Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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03/23/2000 | WO1999067570A3 DRY, LOW NOx CATALYTIC PILOT |
03/22/2000 | EP0987495A1 Method for minimizing thermo-acoustic vibrations in gas turbine combustion chambers |
03/22/2000 | EP0987493A1 Burner for a heat generator |
03/22/2000 | EP0987491A1 Method for preventing flow instabilities in a burner |
03/22/2000 | EP0986717A1 Dual fuel injection method and apparatus |
03/22/2000 | EP0730707B1 Gas valve |
03/21/2000 | US6038863 Burner arrangement for a gas turbine for preventing the ingress of fluids into a fuel passage |
03/21/2000 | US6038862 Vibration damper for a fuel nozzle of a gas turbine engine |
03/21/2000 | US6038861 Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors |
03/21/2000 | US6038852 Wear resistant augmentor fuel manifold clamp |
03/16/2000 | CA2282153A1 Burner for a heat generator |
03/15/2000 | EP0985882A1 Vibration damping in combustors |
03/15/2000 | EP0985810A1 Method and device for minimizing thermo-acoustic oscillations in gas turbine combustion chambers |
03/14/2000 | US6036479 Two-stage pressure atomizer nozzle |
03/14/2000 | US6036467 Apparatus for ultrasonically assisted melt extrusion of fibers |
03/14/2000 | US6035645 Aerodynamic fuel injection system for a gas turbine engine |
03/14/2000 | US6035644 Turbine control valve |
03/09/2000 | WO2000012940A1 Method for operating a gas turbine and corresponding gas turbine |
03/09/2000 | WO2000012939A1 Burner assembly |
03/09/2000 | WO2000012936A1 Burner arrangement with primary and secondary pilot burners |
03/09/2000 | WO2000012933A1 Hybrid burner and method for operating a hybrid burner |
03/09/2000 | WO2000000772A3 DRY, LOW NOx CATALYTIC PILOT |
03/08/2000 | EP0717813B1 Method of operating a gas turbine using an additive feed |
03/07/2000 | US6033207 Flameless combustion and utilization of fuel gases |
03/07/2000 | US6032457 Fuel nozzle guide |
03/07/2000 | US6032361 Gas turbine multi-hole film cooled combustor liner and method of manufacturing |
03/02/2000 | WO2000011404A1 Operating method for a hybrid burner |
03/02/2000 | WO2000011403A1 Elliptical axial combustor swirler |
03/02/2000 | WO2000010951A1 Formation of a stable wax slurry from a fischer-tropsch reactor effluent |
03/02/2000 | DE19839085A1 Brenneranordnung mit primärem und sekundärem Pilotbrenner Burner assembly with primary and secondary pilot burner |
03/01/2000 | EP0982546A2 Combustor baffle |
03/01/2000 | EP0982545A2 A combustion chamber |
03/01/2000 | EP0832397B1 Catalytic gas turbine burner |
02/29/2000 | US6029455 Turbojet engine combustion chamber with heat protecting lining |
02/24/2000 | WO2000009945A1 Arrangement for reduction of acoustinc vibrations in a combustion chamber |
02/23/2000 | EP0663990B1 Injector tip cooling using fuel as the coolant |
02/23/2000 | CN1245250A Fuel injector with replaceable sensor |
02/22/2000 | US6026645 Fuel/air mixing disks for dry low-NOx combustors |
02/22/2000 | US6026644 Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer |
02/16/2000 | EP0979974A2 Method and apparatus for spraying fuel within a gas turbine engine |
02/16/2000 | EP0979972A1 Burner arrangement with a main and a pilot burner and pilot burner for such an arrangement |
02/16/2000 | CN1244909A Combustor dilution bypass system |
02/16/2000 | CN1244645A Method and device for gas burner |
02/09/2000 | EP0978689A2 Gas turbine combustor by-pass valve device |
02/09/2000 | EP0823035B1 Headpiece of a gas turbine ring-shaped combustion chamber |
02/08/2000 | US6021635 Dual orifice liquid fuel and aqueous flow atomizing nozzle having an internal mixing chamber |
02/08/2000 | US6021570 Annular one piece combustor liner |
02/02/2000 | EP0976982A1 Method of operating the combustion chamber of a liquid-fuel gas turbine |
02/02/2000 | CN1049042C Combustion apparatus and combustion method therein |
02/01/2000 | US6018950 Combustion turbine modular cooling panel |
01/26/2000 | EP0974789A1 Method of operating the combustion chamber of a liquid-fuel gas turbine |
01/26/2000 | EP0974788A1 Device for directed noise attenuation in a turbomachine |
01/26/2000 | EP0974735A2 Dimpled impingement baffle |
01/26/2000 | CN1242830A Combustor arrangement |
01/26/2000 | CN1242469A Apparatus for guiding into combustion chamber with fuel and/or water selectively |
01/25/2000 | US6016658 Low emissions combustion system for a gas turbine engine |
01/20/2000 | WO2000003182A1 Igniter with porous sleeve |
01/19/2000 | EP0972993A2 Crossfire tube for gas turbine combustors |
01/19/2000 | EP0972992A2 Combustor liner |
01/19/2000 | EP0972987A2 Fuel injector with a replaceable sensor |
01/19/2000 | EP0971792A2 Nozzle, application for a nozzle and method for injecting a first fluid into a second fluid |
01/18/2000 | US6015285 Catalytic combustion process |
01/16/2000 | CA2276862A1 Fuel injector with a replaceable sensor |
01/12/2000 | EP0971172A1 Gas turbine combustion chamber with silencing wall structure |
01/12/2000 | EP0832399B1 Catalytic ignition burner for a gas turbine |
01/12/2000 | EP0832398B1 Catalytic combustion chamber for a gas turbine |
01/11/2000 | US6013919 Flame sensor with dynamic sensitivity adjustment |
01/06/2000 | WO2000000773A1 A method for starting a combustion device |
01/06/2000 | WO2000000772A2 DRY, LOW NOx CATALYTIC PILOT |
01/06/2000 | WO2000000770A1 Fuel injector for gas turbine engine |
01/05/2000 | EP0969252A2 A combustion chamber |
01/05/2000 | EP0968355A1 Cooling supply manifold assembly for cooling combustion turbine components |
01/05/2000 | DE19829398A1 Gas turbine with reduced noise operation |
01/04/2000 | US6010592 Method and apparatus for increasing the flow rate of a liquid through an orifice |
01/04/2000 | CA2056589C Air fuel mixer for gas turbine combustor |
01/04/2000 | CA2056480C Gas turbine engine fuel manifold |
12/29/1999 | WO1999067570A2 DRY, LOW NOx CATALYTIC PILOT |
12/29/1999 | CN1239766A Premixing fuel injector with improved secondary fuel-air injection |
12/28/1999 | US6006523 Gas turbine combustor with angled tube section |
12/23/1999 | DE19924305A1 Catalytic burner for gas turbine engine |
12/23/1999 | DE19923431A1 Combustion engine containing catalytic reactor |
12/22/1999 | EP0852687B1 Fuel injector arrangement for a combustion apparatus |
12/21/1999 | US6003299 System for modulating air flow through a gas turbine fuel injector |
12/21/1999 | US6003297 Method and apparatus for operating a gas turbine, with fuel injected into its compressor |
12/16/1999 | WO1999064791A1 Combustor cooling method |
12/15/1999 | EP0964206A1 Variable geometry gas turbine combustor chamber |
12/15/1999 | EP0964204A2 Premixing fuel injector with improved secondary fuel-air injection |
12/15/1999 | EP0963534A1 A flameholder device for afterburners in gas turbine engines |
12/14/1999 | US6000212 Catalytic combustion chamber with pilot stage and a method of operation thereof |
12/09/1999 | WO1999063275A1 Film cooling strip for gas turbine engine combustion chamber |
12/09/1999 | WO1999063274A1 Impingement and film cooling for gas turbine combustor walls |
12/09/1999 | WO1999063268A1 Fuel injector |
12/09/1999 | DE19825335A1 Procedure for operation of gas turbine |
12/08/1999 | EP0962704A2 Method and apparatus for use with a gas fueled combustor |
12/08/1999 | EP0962699A2 A fuel injector |
12/08/1999 | EP0961907A1 Combustor arrangement |
12/08/1999 | EP0961906A1 Method for active attenuation of a combustion oscillation, and combustion device |
12/08/1999 | CA2274563A1 Premixing fuel injector with improved secondary fuel-air injection |
12/07/1999 | US5996352 Thermally decoupled swirler for a gas turbine combustor |
12/07/1999 | US5996351 Rapid-quench axially staged combustor |