| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 02/06/2014 | DE102012204777B4 Verfahren zur Herstellung eines Verkleidungselementes sowie Verkleidungselement A method for producing a cladding element and cladding element |
| 02/05/2014 | EP2693124A1 Pilot burner, burner, combustor and gas turbine engine |
| 02/05/2014 | EP2693123A1 Nozzle, gas turbine combustor and gas turbine |
| 02/05/2014 | EP2693122A1 Combustor for gas turbine engine and gas turbine |
| 02/05/2014 | EP2693121A1 Near-wall roughness for damping devices reducing pressure oscillations in combustion systems |
| 02/05/2014 | EP2693120A2 Gas turbine combustion chamber with mixing air openings and air guide elements of modular construction |
| 02/05/2014 | EP2693117A1 Reheat burner and method of mixing fuel/carrier air flow within a reheat burner |
| 02/05/2014 | EP2693021A1 Combustor and gas turbine provided with same |
| 02/05/2014 | EP2691702A1 Turbine combustion system liner |
| 02/05/2014 | CN203421728U Gas nozzle of low-calorific-value industrial gas turbine system |
| 02/05/2014 | CN103562643A Structural frame for gas turbine combustion cap assembly |
| 02/05/2014 | CN103562642A Gas turbine combustion cap assembly |
| 02/05/2014 | CN103562641A Annular combustion chamber for a turbomachine |
| 02/05/2014 | CN103557536A Ceramic heat shield sheet and heat-resistant structure |
| 02/05/2014 | CN102099628B Fuel staging in burner |
| 02/04/2014 | US8640464 Combustion system |
| 01/30/2014 | WO2014018277A1 Flexible combustor bracket |
| 01/30/2014 | US20140026586 Reheat burner and method of mixing fuel/carrier air flow within a reheat burner |
| 01/30/2014 | US20140026584 Compressed air energy storage system having variable generation modes |
| 01/30/2014 | US20140026581 Liner stop for turbine system combustor |
| 01/30/2014 | US20140026580 Combustor dome and heat-shield assembly |
| 01/30/2014 | US20140026579 Burner for a gas turbine |
| 01/30/2014 | US20140026578 Combustor nozzle assembly, combustor equipped with the same, and gas turbine |
| 01/29/2014 | EP2690365A1 Acoustic damper, combustor, and gas turbine |
| 01/29/2014 | EP2690364A2 Combustor dome and heat-shield assembly |
| 01/29/2014 | CN103547866A Turbine combustion system liner |
| 01/29/2014 | CN103542429A Axial swirler for a gas turbine burner |
| 01/29/2014 | CN103542428A Burner arrangement |
| 01/29/2014 | CN103542427A 燃气涡轮燃烧系统 The gas turbine combustion system |
| 01/29/2014 | CN103542426A Premix burner of the multi-cone type for a gas turbine |
| 01/29/2014 | CN101713541B Premixed direct injection nozzle |
| 01/23/2014 | US20140020397 Combustion chamber with a wall section and a brim element |
| 01/23/2014 | US20140020393 Combustor for gas turbine engine and gas turbine |
| 01/23/2014 | US20140020392 Gas turbine |
| 01/23/2014 | US20140020389 Combustor cap assembly |
| 01/22/2014 | EP2686613A1 Heat shield assembly |
| 01/22/2014 | CN103534531A Combustor for gas turbine engine and gas turbine |
| 01/22/2014 | CN103534530A Substrate with shaped cooling holes and methods of manufacture |
| 01/22/2014 | CN103528095A Gas turbine combustor and operating method for gas turbine combustor |
| 01/22/2014 | CN103528094A Dry-type low-nitrogen combustion device for gas fuel of gas turbine |
| 01/22/2014 | CN103528093A Combustion nozzle and an associated method thereof |
| 01/22/2014 | CN103528092A Internal jet airflow pressure-isolation air inlet combustor |
| 01/22/2014 | CN102384489B Small-sized annular combustion chamber with high-capacity heat intensity |
| 01/22/2014 | CN102165258B 燃料喷嘴 Fuel nozzle |
| 01/21/2014 | US8631656 Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities |
| 01/16/2014 | WO2014011265A2 Gas turbine fuel nozzle end cover using au-ni braze and method producing same |
| 01/16/2014 | US20140013764 Axial swirler for a gas turbine burner |
| 01/16/2014 | US20140013763 Fuel-air pre-mixer with prefilmer |
| 01/16/2014 | US20140013762 Combustor and gas turbine provided with same |
| 01/16/2014 | US20140013761 Combustor arrangement, especially for a gas turbine |
| 01/16/2014 | US20140013760 Premix burner of the multi-cone type for a gas turbine |
| 01/16/2014 | US20140013759 Premix burner of the multi-cone type for a gas turbine |
| 01/16/2014 | US20140013754 Power augmentation system with dynamics damping |
| 01/16/2014 | DE102005035085B4 Verfahren zur Einstellung der akustischen Eigenschaften einer Brennkammer Method for adjusting the acoustic characteristics of a combustion chamber |
| 01/15/2014 | EP2685172A2 Can-annular gas turbine combustion system with staged premix-combustion |
| 01/15/2014 | EP2685171A1 Burner arrangement |
| 01/15/2014 | EP2685170A1 Cooled wall structure for the hot gas parts of a gas turbine and method for manufacturing such a structure |
| 01/15/2014 | EP2685164A1 Axial swirler for a gas turbine burner |
| 01/15/2014 | CN203395943U Combustion chamber flame tube |
| 01/15/2014 | CN103518100A Heat shield assembly |
| 01/15/2014 | CN103512048A Cross fire tube retention system for a gas turbine engine |
| 01/15/2014 | CN103512047A Radial rotational flow double fuel nozzle for chemical regenerative cycle |
| 01/15/2014 | CN103512046A Transition duct for a gas turbine |
| 01/14/2014 | CA2713576C Fuel nozzle swirler assembly |
| 01/10/2014 | CA2820071A1 Axial swirler for a gas turbine burner |
| 01/09/2014 | WO2014008347A1 Non-symmetric arrangement of fuel nozzles in a combustor |
| 01/09/2014 | US20140007583 Combustion chamber and a method of mixing fuel and air in a combustion chamber |
| 01/09/2014 | US20140007582 Gas Turbine Combustor and Operating Method for Gas Turbine Combustor |
| 01/09/2014 | US20140007581 Fuel flexible fuel injector |
| 01/09/2014 | US20140007580 Retaining collar for a gas turbine combustion liner |
| 01/09/2014 | US20140007579 Non-symmetric arrangement of fuel nozzles in a combustor |
| 01/09/2014 | CA2820082A1 Gas turbine combustion system |
| 01/08/2014 | EP2682586A2 Gas turbine combustor and operating method for gas turbine combustor |
| 01/08/2014 | EP2681438A2 Fault tolerant control system for distributed micro-thrusters |
| 01/08/2014 | CN103502576A Method of forming multi-panel outer wall of component for use in gas turbine engine |
| 01/08/2014 | CN103499107A Supersonic combustor with heated kerosene as fuel |
| 01/08/2014 | CN103499106A Method for expanding stability limit of supersonic combustion flames |
| 01/03/2014 | WO2014004355A1 High pressure combustor with hot surface ignition |
| 01/03/2014 | WO2013044197A3 A combustor resonator section with an internal thermal barrier coating and method of fabricating the same |
| 01/03/2014 | WO2012090071A8 Multi-fuel injector having seperate air - premixing structures for the plurality of fuels and a consequent common mixing structure before the nozzle outlet |
| 01/03/2014 | CA2877595A1 High pressure combustor with hot surface ignition |
| 01/02/2014 | US20140000269 Combustion nozzle and an associated method thereof |
| 01/02/2014 | US20140000266 Gas Turbine Fuel Nozzle End Cover Using Au-Ni Braze and Method Producing Same |
| 01/02/2014 | US20140000265 Transition duct for a gas turbine |
| 01/02/2014 | US20140000263 Multi-premixer fuel nozzle support system |
| 01/01/2014 | EP2679907A2 Combustion nozzle and an associated method thereof |
| 01/01/2014 | EP2679906A2 Method for servicing a combustor cap assembly for a turbine |
| 01/01/2014 | EP2678610A1 Annular combustion chamber for a turbine engine including improved dilution openings |
| 01/01/2014 | EP2678609A1 Gas turbine combustion chamber |
| 01/01/2014 | CN103486619A Flame tube fixing structure |
| 01/01/2014 | CN103486618A Cyclone for aviation gas turbine engine |
| 01/01/2014 | CN103486617A Dual-fuel low-emission burner for gas turbine |
| 01/01/2014 | CN103486616A Method and device for controlling flame stability of gas turbine combustor |
| 01/01/2014 | CN103486615A Combustor liner cooling assembly for a gas turbine system |
| 01/01/2014 | CN103486591A Tempering-proof nozzle connecting section assembly of combustor of combustion gas turbine |
| 01/01/2014 | CN102235267B Gas turbine engine modified by using retired turbofan engine through low-pressure crest truncation |
| 12/31/2013 | CA2741100C High pressure oxy-fuel combustion system (hiprox) bottoming cycle |
| 12/31/2013 | CA2557047C Fuel nozzle for gas turbine engines |
| 12/27/2013 | WO2013192540A1 Turbine engine combustor wall with non-uniform distribution of effusion apertures |
| 12/27/2013 | WO2013191907A1 A wireless telemetry system including an induction power system |