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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 7925. Отображено 100.
12-01-2012 дата публикации

Fire container assembly

Номер: US20120006316A1
Принадлежит: Outdoor Greatroom Co LLLP

An air-intake assembly adapted for use with a fire container assembly includes a first plate and a plurality of vanes. The plurality of vanes is engaged to the first plate. Each of the vanes includes a first longitudinal side engaged to the first plate and an oppositely disposed second longitudinal side. The plurality of vanes defines a plurality of pathways. A chamber is cooperatively defined by the first plate and the plurality of vanes. The chamber extends through the first plate. The plurality of pathways swirl air about a longitudinal axis of the chamber.

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19-01-2012 дата публикации

Heating system

Номер: US20120012099A1
Автор: David Deng
Принадлежит: Individual

A heating system can include certain pressure sensitive features. These features can be configured to change from a first position to a second position based on a pressure of a fuel flowing into the feature. These features can include, fuel selector valves, pressure regulators, burner nozzles, and oxygen depletion sensor nozzles, among other features.

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26-04-2012 дата публикации

Burner apparatus

Номер: US20120096840A1
Принадлежит: IHI Corp

The present invention is a burner apparatus (S 1 , S 2 , S 3 , S 4 ) that combusts air-fuel mixture (Y) of an oxidizing agent and fuel. This burner apparatus (S 1 , S 2 , S 3 , S 4 ) includes a partitioning component ( 8 ) that separates an ignition chamber (R 2 ) where the air-fuel mixture (Y) is ignited and a combustion holding chamber (R 3 ) where the combustion of the air-fuel mixture (Y) is maintained such that the air-fuel mixture (Y) is able to pass between them, wherein the partitioning component ( 8 ) adjusts the flow rate of the air-fuel mixture (Y) that is supplied from the ignition chamber (R 2 ) to the combustion holding chamber (R 3 ).

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31-05-2012 дата публикации

Fuel injector having tip cooling

Номер: US20120132725A1
Автор: Constantin Dinu
Принадлежит: General Electric Co

According to various embodiments, a system includes a gasification fuel injector. The gasification fuel injector includes a tip portion, an annular coolant chamber disposed in the tip portion, a recessed surface for cooling control and a first structural support extending through the annular coolant chamber. The first structural support divides the annular coolant chamber into a first passage and a second passage.

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14-06-2012 дата публикации

Passive air-fuel mixing prechamber

Номер: US20120144832A1
Принадлежит: General Electric Co

A gas turbine combustion system passive air-fuel mixing prechamber includes one or more fuel passages. Each fuel passage includes at least one downstream fuel injection orifice. One or more fluid conduits connect an upstream portion of at least one fuel passage with one or more air passages such that pressure drops across each fuel injection orifice substantially self-equalize in a passive manner with corresponding air passage pressure drops over a broad range of fuel lower heating value (LHV) from about 150 Btu/scf to about 900 Btu/scf of fuel passing through the fuel passage while mixing with air passing through one or more connected fluid conduits. The effective area of each fluid conduit relative to the corresponding fuel and air passages is dependent upon the desired fuel LHV operating range.

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21-06-2012 дата публикации

Pegless secondary fuel nozzle

Номер: US20120151927A1
Принадлежит: General Electric Co

A unitary fuel injection manifold for a secondary fuel nozzle improves fuel-air mixing and offers flexibility to alter the mixing profile through adaptability to a variety of number, types, and orientation of discharge outlets to the combustion air mixing space around the secondary fuel nozzle. An aerodynamic surface with reduced extension into the mixing space reduces pressures drop and interference with design airflow. Manifold integrity is enhanced by elimination of fillet welds to mount external pegs.

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26-07-2012 дата публикации

Fuel injector assembly

Номер: US20120186259A1
Автор: James B. Hoke
Принадлежит: United Technologies Corp

A fuel injector assembly for a combustor is provided, including a fuel nozzle having an axial inflow swirler and one or more radial inflow swirlers spaced radially outward of the downstream end of the fuel nozzle and mounted to the combustor, wherein the airstreams produced by the swirlers airblast atomize fuel films produced by the fuel nozzle.

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23-08-2012 дата публикации

Apparatus for injecting fluid into a combustion chamber of a combustor

Номер: US20120210717A1
Принадлежит: General Electric Co

A combustor is disclosed having a combustion liner defining a combustion chamber. The combustor may also include a liner cap disposed upstream of the combustion chamber. The liner cap may include a first plate and a second plate. Additionally, the combustor may include a fluid conduit extending between the first and second plates. The fluid conduit may be configured to receive fluid flowing adjacent to the first plate and inject the fluid into the combustion chamber.

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30-08-2012 дата публикации

Rich-lean combustion burner

Номер: US20120219920A1
Принадлежит: Noritz Corp

A row of rich-side flame holes of a combustion burner is arranged in center. Two rows of lean-side flame holes are arranged respectively on sides of the rich-side flame hole row. Two rows of rich-side flame holes are arranged respectively on the outsides of the two lean-side flame hole rows. Supply of lean-side mixture is provided to the lean-side flame hole rows from a tubular part. A lower end part of a central rich-side burner part is projected into a tubular part, into which the rich-side mixture is introduced, to establish lateral fluid communication, with its lower end edge placed in a state of non-contact with the inner surface of the tubular part. First communication holes in fluid communication with an internal space are opened in the lower end part. Communication holes in fluid communication with the outer rich-side flame holes are opened in the inside of the tubular part.

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20-09-2012 дата публикации

Flat fan air assist injectors

Номер: US20120234944A1
Принадлежит: Delavan Inc

An injector for injecting a flat fan of liquid includes an injector body defining a pair of air channels, with each air channel fluidly connected to a respective air inlet. The air channels join one another at a common throat defined in the injector body and are separated by a land defined in the injector body extending from the air inlets to a point proximate the throat. The air channels and a liquid inlet are in proximity to draw liquid out of the liquid inlet into the throat with air flowing through the air channels. A diverging diffuser is provided in fluid communication with the throat. The diffuser includes an impingement surface defined in the injector body opposed to the liquid inlet. The liquid inlet is configured to inject liquid against the impingement surface to form a fan of liquid diverging outward through the diffuser.

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29-11-2012 дата публикации

Plate type burner

Номер: US20120301837A1
Автор: Kazuyuki Akagi
Принадлежит: Rinnai Corp

A plate type burner includes a burner main body and a plurality of burning plates mounted on the open surface of the burner main body. A flange portion enclosing the open surface is formed on the upper surface of the burner main body. The outer edge of each of the burning plates is placed on the flange portion with a sheet of packing interposed therebetween. The outer edge of each of the burning plates is pressed downward by a pressing plate. A clamping plane inclining downward to the outer side is formed on the upper surface of the outer edge of each of the burning plates. Furthermore, an inclined abutting portion contacting the clamping plane of each of the burning plates by a plane of the abutting portion is formed in the pressing plate.

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28-03-2013 дата публикации

Systems and methods involving improved fuel atomization in air blast fuel nozzles of gas turbine engines

Номер: US20130074514A1
Принадлежит: United Technologies Corp

Systems and methods involving improved fuel atomization in air-blast fuel nozzles of gas turbine engines are provided. In this regard, a representative method includes: providing fuel to a chamber defined by an inner surface; and continuously atomizing a portion of the fuel via interaction of the fuel with the inner surface.

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02-05-2013 дата публикации

Burner assembly and methods thereof

Номер: US20130104783A1
Принадлежит: Individual

Embodiments of the present invention generally relate to burner assembly for use in an aggregate drying facility having requisite ultra-low nitrogen oxide emissions. In one embodiment, a burner assembly comprises a single burner apparatus having a centrifugal blower, a transition section, and a frustoconical stabilizer cone from which a flame may exit the burner assembly; a combustible fuel line having a first end connected to a fuel source, and a second end connected to a nozzle for delivering fuel to a combustion chamber within the single burner apparatus; a compressed air line having a first end connected to a compressed air source, and a second end connected to a nozzle for delivering compressed air to the combustion chamber; and a water line having a first end connected to a water source and a second end connected to a nozzle for delivering water to the combustion chamber.

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29-08-2013 дата публикации

Porous insert for a heating element of an oven appliance

Номер: US20130220302A1
Автор: Bai Han
Принадлежит: General Electric Co

An oven appliance is provided having a chamber for cooking food items. A heating element is also provided and, e.g., may be configured for providing heat to the food items in the chamber of the oven appliance. A porous insert is disposed within the heating element. The porous insert can, e.g., improve mixing of gas fuel and air flowing through the heating element and/or regulate the pressure and/or velocity of gas fuel and air flowing through the heating element.

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21-11-2013 дата публикации

Burner for Powdered and/or Particulate Fuels with Adjustable Swirl

Номер: US20130305971A1
Принадлежит: Babcock Borsig Steinmueller GmbH

A burner for powdered and/or particulate fuels having a flow channel for transporting at least one gas stream into a combustion chamber, wherein the flow channel has an annular cross section and a swirl device imparting a swirl to the gas stream in a circumferential direction. The swirl device has at least a first and a second group of deflection means to generate the swirl, that at least the second group of deflection means is attached in a fixed manner to supporting structure that is axially displaceable along the flow channel and/or can be rotated about the longitudinal axis of the flow channel in order to alter the swirl.

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12-12-2013 дата публикации

Combustor assembly having a fuel pre-mixer

Номер: US20130327046A1
Принадлежит: General Electric Co

A combustor assembly having a fuel pre-mixer including a duct for mixing an airflow and a fuel therein. Also included is a center body coaxially aligned within the duct for receiving the fuel from a fuel source and configured to distribute the fuel to at least one axial location within the duct. Further included is a planar vane section in communication with the airflow and the fuel to provide a first injection of fuel and a flow conditioning effect on the airflow. Yet further included is a swirler vane section disposed downstream of the planar vane section, wherein the swirler vane section is configured to provide a second injection of fuel and a mixing of the fuel and the airflow.

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09-01-2014 дата публикации

Gas burner for premixed combustion

Номер: US20140011142A1
Автор: Pierluigi Bertelli
Принадлежит: Bertelli and Partners Srl

A gas burner for premixed combustion is positioned in a combustion chamber and comprises two components, a first defined by a distributor for a gas and air mixture and the second defining the burner shell. The components being close together but spaced apart. The distributor has a perforated distribution surface through which the gas-air mixture passes directed towards the burner shell, which also has a perforated burning surface on which the flame caused by the combustion of said mixture is generated, to create a thermal load within the combustion chamber. The thermal load in this latter is disuniformly distributed.

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13-02-2014 дата публикации

Burner

Номер: US20140041650A1
Принадлежит: LG ELECTRONICS INC

A burner is provided. The burner may include a burner head having mixing pipes through which an air-gas mixture may flow, and a burner cap seated on the burner head and having an opening formed therein. The burner head may include a support wall along its periphery supporting the burner cap thereon and an inner wall formed within the periphery of the support wall, the inner wall having a plurality of flame holes. The center of the burner cap may be positioned within the opening.

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10-04-2014 дата публикации

Burner for a gas turbine

Номер: US20140096502A1
Принадлежит: SIEMENS AG

A burner for a gas turbine is provided. The burner has a pilot combustor, a supply module providing pilot fuel and air into a pilot combustion room enclosed by a pilot burner housing having a tapered exit throat discharging radicals and heat generated in a pilot combustion zone into a main combustion room. An equalizer has holes for main flow air entering a cavity in a radial direction with regard to a burner axis defined by centers of pilot combustion zone and main combustion zone. A fuel injector is downstream the equalizer to supply flow fuel into flow air. A swirler is downstream the injector to give flow distribution to the flow fuel and air entering the main combustion room. A channel leads from the equalizer to the swirler arranged circumferentially around the pilot burner housing to direct the main air flow from the equalizer in axial and circumferential direction.

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10-04-2014 дата публикации

Pilot burner system for water heaters

Номер: US20140096726A1
Принадлежит: Rheem Manufacturing Co

A tube disposed in the combustion chamber of a standing pilot type fuel-fired water heater is used to increase the overall efficiency of the water heater by improving the heat transfer from the pilot flame to the tank during standby periods by funneling the standing pilot flame upwardly through the tube in a manner concentrating the pilot flame heat against an underside portion of the bottom head of the water heater tank. To further increase water heater efficiency, the pilot burner is of a dual input type. Various pilot burner operational algorithm modes are disclosed for causing the pilot burner to operate at a high firing rate during main burner operation, and at a low firing rate during standby periods.

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10-04-2014 дата публикации

Duct burner of hrsg with liner film cooling

Номер: US20140099591A1
Автор: Vladimir S. Polonsky
Принадлежит: Nooter Eriksen Inc

A duct burner assembly for a HRSG having a casing that defines a combustion chamber with a liner for communicating an exhaust gas. A firing runner attaches to the liner and extends through the combustion chamber. The firing runner defines a plurality of orifices for emitting combustible gas and sustaining a flame. A flame stabilizer attaches to the firing runner and is configured to at least partially shield the plurality of orifices from the exhaust gas. A guide plate attaches to the firing runner and is configured to define a slot between the liner and the guide plate. The guide plate has an upstream end and a downstream end wherein the downstream end is closer to the lining than the upstream end to reduce turbulent flow of the exhaust gas through the slot and cool the liner.

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01-01-2015 дата публикации

Fuel nozzle for two fuels

Номер: US20150000285A1
Принадлежит: SIEMENS AG

A fuel nozzle ( 2 ) for two fuels, with an inner pipe ( 5 ) with radially oriented outlet openings ( 7 ) for a first fuel and with an outer pipe ( 6 ), surrounding the inner pipe ( 5 ), with axially oriented outlet openings ( 10 ) for a second fuel; an axially extending groove ( 18 ) on an outer surface of the inner pipe ( 5 ) and a projection ( 19 ) inward from the outer pipe which engages in the groove ( 18 ) as an anti-torsion device ( 17 ) and which is arranged between two axial outlet openings ( 10 ). Alternative groove and projection configurations are disclosed.

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06-01-2022 дата публикации

BURNER, FURNACE AND METHOD OF GENERATING A FLAME

Номер: US20220003407A1
Автор: Richardson Andrew
Принадлежит: Messer Industries USA, Inc.

A burner includes an oxidant feed passage, a fuel feed passage surrounding the oxidant feed passage, an air feed surrounding the fuel feed passage, a movable air flow diverter and, optionally, a flame nozzle. The movable air flow diverter and/or flame nozzle are independently configured to create one or a plurality of gas recirculation regions adjacent the downstream tip of the burner to improve the mixing and reaction of the fuel and oxidant, and overall combustion process efficiency. A related furnace and method for generating a stable flame with the burner are also provided. 1. A burner comprising:an oxidant feed passage;a fuel feed passage surrounding the oxidant feed passage;an air feed surrounding the fuel feed passage; anda movable air flow diverter positionable in the air feed along at least a portion of the fuel feed passage, and including a side wall constructed to proportion distribution of the air feed.2. The burner of claim 1 , wherein the oxidant feed comprises an oxidant selected from the group consisting of at least one of air claim 1 , oxygen-enriched air claim 1 , non-pure oxygen claim 1 , and industrially pure oxygen.3. The burner of claim 1 , wherein the fuel feed comprises a gaseous fuel selected from the group consisting of at least one of methane claim 1 , natural gas claim 1 , liquefied natural gas claim 1 , propane claim 1 , liquefied propane gas claim 1 , butane claim 1 , low BTU gases claim 1 , town gas claim 1 , producer gas claim 1 , hydrogen claim 1 , carbon monoxide claim 1 , and mixtures thereof.4. The burner of claim 1 , wherein the fuel feed comprises an atomized liquid fuel selected from the group consisting of at least one of heavy fuel oil claim 1 , medium fuel oil claim 1 , light fuel oil claim 1 , kerosene claim 1 , diesel claim 1 , and mixtures thereof.5. The burner of claim 1 , wherein the fuel feed comprises a particulate solid fuel selected from the group consisting of at least one of coal claim 1 , coke claim 1 , petroleum ...

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05-01-2017 дата публикации

MULTI BURNER OVNI

Номер: US20170003033A1
Принадлежит:

Present invention relates to a multiple flame burner which allows activating in a selective manner the totality of burners, a part thereof or at least one ring. Said burner has the ability of placing receptacles of different sizes over said burner, in such a way that if a small receptacle were to be used only one ring would be used, a medium sized receptacle would use a part of said rinse and if a large receptacle were to be used, the entire rings would be used 1. A triple ring flame burner comprising:a central burner with a central cover lid and a toroidal burner with a toroidal cover lid, wherein the central burner is found coupled to the toroidal burner by means of at least one bridge;said central burner comprising:a first Venturi tube which receives and emits a first combustible-air pre-mixture for the central burner;a first mixture chamber which receives said first pre-mixture and homogenizes it, creating a first combustible-air mixture;a first distribution channel for distributing the first combustible-air mixture to a plurality of central combustion ports of said central burner;a circumferential groove set on said plurality of main central combustion ports for forming a flame ring;said toroidal burner comprises:second Venturi tube which receives and emits a second combustible-air premixture;a second mixture chamber which receives said second pre-mixture and homogenizes it, creating a second combustible-air mixture;a second distribution channel for distributing the second mixture;an inner crenellated wall and an outer crenellated wall, said crenellated walls separated by the second distribution channel and with at least main. combustion torts and secondary combustion port over the inner crenelated wall, at least one inner barrier rail with inner barrier rail combustion ports; over the outer crenellated wall, at least one outer barrier rail with outer barrier rail combustion ports;a stability and flame transfer chamber with a pair of radial walls which divide ...

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07-01-2016 дата публикации

FLAT-FLAME NOZZLE FOR BURNER

Номер: US20160003472A1
Принадлежит:

According to the present disclosure, a flat-flame nozzle is provided for producing a flat flame in a flame chamber included in a burner assembly. The flat-flame nozzle is configured to conduct fuel from a fuel supply to an ignition zone in the flame chamber. In some illustrative embodiments, the flat-flame nozzle is also configured to conduct oxygen from an oxygen supply to the ignition zone to produce a combustible oxygen-fuel mixture in the flame chamber. In illustrative embodiments, a removable first plate-separation border frame is positioned to lie between a first lower plate and a companion first upper plate. This border frame is configured to cooperate with those plates to form in the flat-flame nozzle a fuel-discharge outlet and a fuel-transport passageway communicating with the fuel-discharge outlet. 1. A burner apparatus comprisinga flat-flame nozzle configured to conduct fuel and to provide means for generating a flat flame when fuel conducted by the flat-flame nozzle is exposed to oxygen to produce an oxygen-fuel mixture that is ignited, wherein the flat-flame nozzle is formed to include a fuel-discharge outlet and a fuel-transport passageway communicating with the fuel-discharge outlet, and the flat-flame nozzle includes a first lower plate, a first upper plate, a removable first plate-separation border frame interposed between the first lower plate and the first upper plate and configured to cooperate with the first lower plate and the first upper plate to form the fuel-discharge outlet and the fuel-transport passageway, and fastener means for releasably retaining the removable first plate-separation border frame in a stationary position between the first lower plate and the first upper plate to establish a first flow velocity of fuel flowing through the fuel-transport passageway toward the fuel-discharge outlet and for allowing replacement of the removable first plate-separation border frame with a removable alternate first plate-separation border ...

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04-01-2018 дата публикации

HIGH TURN-DOWN MODULATING BURNER

Номер: US20180003380A1
Принадлежит:

A high turn-down burner adapted to receive a fuel flow for combustion including an outer housing including a central axis, a side wall having a top edge and a bottom edge, a plurality of apertures disposed on the side wall, a top wall adjoining the side wall at the top edge and a bottom wall adjoining the side wall at the bottom edge; an inner housing including a central axis, a side wall, a plurality of apertures disposed on the side wall, the inner housing is coaxially rotatable with respect to the outer housing; and an actuator adapted to harness and convert the power exerted by the fuel flow to a movement of the inner housing with respect to the outer housing, wherein the alignment of the apertures of the inner and outer housings is adapted to modify an effective combustion area of the burner. 1. A high turn-down burner adapted to receive a fuel flow for combustion , said burner comprising:(a) an outer housing comprising a central axis, a side wall having a top edge and a bottom edge, a plurality of apertures disposed on said side wall, a top wall adjoining said side wall at said top edge and a bottom wall adjoining said side wall at said bottom edge;(b) an inner housing comprising a central axis, a side wall, a plurality of apertures disposed on said side wall, wherein said inner housing is configured to be coaxially inserted in said housing such that said inner housing is coaxially rotatable with respect to said outer housing; and(c) an actuator adapted to harness and convert the power exerted by the fuel flow to a rotation of said inner housing with respect to said outer housing,wherein the alignment of said plurality of apertures of said inner housing and said plurality of apertures of said outer housing are configured such that said rotation is adapted to modify an effective combustion area of said burner which is defined by the amount of overlap between said plurality of apertures of said inner housing and said plurality of apertures of said outer housing. ...

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07-01-2021 дата публикации

GAS COOKING ASSEMBLY AND A HOB COMPRISING THE SAME

Номер: US20210003287A1
Принадлежит:

A gas cooking assembly comprises: (a) a base part () comprising: (a1) a burner body () for installation in a cooktop surface (); (a2) a gas outlet () in the burner body (); and (a3) an ignition source () in the burner body (); and (b) an upper part () comprising: (b1) at least one foot () for supporting the upper part () on the cooktop surface (); (b2) a grate () for supporting a cooking vessel; (b3) an annular flame spreader (); and (b4) a gas inlet () at the bottom side of the flame spreader (); wherein the upper part () is an integral unit that is removable from the base part (), wherein when the upper part () is connected to the base part (), the gas inlet () of the upper part () connects to the gas outlet () of the base part (). 1. A gas cooking assembly comprising:(a) a base part comprising:(a1) a burner body for installation in a cooktop surface;(a2) a gas outlet in the burner body; and(a3) an ignition source in the burner body; and(b) an upper part comprising:(b1) at least one foot for supporting the upper part on the cooktop surface;(b2) a grate for supporting a cooking vessel;(b3) an annular flame spreader; and(b4) a gas inlet at a bottom side of the flame spreader;wherein the upper part is an integral unit that is removable from the base part, wherein when the upper part is connected to the base part, the gas inlet of the upper part connects to the gas outlet of the base part.2. The gas cooking assembly of claim 1 , wherein the grate comprises an annular disk which interposes the flame spreader and which carries a plurality of bars for supporting a cooking vessel.3. The gas cooking assembly of claim 2 , wherein a plurality of legs are attached to the annular disk claim 2 , each said leg having a foot for supporting the upper part on the cooktop surface.4. The gas cooking assembly of claim 3 , wherein the bars extend outwardly beyond the annular disk and merge into the legs.5. The gas cooking assembly of claim 3 , wherein the legs are sized to provide for ...

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03-01-2019 дата публикации

AIR-SHIELDED FUEL INJECTION ASSEMBLY TO FACILITATE REDUCED NOX EMISSIONS IN A COMBUSTOR SYSTEM

Номер: US20190003713A1
Принадлежит:

An air-shielded fuel injection assembly for use in a combustion chamber of a turbine assembly. The air-shielded fuel injection assembly generally includes a fuel manifold including a plurality of fuel injection ports and an air manifold including a plurality of air injection ports. Each of the plurality of fuel injection ports is configured to introduce a fuel column into an annular cavity of a mixer assembly. Each of the plurality of air injection ports is configured to introduce an air curtain about an associated fuel injection column to minimize recirculation upstream of the fuel injection column and increase penetration of the fuel injection column into the cavity. Also disclosed are a mixer assembly and a turbine assembly including the air-shielded fuel injection assembly. 1. An air-shielded fuel injection assembly for use in a combustion chamber of a turbine , the assembly comprising:a fuel manifold including a plurality of fuel injection ports, each fuel injection port configured to inject a fuel radially outward into an annular cavity of a mixer assembly to introduce a fuel injection column extending radially outward into the annular cavity; andan air manifold including a plurality of air injection ports, each air injection port associated with a fuel injection port of the plurality of fuel injection ports and wherein each air injection port is separated from the associated fuel injection port by a distance, each air injection port configured to inject a flow of air radially outward into the annular cavity of the mixer assembly and downstream of the plurality of fuel injection ports, to introduce a downstream air curtain extending radially outward into the annular cavity and downstream of an associated fuel injection column, to minimize recirculation of the fuel injection column and an upstream swirl crossflow and increase penetration of the fuel injection column into the annular cavity.2. The air-shielded fuel injection assembly as claimed in claim 1 , ...

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13-01-2022 дата публикации

CYLINDRICAL BURNER APPARATUS AND METHOD

Номер: US20220010957A1
Автор: Shaffer Yul E.
Принадлежит:

A cylindrical burner apparatus and method which produce low NOemissions and low noise levels without being dependent upon a blower, or natural draft, for providing air flow or flue gas recirculation. A flow of combustion air is induced into the initial tube pass of the burner by discharging a gas fuel from a plurality of discharge ports located in the initial tube pass. At the same time, a flow of recycled flue gas is induced through a bypass duct between a subsequent tube pass of the burner and the initial tube pass by discharging one or more jets of gas fuel through the bypass duct. 1. A cylindrical burner apparatus comprising:an initial tube pass having a longitudinal axis and a rearward end;a first fuel ejection structure or assembly, or an array of ejector elements, comprising a plurality of primary fuel jet discharge ports positioned in the initial tube pass forwardly of the rearward end, at least some of the primary fuel jet discharge ports discharging jets of a gas fuel which induce a flow of combustion air into the initial tube pass through the rearward end:a subsequent tube pass downstream of the initial tube pass;a flue gas recirculation duct having an inlet in fluid communication with an interior of the subsequent tube pass and a discharge in fluid communication with an interior of the initial tube pass; anda second fuel ejection structure or assembly, or an array of ejector elements, comprising one or more secondary fuel jet discharge ports, each of the one or more secondary fuel jet discharge ports discharging a jet of the gas fuel which induces a flow of a recycled flue gas through the flue gas recirculation duct from the interior of the subsequent tube pass to the interior of the initial tube pass.2. The cylindrical burner apparatus of further comprising:the primary fuel jet discharge ports being located in the initial tube pass downstream of the discharge of the flue gas recirculation duct andthe secondary fuel jet discharge ports being positioned ...

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14-01-2016 дата публикации

COMBUSTION BURNER

Номер: US20160008830A1
Принадлежит: TAIYO NIPPON SANSO CORPORATION

An object of the present invention is to provide a combustion burner which is capable of heating or melting a raw material powder efficiently by dispersing the raw material powder, and which is capable of improving a collection rate of the heated or melted raw material powder, the invention providing a combustion burner that forms flame including a dispersal member which is provided in the raw material powder outlet which spouts the raw material powder into the flame, includes first and second inclined surfaces, and which disperses the raw material powder by colliding with the raw material powder that is supplied to the raw material powder outlet. 1. A combustion burner that forms flame comprising:a raw material powder outlets which spouts a raw material powder into the flame;a plurality of first fuel outlets, which are disposed further on an inner side than the raw material powder outlets, and which spout a first fuel;a plurality of first oxidant outlets, which are disposed further on the inner side than the raw material powder outlets, and which spout a first oxidant;a plurality of second fuel outlets which are disposed further on an outer side than the raw material powder outlets, and which spout a second fuel;a plurality of second oxidant outlets which are disposed further on the outer side than the raw material powder outlets, and which spout a second oxidant; anda dispersal member which is provided in the raw material powder outlet, and which disperses the raw material powder by colliding with raw material powder that is supplied to the raw material powder outlet.2. The combustion burner according to claim 1 ,wherein a shape of the raw material powder outlet is a ring form which is partitioned by a leading end of a first circular member and a leading end of a second circular member which is disposed on the outer side of the first circular member, andthe dispersal member includes a first inclined surface that disperses the raw material powder in a direction ...

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11-01-2018 дата публикации

Heat Exchanger Having an Interference Rib

Номер: US20180009070A1
Автор: Donald N. Zimmer
Принадлежит: Lennox Industries Inc

One aspect of this disclosure provides a heat exchanger that comprises a first panel half coupled to a corresponding second panel half that form a passageway having at least a first chamber adjacent an inlet end of the passageway and a second chamber and overlapping interference patterns formed in each of the first and second panel halves that extend along at least a portion of the length of the passageway and located between at least the first and second chambers.

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12-01-2017 дата публикации

Method for monitoring a combustor

Номер: US20170009598A1
Принадлежит: SIEMENS AG

A method for monitoring a combustor comprising: measuring several times a distance between a first wall of the combustor and either a second wall of the combustor or a sensor of the combustor by the sensor, and concluding from a variation in the distances a formation of deposit on the first and/or second wall and/or sensor, and/or a temperature change within the combustor, and/or a pressure change within the combustor.

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09-01-2020 дата публикации

FUEL CONNECTION UNIT

Номер: US20200009942A1
Принадлежит:

A fuel connection unit () for a fuel-operated vehicle heater () includes a connection unit body (), which can be arranged at a heater housing (). A fuel release line connection area () connects a fuel release line leading to a combustion chamber. A fuel feed line connection area () projects from the connection unit body () for connecting a fuel feed line. At least one functional unit (), for influencing the flow of fuel in a fuel flow volume () formed in the connection unit body (), is provided in the connection unit body (). 1. A fuel connection unit for a fuel-operated vehicle heater , the fuel connection unit comprising:a connection unit body to be arranged at a heater housing, the connection unit body having a fuel flow volume in the connection unit body;a fuel release line connection area projecting from the connection unit body for connecting a fuel release line leading to a combustion chamber;a fuel feed line connection area projecting from the connection unit body for connecting a fuel feed line; andat least one functional unit for influencing a flow of fuel in the fuel flow volume, the at least one functional unit being provided in the connection unit body.2. A fuel connection unit in accordance with claim 1 , wherein the at least one functional unit comprises a pulsation damper.3. A fuel connection unit in accordance with claim 2 , wherein the pulsation damper comprises a pressure equalization volume and a flexible separating element separating the pressure equalization volume from the fuel flow volume.4. A fuel connection unit in accordance with claim 3 , wherein:the pulsation damper further comprises a pulsation damper body providing the pressure equalization volume;the flexible separating element is fixed at the pulsation damper body such that the flexible separating element closes the pressure equalization volume.5. A fuel connection unit in accordance with claim 3 , wherein a damper mounting recess receiving the pulsation damper is formed in the ...

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11-01-2018 дата публикации

Variable angle multi-point injection

Номер: US20180010563A1
Принадлежит: Delavan Inc

A nozzle for injecting liquid includes a nozzle body defining a flow channel and a swirl ante-chamber in fluid communication with the flow channel. An injection point orifice is defined in the swirl ante-chamber. The flow channel feeds into the swirl ante-chamber to impart a tangential flow component on fluids entering the swirl ante-chamber to generate swirl on a spray issuing from the injection point orifice. A second flow channel can be included in fluid communication with the swirl ante-chamber. The second flow channel feeds into the swirl ante-chamber in cooperation with or in opposition to the first flow channel. The first flow channel, second flow channel, and swirl ante-chamber are configured and adapted to adjust spray angle of a spray issuing from the injection point orifice by varying flow apportionment among the first and second flow channels.

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09-01-2020 дата публикации

SHAFT ACTUATED SWIRLING COMBUSTION SYSTEM

Номер: US20200011239A1

A combustor having an ion transport membrane therein and an adjustable swirler, which is mechanically connected at an inlet of a combustion zone of the combustor; a combustion system comprising the combustor, a feedback control system adapted to adjust swirler blades of the combustor based on a compositional variation of a fuel stream, and a plurality of feedback control systems to control operational variables within the combustor for an efficient oxy-combustion; and a process for combusting a fuel stream via the combustion system. Various embodiments of the combustor, the combustion system, and the process for combusting the fuel stream are disclosed. 14-. (canceled)5. A shaft actuated swirling combustion system , comprising: a cylindrical vessel with an internal cavity,', 'an ion transport membrane that divides the internal cavity of said cylindrical vessel into a first and a second concentric cylindrical zone, wherein the first concentric cylindrical zone is a feed zone and the second concentric cylindrical zone is a combustion zone,', 'a first inlet and a first outlet located in the feed zone, and a second inlet and a second outlet located in the combustion zone, and', 'a swirler that is connected to the second inlet, wherein the swirler has a plurality of adjustable blades with adjustable angles, a shaft, an outer casing and an actuator that rotates the blades and is secured inside the shaft;, 'a combustor of comprising'}an oxygen supplier located upstream of and fluidly connected to the first inlet via a feed line for supplying an oxygen-containing stream;a fuel supplier located upstream of and fluidly connected to the second inlet via a fuel line for supplying a fuel stream;an expander located downstream of and fluidly connected to the second outlet via an exhaust line for expanding an exhaust stream to generate power;a recycle line that fluidly connects the exhaust line to the fuel line;a mixer located upstream of the combustor and fluidly connected to the ...

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09-01-2020 дата публикации

PROCESS FOR COMBUSTION USING A SHAFT ACTUATED SWIRLING COMBUSTOR

Номер: US20200011240A1

A combustor having an ion transport membrane therein and an adjustable swirler, which is mechanically connected at an inlet of a combustion zone of the combustor; a combustion system comprising the combustor, a feedback control system adapted to adjust swirler blades of the combustor based on a compositional variation of a fuel stream, and a plurality of feedback control systems to control operational variables within the combustor for an efficient oxy-combustion; and a process for combusting a fuel stream via the combustion system. Various embodiments of the combustor, the combustion system, and the process for combusting the fuel stream are disclosed. 116-: (canceled)17: A process for combusting a fuel stream with a shaft actuated swirling combustor comprising:a cylindrical vessel with an internal cavity;an ion transport membrane that divides the internal cavity of said cylindrical vessel into a first and a second concentric cylindrical zone, wherein the first concentric cylindrical zone is a feed zone and the second concentric cylindrical zone is a combustion zone;a first inlet and a first outlet located in the feed zone, and a second inlet and a second outlet located in the combustion zone;a swirler that is connected to the second inlet, wherein the swirler has a plurality of adjustable blades with adjustable angles, a shaft, a casing and an actuator disposed in the shaft;a third concentric cylindrical zone which is sandwiched between the first and the second concentric cylindrical zones, defining a sweep zone; anda third inlet and a third outlet located in the sweep zone, the process comprising:combusting the fuel stream with molecular oxygen in the combustion zone to form an exhaust stream comprising water vapor and carbon dioxide;delivering an oxygen-containing stream to the first inlet of the combustor, wherein molecular oxygen present in the oxygen-containing stream is transported to the sweep zone through the ion transport membrane;flowing a portion of the ...

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09-01-2020 дата публикации

COMBUSTION DEVICE

Номер: US20200011524A1
Принадлежит: GRAND MATE CO., LTD.

A combustion device includes a first cover, a second cover, an infrared generating mesh, and a gas burner assembly, wherein the first cover has a plurality of through holes. A first half portion of the second cover has at least one hollow portion. A second half portion of the second cover is closed. The infrared generating mesh is disposed between the first cover and the second cover. A flame outlet of the gas burner assembly is located within a projection area of the second half portion. In this way, the intensity of the infrared rays generated by the combustion device could be increased and could be uniform. 1. A combustion device , comprising:a first cover having a first outer surface and a first inner surface which face opposite directions, wherein a plurality of through holes penetrating through the first outer surface and the first inner surface are disposed on the first cover;a second cover having a second outer surface and a second inner surface which face opposite directions, wherein the second cover is disposed on the first cover; a chamber is formed between the second inner surface and the first inner surface; the second cover is divided into a first half portion and a second half portion; at least one hollow portion penetrating through the second outer surface and the second inner surface is disposed on the first half portion; the second half portion is closed;an infrared generating mesh disposed between the first cover and the second cover and located in the chamber, wherein the infrared generating mesh is heated by a flame to generate infrared rays, and the generated infrared rays emit through the through holes; anda gas burner assembly having a flame outlet for burning gas to generate the flame to act on the infrared generating mesh, wherein the flame outlet is located within a projection area of the second half portion.2. The combustion device of claim 1 , wherein the first cover has a first peripheral portion; the second cover has a second ...

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21-01-2016 дата публикации

VENTURI DISK NON-EXPOSED FLAME AND ELECTRONIC CONTROLS HEATER

Номер: US20160018131A1
Принадлежит: MOBILE AIR, INC.

A portable heating apparatus includes a housing, a heat source, a fan, and a heat shield. The housing includes a fluid inlet and a fluid outlet. The fluid inlet is in fluid communication with the fluid outlet. The heat source is located within the housing. The fan creates a flow of fluid from the inlet to the outlet and is disposed between the heat source and the outlet. The heat shield is disposed between the heat source and the fan and is operable to restrict the flow of fluid between the heat source and the fan.

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16-01-2020 дата публикации

Smart Fuel Burning System and Method of Operating Same

Номер: US20200018480A1
Автор: Fu Guohong
Принадлежит:

A system configured to generate heat when supplied with a first fuel or a second fuel can include a fuel supply line operatively connected to a fuel source. A valve assembly can be operatively connected to the fuel supply line. A main burner can be operatively connected to the valve assembly. A thermoelectric generating system can be configured to transform heat to electricity. A first pilot burner can include at least one of a first thermocouple and a first Fe-ion sensor. A second pilot burner can include at least one of a second thermocouple and a second Fe-ion sensor. A printed circuit board (PCB) can be operatively connected to the valve assembly and the first and second pilot burners. The PCB can be configured to control operation of the valve assembly based on information received from at least one of the first and second pilot burners. 1. A system configured to generate heat when supplied with either a first fuel or a second fuel , the system comprising:a fuel supply line operatively connected to a fuel source, the fuel supply line being configured to convey either the first fuel or the second fuel;a valve assembly operatively connected to the fuel supply line, the valve assembly being configured to control a flow of fuel therethrough;a main burner operatively connected to the valve assembly, the main burner being configured to generate heat;a thermoelectric generating system operatively connected to the valve assembly, the thermoelectric generating system being configured to transform heat to electricity and including a first pilot burner and a second pilot burner, the first pilot burner including at least one of a first thermocouple and a first Fe-ion sensor, the second pilot burner including at least one of a second thermocouple and a second Fe-ion sensor; anda printed circuit board (PCB) operatively connected to the valve assembly and the first and second pilot burners, the PCB being configured to control operation of the valve assembly based on ...

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25-01-2018 дата публикации

PREFABRICATED INTEGRATED COMBUSTION ASSEMBLIES AND METHODS OF INSTALLING THE SAME INTO A COMBUSTION SYSTEM

Номер: US20180023810A1
Принадлежит:

Embodiments disclosed herein are directed to devices and methods for improving operation of a combustion system. According to various embodiments disclosed herein, a prefabricated integrated combustion assembly is disclosed that may be installed into a combustion chamber of a combustion system. The combustion system may be a new combustion system that is being manufactured or a conventional combustion system that is being retrofitted. 1. A method of installing a prefabricated integrated combustion assembly into a combustion chamber of a combustion system , the method comprising: a mounting plate mountable near a base of the combustion chamber;', 'a fuel nozzle assembly attached to or integrated with the mounting plate, the fuel nozzle assembly including a fuel nozzle and an oxidant outlet;', 'one or more supports attached to or integrated with the mounting plate; and', 'a perforated flame holder supported by the one or more supports and including a body having a plurality of apertures therein; and, 'inserting the prefabricated integrated combustion assembly into the combustion chamber of the combustion system, the prefabricated integrated combustion assembly includingattaching the mounting plate of the prefabricated integrated combustion assembly near the base of the combustion chamber.2. The method of wherein the combustion system produces less NOduring operation than when the perforated flame holder is absent.3. The method of wherein the prefabricated integrated combustion assembly includes insulation at least partially wrapped around the one or more supports.4. The method of wherein the fuel nozzle assembly and the perforated flame holder are positioned at a predetermined distance and have a predetermined orientation relative to each other.5. The method of wherein the oxidant outlet is at least partially defined by a tubular member claim 1 , and the fuel nozzle is at least partially positioned within the tubular member.6. The method of wherein the tubular member ...

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10-02-2022 дата публикации

METHOD FOR APPLYING A CATALYST TO A SURFACE OF THE CATALYTIC COMBUSTION BURNER

Номер: US20220042677A1
Принадлежит:

The present invention is directed to a method for applying a catalyst to the surface of a catalytic combustion burner that allows better distribution of the catalyst on the surface of the end piece of the burner, and thus prevents too high a temperature at the central zone. The present invention is also directed to a catalytic combustion burner which can be coated with a catalyst in accordance with the method of the invention, and to a catalytic combustion bottle adapted to contain a combustible liquid and to receive at its neck a catalytic combustion burner of the invention. 1. Method for applying a catalyst to the surface of a catalytic combustion burner , said catalytic combustion burner being composed of a porous material and comprising:an end piece with an upper part and a lower part, said upper part having a peripheral side wall comprising an inner face delimiting a cavity, an essentially cylindrical outer face, and a crown-shaped upper face, and a sleeve disposed in the extension of said lower part of said end piece, and comprising a cavity adapted to grip a wick intended to convey a combustible composition to the burner, [{'b': 9', '10, 'A) a step of impregnating said outer face and, either, said inner face, said crown of the end piece, or said inner face and said crown, with a catalytic composition comprising at least one catalyst belonging to groups or of the Periodic Table of the Elements;'}, 'B) a step of heat-treating said burner thus impregnated with the catalyst to a temperature Ta of at least 450° C.;, 'said method comprising{'sub': 'c', 'said method being characterized in that said catalytic composition is a non-newtonian fluid exhibiting, before application on the end piece, a dynamic viscosity μof at least 15 mPa·s at 20° C.'}2. Method according to claim 1 , wherein said catalytic composition comprises:{'b': 9', '10, 'between 1% and 5% by weight, relative to the total weight of the catalytic composition, of a catalyst selected from metals ...

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23-01-2020 дата публикации

VEHICLE HEATER

Номер: US20200023712A1
Автор: Collmer Andreas
Принадлежит:

A vehicle heater includes a burner area includes a circumferential wall providing a combustion chamber, a flame tube with a first end forming or adjacent to a part of the combustion chamber circumferential wall and a second flame tube end. A heat exchanger housing has a circumferential wall enclosing the flame tube. A waste gas backflow space is formed, between an outer side of the flame tube and an inner side of the heat exchanger housing circumferential wall, with an inlet area at the second flame tube end and with an outlet area in the area of the first flame tube end. An inner dimension of the circumferential wall increases in the direction from an inlet area of the waste gas backflow space to an outlet area. An outer dimension of the flame tube increases in the direction from the second flame tube end to the first flame tube end. 1. A vehicle heater comprising:a burner configuration comprising a combustion chamber circumferential wall circumferentially enclosing a combustion chamber;a flame tube with a first flame tube end adjoining the combustion chamber circumferential wall or forming at least a part of the combustion chamber circumferential wall or adjoining the combustion chamber circumferential wall and forming at least a part of the combustion chamber circumferential wall and a second flame tube end open in a direction of a flame tube longitudinal axis for the discharge of combustion waste gas;a heat exchanger housing comprising heat exchanger housing circumferential wall circumferentially enclosing the flame tube on a flame tube outside and a heat exchanger housing bottom located axially opposite the second flame tube end, a waste gas backflow space with an inlet area at the second flame tube end and with an outlet area adjacent to the first flame tube end being formed between an outer side of the flame tube and an inner side of the heat exchanger housing circumferential wall, wherein an inner dimension of the heat exchanger housing circumferential wall ...

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01-02-2018 дата публикации

COMBUSTION BURNER AND BOILER

Номер: US20180031232A1
Принадлежит: Mitsubishi Hitachi Power Systems, Ltd.

In this combustion burner and boiler, interference of ignition in a flame stabilizer is suppressed and flame stabilizing performance is improved by providing: a fuel nozzle which ejects a fuel gas that is a mixture of pulverized coal and air; a combustion air nozzle which ejects a fuel gas combustion air from outside of the fuel nozzle; a secondary air nozzle which ejects secondary air from the outside of the combustion air nozzle; and a flame stabilizer which comprises a first flame stabilizer main body which is arranged at the leading end of the fuel nozzle and separated by a prescribed space from the inner wall surface of the fuel nozzle and which forms a ring shape having as the center an axial line along the ejection direction of the fuel gas. 112-. (canceled)13. A combustion burner comprising:a fuel nozzle configured to eject fuel gas obtained by mixing fuel and air;a secondary air nozzle configured to eject air from outside the fuel nozzle;a flame stabilizer including a plurality of flame stabilizer main bodies disposed on a leading end of the fuel nozzle, the plurality of flame stabilizer main bodies being separated from each other by a predetermined space, and separated from an inner wall surface of the fuel nozzle by a predetermined space; anda plurality of support members supporting the plurality of flame stabilizer main bodies on the inner wall surface of the fuel nozzle.14. The combustion burner according to claim 13 , wherein:the plurality of flame stabilizer main bodies are disposed in a lattice form or a staggered form on a surface that is orthogonal to a flow direction of the fuel gas.15. The combustion burner according to claim 13 , wherein:portions of the plurality of flame stabilizer main bodies that face each other are provided with a flat surface portion.16. The combustion burner according to claim 13 , wherein:the flame stabilizer main body forms a triangular cross-sectional shape that widens facing downstream in an ejection direction of the ...

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30-01-2020 дата публикации

NOZZLE

Номер: US20200030828A1
Принадлежит:

A nozzle for an abatement apparatus and a method are disclosed. The nozzle is for abatement apparatus operable to treat an effluent stream from a processing tool, the nozzle comprises: a nozzle body defining a nozzle inlet operable to receive the effluent stream, a nozzle outlet, and a conduit extending between the nozzle inlet and the nozzle outlet and operable to convey the effluent stream in a direction of flow from the nozzle inlet to the nozzle outlet; and an effluent stream rotator configured to impart a rotational component to the effluent stream to rotate the effluent stream around the direction of flow. In this way, the effluent stream is rotated as it passes through the nozzle body. The destruction rate efficiency achieved by an abatement apparatus when receiving such rotating effluent streams has been found to be significantly improved compared to non-rotating effluent streams. 1. A nozzle for abatement apparatus operable to treat an effluent stream from a processing tool , said nozzle comprising: a nozzle inlet operable to receive said effluent stream,', 'a nozzle outlet, and', 'a conduit extending between said nozzle inlet and said nozzle outlet and operable to convey said effluent stream in a direction of flow from said nozzle inlet to said nozzle outlet; and, 'a nozzle body defining'}an effluent stream rotator configured to impart a rotational component to said effluent stream to rotate said effluent stream around said direction of flow.2. The nozzle of claim 1 , wherein said effluent stream rotator is configured to rotate said effluent stream about a flow axis defined by said direction of flow.3. The nozzle of claim 1 , wherein said effluent stream rotator is configured to rotate said effluent stream into a vortex.4. The nozzle of claim 1 , wherein said effluent stream rotator comprises a protruding structure upstanding from a surface of said conduit.5. The nozzle of claim 4 , wherein said protruding structure is helical.6. The nozzle of claim 4 , ...

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17-02-2022 дата публикации

PRE-MIX BURNER ASSEMBLY FOR LOW NOx EMISSION FURNACE

Номер: US20220049875A1
Принадлежит: Lennox Industries Inc

A burner assembly according to aspects of the disclosure includes a burner surface carried by a burner, the burner surface extending outward from a front side of the burner, a housing coupled to the burner on a side opposite the front side of the burner, a gasket disposed between the burner and the housing, a thermally anisotropic protective covering located on the front side of the burner and surrounding a perimeter of the burner surface, and an igniter positioned adjacent to the burner surface.

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31-01-2019 дата публикации

Low emissions combustor assembly for gas turbine engine

Номер: US20190032559A1
Принадлежит: United Technologies Corp

A combustor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a combustion chamber, and a fuel injector assembly in communication with the combustion chamber that has a swirler body situated about a nozzle to define an injector passage that converges to a throat. The throat is defined at a distance from the combustion chamber. The nozzle includes a primary fuel injector along a first fuel injector axis and at least one secondary plain jet fuel injector axially forward of the primary fuel injector.

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31-01-2019 дата публикации

Coal nozzle assembly comprising two flow channels

Номер: US20190032914A1
Принадлежит:

A coal nozzle assembly for a steam generation apparatus comprising an elongated nozzle body having a nozzle tip at one end thereof; said nozzle tip comprising two channels, each channel having curved or buckled flow paths, the nozzle tip further comprising parting means separating the channels from each other, wherein the directions of the flow paths of the channels at their ends distal from the nozzle body enclose an angle between 0° and 90°. This promotes intersecting and shearing the two partial streams outside the nozzle assembly resulting in a better combustion with reduced NOx-emissions. 1. A coal nozzle assembly for a steam generation apparatus comprising an elongated nozzle body having a nozzle tip at one end thereof; said nozzle tip comprising two channels each channel having a curved or buckled flow path , the nozzle tip further comprising means separating the channels from each other , wherein the directions of the flow paths of the channels at their ends distal from the nozzle body enclose an angle greater than 0° and equal to or less than 90°.2. A coal nozzle assembly for a steam generation apparatus comprising an elongated nozzle body and an inner shell having two nozzle tips at one end thereof; the coal nozzle assembly further comprising means being located in the inner shell upstream of said two nozzle tips and splitting the flow from said nozzle body into the two nozzle tips , the directions of the flow paths of the two nozzle tips enclosing an angle (α) greater than 0° and equal to or less than 90°.3. Coal nozzle assembly according to wherein that the nozzle tips are mounted for pivotal movement about an axis being orthogonal with respect to the longitudinal axis of the elongate body or the inner shell.4. Coal nozzle assembly according to wherein at least one of the nozzle body or the inner shell and the nozzle tips partially overlap.5. Coal nozzle assembly according to in wherein the assembly further comprises an air housing.6. Coal nozzle ...

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31-01-2019 дата публикации

Burner

Номер: US20190032916A1
Принадлежит: Rinnai Corp

A burner has: a combustion plate part for ejecting air-fuel mixture; and a flame rod which lies opposite to a portion of the combustion plate part which has a picture-frame-like burner frame; a metal-fiber knit which covers an opening enclosed by the burner frame; and a distribution plate which has formed therein distribution holes and which sandwiches the metal-fiber knit between the burner frame and the distribution plate through the distribution holes and the metal-fiber knit. The flame rod has: a rod base part which lies opposite to a portion of opening peripheral part of the burner frame which is positioned on the same surface level as the opening; and a rod main body part which lies opposite to a portion of the metal-fiber knit. The distance between the rod base part and the opening peripheral part is made smaller than the distance between the rod main body part and the metal-fiber knit.

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30-01-2020 дата публикации

COMBINED BURNER FOR BLOWING OXIDIZING GAS AND FUEL INTO MELTING FURNACE

Номер: US20200032998A1
Автор: BRHEL Jaroslav
Принадлежит: HTT ENGINEERING, SPOL. S R.O.

Combined burner for blowing oxidizing gas and fuel into melting furnace, which is fixedly installed into the furnace and provided with outlet apertures for fuel and oxidizing gas, consists, according to this invention, of fixed part () of the burner () and of a movable nozzle (), which is rotatably installed inside the body () of the fixed pan () of the burner, supply () of the oxidizing gas is connected to the movable nozzle () and it is controlled by actuator (), installed outside of the working space of the furnace, while the axis x2 of the orifice of the movable nozzle () is diverted front the rotation axis x1 of the movable nozzle () by angle a in the range of 5-60° and the movable nozzle () is rotatable around the axis X1 in any direction by angle β in the range of 0-180°. The movable nozzle allows directing blown gases into various places in the furnace. At the same time, the whole burner is fixedly installed in the wall or ceiling, or the cover of the furnace, and the space of the furnace thus remains sealed. 15-. (canceled)6. A combined burner for blowing oxidizing gas and fuel into a melting furnace , the combined burner being fixedly installed into the melting furnace and being provided with outlet apertures for fuel and oxidizing gas , wherein the burner comprises:a fixed part; anda movable nozzle, the movable nozzle having outlets for both fuel and oxidizing gas,wherein the movable nozzle is rotatably installed inside a body of the fixed part of the burner,wherein a supply of the oxidizing gas is connected to the movable nozzle and motion of the movable nozzle is controlled by an actuator, installed outside of a working space of the melting furnace,{'sub': 2', '1', '1, 'wherein an axis xof an orifice of the movable nozzle is diverted from a rotation axis xof the movable nozzle by angle α in the range of 5-60°, and the movable nozzle is rotatable around the rotation axis xin any direction by an angle β in the range of 0-180°.'}7. The combined burner ...

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11-02-2016 дата публикации

Condensate Trap for Heating-Cooling Systems

Номер: US20160040921A1
Принадлежит: Lennox Industries Inc

A condensation trap comprising an inlet chamber, a vent chamber and an outlet chamber. The inlet chamber is configured to receive condensate fluid through an external opening therein. The vent chamber is in fluid communication with the inlet chamber via a first passageway that includes an internal opening of the inlet chamber. The internal opening is located substantially at an opposite end of the vent chamber as the external opening. The outlet chamber is in fluid communication with the vent chamber via a second passageway that includes an internal opening in a sidewall of the vent chamber and an interior opening in an end of the outlet chamber. The outlet chamber is configured to transmit the condensate fluid through an exterior opening located at an opposite end of the outlet chamber. A vent volume portion is greater than a total volume of an internal space of the inlet chamber.

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09-02-2017 дата публикации

DOWN-FIRED BURNER WITH A PERFORATED FLAME HOLDER

Номер: US20170038064A1
Принадлежит:

A down-fired flame burner includes a flame holder positioned below the burner. The flame holder includes a plurality of perforations that collectively confine a combustion reaction of the burner to the flame holder. 1. A down-fired burner comprising:a down-fired fuel nozzle configured to output fuel in a downward direction;an oxidant source configured to output an oxidant; and an input surface facing the down-fired fuel nozzle;', 'an output surface opposite the fuel nozzle; and', 'a plurality of perforations extending from the input surface to the output surface and collectively configured to promote a combustion reaction of the fuel and oxidant within the perforations., 'a flame holder positioned below the down-fired fuel nozzle, the flame holder including2. The down-fired burner of claim 1 , wherein the flame holder is configured to contain a majority of the combustion reaction within the perforations.3. The down-fired burner of claim 1 , wherein the flame holder is configured to contain 80% or more of the combustion reaction within the perforations.4. The down-fired burner of claim 1 , wherein the flame holder is a refractory material.5. The down-fired burner of claim 1 , wherein the flame holder is an integral structure.6. The down-fired burner of claim 1 , wherein the flame holder is configured to initiate the combustion reaction.7. The down-fired burner of claim 1 , comprising a preheating mechanism configured to heat the flame holder prior to starting the combustion reaction.8. The down-fired burner of claim 7 , wherein the preheating mechanism comprises a second fuel nozzle configured to generate a flame adjacent to the flame holder.9. The down-fired burner of claim 7 , wherein the preheating mechanism comprises a laser configured to irradiate the flame holder.10. The down-fired burner of claim 7 , wherein the down-fired fuel nozzle is an adjustable nozzle and the preheating mechanism is configured to move the fuel nozzle closer to the flame holder during a ...

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09-02-2017 дата публикации

Pre-Film Liquid Fuel Cartridge

Номер: US20170038074A1
Принадлежит: General Electric Co

A pre-film liquid fuel cartridge ( 20 ) includes a primary liquid fuel passage ( 106 ), a plurality of inner fuel ports ( 116 ) and a plurality of outer fuel ports ( 124 ) that are in fluid communication with the primary liquid fuel passage. An inner pre-filming surface ( 142 ) is defined downstream from the plurality of inner fuel ports. The inner pre-filming surface ( 142 ) terminates at a first shear edge ( 140 ). An outer pre-filming surface ( 152 ) is defined downstream from the plurality of outer fuel ports. The outer pre-filming surface ( 152 ) terminates at a second shear edge ( 154 ). The first and second shear edges are relatively oriented so that a first pre-filmed liquid fuel sheet exiting the first shear edge intersects with a second pre-filmed liquid fuel sheet exiting the second shear edge, thereby atomizing the first and second pre-filmed liquid fuel sheets.

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12-02-2015 дата публикации

BURNER FOR THE GASIFICATION OF A SOLID FUEL

Номер: US20150041718A1
Принадлежит: SHELL OIL COMPANY

The invention is directed to a burner for the gasification of a solid fuel, comprising a burner front having an opening for discharging a solid fuel, wherein the opening for discharging the solid fuel is fluidly connected to a central passage way and wherein the central passage way has a downstream part wherein the diameter of the passage way increases over a first length and subsequently decreases over a second length terminating at the burner front and wherein inside the downstream part of the central passage way a hollow member is positioned, and wherein the hollow member has an internal increasing diameter and inner decreasing diameter aligned with the increasing and decreasing diameter of the hollow member and wherein the connecting conduits have a discharge opening positioned in the diverging part of the hollow member. 1. A burner for the gasification of a solid fuel , comprising a burner front having an opening for discharging a solid fuel and a single central opening for discharging an oxygen containing gas , wherein the opening for discharging the solid fuel is fluidly connected to a central passage way and wherein the opening for discharging the oxygen containing gas is fluidly connected to an annular passage way for passage of oxygen positioned co-axially with the central passage way andwherein the central passage way has a downstream part wherein the diameter of the passage way increases over a first length and subsequently decreases over a second length terminating at the burner front and wherein inside the downstream part of the central passage way a hollow member is positioned which is closed at one end and has an opening at the burner front, the hollow member having an increasing diameter and decreasing diameter aligned with the increasing and decreasing diameter of the central passage way to form an annular passage for the solid fuel terminating at burner front in a inwardly directed annular opening for discharging the solid fuel{'b': '17', 'and ...

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24-02-2022 дата публикации

BURNER SYSTEM AND METHOD FOR PROVIDING THERMAL ENERGY

Номер: US20220057083A1
Принадлежит:

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. 1. A burner system for providing thermal energy , the burner system comprising:an evaporator device for vaporizing a liquid fuel and providing vaporized fuel,a burner air supply device for providing burner air,a surface burner for burning a fuel mixture comprising the vaporized fuel and burner air to provide an exhaust gas stream,a shielding plate with openings for passing and controlling the thermal energy of the exhaust gas flow of the surface burner, whereinthe surface burner is coupled to the evaporator device via the shielding plate in such a way that, in operation, the exhaust gas flow of the surface burner provides the thermal energy and the evaporation temperature required for complete evaporation of the fuel in the evaporator device, anda tertiary air supply means for supplying tertiary air to the exhaust gas stream to adjust a temperature of the exhaust gas stream by mixing with the tertiary air to form a hot gas stream.2. The burner system according to claim 1 ,whereinthe thermal energy of the exhaust gas flow can be provided in the form of diluted exhaust gas, and this thermal energy is delivered in the form of tempered air directly or via a separately designed heat exchanger device to a device coupled to the burner system, this device being an internal combustion engine or a fuel cell stack or a battery.3. The burner system according to claim 1 ,whereinthe surface burner comprises a burner screen and a metal or ceramic fiber mesh connected together, a diffuser, an ignition ...

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15-02-2018 дата публикации

BURNER

Номер: US20180045406A1
Принадлежит:

A burner comprising a base cup, an annular flame splitter, and a flame cover. The base cup comprises an air inlet channel) and two nozzles in communication with the air inlet channel and arranged upwards. The annular flame splitter arranged on the base cup comprises two Venturi tubes respectively arranged opposite the two nozzles. The annular flame splitter is separated from the base cup to form a gap, thus allowing primary air to enter the two Venturi tubes from the gap to be mixed with a fuel gas sprayed into the two Venturi tubes by the two nozzles to form a gaseous mixture. Groove openings are formed on the top of the annular flame splitter in communication with the mixing cavity. The flame cover covers the mixing cavity and limits the groove openings to define the outlet for the gaseous mixture, thus forming a flame ring. 1. A burner , comprising:a bottom cup having a gas input passage and two nozzles communicated with the gas input passage and arranged upwards;a ring-shaped flame distributor disposed to the bottom cup and comprising two venturi tubes respectively opposite to the two nozzles, the flame distributor being spaced apart from the bottom cup to define a gap therebetween, such that a primary air is allowed to enter the two venturi tubes through the gap to mix with a fuel gas sprayed into the two venturi tubes from the two nozzles so as to form a mixed gas, the flame distributor being provided with a ring-shaped mixing chamber communicated with the venturi tubes, and having a notch formed at a top portion of the flame distributor and communicated with the mixing chamber; anda burner cover disposed to the flame distributor, the burner cover being configured to cover the mixing chamber and limit the notch to define an outlet of the mixed gas, thereby forming a flame ring.2. The burner according to claim 1 , wherein the gas input passage is configured to have a straight line shape claim 1 , and the flame distributor presents a circular-ring shape claim 1 ...

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08-05-2014 дата публикации

Gas turbine burner

Номер: US20140123652A1
Принадлежит: General Electric Co

A gas turbine includes a compressor and at least one combustor downstream from the compressor. The combustor includes a burner having an inner shroud extending axially along at least a portion of the burner, an outer shroud radially separated from the inner shroud and extending axially along at least a portion of the burner, and a plurality of stator vanes extending radially between the inner shroud and the outer shroud. The stator vanes have an inner end proximate the inner shroud and an outer end proximate the outer shroud. The burner further includes a vortex tip at one of either the inner end or the outer end of the stator vanes. The vortex tip provides a gap between the inner end and the inner shroud or the outer end and the outer shroud, and the vortex tip includes a plurality of fuel ports. The gas turbine further includes a turbine downstream from the combustor.

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19-02-2015 дата публикации

LOW NOx BURNER

Номер: US20150050605A1
Принадлежит: Haul All Equipment Ltd

A low NOx burner has a housing that includes a burner head defining a gas manifold and a primary flame zone downstream of the burner head. The burner has a gas inlet for receiving gas. Flow-through air vents are disposed around a center of the burner head and extending through the burner head thereby enabling cold core air to flow from an annular core space upstream of the burner head to the primary flame zone downstream of the burner head. The burner also includes a plurality of premix air vents in fluid communication with the manifold for premixing air and gas within the manifold and for emitting premixed air and gas into the primary flame zone. A plurality of staging pipes extend from the manifold into the primary flame zone for conveying gas into the primary flame zone. The burner includes an ignition device extending into the primary flame zone.

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03-03-2022 дата публикации

Torch Heat Shield

Номер: US20220065443A1
Автор: Aaron GOMEZ
Принадлежит: Individual

A torch heat shield attachment for a butane torch or similar device includes an outer mesh material that is wrapper around an inner aluminum cylinder. The outer mesh material forms an outer mesh cylinder spaced around an inner mesh cylinder via a plurality of fasteners that secure the mesh in its cylindrical shape while spacing the formed inner and outer mesh cylinders to form a gap therebetween. The fasteners are removable and rearrangeable to customize the appearance of the torch heat shield. The aluminum plate, the two mesh cylinders formed by the mesh material, and the gap formed between the two mesh cylinders help to shield a user of the torch from excess heat by dissipating the heat from the torch tip.

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03-03-2022 дата публикации

LOW-NOX AIR HEATING SWIRL BURNER

Номер: US20220065444A1
Принадлежит:

A low NOx air heating swirl burner includes at least one burner unit, the burner unit comprising a combustion air duct, a fuel gas supply pipeline, a combustion nozzle and a fire protection baffle. The fire protection baffle comprises a fin and a base plate for generating swirl combustion air. The base plate includes a plurality of elongated holes and air guide blades disposed obliquely on air outlet sides of the elongated holes. The combustion air flows out of the elongated holes in the base plate of the fire protection baffle, generates a rotational flow under the action of the air guide blades to be strongly mixed with fuel gas sprayed from the combustion nozzle for combustion. The burner is in a modular form, which can adopt a corresponding splicing shape according to structural features of a heating space to meet the heating requirement.

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26-02-2015 дата публикации

Airblast fuel injector

Номер: US20150052899A1
Автор: Ian James Toon
Принадлежит: Rolls Royce PLC

An airblast fuel injector for a gas turbine engine fuel spray nozzle has, in order from radially inner to outer, a coaxial arrangement of an inner air swirler passage, an annular fuel passage, an annular outer air swirler passage, and an annular shroud air swirler passage. The injector further has an annular shroud having an inner surface profile. Relative to the overall axial direction of flow through the injector the shroud inner surface profile has a convergent section followed by a divergent section, the transition of which forming a first inwardly directed annular nose. The injector further has an annular wall having an outer surface profile, and having an inner surface profile. Relative to the overall axial direction of flow through the injector the wall outer surface profile has a convergent section followed by an outwardly turning section which faces across the shroud air passage to the first nose.

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26-02-2015 дата публикации

Fuel-burning fireplace

Номер: US20150053200A1
Автор: Gilles-Andre Poupart
Принадлежит: Eco-Feu

A burner system for a fuel-burning fireplace having a fuel container with at least one aperture for combusting the fuel contained therein and an adjustable flame regulator for regulating a size of the flame. The flame regulator comprises a shutter for covering the aperture having a shape corresponding to the aperture, the shutter being variably adjustable between a first position (covered aperture) and a second position (exposed aperture); a handle extending from the burner system for variably adjusting the shutter; and a connecting member for connecting the shutter to the handle, the connecting member being secured to at least two extremities of the shutter; wherein movement of the handle allows a balanced movement of the shutter over the aperture.

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23-02-2017 дата публикации

FIELD-READY OVEN

Номер: US20170049266A1
Принадлежит: GHT GLOBAL HEATING TECHNOLOGIES AG

A field-ready oven has reinforced telescoped side walls that extend and hold a base, shelf, tray support and cover spaced apart. A low air intake and a semipermeable membrane deliver air and vapor fuel to catalyst pads on the shelf. Radiant heat from exothermic reaction is diffused over a bottom of a tray. Hot gas circulates around the diffuser and tray with a chimney effect before exhausting. A lid on the cover lifts for access to the tray. A fuel container in the oven forces fuel through a capillary restriction to limit fuel flow. A spring in the container is released to start fuel flow. 1. An apparatus comprising a field-ready oven comprising:an oven box having a cover having a top surface, cover side walls and at least one support for holding at least one tray of contents and a base having a bottom surface, a false bottom and base side walls, wherein the false bottom is spaced above the base bottom surface and wherein the base bottom surface, base false bottom and base side walls define a false bottom cavity in the base;wherein the cover top surface, base false bottom and side walls define an oven cavity in the oven box for containing at least one tray of contents;at least one catalytic heater assembly within the oven cavity that is configured for a flameless catalytic chemical reaction and comprised of one or more catalyst pads and a semipermeable or porous membrane for delivery of fuel vapor to the one or more catalyst pads;a fuel source in communication with the catalytic heater assembly for allowing fuel to flow to the catalyst pad;a fuel motivator connected to the fuel source;an initiation system connected to the fuel motivator;at least one tray of contents having a top surface, bottom surface and sides;at least one air entry port in the base side walls near the lower portion of the base for admitting air into the false bottom cavity;at least one air flow opening in the base false bottom for passage of air from the false bottom cavity into the oven cavity, ...

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13-02-2020 дата публикации

Solid Fuel Burning System and Method with Electronic Ignition

Номер: US20200049344A1
Автор: Masterson Daniel J.
Принадлежит:

A solid fuel burning system and method with an electronic ignition system is provided having a filament and a filament support. The filament support positions the filament adjacent the wick or bridge within a hollow core. 1. A wax burning system comprising:a melted wax reservoir;a melting grate configured to receive a solid wax, the melting grate located above at least a portion of the melted wax reservoir so that wax melted on the melting grate can be received into the melted wax reservoir;a wick comprising a hollow core, and an upper exit opening in communication with the hollow core;an electronic ignition system comprising a filament and a filament support, the filament is attached to the filament support, the filament support positions the filament adjacent the wick, the filament is configured to receive power from a power source and to generate heat.2. The system of claim 1 , the filament and the filament support are located within the hollow core of the wick.3. The system of claim 1 , wherein the electronic ignition system comprises an electronic circuit; the filament is connected to the electronic circuit; the electronic circuit is configured to direct power from a power source to the filament claim 1 , to generate heat at the filament.4. The system of claim 3 , wherein the electronic ignition system comprises a switch claim 3 , the switch is connected to the electronic circuit claim 3 , the electronic circuit is configured to direct power from a power source to the filament claim 3 , to generate heat at the filament claim 3 , when the switch is activated.5. The system of claim 4 , wherein the electronic ignition system comprises a timer and the electronic ignition system is configured to direct power to the filament for a predetermined amount of time after the switch is activated.6. The system of claim 1 , wherein the electronic ignition system is configured to direct power from a power source to the filament to generate heat at the filament above 375 ...

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13-02-2020 дата публикации

GAS BURNER FOR BOILER

Номер: US20200049345A1
Принадлежит:

A gas burner () comprises a support plate () with a passage opening () for the gas and an annular wall () formed around the passage opening (), a diffusing wall () and a further flow element () inserted on the annular wall () in flow communication with the passage opening (), wherein the annular wall () forms a plurality of punches () with a recess () and an opposite projection (), wherein the recess () accommodates a locking protuberance () of the diffusing wall () and the projection () extends in a locking hole () of the further flow element (). 11. Gas burner () for boiler , comprising:{'b': '19', 'a diffusing wall () on which the combustion takes place,'}{'b': 2', '1', '2', '8', '11', '8', '12', '14, 'a support plate () for the connection of the burner () to a combustion chamber, said support plate () having a passage opening () for the gas and a continuous or interrupted annular wall () formed around the passage opening () and having a radially inner surface () and a radially outer surface (),'}{'b': 20', '21', '22, 'optionally a further flow element (, , ),'}{'b': 19', '20', '21', '22', '2', '8', '33', '34', '11, 'wherein the diffusing wall () and, optionally, the additional flow element (, , ), are connected to the support plate () and in flow communication with the passage opening () by mutual insertion of an annular end region (, ) thereof with the annular wall (),'}{'b': 16', '11', '17', '14', '23', '12, 'characterized in that a plurality of punches () is formed in the annular wall () forming each a recess () in the radially outer surface () and a corresponding projection () on the radially inner surface (),'}{'b': 17', '25', '33', '19', '23', '24', '33', '34', '20', '21', '22', '19, 'wherein the recess () is adapted to accommodate a locking protuberance () of the end region () of the diffusing wall () and the projection () is adapted to extend in a locking hole () of the end region (; ) of the further flow element (, , ) and/or of the diffusing wall ().'} ...

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13-02-2020 дата публикации

BURNERS FOR CONVERSION OF METHANE TO OLEFINS, AROMATICS, AND NANOPARTICLES

Номер: US20200049346A1
Принадлежит:

Embodiments of the present disclosure describe burner () configurations used in an industrial process to convert methane to olefins, aromatics, and nanoparticles/nanomaterials. Both a vitiated coflow burner and piloted turbulent burner with inhomogeneous inlets are disclosed. 1. A method of controlling secondary reactions of a burner of combustion products using injected methane , the method comprising:establishing a jet flame in coaxial flow of hot combustion products from a premixed vitiated coflow of gas passing through a porous plate or catalytic monolith, said jet flame established by gas exiting from a central tube;providing a tube positioner to translate the tip of the central tube to an offset height relative to the porous plate or catalytic monolith; andcontrolling the tube positioner to vary the offset height of the central tube tip in a dynamic manner based on chemical inputs, with said controlling resulting in different secondary reactions of combustion products from the burner.2. The method of claim 1 , wherein the central tube is a blunt-tipped tube and the gas exiting the central tube is methane.3. The method of claim 1 , wherein the coflow gas is a combination of methane and oxygen.4. The method of claim 1 , wherein offset height of the central tube tip is controlled to provide both a methane/oxygen combustion process and subsequent pyrolysis of methane to form olefins claim 1 , aromatics or nanoparticles.5. A method of controlling secondary reactions of a burner of combustion products using injected methane claim 1 , the method comprising:establishing a jet flame in coaxial flow of hot combustion products from gas passing through a porous plate or catalytic monolith, with said jet flame established by a piloted turbulent burner with inhomogeneous inlets and defining three concentric tubes;providing a tube positioner to translate an innermost one of the three concentric tubs to different positions relative to an intermediate tube; andcontrolling the ...

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10-03-2022 дата публикации

ASSEMBLY AND METHOD FOR INJECTING A GASEOUS COMBUSTION AGENT

Номер: US20220074592A1
Принадлежит:

An assembly for injecting a gaseous combustion agent into a combustion zone, the assembly having a chamber having an inlet, through which the agent is introduced into the assembly; at least one primary injector configured to convey a primary flow of the agent from the chamber toward the combustion zone, at least one secondary injector for conveying a secondary flow of the agent from the chamber toward the combustion zone, a pressure detector; a regulating; and a control system connected to the pressure detector and to the regulating system, the control system controlling the regulating system so that the flow section of the at least one secondary passage is regulated as a function of the pressure or of the variation in pressure detected by the pressure detector. 115.-. (canceled)16. An assembly for injecting a gaseous combustion agent into a combustion zone , which gaseous combustion agent is selected from gaseous fuels and gaseous oxidants , the assembly comprising:a chamber comprising an inlet, through which the agent is introduced into the assembly;at least one primary injector configured to convey a primary flow of the agent from the chamber toward the combustion zone and for injecting said primary flow into the combustion zone, said at least one primary injector being fluidly connected to the chamber by means of at least one primary passage;at least one secondary injector for conveying a secondary flow of the agent from the chamber toward the combustion zone and for injecting said secondary flow into the combustion zone, said at least one secondary injector being fluidly connected to the chamber by means of at least one secondary passage;a pressure detector for detecting a gas pressure or a variation in gas pressure in the chamber;a regulating system for regulating a flow section of the at least one secondary passage; anda control system connected to the pressure detector and to the regulating system, the control system controlling the regulating system so that ...

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03-03-2016 дата публикации

Burners for submerged combustion

Номер: US20160060154A1
Принадлежит: Corning Inc

A burner for submerged combustion melting that mixes a first gas and a second gas inside the burner and emits the mixed gas through a nozzle for combustion below the surface of the material being melted. The burner includes a hollow tube and a static mixer inside the tube that mixes the first gas and the second gas as they travel through the tube. The mixed first and second gas exits a nozzle on a top end of the tube and is ignited to generate a flame below the surface of the material being melted, which may be a glass material.

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03-03-2016 дата публикации

BURNER

Номер: US20160061443A1
Принадлежит: Haldor Topsoe A/S

A burner with a plurality of oxidant gas pipes distributed throughout the cross section of the burner and process gas in plug flow provides even mixing of the oxidant and the process gas. 1. Burner for a catalytic reactor comprising an oxidant gas inlet , a process gas inlet , a plurality of oxidant gas pipes connected to the oxidant gas inlet at their upstream end and an oxidant nozzle at the downstream end of each pipe , wherein the pipes are arranged with sufficient spacing between the downstream end of adjacent pipes to ensure that the process gas flows between the pipes before mixing with the oxidant gas , the length of each pipe is at least five times the inner diameter of the pipe.2. Burner according to claim 1 , wherein a plurality of the oxidant nozzles have a non-circular outlet opening cross-section.3. Burner according to claim 2 , wherein said non-circular outlet opening cross section is oval.4. Burner according to claim 2 , wherein said oxidant nozzle non-circular outlet opening cross sections are achieved by pressing the outlet of the pipes from at least two opposing sides until a plastic deformation of said pipes is achieved.5. Burner according to claim 1 , wherein the orientation of each oxidant nozzle define an oxidant gas outlet direction and wherein the outlet direction of at least two oxidant nozzles are not parallel.6. Burner according to claim 1 , wherein at least one perforated plate is located between the process gas inlet and the oxidant nozzle outlet openings claim 1 , thereby balancing the process gas flow across the cross section of the burner.7. Burner according to claim 6 , wherein two perforated plates are located between the process gas inlet and the oxidant nozzle outlet openings claim 6 , thereby balancing the process gas flow across the cross section of the burner towards a plug flow but minimizing the pressure loss caused by the perforated plates.8. Burner according to claim 7 , wherein the distance between the two perforated ...

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01-03-2018 дата публикации

FUEL NOZZLE

Номер: US20180058694A1
Принадлежит:

A method for delivering fuel from a fuel nozzle of a combustor of a gas turbine engine includes directing fuel from a fuel source through a flow splitter to provide at least two concentric fuel flows, filming the concentric two fuel flows on concentrically arranged inwardly facing filming surfaces that are disposed downstream of the flow splitter, and atomizing the concentric fuel flows into a core air flow. 1. A method for delivering fuel from a fuel nozzle of a combustor of a gas turbine engine , the method comprising:directing a core air flow through a primary air passage of the fuel nozzle, the primary air passage extending centrally within the fuel nozzle and terminating at an exit located at a downstream end of the fuel nozzle;directing fuel from a fuel source through a flow splitter to provide at least two concentric fuel flows, the flow splitter disposed downstream of the exit of the primary air passage;filming the at least two concentric two fuel flows on concentrically arranged and radially inwardly facing filming surfaces disposed downstream of the flow splitter; andatomizing the at least two concentric fuel flows into the core air flow exiting the primary air passage.2. The method of claim 1 , further comprising imparting a momentum to the pressurised fuel before filming the at least two concentric two fuel flows; anddirecting the fuel comprises directing a portion of the pressurised fuel toward the flow splitter by the action of a tangential component of a velocity of the pressurised fuel.3. The method of claim 1 , wherein directing the fuel through the flow splitter comprises directing a portion of the flow through a plurality of bifurcating passages disposed radially outwardly of a first fuel passageway and communicating with a second fuel passageway claim 1 , the first fuel passageway include one of the filming surfaces and the second fuel passageway include the other one of the filming surfaces.4. The method of claim 3 , further comprising forming ...

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01-03-2018 дата публикации

METHOD FOR OPERATING A COMBUSTION SYSTEM

Номер: US20180058697A1
Автор: Öfverstedt Tomas
Принадлежит: SIEMENS AKTIENGESELLSCHAFT

A method for operating a combustion system of a combustion section of a gas turbine engine having at least one main burner arrangement and at least one pilot burner arrangement, wherein the at least one main burner arrangement and the at least one pilot burner arrangement are operated with an air-fuel mixture. The method includes: operating the at least one main burner arrangement with O-lean air, enriching an air of the air-fuel mixture of the at least one pilot burner arrangement and/or a fuel of the air-fuel mixture of the at least one pilot burner arrangement and/or the air-fuel mixture of the at least one pilot burner arrangement with oxygen and preferably with pure oxygen. 1. A method for operating a combustion system of a combustion section of a gas turbine engine comprising at least one main burner arrangement and at least one pilot burner arrangement , wherein the at least one main burner arrangement and the at least one pilot burner arrangement are operated with an air-fuel mixture ,wherein the method comprises:{'sub': '2', 'operating the at least one main burner arrangement with O-lean air,'}enriching an air of the air-fuel mixture of the at least one pilot burner arrangement and/or a fuel of the air-fuel mixture of the at least one pilot burner arrangement and/or the air-fuel mixture of the at least one pilot burner arrangement with oxygen.2. The method according to claim 1 , further comprising:enriching the air of the air-fuel mixture of the at least one pilot burner arrangement and/or the fuel of the air-fuel mixture of the at least one pilot burner arrangement and/or the air-fuel mixture of the at least one pilot burner arrangement with oxygen so that an oxygen content of the air-fuel mixture burned by the at least one pilot burner arrangement is at least 5% higher than an oxygen content of the air feed to the at least one pilot burner arrangement beforehand of a mixing with the oxygen.3. The method according to claim 1 ,{'sub': '2', 'wherein the air ...

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12-03-2015 дата публикации

Integrated heat shield

Номер: US20150069148A1
Принадлежит: Delavan Inc

A fuel injector for a gas turbine engine includes a nozzle tip assembly having a substantially monolithically formed nozzle body. The nozzle body has an annular outlet chamber for issuing a spray from the nozzle tip. A feed channel is in fluid communication with the outlet chamber through a feed passage. A heat shield void substantially surrounds the feed channel(s).

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17-03-2022 дата публикации

FUEL NOZZLE AIR SWIRLER

Номер: US20220082258A1
Принадлежит: Raytheon Technologies Corporation

A guide plate for a swirler assembly is disclosed. In various embodiments, the guide plate includes a guide plate flange configured for engagement with a swirler body having a plurality of primary swirler inlets; and a first plurality of purge holes extending through the guide plate flange and configured to introduce a first vectored purge flow into the swirler body. 1. A guide plate for a swirler assembly , comprising:a guide plate flange configured for engagement with a swirler body having a plurality of primary swirler inlets; anda first plurality of purge holes extending through the guide plate flange and configured to introduce a first vectored purge flow into the swirler body.2. The guide plate of claim 1 , wherein each of the first plurality of purge holes is defined by a first axial angle with respect to a longitudinal axis extending through the swirler body.3. The guide plate of claim 2 , wherein the first axial angle is from about zero degrees to about sixty degrees.4. The guide plate of claim 3 , wherein each of the first plurality of purge holes is defined by a first radial angle with respect to a radial axis extending through the swirler body.5. The guide plate of claim 4 , wherein the first radial angle is from about zero degrees to about sixty degrees.6. The guide plate of claim 1 , further comprising a second plurality of purge holes extending through the guide plate flange and configured to introduce a second vectored purge flow into the swirler body.7. The guide plate of claim 6 , wherein each of the first plurality of purge holes has a first entrance opening positioned at a first radial entrance position and each of the second plurality of purge holes has a second entrance opening positioned at a second radial entrance position claim 6 , the second radial entrance position being different from the first radial entrance position.8. The guide plate of claim 6 , wherein each of the first plurality of purge holes has a first exit opening positioned at ...

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10-03-2016 дата публикации

SYSTEM AND METHOD FOR REDUCING EMISSIONS FROM A BOILER

Номер: US20160069562A1
Принадлежит:

A system and method for reducing emissions from a boiler. A boiler generally has a combustion area. The system further includes a fuel pipe for delivering fuel. The system further includes a conduit. A bore extends through the conduit. The bore of the conduit is in fluid communication with the fuel pipe and the combustion area of the boiler. A pre-ignition source is positioned in the conduit. The pre-ignition source operates to pre-ignite at least a portion of the fuel flowing through the conduit. 1. A system for reducing emissions in a boiler having a combustion area , comprising:a plurality of coal supply elevations in the combustion area, each fuel supply elevation including a conduit having a bore extending there through, the bore being in fluid communication with a fuel pipe and the combustion area of the boiler; anda pre-ignition source positioned in the conduit disposed at the lowest fuel supply elevation and operable to pre-ignite at least a portion of the fuel flowing through conduit prior to the fuel entering the combustion area;wherein the conduit disposed above the lowest fuel supply elevation does not include a pre-ignition source to pre-ignite any portion of the fuel flowing there through.2. The system of claim 1 , wherein the fuel comprises carbonaceous fuel.3. The system of claim 2 , wherein the fuel comprises pulverized coal.4. The system of claim 3 , wherein the pre-ignition source continually pre-ignites at least a portion of the fuel flowing through the conduit disposed at the lowest fuel supply elevation during regular operation of the boiler.5. The system of claim 4 , wherein the ignition source operates throughout a boiler load range.6. The system of claim 1 , further comprising:{'b': '50', 'a first pre-ignition conduit defining a first bore extending there through, the first pre-ignition conduit being disposed in the bore of the conduit disposed at the lowest fuel supply elevation, the pre-ignition source () being positioned in the bore of ...

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10-03-2016 дата публикации

Device for burning pre-mixed gas

Номер: US20160069563A1
Автор: Yves Cazard
Принадлежит: YAHTEC

A device for burning premixed gas, including a ventilator ( 1 ) for drawing in the air/gas mixture, a gas-supply valve ( 2 ), a gas injector ( 3 ), and a venturi ( 4 ) interposed between said injector ( 3 ) and the ventilator ( 1 ), so as to create a negative pressure on the gas valve ( 2 ), The venturi ( 4 ) includes a movable part ( 40 ) capable of moving under the action of said ventilator ( 1 ) and a restoring spring ( 43 ), the displacement of said movable part being capable modifying the cross-sections of the passages ( 41, 42 ) for gas (G) and air (A).

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10-03-2016 дата публикации

TOP PORTED BURNER

Номер: US20160069564A1
Автор: AHMED MALLIK
Принадлежит:

A burner with a tubular body has a proximal end, a distal end, and a medial portion therebetween and further defining an upper side and a lower side. The burner has a gas orifice on the proximal. A plurality of burner ports open on the top side and span between the medial portion to the distal end. At least one carry over port opens between the top side and bottom side of the body proximal to the plurality of burner ports. At least one transition ports opens on the medial portion of the body between the at least one carry over port and the plurality of burner ports. 1. A burner comprising:a tubular body having a proximal end, a distal end, and a medial portion therebetween and further defining an upper side and a lower side;a gas orifice on the proximal end;a plurality of burner ports opening on the top side and spanning between the medial portion to the distal end;at least one carry over port opening between the top side and bottom side of the body proximal to the plurality of burner ports; andat least one transition ports opening on the medial portion of the body between the at least one carry over port and the plurality of burner ports.2. The burner of claim 1 , further comprising a carry over tube oriented perpendicularly to the tubular body and aligned proximate to the at least one carry over port.3. The burner of claim 2 , wherein the carry over tube is offset distally from a center of the at least one carry over port.4. The burner of claim 1 , further comprising an upper stud inserted partially into the tubular body from the upper side and distally from a center of the at least one carry over port.5. The burner of claim 4 , further comprising a lower stud inserted partially into the tubular body from the lower side and distally from the upper stud.6. The burner of claim 5 , wherein the upper and stud and lower stud are both located proximally to the plurality of burner ports.7. The burner of claim 1 , wherein the tubular body comprises a front piece and a ...

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09-03-2017 дата публикации

Heating assembly

Номер: US20170067631A1
Автор: David Deng
Принадлежит: Individual

A heating assembly can be used in a dual fuel heater to mix air with fuel to be combusted at the burner. The heating assembly can include a burner, a first nozzle, a second nozzle, a first conduit and a second conduit. The first conduit can have an opening configured to allow air to mix with fuel injected into the first conduit by the first nozzle.

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11-03-2021 дата публикации

BURNER OF GAS STOVE

Номер: US20210071863A1
Принадлежит: GRAND MATE CO., LTD.

A burner of a gas stove includes a burner body, a partition member, and at least one flame cover. The burner body includes an inlet portion and a base. The inlet portion has at least one inlet passage for injecting gas and air, and the base has at least one mixture passage for mixing the gas and the air. The at least one mixture passage communicates with the at least one inlet passage. The partition member has a plurality of through holes and covers the at least one mixture passage. The at least one flame cover has a plurality of flame holes and covers the partition member. Whereby, the size of the burner of the gas stove could be reduced significantly, and the gas could mix with the air effectively and uniformly. 1. A burner of a gas stove , comprising:a burner body including an inlet portion and a base, wherein the inlet portion has at least one inlet passage for injecting gas and air, the base has at least one mixture passage for mixing the gas and the air; the at least one mixture passage is annular; an end of the at least one mixture passage communicates with the at least one inlet passage, and another end of the at least one mixture passage is a closed end;a partition member mounted on the base and covering the at least one mixture passage; wherein the partition member has a plurality of through holes communicating with the at least one mixture passage, and the plurality of through holes arranged along a circumferential direction of the at least one mixture passage; andat least one flame cover covering the partition member, wherein at least one chamber is formed between the at least one flame cover and the partition member; the at least one flame cover has a plurality of flame holes arranged in a ring shape and communicating with the at least one chamber; the at least one chamber communicates with the at least one mixture passage through the plurality of through holes of the partition member.2. The burner of the gas stove of claim 1 , wherein the base has two ...

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17-03-2016 дата публикации

CENTRAL BURNER FOR MULTI-FUEL MULTIPLE LANCE BURNER SYSTEM

Номер: US20160076763A1
Принадлежит: LOESCHE GmbH

The invention relates to a central burner for multi-fuel multiple lance burner systems having a central lance with an inner pipe and an outer pipe. The inner pipe and the outer pipe form an annular clearance duct. A plurality of outer lances are arranged around the central lance. A funnel-like mixing device is provided in the extension of the annular clearance duct in the region of the end of the inner pipe. This funnel-like mixing device has openings in its wall for combustion media to flow through. The outer lances each have a nozzle which has openings along the lateral circumferential area, said openings being arranged asymmetrically. 11. Central burner () for multi-fuel multiple lance burner systems ,{'b': 10', '11', '12, 'having a central lance () with an inner pipe () and an outer pipe () which are provided coaxially relative to each other,'}{'b': 11', '12', '13', '13, 'wherein the inner pipe () and the outer pipe () are arranged spaced apart from each other in the radial direction to form an annular clearance duct (), and combustion media can be conveyable through the annular clearance duct (),'}{'b': 12', '10', '61', '60, 'wherein the outer pipe () of the central lance () extends from a first feed chamber () to a combustion chamber (),'}{'b': 21', '10', '21', '62', '60, 'wherein a plurality of outer lances () are arranged around the central lance (), said outer lances () extending from at least a second feed chamber () to the combustion chamber (),'}{'b': 12', '60', '11, 'wherein the outer pipe () extends further into the combustion chamber () than the inner pipe (),'}{'b': 14', '13', '11, 'wherein a funnel-like mixing device () is provided in the extension of the annular clearance duct () in the region of the end of the inner pipe (),'}{'b': 14', '11', '11, 'said mixing device () having an opening in the region of the end of the inner pipe (), said opening corresponding substantially to the diameter of the inner pipe (),'}{'b': 14', '13', '11', '12, ' ...

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05-03-2020 дата публикации

GAS BURNER ARRANGEMENT AND HOB COMPRISING A GAS BURNER ARRANGEMENT

Номер: US20200072462A1
Автор: Rasi Fabio
Принадлежит:

The invention relates to a gas burner arrangement comprising: —a gas burner () with at least three burner sections (); —a gas tap () comprising at least one gas inlet () coupled with a gas supply line () and two gas outlets (); —a divider entity () comprising a divider inlet () and two or more divider outlets (); —an on/off valve () adapted to open/close a gas line; wherein a first burner section () is coupled with a first gas outlet () of the gas tap (), wherein the second gas outlet () of the gas tap () is coupled with the divider inlet (), wherein a first divider outlet () is coupled with a second burner section (), wherein the second divider outlet () is at least indirectly coupled with an inlet () of the on/off valve () and the outlet () of the on/off valve () is coupled with the third burner section (). 2. Gas burner arrangement according to claim 1 , wherein the first gas outlet of the gas tap is a secondary gas outlet and the second gas outlet of the gas tap is a main outlet.3. Gas burner arrangement according to claim 1 , wherein the gas tap comprises a safety valve coupled with a flame control entity arranged at the gas burner.4. Gas burner arrangement according to claim 2 , wherein the safety valve is adapted to shut off a gas connection between the gas inlet and the gas outlets of the gas tap based on information provided by the flame control entity.5. Gas burner arrangement according to claim 3 , wherein the safety valve is a magnetic valve.6. Gas burner arrangement according to claim 1 , said burner sections being concentric claim 1 , ring-shaped burner sections.7. Gas burner arrangement according to claim 1 , wherein the first burner section is an inner burner section claim 1 , the second burner section is a middle burner section and the third burner section is an outer burner section.8. Gas burner arrangement according to claim 7 , wherein sizes of the burner sections increase from the first to the third burner section.9. Gas burner arrangement ...

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14-03-2019 дата публикации

SPRAY NOZZLE

Номер: US20190078784A1
Принадлежит: ROLLS-ROYCE PLC

A fuel spray nozzle, for atomising liquid fuel in gas, including: an gas passage; a liquid fuel passage; a swirler provided in the gas passage and including vanes such that, when gas passes through the gas passage, the swirler produces a jet flow of gas from between adjacent vanes and a turbulent flow of gas in the wake of each vane; a prefilming surface for receiving liquid fuel from the liquid fuel passage, and gas from the gas passage, wherein the prefilming surface includes areas that receive jet flow of gas from the gas passage, in use; wherein the fuel spray nozzle is configured to direct the liquid fuel passing through the liquid fuel passage to the areas on the prefilming surface that receive a jet flow of gas from the gas passage. 1. A fuel spray nozzle , for atomising liquid fuel in a gas , comprising:a gas passage;a liquid fuel passage;a swirler provided in the gas passage and comprising vanes such that, when gas passes through the gas passage, the swirler produces a jet flow of gas from between adjacent vanes and a turbulent flow of gas in the wake of each vane;a prefilming surface configured to receive liquid fuel from the liquid fuel passage, and to receive gas from the gas passage, wherein the prefilming surface comprises areas that, in use, receive jet flow of gas from the gas passage;wherein the fuel spray nozzle is configured to direct the bulk of the liquid fuel passing through the liquid fuel passage to the areas on the prefilming surface that receive a jet flow of gas from the gas passage.2. A fuel spray nozzle according to claim 1 , further comprising apertures for supplying liquid fuel to the liquid fuel passage.3. A fuel spray nozzle according to claim 2 , wherein the apertures are configured to direct liquid fuel through the liquid fuel passage to the areas on the prefilming surface that receive a jet flow of gas from the gas passage.4. A fuel spray nozzle according to claim 2 , wherein the number of apertures is the same as the number of ...

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24-03-2016 дата публикации

Burner

Номер: US20160084497A1
Принадлежит: Kiln Flame Systems Ltd

This invention relates to a burner 100 including a burner body 110 having a burner chamber with a backing plate 122 and having a burner element received in the burner chamber, the burner element having a plurality of gas nozzles 117 for supplying gas into the burner mounted therein for rotational movement such that the direction of gas exiting the gas nozzle can be adjusted. The burner is characterized by means for rotating the gas nozzles 117 which are provided on the backing plate 121 and by releasable means for retaining each gas nozzle 117 in a plurality of rotational configurations provided outside the burner chamber. The burner allows for tuning of gas flow from outside the burner while it is in use.

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24-03-2016 дата публикации

Fuel nozzle

Номер: US20160084503A1
Принадлежит: Pratt and Whitney Canada Corp

A fuel nozzle for a combustor of a gas turbine engine includes a body defining an axial direction and a radial direction, a primary air passageway centrally defined axially in the body, and a plurality of concentrically-arranged nozzle tip projections disposed at a downstream portion of the body. Each of the plurality of nozzle tip projections has a radially inwardly facing fuel filming surface communicating with respective fuel passages. The fuel filming surfaces are disposed radially outwardly of an outlet of the primary air passageway. A method for delivering fuel from a fuel nozzle of a combustor of a gas turbine engine is also presented.

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31-03-2022 дата публикации

AIRCRAFT FUEL NOZZLE

Номер: US20220099290A1
Принадлежит:

A fuel injector for an aircraft gas turbine engine includes a housing stem, a fuel nozzle coupled to the housing stem, and a fuel conduit extending through the housing stem and into the fuel nozzle where the fuel conduit bends to extend in a longitudinal downstream direction within the fuel nozzle. The fuel conduit is configured to transport bulk fuel flow further along the nozzle before being split downstream in the fuel circuit for final spray distribution, thereby promoting lower fuel temperatures. The fuel nozzle may minimize metal-to-metal contact between an external wall of the nozzle in thermal communication with ambient environment and an internal portion of the nozzle in thermal communication with the fuel circuit to minimize heat pick-up in the fuel. The fuel conduit may include a coiled section within a cavity of the fuel nozzle for compensating for thermal growth mismatches of the fuel injector. 1. A fuel injector , comprising:a housing stem;a fuel nozzle operatively coupled to the housing stem, the fuel nozzle extending in a longitudinal direction between an upstream end and a downstream discharge end of the fuel nozzle, the fuel nozzle comprising a fuel circuit having an inlet section and an outlet section; anda fuel conduit extending through the housing stem into the fuel nozzle to form the inlet section of the fuel circuit, and extending through the fuel nozzle in the longitudinal direction toward the downstream discharge end to form an upstream portion of the fuel circuit;wherein the fuel conduit is configured to provide bulk fuel flow through the housing stem and the upstream portion of the fuel circuit, the fuel conduit fluidly connecting downstream to a fuel manifold located at an intermediate longitudinal position in the fuel nozzle between the upstream end and the downstream discharge end, the fuel manifold being configured to split the bulk fuel flow into a plurality of fuel flow passages in a downstream portion of the fuel circuit for fuel ...

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31-03-2022 дата публикации

PORTABLE HOT AIR GENERATOR APPARATUS COMPRISING A DAMPING SYSTEM

Номер: US20220099292A1
Автор: CLEMENT François
Принадлежит:

Disclosed is a portable hot air generator apparatus which includes a handle and a body forming a Venturi and, furthermore, a damping system between the handle and the body. 1. A portable hot air generator apparatus comprising:a handle and a body which extends along a horizontal main axis and substantially symmetrical relative to a vertical longitudinal plane; anda system for damping between said handle and said body, so that the handle does not have direct contact with the body.2. The apparatus according to claim 1 , wherein the damping system comprises at least one damper claim 1 , each damper comprising a housing claim 1 , a cleat and a damping material claim 1 , said housing being formed in the handle claim 1 , said cleat being integral with the body claim 1 , and claim 1 , said material forming an elastic grip for one end of the cleat in the housing claim 1 , at a distance from the walls of said housing.3. The apparatus according to claim 2 , wherein the cleat comprises a shank which extends vertically downwards from the body and a crossbar at a distal end from said shank claim 2 , and wherein the housing comprises an opening for the passage of the shank with clearance.4. The apparatus according to claim 2 , wherein the cleat is a fold in the sheet of the body which forms a tab engaging in the damping material.5. The apparatus according to claim 2 , wherein the handle comprises two shells substantially symmetrical to each other relative to the plane of symmetry claim 2 , each of said shells forming a part of the housing which is open laterally.6. The apparatus according to claim 2 , further comprising two dampers.7. The apparatus according to claim 1 , wherein the damping system comprises at least one damper in the shape of a ring that surrounds the body.8. The apparatus according to claim 1 , wherein the handle comprises two shells substantially symmetrical to each other relative to the plane of symmetry claim 1 , each of said shells comprising ribs claim 1 , ...

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31-03-2022 дата публикации

FUEL INJECTION

Номер: US20220099299A1
Принадлежит: ROLLS-ROYCE PLC

A direct fuel injection system () is shown for injecting hydrogen fuel into a gas turbine combustor, the fuel injection system comprising a plurality of fuel injector blocks (). Each fuel injector block includes one or more air admission ducts () for receiving air from a diffuser and an air outlet for delivering air into a mixing zone for combustion with fuel. Each fuel injector block also includes a fuel admission duct or aperture having a fuel inlet for receiving fuel (F) from a manifold, and a fuel outlet for delivering fuel into the mixing zone. 1. A direct fuel injection system for injecting hydrogen fuel into a gas turbine combustor , the fuel injection system comprising a plurality of fuel injector blocks , each of which includes:a fuel admission duct having a fuel inlet for receiving fuel from a manifold, a fuel outlet for delivering fuel into a mixing zone and a central axis extending from said fuel inlet to said fuel outlet;a plurality of air admission ducts distributed around the fuel admission duct, and having an air inlet for receiving air from a diffuser and an air outlet for delivering air into the mixing zone for combustion with said fuel.2. The fuel injection system of claim 1 , in which the fuel injector blocks are configured to substantially tesselate adjacent to one another.3. The fuel injection system of claim 2 , in which the fuel injector blocks are substantially tessellated adjacent to one another to form an annulus for an annular gas turbine combustor.4. The fuel injection system of claim 1 , in which the injection system comprises a plurality of separator sectors claim 1 , each sector being made up of a subset of tessellated fuel injector blocks.5. The fuel injection system of claim 2 , in which the fuel injector blocks have a quadrilateral profile in the plane of tessellation.6. The fuel injection system claim 2 , in which the fuel injector blocks have a hexagonal profile in the plane of tessellation.7. The fuel injection system of claim 1 ...

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25-03-2021 дата публикации

ADJUSTABLE FUME TUBE BURNER

Номер: US20210087099A1
Принадлежит:

A method of forming an optical fiber preform includes the steps: igniting a burner having a fume tube assembly to produce a first spray size of silicon dioxide particles; depositing the silicon dioxide particles on a core cane to produce a soot blank; and adjusting an effective diameter of an aperture of the fume tube assembly to produce a second spray size of the silicon dioxide particles. The second spray size is larger than the first spray size. 1. A method of forming an optical fiber preform , comprising the steps:igniting a burner having a fume tube assembly to produce a first spray size of silicon dioxide particles;depositing the silicon dioxide particles on a core cane to produce a soot blank; andadjusting an effective diameter of an aperture of the fume tube assembly to produce a second spray size of the silicon dioxide particles, wherein the second spray size is larger than the first spray size.2. The method of claim 1 , wherein the step of adjusting the effective diameter of the aperture is performed while depositing the silicon dioxide particles.3. The method of claim 1 , further comprising the step of:emitting a gas proximate the fume tube assembly.4. The method of claim 3 , further comprising the step of:increasing a flow rate of the emitted gas after adjusting the effective diameter of the aperture.5. The method of claim 1 , wherein the step of adjusting the effective diameter of the aperture of the fume tube assembly further comprises the step of:moving a second fume tube within a first fume tube.6. The method of claim 5 , wherein the step of adjusting the effective diameter of the aperture of the fume tube assembly further comprises the step of:decoupling a tapered region of the second tube with a tapered region of the first tube.7. The method of claim 1 , wherein the step of adjusting the effective diameter of the aperture of the fume tube assembly further comprises the step of:moving a second fume tube and a third fume tube within a first fume tube ...

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31-03-2016 дата публикации

GAS BURNER ASSEMBLY FOR A COOKING HOB

Номер: US20160091210A1
Автор: Ceccoli Carlo Andrea
Принадлежит:

A gas burner assembly for a cooking hob, in particular for a domestic cooking hob, includes at least two burner bases arranged side-by-side-and a burner crown element arranged or arrangeable above the burner bases. At least one burner cap is arranged or arrangeable above the burner crown element. The burner bases are adjustable separately. The burner crown element includes a bottom plate subdivided into at least two portions arranged side-by-side. Each portion of the bottom plate is arranged or arrangeable above one of the burner bases. The burner crown element includes at least two side walls. Each side wall encloses one of the portions of the bottom plate. The burner crown element includes flame ports formed in the side walls. The flame ports are arranged in those sections of the side walls arranged opposite to the adjacent portion or portions of the bottom plate. 110. Gas burner assembly () for a cooking hob , wherein{'b': 10', '11', '12, 'the gas burner assembly () comprises at least two burner bases (, ) arranged side-by-side,'}{'b': 10', '14', '11', '12, 'the gas burner assembly () comprises a burner crown element () arranged or arrangeable above the at least two burner bases (, ),'}{'b': 10', '16', '14, 'the gas burner assembly () comprises at least one burner cap () arranged or arrangeable above the burner crown element (),'}{'b': 11', '12, 'the at least two burner bases (, ) are adjustable separately,'}{'b': 14', '24, 'the burner crown element () includes a bottom plate () subdivided into at least two portions arranged side-by-side,'}{'b': 24', '11', '12, 'each portion of the bottom plate () is arranged or arrangeable above one of the at least two burner bases (, ),'}{'b': 14', '28, 'the burner crown element () includes at least two side walls (),'}{'b': 28', '24, 'each side wall () encloses one of the at least two portions of the bottom plate (),'}{'b': 14', '30', '28, 'the burner crown element () includes a plurality of flame ports () formed in the side ...

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30-03-2017 дата публикации

HEATING ASSEMBLY

Номер: US20170089570A1
Автор: Deng David
Принадлежит:

A heating assembly can be used with one of a first fuel type or a second fuel type different than the first. The heating assembly can include a housing have a first actuation member and a second actuation member. The first and second actuation members can be positioned within respective first and second fuel hook-ups. The first and second actuation members can be configured such that connecting a fuel source to the heater assembly moves one of the actuation members from a first position to a second position to control flow through the heating assembly. 1. A heater assembly for use with one of a first fuel type or a second fuel type different than the first , the heater assembly comprising: a first fuel hook-up for connecting a first fuel type to the heater assembly;', 'a second hook-up for connecting a second fuel type to the heater assembly;', 'a first outlet in fluid communication with both the first and second fuel hook-ups;', 'a first inlet;', 'a second inlet;', 'a second outlet;', 'a third outlet; and', 'a fourth outlet, 'a housing comprising 'wherein in the first actuation member first position, fuel flow through the first fuel hook-up and between the second inlet and fourth outlet is prevented and in the first actuation member second position, fuel flow through the first fuel hook-up and between the second inlet and fourth outlet is permitted;', 'a first actuation member having an end located within the first fuel hook-up and having a first actuation member first position and a second position, the actuation member configured such that connecting a fuel source to the heater assembly at the first fuel hook-up moves the actuation member from the first actuation member first position to the second position,'} 'wherein in the second actuation member first position, fuel flow through the second fuel hook-up and between the first inlet and the third outlet is prevented and in the second actuation member second position, fuel flow through the second fuel hook-up and ...

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05-05-2022 дата публикации

Cylindrical burner apparatus and method

Номер: US20220136693A1
Автор: Yul E. Shaffer
Принадлежит: Gastech Engineering LLC

A cylindrical burner apparatus and method which produce low NO x emissions and low noise levels without being dependent upon a blower, or natural draft, for providing air flow. A flow of combustion air is induced into a cylindrical burner lube by discharging a gas fuel from a plurality of discharge ports located inside the rearward end of the tube. At least some of the discharge ports are oriented to direct jets of the gas fuel toward flame stabilization structures positioned downstream of the discharge ports.

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05-05-2022 дата публикации

CYLINDRICAL BURNER APPARATUS AND METHOD

Номер: US20220136694A1
Автор: Shaffer Yul E.
Принадлежит:

A cylindrical burner apparatus and method which produce low NOemissions and low noise levels without being dependent upon a blower, or natural draft, for providing air flow or flue gas recirculation. A flow of combustion air is induced into an initial tube pass of the burner by discharging a gas fuel from a plurality of discharge ports located in the initial tube pass. At the same time, a flow of recycled flue gas is induced through a bypass duct between a subsequent tube pass of the burner and the initial tube pass by discharging one or more jets of gas fuel through the bypass duct.

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19-03-2020 дата публикации

INFRARED RADIATOR

Номер: US20200088403A1
Принадлежит:

An infrared radiator for the heat treatment of a material web includes an incandescent body with a flow-receiving surface to be impinged by a gas-air mixture that is supplied to the infrared radiator and to be heated by combustion of the gas-air mixture. The incandescent body is manufactured as a sheet material that is formed of a multiplicity of threads. The sheet material is manufactured by primary forming. 111-. (canceled)12. An infrared radiator for the heat treatment of a material web , the infrared radiator comprising:an incandescent body having a flow-receiving surface to be impinged by a gas-air mixture supplied to the infrared radiator and to be heated by a combustion of the gas-air mixture;said incandescent body being manufactured as a sheet material formed of a multiplicity of threads and said sheet material being manufactured by primary forming.13. The infrared radiator according to claim 12 , wherein said sheet material is a self-supporting sheet material.14. The infrared radiator according to claim 12 , wherein said threads of said sheet material are interconnected in an articulated manner at respective intersection points.15. The infrared radiator according to claim 12 , wherein said threads are formed spirally and said sheet material is a spiral braid with two directly adjacent threads respectively connected to one another in each case by meshing at intersection points.16. The infrared radiator according to claim 12 , wherein said sheet material is a woven fabric claim 12 , comprising threads that serve as warp threads and that are interwoven at intersection points with threads that serve as weft threads claim 12 , and wherein said threads have a wave-shaped outer contour.17. The infrared radiator according to claim 16 , wherein said woven fabric is a plain weave claim 16 , with directly adjacent threads that serve as weft threads weaving alternately through threads that serve as warp threads claim 16 , along different weaving paths.18. The infrared ...

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01-04-2021 дата публикации

Gas Turbine Combustor and its Operating Method

Номер: US20210095599A1
Принадлежит:

A hydrogen content fuel can be stably ignited using a gaseous fuel that does not contain hydrogen and dispersibility of the hydrogen content fuel is enhanced. 1. A gas turbine combustor comprising a startup fuel pipe in which a startup fuel circulates;', 'a first main fuel pipe in which a main fuel circulates;', 'a second main fuel pipe in which the main fuel circulates;', 'a fuel mixer to which the startup fuel pipe and the first main fuel pipe are connected;', 'an inner fuel nozzle to which the fuel mixer is connected;', 'a plurality of outer fuel nozzles to which the second main fuel pipe is connected;', 'a startup fuel control valve provided in the startup fuel pipe;', 'a first fuel control valve provided in the first main fuel pipe; and', 'a second fuel control valve provided in the second main fuel pipe., 'a burner including2. The gas turbine combustor according to claim 1 , further comprising:a controller configured to control the startup fuel control valve, the first fuel control valve, and the second fuel control valve, whereinthe controller executes procedures including(1) raising an opening degree of the startup fuel control valve to supply the startup fuel to the inner fuel nozzle,(2) raising an opening degree of the second fuel control valve to supply the main fuel to the plurality of outer fuel nozzles when a gas turbine load rises up to a first set value, and(3) raising an opening degree of the first fuel control valve to supply a mixed gaseous fuel of the startup fuel and the main fuel to the inner fuel nozzle when the gas turbine load further rises up to a second set value.3. The gas turbine combustor according to claim 2 , whereinthe controller executes procedures including(4) closing the first fuel control valve to stop to supply the main fuel to the inner fuel nozzle, and lowering the opening degree of the second fuel control valve when the opening degree of the second fuel control valve is lowered and the gas turbine load falls down to a third ...

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01-04-2021 дата публикации

Fuel spray nozzle

Номер: US20210095851A1
Автор: Tomasz STANKOWSKI
Принадлежит: Rolls Royce PLC

Fuel spray nozzle for generating a spray of atomised liquid fuel in a combustor of a gas turbine engine. The nozzle includes a flow circuit that has in flow series: a gallery that receives fuel flow, plural circumferentially-spaced restrictor passages arranged in a row around the nozzle, plural conditioning passages configured to impart a circumferential component to their respective portions of the fuel flow, and an annular spin chamber which forms a swirling fuel flow which is discharged at an exit port. The restrictor passages form flow restrictions which in use produce a pressure differential between the gallery and the spin chamber to evenly circumferentially distribute the fuel flow between the restrictor passages. The conditioning passages have increased flow cross-sectional areas relative to the flow cross-sectional areas of the restrictor passages, such that the restrictor passages produce substantially all of the pressure differential between the gallery and the spin chamber.

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28-03-2019 дата публикации

Premixed fuel nozzle

Номер: US20190093895A1
Принадлежит: General Electric Co

The present disclosure is directed to a fuel injector assembly and a gas turbine engine including the fuel injector assembly. The fuel injector assembly includes a centerbody extended along a lengthwise direction. The centerbody defines a first fuel nozzle. An annular shroud defining a second fuel nozzle surrounds the centerbody and is extended along the lengthwise direction. A passage is defined through the annular shroud and extended generally along the lengthwise direction. The passage defines an exit opening disposed at a downstream end adjacent to the combustion chamber and in fluid communication therewith. The annular shroud defines a fuel inlet opening disposed at an upstream end of the passage. The annular shroud further defines an air inlet opening in fluid communication with the passage. The air inlet opening is disposed between the fuel inlet opening and the exit opening.

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28-03-2019 дата публикации

Fuel spray nozzle comprising axially projecting air guiding element for a combustion chamber of a gas turbine engine

Номер: US20190093897A1
Принадлежит: Rolls Royce Deutschland Ltd and Co KG

A combustion chamber assembly group includes a nozzle providing a fuel-air mixture at a nozzle exit opening. An end of a fuel guiding channel is bordered at the nozzle exit opening by a flow-off edge located radially outside, and an air guiding element of an air guiding channel of the nozzle located radially outside projects with respect to this flow-off edge in the axial direction with respect to a nozzle longitudinal axis such that: a reference angle present between the nozzle longitudinal axis and a straight boundary line extending through a point at the flow-off edge and tangentially to the axially projecting air guiding element, and/or a reference angle present between the nozzle longitudinal axis and a straight boundary line extending through a point at the flow-off edge and a point of the air guiding element that projects maximally beyond the flow-off edge in the axial direction is ≤50°.

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28-03-2019 дата публикации

Method for converting a gas boiler into a liquid-fuel boiler

Номер: US20190093918A1
Автор: Giovanni Pisani
Принадлежит: ICI Caldaie SpA

A method for converting a gas boiler into a liquid-fuel boiler. The gas boiler comprises an enclosure which accommodates a firebox, which forms a combustion chamber and is provided with a supporting wall which supports a burner provided with a combustion head, which protrudes from the supporting wall and has a substantially cylindrical shape with an internal cavity formed axially; the enclosure is provided with a passage in which an atomizing nozzle, connected to a liquid fuel supply duct, and at least one ignition electrode are inserted from the outside; a snorkel-shaped body is also applied to the end of the combustion head that is opposite with respect to the supporting wall and the supply duct is connected supply duct is connected to a pressurized source of liquid fuel.

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28-03-2019 дата публикации

COOLING APPARATUS OF HEATING FURNACE

Номер: US20190093952A1
Принадлежит: CHUGAI RO CO., LTD.

According to the present invention, in a heating furnace in which a fuel is burned by mixing the fuel supplied through a fuel supply pipe with combustion air supplied through a combustion air supply pipe by a combustion burner, a cooling medium guiding pipe through which cooling air for cooling the fuel supply pipe is guided into the furnace is provided to the outer peripheral side of the fuel supply pipe, and a cooling water supply pipe through which cooling water is supplied via a cooling water adjusting valve is connected to the cooling medium guiding pipe. 1. A heating furnace comprising a combustion burner which mixes a fuel supplied through a fuel supply pipe with a combustion air supplied through a combustion air supply pipe and burns the fuel in the inside of the furnace , whereina cooling medium guiding pipe which guides a cooling air for cooling the fuel supply pipe to the inside of furnace is arranged on an outer peripheral side of the fuel supply pipe, anda cooling water supply pipe for supplying a cooling water via a cooling water adjusting valve is connected to the cooling medium guiding pipe.2. The heating furnace according to claim 1 , whereinwhen the combustion burner mixes the fuel supplied through the fuel supply pipe with the combustion air supplied through the combustion air supply pipe and burns the fuel in the inside of furnace, the fuel supply pipe is cooled with the cooling air guided to the inside of furnace through the cooling medium guiding pipe arranged on the outer peripheral side of the fuel supply pipe, and when the inside of furnace is cooled, the combustion by the combustion burner is stopped while the cooling water adjusting valve is opened to guide the cooling water through the cooling water supply pipe into the cooling medium guiding pipe so that the cooling water is sprayed from the cooling medium guiding pipe to the inside of furnace.3. The heating furnace according to claim 2 , wherein when the cooling water is sprayed from ...

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12-04-2018 дата публикации

HIGH EFFICIENCY RADIANT HEATER

Номер: US20180100648A1
Принадлежит:

A radiant tube heater with a burner assembly, a radiant tube assembly and a combustion air pre-heater, wherein the burner assembly comprises: a burner fuel nozzle; a plenum chamber and a pre-mixer chamber; the plenum chamber having a combustion air inlet; wherein in use: combustion air flows from said plenum chamber through an orifice to said pre-mixer where said air is mixed with burner fuel entering said pre-mixer through said nozzle prior to being combusted at a burner head; said pre-mixer being at least partly located within said radiant tube assembly; and where in use at least part of the combustion air supplied to said plenum is preheated in said air pre-heater using residual sensible heat of the hot combustion gas products of the heater. 1. (canceled)2. A radiant tube heater comprising:a burner assembly including a combustion inlet, the burner to produce combustion air using pre-combustion air;a radiant tube assembly connected to the burner assembly, the radiant tube assembly to deliver combustion air to a radiant tube discharge; a housing coupled to the radiant tube discharge and the combustion inlet;', a first pre-combustion duct and a second pre-combustion duct parallel to the first pre-combustion duct;', 'a member connected the first and second pre-combustion ducts to direct the pre-combustion air from the first pre-combustion duct to the second pre-combustion duct; and', 'a plurality of combustion channels connected to the first pre-combustion duct and the second pre-combustion duct., 'a pre-heater block located in the housing, the pre-heater block comprising], 'a combustion pre-heater comprising3. The radiant tube heater of claim 2 , wherein the radiant tube assembly comprises a u-shaped heater connected to the burner assembly.4. The radiant tube heater of claim 2 , further comprising:an outlet duct connecting the pre-heater block to an inlet of the burner assembly, the outlet duct to deliver the heated pre-combustion air to the burner assembly inlet.5. ...

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12-04-2018 дата публикации

Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device

Номер: US20180100651A1
Принадлежит: ANSALDO ENERGIA SWITZERLAND AG

A combustor device for a gas turbines engines includes first and a second tubular members telescopically fitted in axially sliding manner to one another with interposition of annular centering and sealing which include at least a centering annular shoulder and a sealing ring arranged coaxial to one another. The sealing ring is axially spaced apart from the centering annular shoulder so that an axial distance between the centering annular shoulder and the sealing ring is greater than a maximum axial movement allowed between the first and said second tubular members.

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26-03-2020 дата публикации

ATOMIZATION BURNER WITH FLEXIBLE FIRE RATE

Номер: US20200096195A1
Принадлежит: BABINGTON TECHNOLOGY, INC.

A burner includes an atomizing chamber, a flame tube in front of the atomizing chamber adapted to direct combusting fuel introduced by the atomizing chamber along an interior of the flame tube, and a controller. The controller is programmed to independently control rate of fuel flow to the atomizing chamber, rate of atomizing air flow to the atomizing chamber, and rate of combustion air to the flame tub. The controller is also programmed to perform operations including regulating, based on output of a gas sensor, at least the rate of combustion air to the flame tube to substantially maintain a first predetermined amount of excess air in the flame tube. 1. A burner , comprising:an atomizing chamber;a flame tube in front of the atomizing chamber, adapted to direct combusting fuel introduced by the atomizing chamber along an interior of the flame tube; and 'regulating, based on output of a gas sensor, at least the rate of combustion air to the flame tube to substantially maintain a first predetermined amount of excess air in the flame tube.', 'a controller programmed to independently control rate of fuel flow to the atomizing chamber, rate of atomizing air flow to the atomizing chamber, and rate of combustion air to the flame tube, the controller being programmed to perform operations comprising2. The burner of claim 1 , the controller being further programmed to perform operations comprising:increasing, in response to an absence of reliable output from the gas sensor, the at least the rate of combustion air to the flame tube to transition to a second predetermined amount of excess air in the flame tube, the second predetermined amount of air being higher than the first predetermined amount of excess air.3. The burner of claim 2 , the controller being further programmed to perform operations comprising:regulating, after the increasing, at least the rate of combustion air to the flame tube to maintain the second predetermined amount of excess air in the flame tube.4. ...

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