused by burning gases escaping from the burner port does not impinge upon the lower portion. The cross-section of the elongated conduit member burner provides an increased volumetric flow rate which does not require gas pressure equalization means to provide uniform heat generation across the length of the burner.

Abstract: A gas burner includes an L-shaped inner gas delivery pipe disposed between a burner base and an inner gas outlet member. The inner gas delivery pipe is provided with a first regulating tube for adjusting the length of a horizontal section of the inner gas delivery pipe. The gas burner further includes at least one L-shaped outer gas delivery pipe disposed between the burner base and an annular outer gas outlet member that is disposed around the inner gas outlet member. The outer gas delivery pipe is provided with a second regulating tube for adjusting the length of a horizontal section of the outer gas delivery pipe located on one side of the inner gas delivery pipe.

Abstract: The invention relates to a nozzle for a combustion device in which an improved flame shape is achieved in that a bundle comprising a plurality of small tubes is arranged in an outer tube.

Abstract: A gaseous fuel burner with a base formed of cast aluminum and a wafer cooperating with the base for forming an annular of flame generating ports. A cap is received over the wafer and forms a dead air space for reducing the temperature rise of the cap. The wafer and base are formed of aluminum or brass and the cap is either formed of cast iron or cast aluminum with a porcelainized steel disc insert on the upper surface.

Abstract: A fluid atomizer and spraying means which is made up of: a mixing chamber into which the fluid to be atomized and the atomizing gas are introduced and in which the fluid is admixed with and dispersed in the gas; a generally conical nozzle means extending from the mixing chamber through which the mixed fluid and gas are forced; and a chamber into which the atomized mixed fluid and gas is sprayed. The conical nozzle means is suitably a relatively narrow frustro-conical passageway which contains support-spacer means which is generally parallel to the direction of flow through the passageway. At least one such support-spacer means is provided which extends from the end of the passageway proximate to the mixing chamber to the end of the passageway proximate to the chamber into which the mixture is sprayed. The preferred use of this apparatus is in atomizing fuel oil with steam and spraying such atomized mixture into a combustion chamber where it is contacted with combustion air.

Abstract: A process and apparatus for combustion of fuel which results in reduction of nitrogen oxides and carbon monoxides emissions. Fuel and primary air are preferably premixed and introduced into a combustion chamber. Secondary air is introduced through a plurality of secondary air ports which are positioned about a venturi nozzle or flame holder disk mounted with respect to a combustion chamber wall. The secondary air flowing through the secondary air ports forms relatively high velocity and momentum secondary air jets that promote rapid mixing of the fuel and primary air mixture into the secondary air flow, such that a combustion flame is established at a periphery of the secondary air jets.

Abstract: A low pressure atomizer is used for the atomization of liquids, such as atomization of fuels found in industrial burners. An atomizer body has an atomizing chamber therein and an annular liquid conduit having an annular diffusion member therein. The diffusion member is shaped to direct liquid passing thereby and into the atomizing chamber and forces the liquid to enter the chamber adjacent the walls thereof. The atomizer body has a first annular gas conduit and a tangential gas port connected between the annular gas conduit and the liquid conduit so that the gas impinges tangentially against the liquid to shear and rotate the liquid entering the atomization chamber. A second annular gas conduit has an angled open into the atomizing chamber to further shear the liquid and gas mixture in the atomizer chamber so that a low pressure atomizer atomizes a liquid with low pressure gas streams.

Abstract: A gas burner is interconnected with structure such as a range top wall or mixing tube flange by interengagement of a mounting projection and a locking hole. The locking hole has an entry portion and a narrower capture portion. The mounting projection has a neck portion and an enlarged head portion. The enlarged head portion is inserted through the entry portion of the locking hole and the neck portion is then shifted into the capture portion to accomplish a locking function. In one arrangement the gas burner is of mild cold rolled steel and the mounting projection is formed integral and of one single piece with the burner wall. In another arrangement, the burner is formed of galvanized or stainless steel, and the locking projection is formed integral and of one single piece with the cooperating mounting element. In another arrangement, the burner is supported by a bracket having mounting projections.

Abstract: The invention relates to a burner (1) which is operated with a lean gas (8) (LBTU gas) and comprises at least two hollow, conical partial bodies (2, 3) which are nested in one another in the direction of flow. By offsetting the longitudinal axes of symmetry (2a, 3a) relative to one another, tangential ducts (2b, 3b) are formed through which combustion air (4) flows into the conical cavity (5). Parallel to these ducts (2b, 3b) there are further ducts (6, 7), formed by dividing walls (6a, 7a), through which the-lean gas (8) likewise flows into the conical cavity (5) at a similar rate to the combustion air (4).

Abstract: The apparatus consists basically of an atmospheric burner, a combustion chamber, and means for creating a vacuum within the combustion chamber. To provide optimum combustion using different gases from one gas family, means for detecting at least one apparatus temperature and means for controlling the primary air flow according to the temperature detected are provided. Various applications are described wherein the temperature is measured at the surface of a burner diffuser and the primary air is controlled to keep the temperature below a critical value and the flame stable. For improved operation at the ignition stage, the flow rate of the primary air is set at a comparatively low predetermined starting value.

Abstract: A nozzle mixing line burner includes a line-burner combustion chamber and a nozzle body coupled to the chamber. The nozzle body includes a first channel having a first inlet receiving air, a second inlet receiving fuel, an air and fuel mixing chamber communicating with the first and second inlets and for discharging an air and fuel mixture created within the air and fuel mixing chamber along a first flow path out from the nozzle body. The nozzle body further includes a first opening receiving air, a second opening receiving fuel, and an air and fuel combining chamber communicating with the first and second openings and an exit for discharging a second air and fuel mixture created in the air and fuel combining chamber along a second flow path out from the nozzle body. The second flow path intersects the first flow path at an impingement point in the combustion chamber to cause impingement of the mixtures carried along the first and second flow paths to create flame stability.

Abstract: A gas burner of the type in which a inflammable mixture is caused to flow out of a diffuser, is formed of a plurality of parallel slots separated by grid elements, and distributed into a pair of grids separated by an elongate screen extending between the two grids. The burner includes at least one elongate slot extending perpendicular to said screen along the width of said grid pair, perpendicular to the screen, near the grids, and adapted to take up relative dimensional variations of said screen and the grid elements brought about by differential heatings of the screen and the burner walls surrounding the diffuser.

Abstract: An atmospheric gas burner includes a burner ring having a plurality of gas outlet ducts defining a respective plurality of gas outlet openings and each having a center axis extending at an angle greater than 0.degree. relative to a radius of the respective outlet opening, and a burner cover overlying the burner ring with the burner ring having a portion projecting beyond outer edges of lower regions of the gas outlet openings, and the burner cover having a portion which overhangs about the outer edges of upper regions of the gas outlet openings.

Abstract: A method and apparatus for producing a gas-fired flame which simulates a wood-burning flame. The apparatus includes an elongated slot which is port loaded to produce a buoyancy controlled flame which flickers and closely resembles a wood-burning flame.

Abstract: The disclosed methods and apparatus for mixing a secondary fluid with a primary fluid have utility in venturi and other fluid mixing systems in agriculture, fluid, fuel combustion and other fields where liquid or gaseous chemicals, liquid or gaseous fuels or other fluids are entrained in a stream of water, air or other gaseous or liquid primary fluid. One of these methods provides for the primary fluid (21) a first flow channel (65) deceasing in a direction of flow of primary fluid, utilizes dynamic energy of that primary fluid to induce secondary fluid (35) into that primary fluid, and provides for the primary fluid with induced secondary fluid a second flow channel (66) increasing in a direction of flow of that primary fluid with induced secondary fluid, while arranging corresponding sides 67 and 68 of these first and second flow channels along a plane common to said first and second channels.

Abstract: A gas burner for an open top stove is provided that generally includes three sections that can be separated from one another: a burner body, a burner head, and a drip cover. Forming the bottom of the burner and connected to a gas source is the burner body, which is generally donut-shaped and has an open-topped channel for carrying gas. Seated atop the burner body is the burner head, which is also donut-shaped and includes an open bottomed, internal gas channel that communicates with the open-topped channel of the burner body. The burner head includes two adjacent rows of flame ports that encircle an outer peripheral surface of the burner head and communicate with the internal gas channel. The flame ports of an upper of the two rows are smaller than the flame ports of the lower row. The burner head also includes a third row of flame ports encircling an upper inner peripheral surface of the burner head around the central void.

Abstract: A fuel oil burner has an inlet tube connected to a source of fuel oil and openings in that tube for introducing air or steam into the stream of fuel oil. Located downstream of the openings in the inlet tube is an atomizing element consisting of a plurality of stacks of corrugated plates. The plates in each stack are positioned so that adjacent plates have corrugation directions which are skewed. The configuration of the corrugated plates in each stack provides a plurality of intersecting pathways creating turbulent flow through the atomizing element to atomize or break the fuel oil into small droplets.

Abstract: A compact gas-fired radiant space heater is adapted for residential use, having an output in the 20k BTU to 40k BTU/hr range and exterior dimensions small enough to allow it to be installed in a standard two foot by four foot suspended ceiling opening. A radiator tube having a total length of approximately 15 feet is bent into a serpentine shape, and combustion control components are housed within a plenum chamber supplying combustion air to the tube, both the tube and the chamber being encircled by a frame that fits within the two foot by four foot opening. The combustion control components are attached to a chassis plate whereby the components are removable from the plenum chamber as a unit to enhance serviceability of the heater. A burner venturi of novel configuration produces a flame that is less than four feet long yet which is relatively quiet.

Abstract: A radiation gas burner comprises a burner stone having an axis and a front surface over which a flame is distributed and which is heated by the flame so as to radiate heat, the burner stone being ring-shaped, an outlet pipe arranged radially inwardly of the burner stone and having an inner cylindrical space with an axially rear inlet and an axially front outlet, means for supplying fuel into the rear inlet of the inner cylindrical space of the outlet pipe, first passage means extending from the front surface of the burner stone and through the burner stone rearwardly, second passage means through which a primary air is supplied into the rear inlet of the inner cylindrical space of the outlet pipe to form a fuel-gas mixture which is supplied through the outlet pipe and exits through the front outlet, and third passage means through which secondary air passes through the burner and exits at the front surface, the first passage means for recirculating combustion products through the burner stone communicating wi

Abstract: A mixing unit for mixing gaseous fuel and combustion air includes a fuel supply chamber adapted to receive a supply of fuel, an air supply chamber adapted to receive a supply of combustion air, and a manifold separating the air supply chamber and a transfer conduit which is adapted to deliver the fuel-air mixture to a burner. The manifold is formed with air ports establishing communication between the air supply chamber and the transfer conduit such that multiple streams of combustion air flow through the manifold and into the transfer conduit. The manifold is further formed with fuel supply cavities which communicate with the fuel supply chamber and which alternate with the air ports in the manifold. Multiple fuel ports connect each air port with the adjacent cavities such that multiple sets of oppositely directed jets of fuel mix with the combustion air as the combustion air flows through the manifold.