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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...
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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...
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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...
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WO/2015/070188A1 |
A combustion system includes an electrically actuated flame location control mechanism.
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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...
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WO/2015/067482A1 |
The invention relates to a burner arrangement (1) for a combustion chamber, in particular a gas turbine combustion chamber, for burning fluidic fuels, having a main burner (2) and a pilot burner (3), arranged centrally therein, which ser...
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WO/2015/063733A1 |
A lance injector for injecting fuel oil into a gas turbine combustion chamber includes: a tubular casing (33), extending along a main axis (A); a first inner supply conduit (35) housed in the casing (33) and coupled, at a respective supp...
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WO/2015/060089A1 |
Provided are a burner tip, combustion burner, and boiler, provided with: a mixing chamber (92) provided in the interior thereof; a plurality of first mixed fluid nozzles (84, 85) that are disposed at prescribed intervals along the circum...
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WO/2015/051226A1 |
A burner (100) includes a cylindrical tube (110) that terminates in a burner discharge end (115) An annular disk (114) defines a hole (116). An oxidizer intake (120) delivers oxidizer into the tube (110). A fuel nozzle (140) delivers fue...
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WO/2015/050987A1 |
A method of manufacturing a fuel component for a gas turbine engine combustor includes additive manufacturing a sacrificial core and manufacturing a fuel component body at least partially around the sacrificial core. The sacrificial core...
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WO/2015/045835A1 |
This burner tip, a combustion, and boiler are provided with: a mixing chamber (84) provided in the interior; a plurality of mixed fluid spray holes (82) which are arranged at predetermined spacing in the circumferential direction, and wh...
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WO/2015/044908A1 |
A lance injector includes: an outer tubular body (15) and an inner tubular body (16), which extend along a common axis (A) and define a first fluid line (22) in a gap between the outer tubular body (15) and the inner tubular body (16), a...
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WO/2015/042614A1 |
A burner system includes a plurality of burners, each having a nozzle positioned to emit a stream of fuel into a combustion volume, and a perforated flame holder, including a plurality of apertures extending between first and second face...
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WO/2015/042615A1 |
A horizontally-fired flame burner includes a flame holder positioned laterally from the burner. The flame holder includes a plurality of perforations that collectively confine a combustion reaction of the burner to the flame holder.
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WO/2015/038024A1 |
Methods and systems of burning a multi-phase hydrocarbon fluid include determining a water content of the multi-phase hydrocarbon fluid, communicating the multiphase hydrocarbon fluid to a fuel port of a burner in a primary fuel flow,...
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WO/2015/032295A1 |
A fuel supply - vaporization - pressure regulation - premixed combustion system and thermoelectric power generation apparatus and method comprising said system, the fuel supply - vaporization - pressure regulation - premixed combustion s...
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WO/2015/023042A1 |
The present invention relates to a swirler. A swirler according to an embodiment of the present invention comprises: a casing; a pilot body placed inside the casing; and a plurality of vanes arranged along the periphery of the pilot body...
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WO/2015/014338A1 |
A burner arrangement (1) for a mobile heating appliance that is operated with liquid fuel is provided, the burner arrangement having: a combustion chamber (2) for the conversion of fuel with combustion air in a combustion flame, which co...
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WO/2015/010622A1 |
A burner nozzle comprises a fuel passage (7) and a combustion improver passage (2), wherein the combustion improver passage (2) is positioned within the fuel passage (7). An annular jet orifice made up of the inner wall of a nozzle outle...
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WO/2014/197072A2 |
A fuel nozzle for a combustor a gas turbine engine includes a flange with a first locator.
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WO/2014/177371A1 |
The invention relates to a burner lance (60), which can be arranged with a longitudinal axis (23) in a main flow direction inside a burner of a gas turbine. A downstream end of the burner lance (60) forms a burner lance tip (62), which i...
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WO/2014/171639A1 |
Disclosed is a gas burner which comprises: a chamber member into which flows alcohol water gas comprising alcohol and a water fraction, for burning; a heating body surrounding the chamber member; a heat-retaining heat-storage material su...
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WO/2014/147325A1 |
The invention mainly relates to a system (24) for injecting air and fuel for the annular combustion chamber bottom (10) of a turbine engine, comprising at least two devices for injecting fuel, among which are a central injector (26) and ...
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WO/2014/142305A1 |
A spray nozzle is equipped with a spray fluid flow path and a spray medium flow path, and is provided with first branch flow paths branching from the spray fluid flow path and second branch flow paths branching from the spray medium flow...
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WO/2014/141424A1 |
A spray nozzle is equipped with a spray fluid flow path and a spray medium flow path, and is provided with first branch flow paths branching from the spray fluid flow path and second branch flow paths branching from the spray medium flow...
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WO/2014/137412A1 |
A gas turbine engine device is disclosed for mixing fuel and air prior to a combustion. The device includes a pilot mixer (60) and a main mixer (62) each having a fuel opening (88, 68) for the delivery of fuel to one or more passages. In...
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WO/2014/128446A1 |
The invention comprises an effluent burner comprising a rotatable, hollow shaft with a first end for attaching to an effluent source and a second, output end, wherein the first and second ends are in fluid communication with each other; ...
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WO/2014/117625A1 |
A burner comprises a heat conduction cover body, a fuel pipe, and a nozzle. A cavity and a fire outlet are disposed in the heat conduction cover body. The fire outlet communicates with the cavity. The nozzle is mounted in the cavity. A s...
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WO/2014/097812A1 |
The purpose of the present invention is to provide a spray nozzle which both promotes atomization of the whole spray fluid by promoting atomization of the central portion of the spray in which the particle diameters in the spray fluid ar...
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WO/2014/090493A1 |
The present invention relates to a combustion chamber for a gas turbine. The combustion chamber comprises a pilot burner device, a fuel injector (102) and an ignitor unit (103). The pilot burner device comprises a pilot body (100) with a...
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WO/2014/090495A1 |
The present invention relates to a combustion chamber (120) for a gas turbine. The combustion chamber (120) comprises a pilot burner device, a fuel injector (102), an ignitor unit (103) and an air blast injector (104). The pilot burner d...
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WO/2014/081334A1 |
A liquid fuel cartridge assembly for a gas turbine combustor comprising an elongated stem provided with a fuel injector tip at an aft end of said stem, said injector tip provided with a pilot fuel passage extending to a pilot fuel orific...
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WO/2014/076812A1 |
A spray nozzle (1) that uses a spray medium to spray and burn a liquid fuel, wherein a fluid mixture (8) is formed by mixing a spray fluid (2) and a spray medium (3) in first convergence sections (91) of the spray nozzle, with this fluid...
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WO/2014/073279A1 |
A burner (20) is provided with: a cylinder section (21) having a premixing chamber (27) in which a mixed gas which contains fuel is formed, and also having a combustion chamber (28) in which the fuel combusts; a first pipe (41) for suppl...
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WO/2014/068275A1 |
A burner inlet assembly (200) and a method are disclosed. The burner inlet assembly (200) is for generating a fluid pulse deliverable to assist in removal of residues in a burner and comprises: a fluid accumulator (16) chargeable with a ...
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WO/2014/063845A1 |
The invention relates to a heating device operated with liquid fuel, having a fuel pump (1) that comprises a displacement element (2) and is used to suction the liquid fuel out of a tank (6) and feed it to a pressure-conducting region (7...
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WO/2014/062076A1 |
A multiphase burner for flaring gaseous/liquid combustable mixtures is disclosed. The burner may include a hollow base with an inlet for receiving the combustable gas/liquid mixture as well as a distal end that may be coupled to or th...
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WO/2014/053730A2 |
The invention relates to a start-up injector for a turbine engine combustion chamber, said injector comprising: a fuel injection circuit; and a fuel ignition circuit including a fuel injector supplied by the fuel injection circuit and a ...
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WO/2014/055864A1 |
A liquid vaporization system according to the present invention includes the application of energy, including pulsed electrical discharges, sparks or continuous arcs, to or within a spray comprising a liquid that may be combined with a f...
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WO/2014/050375A1 |
A burner is provided with a partition wall (49) for separating a mixing chamber (47) which generates a mixed gas and a combustion chamber (48) which combusts the mixed gas. Connection passages (50) which connect to both the mixing chambe...
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WO/2014/042363A1 |
A combustion apparatus according to the present invention includes: a fuel storage device in which a fuel is stored; and a main body connected with the fuel storage device by using a flexible pipe so as to be supplied with the fuel and c...
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WO/2014/030242A1 |
A combustion system provided with: a fuel tank; a pump for adding pressure to fuel supplied from the fuel tank; a first nozzle part for spraying the pressurized fuel in the combustion chamber; a supply pipe for coupling the first nozzle ...
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WO/2014/027596A1 |
A burner contains a tubular inner cylinder (33) and a tubular outer cylinder (31). The inner cylinder (33) mixes fuel and air. The outer cylinder (31) encloses the inner cylinder (33). An air-fuel mixture outlet (42) is formed on the per...
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WO/2014/024942A1 |
A burner (20) comprising: a first pipe section (30) having a discharge port (32) that discharges combustion gas formed therein; a second pipe section (40) that extends inside the first pipe section (30) towards the discharge port (32) an...
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WO/2014/024842A1 |
A burner tip, combustion burner, and a boiler improve combustibility by promoting atomization of liquid fuel by being provided with: a mixing chamber (56) provided in the interior; a plurality of mixed liquid spray holes (52, 53, 54) dis...
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WO/2014/024953A1 |
A burner for exhaust gas purification devices comprising: a pipe section comprising a premixing chamber for mixing combustion air and fuel and generating a premixed air, a combustion chamber for combusting the premixed air and generating...
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WO/2014/024944A1 |
A burner for exhaust gas purification devices, comprising a base, a first pipe section, and a second pipe section. The first pipe section has a base end section, a tip section, a combustion chamber wherein combustion air and fuel are com...
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WO/2014/024813A1 |
The present invention provides a spray nozzle with which atomization of a spray fluid can be promoted and the amount of a spray medium used, as well as the pressurization of the spray medium, can be reduced. This spray nozzle is characte...
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WO/2014/024943A1 |
A burner for exhaust gas purification devices, comprising a base section, a first pipe section, and a second pipe section. The first pipe section has a base end section, a tip section, a combustion chamber, and a discharge port from whic...
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WO/2014/016553A1 |
An inlet assembly for a burner and a method are disclosed. The inlet assembly for a burner comprises: a manifold having an inlet aperture and a coaxially aligned outlet aperture, the manifold having a nozzle bore extending along a longit...
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