| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
|---|
| 05/26/2010 | CN1818527B Heat shield |
| 05/26/2010 | CN1707080B Methods and apparatus for low emission gas turbine energy generation |
| 05/26/2010 | CN1704574B Fuel nozzle and method for cooling fuel nozzle |
| 05/26/2010 | CN1621671B Method and device for monitoring gas turbine combustion dynamics |
| 05/26/2010 | CN1487237B Combustor radome for combustion gas worm gear engine |
| 05/26/2010 | CN1441198B Ripple type casing for gas turbine engine burner and its forming method |
| 05/26/2010 | CN1432762B Stress eliminating method and device for combustor casing in gas turbine |
| 05/26/2010 | CN101713550A Flame tube with central cyclone |
| 05/26/2010 | CN101713549A System and method for air-fuel mixing in gas turbines |
| 05/26/2010 | CN101713548A Tubular fuel injector for secondary fuel nozzle |
| 05/26/2010 | CN101713547A Circumferential fuel circuit divider |
| 05/26/2010 | CN101713546A Low-pollution combustor for various fuels |
| 05/25/2010 | US7721553 Method and apparatus for detecting a flashback condition in a gas turbine |
| 05/25/2010 | US7721545 Device for injecting a mixture of air and fuel, combustion chamber and turbomachine both equipped with such a device |
| 05/25/2010 | US7721437 Methods for assembling gas turbine engine combustors |
| 05/20/2010 | WO2009053417A3 Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring |
| 05/20/2010 | US20100122537 Combustors with inserts between dual wall liners |
| 05/20/2010 | DE112008001448T5 Kraftstoffinjektor mit Helmholtz-Resonatoren für einen Turbinenmotor Fuel injector with Helmholtz resonators for a turbine engine |
| 05/20/2010 | DE102009044513A1 Integrierte Brennkammeranordnung und Erststufen-Leitdüse für eine Gasturbine und Verfahren Integrated combustor assembly and first-stage guide nozzle for a gas turbine and procedures |
| 05/20/2010 | DE102008057428A1 Schutzstruktur und deren Verwendung Protective structure and the use thereof |
| 05/19/2010 | EP2187129A1 Gas turbine |
| 05/19/2010 | EP2187128A1 Combustor |
| 05/19/2010 | EP2187127A1 Gas turbine combustor |
| 05/19/2010 | EP2187126A1 Plasma flow controlled diffuser system |
| 05/19/2010 | EP2187125A1 Method and device for damping combustion oscillation |
| 05/19/2010 | EP2187022A1 Cooling structure for gas-turbine combustor |
| 05/19/2010 | EP2187021A1 Gas turbine combustor |
| 05/19/2010 | EP2185869A2 A multi-stage axial combustion system |
| 05/19/2010 | EP2185868A1 Device and method for regulating the exhaust temperature of a gas turbine |
| 05/19/2010 | CN201476063U Fuel manifold of combustion chamber |
| 05/19/2010 | CN101709884A Premixing and pre-evaporating combustion chamber |
| 05/19/2010 | CN101709660A Low btu fuel flow ratio duct burner for heating and heat recovery systems |
| 05/19/2010 | CN101709656A Coupling method for improving blade cooling efficiency and combustion efficiency of interstage/afterburner/channel combustion chambers |
| 05/19/2010 | CN101166935B Process and device for regulating the course of a gas turbine combustion chamber |
| 05/18/2010 | US7717700 Hybrid burner and associated operating method |
| 05/18/2010 | CA2454922C Process of removing a ceramic coating deposit in a surface hole of a component |
| 05/18/2010 | CA2451303C Methods for replacing combustor liners |
| 05/14/2010 | WO2010052662A2 Single can combustor gas turbine with bifurcated hot gas header and dilution air differentiated flow |
| 05/14/2010 | WO2010052434A2 System and method for washing and purging the liquid fuel system of a turbine with water |
| 05/14/2010 | WO2010023319A3 Device for mounting a flame-holder arm on an afterburner casing |
| 05/14/2010 | WO2009056518A3 Combustion chamber for gas turbines, including an igniter |
| 05/13/2010 | US20100115967 Eccentric chamfer at inlet of branches in a flow channel |
| 05/13/2010 | US20100115953 Integrated Combustor and Stage 1 Nozzle in a Gas Turbine and Method |
| 05/12/2010 | EP2184542A2 Fuel nozzle assembly for use with a gas turbine engine and method of assembling same |
| 05/12/2010 | CN201461131U Self-priming jet engine for aircraft |
| 05/11/2010 | US7712314 Venturi cooling system |
| 05/11/2010 | CA2676773A1 Fuel injector |
| 05/11/2010 | CA2459187C Sector staging combustor |
| 05/06/2010 | WO2010049206A1 Burner inserts for a gas turbine combustion chamber and gas turbine |
| 05/06/2010 | WO2009123851A3 Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities |
| 05/06/2010 | WO2009038625A3 A multi-stage axial combustion system |
| 05/06/2010 | US20100107651 Hybrid propulsive engine including at least one independently rotatable compressor stator |
| 05/06/2010 | US20100107647 Toroidal boundary layer gas turbine |
| 05/06/2010 | US20100107639 Fuel nozzle assembly for use with a gas turbine engine and method of assembling same |
| 05/05/2010 | EP2182290A1 Gas turbine combustor |
| 05/05/2010 | EP2182289A2 Method and apparatus for affecting a recirculation zone in a combustor cross flow |
| 05/05/2010 | EP2182288A2 Triple swirl gas turbine combustor |
| 05/05/2010 | EP2182287A2 Diluent Shroud for Combustor |
| 05/05/2010 | EP2182286A2 Combustor Liner Cooling Flow Disseminator and Related Method |
| 05/05/2010 | EP2182285A1 Burner insert for a gas turbine combustion chamber and gas turbine |
| 05/05/2010 | EP2182195A1 Gas turbine combustor |
| 05/05/2010 | EP1540247B1 Stress relief feature for aerated gas turbine fuel injector |
| 05/04/2010 | US7707836 Venturi cooling system |
| 05/04/2010 | CA2420313C Multimode injection system for an air/gasoline mixture in a combustion chamber |
| 04/29/2010 | US20100101232 Compliant metal support for ceramic combustor liner in a gas turbine engine |
| 04/29/2010 | US20100101208 Systems and Methods Involving Reduced Thermo-Acoustic Coupling of Gas Turbine Engine Augmentors |
| 04/28/2010 | EP2180311A1 Optical sensor and method for three-dimensional combustion sensing and combustion control system |
| 04/28/2010 | EP2180256A2 Dual wall structure for use in a combustor of a gas turbine engine |
| 04/28/2010 | CN1878986B Device for stabilizing combustion in gas turbine engines |
| 04/27/2010 | US7703288 Fuel nozzle having swirler-integrated radial fuel jet |
| 04/27/2010 | CA2454278C Method for operating a burner of a gas turbine, and power plant installation |
| 04/22/2010 | WO2010044958A1 Methods and systems for controlling the products of combustion |
| 04/22/2010 | WO2010024989A3 Multi passage fuel manifold and methods of construction |
| 04/22/2010 | US20100095679 Dual wall structure for use in a combustor of a gas turbine engine |
| 04/22/2010 | US20100095676 Multiple Tube Premixing Device |
| 04/22/2010 | US20100095675 Combustor Burner Vanelets |
| 04/22/2010 | DE102009043829A1 Mehrfachrohr-Vormischvorrichtung Multiple tube premix |
| 04/22/2010 | DE102009026400A1 Systeme und Verfahren für gestufte Verbrennung Systems and methods for staged combustion |
| 04/22/2010 | DE102009026364A1 Leitschäufelchen eines Brenners für eine Brennkammer Leitschäufelchen a burner for a combustion chamber |
| 04/22/2010 | DE102008052602A1 Swirler useful in burner of gas turbine, comprises blade having inlet openings, inner supply tube that supplies fuel to the openings and distributor feed that supplies fuel to blade, where the openings are produced by spark-erosion machine |
| 04/22/2010 | DE102006042124B4 Gasturbinenbrennkammer A gas turbine combustor |
| 04/22/2010 | CA2737133A1 Methods and systems for controlling the products of combustion |
| 04/22/2010 | CA2674070A1 Gas turbine combustor repair using a make-up ring |
| 04/21/2010 | EP2177835A2 Fuel delivery system for a turbine engine |
| 04/21/2010 | EP2177834A2 Method and apparatus of introducing diluent flow into a combustor |
| 04/21/2010 | EP2177833A2 Metering of diluent flow in combustor |
| 04/21/2010 | EP2177832A2 Method and apparatus for introducing diluent flow into a combustor |
| 04/21/2010 | EP2177831A2 Method and apparatus of fuel nozzle diluent introduction |
| 04/15/2010 | WO2010042136A2 Alternately swirling mains in lean premixed gas turbine combustors |
| 04/15/2010 | WO2010017345A3 Multistage gas furnace having split manifold |
| 04/15/2010 | WO2009121781A8 Pilot combustor in a burner |
| 04/15/2010 | WO2009078891A3 Secondary fuel delivery system |
| 04/15/2010 | WO2009039142A3 Flexure seal for fuel injection nozzle |
| 04/15/2010 | US20100089068 Combustion liner damper |
| 04/15/2010 | US20100089066 Cool flame combustion |
| 04/15/2010 | US20100089065 Fuel delivery system for a turbine engine |
| 04/15/2010 | DE102009043894A1 Unterteilter Brennkammerdeckel Divided combustion chamber lid |
| 04/14/2010 | EP2175118A2 Gasifier and cyclone separator for coal combustion |
| 04/14/2010 | CN101694301A Counter-flow flame combustion chamber |
| 04/13/2010 | US7694522 Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine |