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Matches 1 - 50 out of 19,496

Document Document Title
WO/2017/005616A1
A burner device for cooking food comprising a general structure (10), at least one air supply tube (11, 12) to a vaporizer (13), associated with a heating resistance (14) of the air supplied, which passes in its interior, a nozzle (15) f...  
WO/2017/003649A1
A system includes a fuel nozzle including a first wall disposed about a central axis, a second wall disposed about the first wall, and a plurality of lobes disposed between the first and second walls, wherein the plurality of lobes is sp...  
WO/2016/209825A1
The subject matter of this specification can be embodied in, among other things, a fluid flow trim apparatus includes an outer housing defining a cavity having an interior surface and an end wall having an orifice therethrough, a valve b...  
WO/2016/182565A1
A burner nozzle includes an outer housing, and a nozzle and a piston receivable within the outer housing. The piston is movable between an open position, where air and a well product are able to enter an atomizing chamber to generate an ...  
WO/2016/159709A1
The present invention relates to an oil-fired boiler having a combustion gas path guide, the oil-fired boiler comprising: a combustion chamber wall body for encompassing a combustion chamber in which combustion is performed by a burner; ...  
WO/2016/156868A1
An atomizer (210) for a burner comprising an atomization region (208), a proximal end (202) comprising at least one inlet configured to allow fuel and/or an atomizing medium to enter the atomization region (208), a distal end (204) compr...  
WO/2016/155350A1
An alcohol-based fuel cyclone atomizing burner comprises an electromagnetic pump (1), an atomization oil nozzle (2), an intelligent burning control system (6), a burner group (3), a blower (4), and an ignition flame ion probe (5). The au...  
WO/2016/160037A1
A combustion system comprises a discharge nozzle with concentric air and fuel orifices. A fuel conduit is coupled to each fuel orifice while an air conduit is coupled to each air orifice. The fuel and air only mixing with one another upo...  
WO/2016/138271A1
An injector including a housing having a fluid channel for fluid and a plurality of injector modules fluidly connected to the fluid channel, where each injector module includes a spray cup having a plurality of radial air passages for di...  
WO/2016/113495A1
The invention relates to a turbine engine combustion assembly (20), which includes: an annular flame tube (21) including a front wall (23), a rear wall (24) and a bottom (22) arranged facing an engine shaft (30); an injection wheel (41) ...  
WO/2016/104430A1
Provided are a burner tip, a combustion burner, and a boiler, which are provided with: a mixing chamber (92) situated in the interior; a plurality of mixed fluid jet holes (84a, 85a, 86a, 87a) that communicate at the basal ends thereof w...  
WO/2016/094648A1
A liquid fuel combustion device utilizes waste and contaminated oils without the need for pre-processing or filtering the fuel stock. And a waste oil fuel burner comprises: a plenum; a pre-combustion chamber located within the plenum; a ...  
WO/2016/089821A1
A feed injector for a circulating fluid bed reactor is fitted with a discharge nozzle with a circular, radially notched discharge orifice to improve the surface-to-volume ratio of the spray pattern formed by the nozzle. The feed injector...  
WO/2016/085494A1
Apparatus and method for a combustion turbine engine are provided. The apparatus includes a fuel-injecting lance (12) to convey a liquid fuel to a downstream end (16) ofthe lance. At least onejet in cross- flow injector (18) may be dispo...  
WO/2016/068922A1
A pilot burner (15) and method for stabilizing a pilot flame in a combustor (14) of a gas turbine engine are provided. The pilot burner includes a fuel nozzle (17) having at least one orifice having a cross-sectional profile effective to...  
WO/2016/037966A1
The invention relates to a burner comprising a pre-mixing passage (68) that is delimited radially outwardly by a wall and, in operation, is used to mix fuel and air, a burner lance (72, 94) and a plurality of fuel injectors being arrange...  
WO/2016/038016A1
The invention relates to a burner for a gas turbine, comprising a burner lance (58, 72) and/or burner hub (94), a burner passage (60, 68, 100) which at least partially surrounds said burner lance and/or burner hub, and a fuel supply arra...  
WO/2016/028760A1
A gas turbine combustor assembly includes a primary combustion chamber in fluid communication with a primary fuel injector and a primary air inlet. A torch igniter is carried by the primary combustion chamber, and includes an auxiliary c...  
WO/2016/024975A1
A multi-functional fuel nozzle (10) for a combustion turbine engine is provided. A nozzle cap (50) may be disposed at a downstream end of the nozzle. A heat shield (60) is mounted onto the nozzle cap. A plurality of cooling channels (62)...  
WO/2016/024976A1
A multi-functional fuel nozzle (10) for a combustion turbine engine is provided. An annular fuel-injecting lance (12) may include a first fluid circuit (14) and a second fluid circuit (16). One of the first and second fluid circuits duri...  
WO/2016/024977A1
A nozzle cap (82) is disposed at a downstream end of the nozzle. The nozzle cap includes a bore arranged to accommodate a downstream portion of a fluid-injecting lance that extends along a longitudinal axis (18) of the nozzle. The downst...  
WO/2016/018483A1
A multiple fuel capable, pre-mixed, low emission injector (10) is provided which is particularly suited for burning high flame speed fuels. The fuel injector (10) includes an injector body (20,22) having a preliminary pre-mixing chamber ...  
WO/2016/016116A1
The invention relates to a burner (2) for a combustion machine, having a pilot burner (4), which extends in the axial direction (A), having a nozzle chamber (10), having a burner region (6) and having a cover plate (20) which is arranged...  
WO/2016/016817A1
A burner (1) for an industrial oven of the non-regenerative type comprises: a burner body (2), a combustion chamber (3) into which a fuel means and air are introduced, first introducing means (13) for introducing the fuel means into the ...  
WO/2016/015713A1
A film evaporator burner arrangement (1) is provided, having: a combustion chamber arrangement comprising a combustion chamber (2) for the conversion of a fuel-air mixture with the release of heat, which extends in the axial direction al...  
WO/2016/008486A1
A fuel cell system comprising a fuel cell stack, an evaporator for evaporating a mixture of methanol and water to be forwarded through a catalytic reformer for producing portions of free hydrogen. The fuel cell stack being composed of a ...  
WO/2016/003883A1
A system and method for electrically charging a combustion flame with a power supply.  
WO/2015/182694A1
A burner (20) includes a combustion unit (21), a fuel supply unit (22), a vaporizer (30), an air supply unit (45), and a control unit (50). The fuel supply unit (22) supplies fuel to the combustion unit (21). The vaporizer (30) uses an e...  
WO/2015/181762A1
The present invention regards a burner device for furnaces comprising a main tubular body (2) having an outer end (2a) and an inner end (2b), an opening (6) for introducing a comburent fluid and a conduit (7) for transferring or transpor...  
WO/2015/165735A1
A burner (30) for a combustor (56) of a gas turbine combustor (16) comprises a body (53) having a surface (64) and a burner axis (50), a fuel lance (56), an igniter (58) and a main air flow passage (62) or passages (62). The main air flo...  
WO/2015/166017A1
A fuel lance (56) for a burner (30) of a combustor (16) of a gas turbine combustor (16), has an axis (79) and comprises a fuel lance body (68) defining a fuel flow passage (70) and a liquid fuel tip (72) attached to the fuel lance body (...  
WO/2015/158489A1
The invention relates to a burner having an air supply and premix duct which is of essentially annular cross-section and through which flow, in operation, air and fuel, and which is formed by an outer jacket and a hub and in which there ...  
WO/2015/147934A1
A fuel nozzle includes: an outer body (36) extending parallel to a centerline axis (26), having a generally cylindrical exterior surface (88), forward and aft ends (82, 84), and a plurality of openings (94) through the exterior surface (...  
WO/2015/147935A1
A fuel nozzle apparatus (10) for a gas turbine engine includes: a fuel discharge element (24) having a discharge orifice (50) communicating with a fuel supply connection (104); a static supporting structure (36); and a cantilevered flexi...  
WO/2015/137683A1
The present invention relates to a burner device capable of reducing fuel, which is configured such that hydrogen water is atomized by regenerative combustion and preheated to a reaction temperature for thermochemical hybrid cycle therma...  
WO/2015/136609A1
The purpose of the present invention is to provide a combustion burner capable of retaining a flame stabilizing function for a long time without causing erosion of a swirler even if a flame retardant component-containing fuel is used. Th...  
WO/2015/123495A3
The present disclosure describes a recovery boiler startup burner assembly that can mitigate the harmful effects of smelt fouling, airflow interference, and operator exposure to hot air from the furnace and win box through use of an extr...  
WO/2015/121063A1
Fuel injection means for a swirler of a burner of a gas turbine engine, swirler for a burner of a gas turbine engine, burner of a gas turbine engine and gas turbine engine. The present invention is related to fuel injection means (50) fo...  
WO/2015/122793A1
Proposed is a variant of a pneumatic atomizer comprising a housing (1) with an internal annular gas chamber (3) and a pipe (2) for supplying a compressed gas thereto, a liquid supply pipe (4) disposed along the axis of the housing and tr...  
WO/2015/112385A1
One embodiment includes a fuel injector. The fuel injector assembly comprises a conduit for conveying fuel from a fuel inlet to a nozzle. The conduit is located in a support, with the conduit, the nozzle, and the support being a single u...  
WO/2015/108833A1
[0031] Methods and systems of burning waste effluent include controlling flow of waste effluent to burner nozzles using flow control elements. The flow control elements are biased toward closed positions using biasing forces, wherein red...  
WO/2015/093377A1
A burner tip, a combustion burner, and a boiler, provided with: a mixing chamber (85), provided in the interior; multiple mixed-fluid spray holes (82, 83, 84) which are arranged at prescribed intervals in the circumferential direction, a...  
WO/2015/083124A1
Combustion apparatuses (e.g., burners) and methods, such as those configured to encourage mixing of fluid, flame stability, and synthesis of materials (e.g., nanoparticles), among other things.  
WO/2015/080807A1
Method and system is described for enhanced oil release management system by using one or more booms, one or more skimmers and one or more floating burners. The method and system may include skimmers to capture a fluid that is supplied t...  
WO/2015/076692A1
A gas turbine system is provided. The gas turbine system includes a combustor assembly. At least one liquid fuel cartridge in the combustor assembly includes at least one flexible tube section coupled within a housing. An elongated in...  
WO/2015/075389A1
The invention relates to a multi-point fuel injection device (1) for an aircraft engine (M), comprising an inlet line (10), at least two injection lines (11, 12), and a purge line (14), a fuel distributor member (2) connected to each lin...  
WO/2015/076620A1
The present invention provides an injection nozzle introduction device for a smelting furnace, the device comprising: a body coupled and arranged on one side of a smelting furnace to support an injection nozzle such that the same can sli...  
WO/2015/076692A8
A gas turbine system is provided. The gas turbine system includes a combustor assembly. At least one liquid fuel cartridge in the combustor assembly includes at least one flexible tube section coupled within a housing. An elongated in...  
WO/2015/070188A1
A combustion system includes an electrically actuated flame location control mechanism.  
WO/2015/069131A1
A liquid fuel cartridge for a gas turbine fuel nozzle includes a tube having an inlet end and an outlet end with one or more fuel exit orifices; and a homogenizer located within the tube, adjacent and upstream of the outlet end. The h...  

Matches 1 - 50 out of 19,496