| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 12/27/2013 | WO2013029984A3 Combustion chamber for a gas turbine plant |
| 12/27/2013 | CA2876399A1 A wireless telemetry system including an induction power system |
| 12/26/2013 | US20130341912 Fuel injector bearing plate assembly and swirler assembly |
| 12/26/2013 | US20130340437 Turbine engine combustor wall with non-uniform distribution of effusion apertures |
| 12/25/2013 | EP2677240A2 Active purge mechanism with backflow preventer for gas turbine fuel injectors |
| 12/25/2013 | EP2677239A1 Method for operating a two stage gas turbine combustion chamber |
| 12/25/2013 | EP2440367B1 Method for reducing the diameter of an opening |
| 12/25/2013 | CN103471136A Combustor assembly having a fuel pre-mixer |
| 12/25/2013 | CN103471135A Jet-stream air suction and jet combustor |
| 12/25/2013 | CN103471134A Impingement cooled combustor |
| 12/25/2013 | CN101532679B Lean direct injection combustion system |
| 12/24/2013 | CA2513982C Reactor |
| 12/19/2013 | WO2013188645A2 Gas turbine engine wall |
| 12/19/2013 | WO2013122643A3 Device to lower nox in a gas turbine engine combustion system |
| 12/19/2013 | WO2013121132A3 Air and fuel injection device for a turbomachine combustion chamber |
| 12/19/2013 | WO2013060974A3 Annular combustion chamber in a turbomachine |
| 12/19/2013 | WO2013045792A3 Annular combustion chamber for a turbine engine |
| 12/19/2013 | WO2013013740A3 Gas turbine centripetal annular combustion chamber and method for flow guidance |
| 12/19/2013 | WO2012161905A3 Thermally compliant support for a combustion system |
| 12/19/2013 | US20130333389 Cross fire tube retention system for a gas turbine engine |
| 12/19/2013 | US20130333387 Annular combustion chamber for a turbine engine including improved dilution openings |
| 12/19/2013 | CA2875028A1 Gas turbine engine wall |
| 12/18/2013 | EP2674679A2 Cross fire tube retention system for a gas turbine engine |
| 12/18/2013 | EP2674678A2 Method of manufacturing an impingement sleeve for a turbine engine combustor |
| 12/18/2013 | EP2674677A2 Combustor liner cooling assembly for a gas turbine system |
| 12/18/2013 | CN103459928A Ultra low emissions gas turbine combustor |
| 12/18/2013 | CN103459080A Hollow curved plate, method for manufacturing same, and burner for gas turbine |
| 12/18/2013 | CN103453555A Combustor with multiple combustion zones |
| 12/18/2013 | CN103453554A Fuel injection assembly for use in turbine engines and method of assembling same |
| 12/18/2013 | CN103453553A Turbomachine combustor nozzle and forming method thereof |
| 12/18/2013 | CN103452595A Novel air film hole with improved cooling efficiency |
| 12/17/2013 | US8607571 Lean burn injectors having a main fuel circuit and one of multiple pilot fuel circuits with prefiliming air-blast atomizers |
| 12/17/2013 | US8607570 Airblown syngas fuel nozzle with diluent openings |
| 12/12/2013 | WO2013184504A1 Combustor liner with reduced cooling dilution openings |
| 12/12/2013 | WO2013184502A1 Combustor liner with improved film cooling |
| 12/12/2013 | WO2013184496A1 Combustor liner with convergent cooling channel |
| 12/12/2013 | WO2013184495A2 Combustor liner with decreased liner cooling |
| 12/12/2013 | WO2013183618A1 Fuel injection device |
| 12/12/2013 | US20130327056 Combustor liner with decreased liner cooling |
| 12/12/2013 | US20130327049 Combustor liner with reduced cooling dilution openings |
| 12/12/2013 | US20130327048 Combustor liner with convergent cooling channel |
| 12/12/2013 | US20130327046 Combustor assembly having a fuel pre-mixer |
| 12/11/2013 | EP2672185A2 Combustor with a brief severe quench zone |
| 12/11/2013 | EP2672184A2 Method and apparatus for a fuel nozzle assembly for use with a combustor |
| 12/11/2013 | EP2672183A2 Combustor assembly having a fuel pre-mixer |
| 12/11/2013 | EP2672182A2 Impingment cooled combustor |
| 12/11/2013 | EP2672181A2 Controlling flame stability of a gas turbine combustor |
| 12/11/2013 | EP2671028A1 Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector |
| 12/11/2013 | CN103443421A Combustor and gas turbine provided with same |
| 12/11/2013 | CN103438480A Nozzle and combustor for a gas turbine engine, and corresponding methods |
| 12/11/2013 | CN102242939B Prefilming three-stage pre-mixing and pre-evaporating low-pollution combustor |
| 12/11/2013 | CN102200291B Pneumatic primary level graded low-pollution combustion chamber |
| 12/11/2013 | CN102175044B Mixing combustion guide coupling structure of combustion chamber |
| 12/11/2013 | CN101737803B Fuel nozzle assembly of a gas turbine engine and gas turbine engine |
| 12/10/2013 | US8601818 Conical gas turbine burner having a fuel lance with inclined side nozzles |
| 12/05/2013 | WO2013180424A1 Apparatus for a fuel-air pre-mixture using a rotary injection device and a gas turbine burner mounting the same |
| 12/05/2013 | WO2013178941A1 Method for compacting anodic paints, including the collision of sandblasting jets |
| 12/05/2013 | US20130318992 Combustor with a Brief Severe Quench Zone |
| 12/05/2013 | US20130318991 Combustor With Multiple Combustion Zones With Injector Placement for Component Durability |
| 12/05/2013 | US20130318978 Liner assembly |
| 12/05/2013 | US20130318976 Turbomachine combustor nozzle and method of forming the same |
| 12/05/2013 | US20130318975 Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same |
| 12/05/2013 | CA2874833A1 Method for compacting anodic paints, including the collision of sandblasting jets |
| 12/04/2013 | EP2669581A2 Combustor with multiple combustion zones with injector placement for component durability |
| 12/04/2013 | EP2669580A2 Fuel injection assembly for use in turbine engines and method of assembling same |
| 12/04/2013 | EP2669579A2 Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same |
| 12/04/2013 | EP2669577A1 Flame detection in no-flame region of gas turbine |
| 12/04/2013 | EP2667999A1 Method for perforating a wall of a combustion chamber |
| 12/04/2013 | EP2116770B1 Combustor dynamic attenuation and cooling arrangement |
| 12/04/2013 | CN103423774A Sealed connecting structure of combustion chamber flame tube with pressure stabilizing chamber and transition section |
| 12/04/2013 | CN103423773A 二次燃烧系统 Secondary combustion system |
| 12/04/2013 | CN103423772A Liquid cartridge with passively fueled premixed air blast circuit for gas operation |
| 12/04/2013 | CN103423771A Turbomachine combustor and method for adjusting combustion dynamics in the same |
| 12/04/2013 | CN103423770A 燃料喷嘴帽 Fuel nozzle cap |
| 12/04/2013 | CN103423769A 燃料喷嘴帽 Fuel nozzle cap |
| 12/04/2013 | CN103423768A Bleed air purging system of dual-fuel combustor nozzle itself |
| 12/04/2013 | CN102022754B Circumferentially self expanding combustor support for a turbine engine |
| 12/04/2013 | CN101551119B Replaceable orifice for combustion tuning and related method |
| 12/03/2013 | US8596074 Gas turbine combustor |
| 12/03/2013 | US8596035 Apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbines |
| 12/03/2013 | CA2620415C Hydrostatic flow barrier for flexible fuel manifold |
| 12/03/2013 | CA2533253C High velocity oxygen fuel (hvof) liquid fuel gun and burner design |
| 11/28/2013 | WO2013176876A1 Liquid-gas mixer and turbulator therefor |
| 11/28/2013 | WO2013175126A2 Turbomachine combustion chamber shell ring |
| 11/28/2013 | US20130312420 Chamber-bottom baffle, combustion chamber comprising same and gas turbine engine fitted therewith |
| 11/28/2013 | US20130312385 Gas turbine system having a plasma actuator flow control arrangement |
| 11/28/2013 | DE102005038395B4 Brennkammerkühlung mit geneigten segmentierten Flächen Combustion chamber cooling with inclined surfaces segmented |
| 11/27/2013 | EP2667099A2 Liquid cartridge with passively fueled premixed air blast circuit for gas operation |
| 11/27/2013 | EP2667098A2 Liquid swirler flow control |
| 11/27/2013 | EP2667096A2 Turbomachine combustor and method for adjusting combustion dynamics in the same |
| 11/27/2013 | CN203309935U Single-liner type combustion gas turbine combustion chamber |
| 11/27/2013 | CN203309934U Combustion chamber of aero-engine |
| 11/27/2013 | CN103415743A Annular combustion chamber for a turbine engine including improved dilution openings |
| 11/27/2013 | CN103411236A Opening side skirt plate type on-duty flame stabilizer |
| 11/27/2013 | CN101772628B Fuel control method and fuel control apparatus for gas turbine and gas turbine |
| 11/26/2013 | US8590313 Precision counter-swirl combustor |
| 11/26/2013 | CA2545618C Cooled support boss for a combustor in a gas turbine engine |
| 11/21/2013 | WO2013173162A2 Multistaged lean prevaporizing premixing fuel injector |
| 11/21/2013 | WO2013172770A1 Fuel injection system for use in a catalytic heater and reactor for operating catalytic combustion of liquid fuels |
| 11/21/2013 | WO2013143983A3 Mixing arrangement for mixing a fuel with a stream of oxygen containing gas |