45results about "Burner ignition devics" patented technology

A heating appliance (1) is proposed, comprising a conveying device (2) for conveying combustion air to a burner (3), a Venturi device (15) arranged downstream of the conveying device (2), and a gas valve (5) connected to a gas supply (8). A control line (17) is connected downstream of the Venturi device (15) to the gas valve (5) with respect to a flow direction (16) of the heating appliance (1), and the gas valve (5) is configured to adjust the fuel gas flow rate to the reference pressure of the control line (17). The heating appliance (1) enables an extended modulation range, in particular allowing the operation of the heating appliance (1) at high power levels. Furthermore, a method for commissioning the heating appliance and a computer program are described.

A microburner configured to test a combustion reaction and its effects on surrounding structures is disclosed.SOLUTION: Microburner 100 includes a leak plate 108 having a test opening 110 configured to simulate a microleak of a gaseous fuel into a combustion environment 101 containing a reactant gas to test a combustion reaction between the reactant gas and the gaseous fuel within the combustion environment. The microburner also includes a gas supply line 112 coupleable to the leak plate and configured to supply gaseous fuel through the test opening and into the combustion environment when coupled. The microburner further comprises an ignition source 114 configured to initiate a combustion reaction between the reactant gas and the gaseous fuel within the combustion environment.SELECTED DRAWING: Figure 1

The application discloses a honeycomb matrix plate type ultra-low nitrogen gas burner, which comprises a burner head, a gas pipeline connected with the burner head and an air channel connected with the burner head; the burner head comprises a gas bin and an air bin, one end of the air bin is connected with the air channel, one end of the gas bin is connected with the gas pipeline, and a distribution cover is arranged on the burning end of the burner head and connected with the gas bin and the air bin; a combustion nozzle and an ignition port are arranged on the distribution cover, the combustion nozzle is distributed in a honeycomb shape on the distribution cover, and the ignition port is at least provided with two and is staggered with the combustion nozzle; the honeycomb matrix plate type ultra-low nitrogen gas burner can realize multi-point combustion, multi-point cross ignition and low nitrogen emission.

A low NOx burner system using two-fluid injection according to the present invention comprises: a water supply unit that pumps water from a water storage tank therein and supplies the water to a steaming unit in a combustion chamber via a water supply pipe; a pyrolysis oil supply unit that pumps pyrolysis oil from a pyrolysis oil storage tank therein and supplies the pyrolysis oil to an injection nozzle unit in the combustion chamber via a pyrolysis oil supply pipe; a starting oil supply unit that pumps a starting oil from a starting oil storage tank therein and supplies the starting oil to the injection nozzle unit in the combustion chamber via a starting oil supply pipe; and a precipitate discharge unit that is provided in a longitudinal-transverse joint zone of a pyrolysis supply pipe disposed between the pyrolysis oil storage tank and the injection nozzle unit, and can discharge precipitates contained in the pyrolysis oil and precipitated under the control of a control unit.

A method for the failsafe and lean ignition of a fuel gas-air mixture on a gas burner (6), which is mixed in a mixing device (4) arranged upstream of the gas burner (6). A control valve (2) along the fuel gas flow path has an actuator (21) and a throttle element (23), moved by the actuator (21), for the closed-loop control of a flow rate of the fuel gas flowing into the mixing device (4). A test is performed to determine whether the throttle element (23) is in the throttle reference position when the actuator (21) is in the actuator reference position. The throttle element (23) is moved in a flow rate-increasing manner starting at a start time (tD). The flow rate-increasing movement of the throttle element (23) is stopped as soon as at least one of multiple predetermined termination conditions occurs.

A one-piece combination valve, including: a valve body, provided with an air guide chamber and an air inlet chamber, the air guide chamber being configured with a first air outlet and a second air outlet; an electromagnetic valve assembly, fixedly connected to the valve body; and a plug valve assembly, connected to the valve body. A plug valve core of the plug valve assembly is driven under force to translate toward an electromagnetic valve core of the electromagnetic valve assembly and to be abutted against the electromagnetic valve core, so that the air guide chamber is in communication with the air inlet chamber, or a plug valve core of the plug valve assembly is driven under force to be rotated about a central axis of its own, so that at least one of the first air outlet and the second air outlet is / are in communication with the air guide chamber.

The application discloses a snail-shaped element combustor ignition and stable combustion device and method, which comprises an inlet structure, a combustor shell, a wall surface necking concentration weir, an arc-shaped expansion channel, an outlet structure and an ignition device; the inlet structure is connected to one side of the bottom of the combustor shell, and the outlet structure is connected to the other side of the bottom of the combustor shell; the arc-shaped expansion channel and the wall surface necking concentration weir are arranged on the inner wall of the combustor shell, the arc-shaped expansion channel is located on the side where the outlet structure is arranged, and the arc-shaped expansion channel is a cold pulverized coal gas flow outlet channel, receives a high-speed primary air flow and mixed high-temperature flue gas flow, gradually expands along the circular shell, continuously receives radiation and mixed heating of a flame center in the expansion flow process, and is ignited stably; the wall surface necking concentration weir is located on the side where the inlet structure is arranged, the wall surface necking concentration weir concentrates un-gasified hot coke powder in high-temperature gas, and sends the un-gasified hot coke powder to a primary air nozzle outlet, so that the concentration and heat of the coal coke powder at an ignition position are increased; and the ignition device is arranged at the outlet of a primary air flow deformation channel or the primary air nozzle outlet.

The invention discloses a burner assembly and a cooker. The burner assembly includes a first burner and a second burner. The first burner is of a ring shape and has first flame holes formed on an inner circumferential edge of the first burner. The second burner is of a ring shape and has second flame holes formed on an inner circumferential edge of the second burner. The second burner is disposed above the first burner and has an inner diameter greater than an inner diameter of the first burner. In the burner assembly, the second burner is disposed above the first burner, and the inner diameter of the second burner is greater than the inner diameter of the first burner. Therefore, when ignition of the first burner is successful, the second burner can be ignited from an inner circumference of the second burner in a manner of flame upward spread, to ensure flame uniformity of a pot bottom. This design is simple in structure, and convenient and quick.

A method for starting a heating appliance (1) is proposed, comprising a conveying device (2) for conveying a combustion mixture of fuel gas and combustion air to a burner (3), an ignition device (12) for the combustion mixture, and a gas valve (5), wherein, prior to the commissioning of the conveying device (2), the gas valve (5) is briefly opened (32), thereby filling the gas valve (5) with fuel gas. The duration of the brief opening (32) of the gas valve (5) can be a maximum of half the regular safety period (35) for commissioning the heating appliance (1). This reduces the influence of time delays, caused by a longer period since the last interruption of burner operation, between the opening of the gas valve (5) and the commencement and stabilization of the fuel gas flow.

A gas burner (1) according to one aspect of the present invention includes a fuel supply pipe (10) extending in a predetermined combustion air jet direction and supplied with fuel gas, an air jet port (40) arranged around the fuel supply pipe (10) and jetting combustion air in the combustion air jet direction, and multiple outflow nozzles (70) extending so as not to protrude outward from the fuel supply pipe (10) beyond the air jet port (40) and so as to form an acute inclination angle with respect to the combustion air jet direction and having tip ends forming fuel outlet ports (71) through which the fuel gas flows out.

Disclosed in the present invention are: a hydrogen burner forming a flat flame, in which a plurality of nozzles are arranged on a plane, allowing formation of a flame having a shape corresponding to the plane, in front of the plane; and a control method capable of preventing the backfire phenomenon of the hydrogen burner.

A method for commissioning a heating appliance (1) comprising a conveying device (2) for conveying combustion air to a burner (3), a Venturi device (15) which is arranged downstream of the conveying device (2) with respect to a flow direction (16) of the heating appliance (1), a gas valve (5) which is configured to add fuel gas to a mass flow of the combustion air conveyed by the conveying device (2), a flame detector (19) and an ignition device (18), wherein the heating appliance (1) starts up to a predetermined starting power of the conveying device (2) during commissioning, comprising the following steps: a) detecting an ignition period (23) from the opening of the gas valve (5) until a flame is detected by the flame detector (17), b) comparing the ignition period (23) detected in step a) with a previously known reference period (36), and c) adjusting the starting power of the conveying device (2).if a deviation identified in step b) as part of the comparison reaches or exceeds a predetermined value.

The invention relates to a method for initiating or igniting a mixture of an oxidizer and a fuel in a combustion chamber of a space launcher, characterized in that it comprises implementing a step of injecting decomposed hydrogen peroxide (HTP) via a catalyst so as to obtain a predetermined ignition temperature. Figure to be published with the abstract: Fig. 1

The invention relates to a microburner apparatus and an associated method. Disclosed herein is a microburner configured to test combustion reactions and their effects on surrounding structures. The micro-combustor includes a leak plate having a test orifice configured to simulate a micro-leak of a gaseous fuel to a combustion environment containing a reactant gas to test a combustion reaction between the reactant gas and the gaseous fuel within the combustion environment. The microburner also includes a gas supply line coupleable to the leak plate, and when coupled, the gas supply line is configured to supply gaseous fuel through the test orifice and into the combustion environment. The microburner also includes an ignition source configured to initiate a combustion reaction between the reactant gas and the gaseous fuel within the combustion environment.

The invention relates to a gas cooking and / or gas grilling system (1) comprising: a main valve (3); a plurality of burner units (4) each having a valve (5); a pilot burner (6) having a flame detector (7) and an ignition electrode (8); and a control device (9); wherein the main valve (3) is connected or can be connected on the input side to a gas inlet (10) for connection to a gas source and is connected on the output side to each of the valves (5) of the burner units (4) and to the pilot burner (6), wherein the pilot burner (6) has a pipe (13) which is arranged on the burner units (4) and has a plurality of gas outlets (22), wherein the flame detector (7) is arranged at one end (14, 15) of the pipe (13) and wherein the ignition electrode (8) is arranged at another end (14, 15) of the pipe (13), wherein the control device (9) is designed to logically release the valves (5) of the burner units (4) for actuation when the flame detector (7) has detected a flame. The invention also relates to a pilot burner (6) and to a method for starting a gas cooking or gas grilling system (1).

A burner includes a mixing chamber having therein a space in which fuel and air are mixed to form a mixture, a chamber lower cover that is coupled to the mixing chamber while covering an opening formed in the mixing chamber in a reference direction and has a combustion opening opened in the reference direction, a porous distribution unit that includes a metallic sintered material, through which the mixture passes in the reference direction, and covers the combustion opening, a distribution plate that has a plurality of distribution through-holes, through which the mixture passing through the porous distribution unit passes, and covers the combustion opening on the downstream side of the porous distribution unit in the reference direction, and an ignition unit that covers the combustion opening on the downstream side of the distribution plate to ignite the mixture passing through the distribution plate.

The present invention relates to a burner system for providing thermal energy comprising an evaporator device for evaporating a liquid alcohol fuel, a burner air supply means, a burner device for burning a fuel mixture comprising vaporized fuel and burner air to provide an exhaust gas stream, a functions device for controlling the thermal energy of the exhaust gas flow, wherein the burner device provides the thermal energy for evaporation in the evaporator device during operation.

A hydrogen gas burner includes a first, axially extending, tubular pipe having an axial slot in a sidewall thereof. An axially elongate duct projects radially outwardly from the axial slot and is in fluid communication with an interior of the pipe. The axially elongate duct has through-holes formed through a wall thereof, communicating the interior of the pipe with an exterior thereof. A second, axially extending, tubular pipe, has an axial opening in a sidewall thereof, the axial opening spanning at least a portion of an axial extent of the second pipe. The first pipe is substantially nested within the second pipe and the axially elongate duct projects radially outwardly through the axial opening. A combination gas valve and pressure regulator fluidly connects hydrogen gas with the first pipe. An igniter ignites and initiates combustion of the hydrogen gas exiting from the first pipe and duct via the through-holes.

The invention relates to a burner (10) for an exhaust tract through which exhaust gas of an internal combustion engine of a motor vehicle flows, with an ignition device (16) and with a combustion chamber (12) in which a mixture comprising air and fuel is to be ignited and thereby combusted by means of the ignition device (16), wherein at least one cover element (50) is movable between at least a first position (52), in which the ignition device (16) is at least partially covered by the cover element (50), and at least a second position, in which the ignition device (16) is released by the cover element (50).

Disclosed herein is a micro burner configured for testing a combustion reaction and its effect on surrounding structures. The micro burner includes a leak plate having a testing aperture that is configured to simulate a microleak of a gaseous fuel into a combustion environment, containing a reaction gas, to test a combustion reaction between the reaction gas and the gaseous fuel within the combustion environment. The micro burner also includes a gas supply line couplable to the leak plate and, when coupled, configured to supply the gaseous fuel through the testing aperture and into the combustion environment. The micro burner further includes an ignition source configured to initiate the combustion reaction between the reaction gas and the gaseous fuel within the combustion environment.

The disclosure relates to a gas-heated infrared radiation emitter comprising at least one radiating screen, which is for example made of ceramic and / or metal, in the form of at least one plate comprising a lower main surface and an upper main surface that are distant from each other, and a plurality of through-prisms, which are preferably hollow, extending from the lower main surface to the upper main surface, each prism being defined by a polygonal base and by an axis. The prisms may be juxtaposed with one another so that their polygonal bases form a tiling of at least one portion of the lower and upper main surfaces of said plate.

A burner includes a mixing chamber having therein a space in which fuel and air are mixed to form a mixture, a chamber lower cover that is coupled to the mixing chamber while covering an opening formed in the mixing chamber in a reference direction and has a combustion opening opened in the reference direction, a porous distribution unit that includes a metallic sintered material, through which the mixture passes in the reference direction, and covers the combustion opening, a distribution plate that has a plurality of distribution through-holes, through which the mixture passing through the porous distribution unit passes, and covers the combustion opening on the downstream side of the porous distribution unit in the reference direction, and an ignition unit that covers the combustion opening on the downstream side of the distribution plate to ignite the mixture passing through the distribution plate.

In a combustion apparatus that includes a burner constituted by a burner body, an inside of which an air-fuel mixture is supplied to and one surface of which is made into an open surface, and a combustion plate covering the open surface of the burner body, and a combustion box enclosing a combustion space of the air-fuel mixture ejecting from the combustion plate, an offset part that is positioned at a portion which is away from the swelling part in an inflow direction of the air-fuel mixture to the inner chamber and does not oppose to a tip part(s) of the ignition electrode(s) through the combustion plate is provided with the opposite wall of the burner body and the offset part offsets to a combustion-plate side so that a distance between the offset part and the combustion plate becomes shorter than that between the combustion plate and a general part of the opposite wall except the swelling part and the offset part.

A method for heating reactor using a multi-function burner comprising feeding primary fuel through an annular channel, feeding oxygen through a central channel within the annular channel, and feeding an auxiliary fuel through a central lance within the central channel to produce a flame extending into a furnace having a temperature and a pressure; wherein the flow rate of the auxiliary fuel and oxygen are increased while maintaining an equivalence ratio below 1 to increase the temperature of the furnace; wherein after the furnace temperature exceeds the auto-ignition temperature of the primary fuel, increasing the flow rate of the primary fuel to increase the equivalence ratio to be greater than 1.

A system and method for igniting a coal-air-fuel mixture includes a burner (14) having a burner tube (100) and a first flow guide (118), the burner tube being operable to deliver a flowing fuel-air mixture to a furnace for combustion therein, the first flow guide disposed within the tube and operable to guide a first portion of the flowing fuel-air mixture to a specific location within the burner tube. The system also includes a laser igniter (17) within the burner tube (130), the laser igniter comprising a laser tube (110) and a laser source (150), the laser tube having a first end with a laser input and a second end with a light output, the laser source being operatively coupled to the laser input. The laser source includes a laser. The laser igniter guides photons from the light output to the location within the burner tube to ignite at least a portion of the first portion of the fuel.

A system for generating thermal energy, comprising an electrolysis device that performs electrolysis of water to generate an electrolysis product material containing gaseous molecular hydrogen, and a furnace that is fluidly connected to the electrolysis device, receives at least the gaseous molecular hydrogen of the electrolysis product material, and is configured to burn the received gaseous molecular hydrogen. The combustion products are heated by the thermal energy generated by the combustion, and heated combustion products are generated. The heated combustion products heat the ambient air, and heated ambient air and cooled combustion products are generated. The cooled combustion products are reheated by the generated thermal energy and mixed with the heated ambient air to generate a heated gas mixture.

The present disclosure generally relates to fuel burners, for example, for use with photonic crystals as part of thermophotovoltaic power generators or with other thermal power generators. In certain aspects, fuel is supplied into a reaction tube and mixed between swirling streams of gases moving in opposite directions (e.g., clockwise and counterclockwise) within the tube. This may allow for rapid mixing and relatively complete oxidation or combustion of the fuel. Heat may be extracted from the heated exhaust and may be supplied to a thermal power generator to produce power.

A turbine engine having a combustion section. The combustion section may have a combustor, at least one fuel cup, and at least one ignition tube. The combustor may include a combustor liner and a domed wall that together at least partially define a combustion chamber. The at least one fuel cup may include a swirler and a fuel injector. The at least one ignition tube may include an outlet directly fluidly coupled to the combustion chamber.

The natural gas combustion device with the flameout protection function comprises a furnace base, a gas-electric valve head and an igniter, a gas nozzle is arranged in the middle of the furnace base, the gas-electric valve head can control gas to be input into the gas nozzle and control the igniter to complete ignition, a plurality of sets of gas outlet holes are formed in the side wall of the upper end of the gas nozzle, and the gas outlet holes are communicated with the gas nozzle. The gas nozzle is provided with a flame-out protection assembly, the flame-out protection assembly comprises a thermoelectric oil induction needle, the thermoelectric oil induction needle is fixedly installed on one side of the gas nozzle, a connecting line is arranged between the thermoelectric oil induction needle and the gas-electric valve head, and after the thermoelectric oil induction needle induces temperature rise, an electromagnetic valve in the gas-electric valve head can be automatically separated through the effect of the connecting line; according to the gas stove, the thermoelectric oil induction needle and the movable blocking piece serve as dual flameout protection, the safety of the gas stove is improved, gas remaining in a pipeline can be prevented from flowing into air, and gas waste is reduced.

A hydrogen gas burner includes a first, axially extending, tubular pipe having an axial slot in a sidewall thereof. An axially elongate duct projects radially outwardly from the axial slot and is in fluid communication with an interior of the pipe. The axially elongate duct has through-holes formed through a wall thereof, communicating the interior of the pipe with an exterior thereof. A second, axially extending, tubular pipe, has an axial opening in a sidewall thereof, the axial opening spanning at least a portion of an axial extent of the second pipe. The first pipe is substantially nested within the second pipe and the axially elongate duct projects radially outwardly through the axial opening. A combination gas valve and pressure regulator fluidly connects hydrogen gas with the first pipe. An igniter ignites and initiates combustion of the hydrogen gas exiting from the first pipe and duct via the through-holes.