| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 03/20/2013 | CN202813440U Combustion chamber of small-sized turbine jet engine |
| 03/20/2013 | CN1609513B Methods and apparatus for attaching swirlers to turbine engine combustors |
| 03/20/2013 | CN102985758A Tangential combustor with vaneless turbine for use on gas turbine engines |
| 03/20/2013 | CN102985757A Ignition procedure for a turbine engine combustion chamber |
| 03/20/2013 | CN102980209A Plasma catalysis ignition integrated nozzle |
| 03/20/2013 | CN102980208A Dual-fuel spray nozzle for oil-gas automatic switching in chemical heat return circulation |
| 03/20/2013 | CN102980207A Method for switching over a combustion device |
| 03/20/2013 | CN102980206A Flame stabilizer and engine combustion chamber comprising same |
| 03/19/2013 | US8397510 Combustor for gas turbine |
| 03/19/2013 | CA2724460C Combustion device and method for controlling combustion device |
| 03/14/2013 | WO2013036198A1 Burner comprising a reactor for catalytic burning |
| 03/14/2013 | WO2013035474A1 Gas turbine combustor |
| 03/14/2013 | WO2010115921A3 Method for analysing the humming tendency of a combustion chamber, and method for controlling a gas turbine |
| 03/14/2013 | US20130061598 System and method for conditioning a working fluid in a combustor |
| 03/14/2013 | US20130061593 System and method for controlling a combustor assembly |
| 03/13/2013 | EP2568221A2 Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber |
| 03/13/2013 | EP2568220A2 System and method for damping combustor nozzle vibrations |
| 03/13/2013 | EP2568219A1 System and method for controlling a combustor assembly |
| 03/13/2013 | EP2568218A2 Fuel gas pressure control system and method for reducing gas turbine fuel supply pressure requirements |
| 03/13/2013 | EP2567785A1 Method to machine a workpiece and arrangement comprising a support-structure and a workpiece |
| 03/13/2013 | CN202792105U Shell, cooling structure of flame tube and combustion chamber |
| 03/13/2013 | CN202792104U Flame tube wall plate, flame tube and combustion chamber of combustion gas turbine |
| 03/13/2013 | CN102971510A Air recovery-type cooling structure for air-cooled gas turbine combustor |
| 03/13/2013 | CN102966976A Injection nozzle assembly for a gas turbomachine |
| 03/13/2013 | CN102966975A Infrared low-temperature combustion device and method of dual working medium combined-cycle turbine |
| 03/13/2013 | CN102966974A Supersonic combustor wall surface concave cavity structure and engine combustor comprising same |
| 03/12/2013 | US8393161 Combustion chamber and gas turbine installation |
| 03/12/2013 | US8393159 Gas turbine combustor and fuel supply method for same |
| 03/12/2013 | CA2577770C Hybrid burner lance |
| 03/07/2013 | WO2013030492A1 Combustion chamber wall |
| 03/07/2013 | WO2013030230A2 Device for installing and removing a component on or in a stationary gas turbine and method for installing and removing a component of a stationary gas turbine |
| 03/07/2013 | WO2013029981A1 Combustion chamber for a gas turbine plant |
| 03/07/2013 | WO2013029980A1 Process for producing refractory ceramics for gas turbine plants |
| 03/07/2013 | US20130055716 Gas-turbine combustion chamber with a holding means of a seal for an attachment |
| 03/07/2013 | DE102011081962A1 Brennkammer für eine Gasturbinenanlage Combustor for a gas turbine plant |
| 03/07/2013 | CA2847324A1 Device for installing and removing a component on or in a stationary gas turbine and method for installing and removing a component of a stationary gas turbine |
| 03/07/2013 | CA2843690A1 Combustion chamber wall |
| 03/06/2013 | EP2565541A2 Injection nozzle assembly for a gas turbomachine |
| 03/06/2013 | EP2565539A1 Method for operating a combustion device |
| 03/06/2013 | EP2565427A1 Method for switching over a combustion device of a gas turbine engine from operation with a first premixed fuel to a second premixed fuel |
| 03/06/2013 | EP2565399A1 Device for assembling and disassembling a component of or in a stationary gas turbine and method for assembling and disassembling a component of a stationary gas turbine |
| 03/06/2013 | CN102959334A A combustion apparatus |
| 03/06/2013 | CN102959333A A combustion apparatus and gas turbine engine |
| 03/06/2013 | CN102959206A System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor |
| 03/06/2013 | CN102954495A Combustor resonator |
| 03/06/2013 | CN102954494A Flow adjustment orifice systems for fuel nozzles for a gas turbine engine |
| 03/06/2013 | CN102954493A Micromixer heat shield |
| 03/06/2013 | CN102954492A System and method for reducing combustion dynamic performance in combustor |
| 03/06/2013 | CN102954488A Ignition system for a gas turbine combustor |
| 03/06/2013 | CN102953821A Method for operating a gas turbine and gas turbin unit for carrying out the method |
| 03/06/2013 | CN102175045B Low-emission combustion chamber with main combustible stage head part multi-point slant oil taking |
| 03/06/2013 | CN101675227B Cooling structure for gas-turbine combustor |
| 03/06/2013 | CN101446421B Internal manifold air extraction system for IGCC combustor and method |
| 03/06/2013 | CN101373075B Turbine fuel delivery apparatus and system |
| 03/06/2013 | CA2776530A1 Pin fin arrangement for heat shield of gas turbine engine |
| 02/28/2013 | WO2013028562A1 Split control unit |
| 02/28/2013 | WO2013028561A1 Staged cooling flow nozzle valve |
| 02/28/2013 | WO2013028163A1 Tangential and flameless annular combustor for use on gas turbine engines |
| 02/28/2013 | WO2011149973A8 Tangential combustor with vaneless turbine for use on gas turbine engines |
| 02/28/2013 | WO2010096817A3 Combustion system |
| 02/28/2013 | US20130047621 Multi-pierced combustion chamber with counter-rotating tangential flows |
| 02/28/2013 | US20130047620 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 02/28/2013 | US20130047619 Injection nozzle assembly for a gas turbomachine |
| 02/28/2013 | US20130047618 Wall elements for gas turbine engines |
| 02/27/2013 | EP2562479A2 Wall elements for gas turbine engines |
| 02/27/2013 | EP2562394A1 Fuel supply device of gas turbine engine |
| 02/27/2013 | CN202757150U Plasma catalysis gas rotational flow nozzle |
| 02/27/2013 | CN202757149U Plasma strengthen atomization nozzle |
| 02/27/2013 | CN102947650A Turbine burner |
| 02/27/2013 | CN102944027A Gas combustion chamber for Stirling engine |
| 02/21/2013 | WO2013023913A2 Pressure casting slip and refractory ceramic produced therefrom for gas turbine units |
| 02/21/2013 | WO2013023886A1 Combustion arrangement and turbine comprising a damping facility |
| 02/21/2013 | US20130042623 Conical reverse-flow combustion chamber for a turbomachine |
| 02/21/2013 | US20130042620 Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology |
| 02/21/2013 | US20130042619 Combustor resonator |
| 02/21/2013 | DE102011081112A1 Verfahren zur Herstellung eines Bauteils für hohe thermische Belastungen, ein Bauteil herstellbar mit dem Verfahren und ein Flugzeugtriebwerk mit dem Bauteil A method for producing a component for high thermal loads, a component produced by the method and an aircraft engine with the component |
| 02/20/2013 | EP2559948A1 Gas turbine control device |
| 02/20/2013 | EP2559947A2 Micromixer Heat Shield |
| 02/20/2013 | EP2559946A2 System and method for reducing combustion dynamics in a combustor |
| 02/20/2013 | EP2559945A1 Combustion arrangement and turbine comprising a damping facility |
| 02/20/2013 | EP2559944A2 Combustor Resonator |
| 02/20/2013 | EP2559942A1 Gas turbine combustion chamber head with cooling and damping |
| 02/20/2013 | EP2559940A1 Flow adjustment orifice systems for fuel nozzles for a gas turbine engine |
| 02/20/2013 | EP2559678A1 Pressure-cast slip and fire-resistant ceramic for gas turbine assemblies produced using the same |
| 02/20/2013 | EP2558781A1 Swirl generator for a torch |
| 02/20/2013 | CN102937300A Diluting-agent graded injection system for gas turbine |
| 02/19/2013 | US8375726 Combustor assembly in a gas turbine engine |
| 02/19/2013 | US8375721 Burners for a gas turbine engine |
| 02/19/2013 | CA2605220C Gas turbine internal manifold mounting arrangement |
| 02/19/2013 | CA2594321C Fuel conveying member for a gas turbine engine |
| 02/17/2013 | CA2779318A1 Flow balancing valve |
| 02/14/2013 | WO2013023147A1 Combustor |
| 02/14/2013 | WO2013022539A1 Improved multi-fuel injection nozzle |
| 02/14/2013 | WO2013022367A1 System for injecting fuel in a gas turbine engine |
| 02/14/2013 | WO2013021354A2 Ceramic tile for combustion chambers lining, in particular of gas turbines, and manufacturing method thereof |
| 02/14/2013 | US20130040255 System for gasification fuel injection |
| 02/14/2013 | US20130036742 Combustor liner cooling system |
| 02/14/2013 | CA2844693A1 Combustor |
| 02/13/2013 | EP2557362A2 Turbomachine combustor assembly |
| 02/13/2013 | EP2557361A2 System and method for monitoring a combustor |