| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 07/10/2013 | CN203052722U Combustion chamber machine box |
| 07/10/2013 | CN203052721U Swirler blade and swirler for engine |
| 07/10/2013 | CN103196159A Annular grading trapped vortex combustor |
| 07/10/2013 | CN103196158A Combustor and method for distributing fuel in the combustor |
| 07/10/2013 | CN103196157A System and method for supplying a working fluid to a combustor |
| 07/10/2013 | CN103196156A Combustor fuel nozzle and method for supplying fuel to a combustor |
| 07/10/2013 | CN103196155A System comprising fuel nozzles for injecting fuel in a gas turbine combustor |
| 07/10/2013 | CN103196154A Combustor and method for distributing fuel in the combustor |
| 07/10/2013 | CN103196153A Combustor of a turbomachine |
| 07/10/2013 | CN103195612A Multifunctional turbofan jet engine |
| 07/10/2013 | CN103195587A Fuel flow control method and fuel flow control system of gas turbine combustor for humid air gas turbine |
| 07/09/2013 | US8479518 System for supplying a working fluid to a combustor |
| 07/09/2013 | US8479492 Hybrid slinger combustion system |
| 07/04/2013 | WO2013102136A2 Fuel injector |
| 07/04/2013 | WO2013096989A1 Rijke type combustion arrangement and method |
| 07/04/2013 | WO2012107257A3 Burner carrier having separate inner flange and outer flange |
| 07/04/2013 | US20130167547 Turbine engine and method for flowing air in a turbine engine |
| 07/04/2013 | US20130167546 Gas turbine engine combustor |
| 07/04/2013 | US20130167545 Combustor system for use in turbine engines and methods of operating a turbine engine |
| 07/04/2013 | US20130167544 Fuel injector |
| 07/04/2013 | US20130167543 Methods and systems for cooling a transition nozzle |
| 07/04/2013 | US20130167539 Fuel nozzles for injecting fuel in a gas turbine combustor |
| 07/04/2013 | US20130167537 Quick disconnect combustion endcover |
| 07/03/2013 | EP2609372A2 Combustion chamber for an aircraft engine, and method for attaching an injection system in a combustion chamber of an aircraft engine |
| 07/03/2013 | EP2609368A1 Burner arrangement |
| 07/03/2013 | CN103189619A Gas turbine combustor with mounting for helmholtz resonators |
| 07/03/2013 | CN103185355A Premixing pre-evaporation low-pollution combustion chamber with multi-point axial double-stage air auxiliary atomizing nozzle main combustion stage |
| 07/03/2013 | CN103185354A Methods and systems for cooling a transition nozzle |
| 07/03/2013 | CN103185353A Combustor assembly for use in a turbine engine and methods of assembling same |
| 07/03/2013 | CN103185348A Fuel distribution manifold |
| 07/03/2013 | CN103184899A Turbine engine and method for flowing air in a turbine engine |
| 07/02/2013 | US8475160 Low emissions combustion apparatus and method |
| 06/27/2013 | WO2013096591A2 Can annular combustion arrangement with flow tripping device |
| 06/27/2013 | WO2013094380A1 Gas turbine engine provided with scroll |
| 06/27/2013 | WO2013094379A1 Control method and control device for lean-fuel suction gas turbine |
| 06/27/2013 | WO2013021354A3 Ceramic tile for combustion chambers lining, in particular of gas turbines, and manufacturing method thereof |
| 06/27/2013 | US20130160457 System and method for improved combustor temperature uniformity |
| 06/27/2013 | US20130160453 Combustor and gas turbine |
| 06/27/2013 | US20130160423 Can annular combustion arrangement with flow tripping device |
| 06/26/2013 | EP2607787A1 System and method for improved combustor temperature uniformity |
| 06/26/2013 | EP2607669A1 System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor |
| 06/26/2013 | EP2606282A1 Burner for a gas turbine |
| 06/26/2013 | EP2606281A1 Gas-turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzle |
| 06/26/2013 | EP2606280A1 Burner for a gas turbine |
| 06/26/2013 | CN103175223A Gas circuit axial grading type dual-fuel nozzle |
| 06/26/2013 | CN103175222A Air combustion-supporting dual-fuel nozzle used for chemical regenerative cycle |
| 06/26/2013 | CN103175221A Gas-assisted dual-fuel nozzle used for chemical regenerative cycle |
| 06/26/2013 | CN103175220A Dual-fuel nozzle used for chemical regenerative cycle |
| 06/26/2013 | CN103175219A Venturi tube device used for head portion of chemical regenerative cycle combustor |
| 06/26/2013 | CN103175218A System and method for improved combustor temperature uniformity |
| 06/26/2013 | CN101713546B Low-pollution combustor for various fuels |
| 06/25/2013 | US8468832 Combustor, method of supplying fuel to same, and method of modifying same |
| 06/25/2013 | CA2558897C Redundant fuel manifold sealing arrangement |
| 06/20/2013 | WO2013089250A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089173A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013087310A1 Fuel nozzle for two fuels |
| 06/20/2013 | WO2012063127A8 Ultra low emissions gas turbine combustor |
| 06/20/2013 | WO2012007488A3 A burner for a gas combustor and a method of operating the burner thereof |
| 06/20/2013 | US20130152603 Combustion chamber for an aircraft engine, and method for attaching an injection system in a combustion chamber of an aircraft engine |
| 06/20/2013 | US20130152594 Gas turbine and fuel injector for the same |
| 06/20/2013 | US20130152593 Gas turbine and fuel injector for the same |
| 06/20/2013 | US20130152591 System of integrating baffles for enhanced cooling of cmc liners |
| 06/20/2013 | US20130152590 Fuel manifold with jumper tubes |
| 06/19/2013 | EP2604927A2 System for aerodynamically enhanced premixer for reduced emissions |
| 06/19/2013 | EP2604926A1 System of integrating baffles for enhanced cooling of CMC liners |
| 06/19/2013 | EP2604919A1 Fuel injector for two combustible materials |
| 06/19/2013 | EP2383515B1 Combustion system for dampening such a combustion system |
| 06/19/2013 | CN203010676U Unit nozzle for mass-flow medium-and-low heat value fuel |
| 06/19/2013 | CN103162312A System for aerodynamically enhanced premixer for reduced emissions |
| 06/19/2013 | CN103162311A System of integrating baffles for enhanced cooling of cmc liners |
| 06/19/2013 | CN101625131B Lobe nozzles for fuel and air injection |
| 06/19/2013 | CN101476725B Integrated fuel nozzle IFC |
| 06/16/2013 | CA2798269A1 System of integrating baffles for enhanced cooling of cmc liners |
| 06/13/2013 | WO2013085411A1 Multi-zone combustor |
| 06/13/2013 | WO2013084763A1 Lean fuel sucking gas turbine |
| 06/13/2013 | WO2013083348A2 Combustion chamber for a gas turbine and gas turbine as well as a method |
| 06/13/2013 | US20130145767 Two-stage combustor for gas turbine engine |
| 06/13/2013 | US20130145766 Two-stage combustor for gas turbine engine |
| 06/13/2013 | US20130145765 System for aerodynamically enhanced premixer for reduced emissions |
| 06/13/2013 | US20130145741 Two-stage combustor for gas turbine engine |
| 06/13/2013 | CA2798309A1 System for aerodynamically enhanced premixer for reduced emissions |
| 06/12/2013 | EP2602550A1 Combustion chamber for a gas turbine and gas turbine |
| 06/12/2013 | EP2602549A1 Combustion chamber for a gas turbine, gas turbine and method |
| 06/12/2013 | EP2602548A1 Leaf spring damper for a turbine engine fuel delivery system |
| 06/12/2013 | EP2602439A1 Coolable hot gas component for a gas turbine |
| 06/12/2013 | EP2601447A2 Gas turbine combustion chamber |
| 06/12/2013 | CN202993265U Lean partial pre-mixing and pre-evaporation combustion chamber |
| 06/12/2013 | CN103154616A Combustion device with pulsed fuel split |
| 06/12/2013 | CN103148514A Two-stage radial lean combustion pre-mixing type low-emission gas nozzle |
| 06/12/2013 | CN102287854B Afterburning-type supercritical-pressure gas-liquid fuel-generator combustion-chamber redundancy-cooling device |
| 06/11/2013 | US8459041 Leaf seal for transition duct in turbine system |
| 06/11/2013 | CA2575277C Segmented effusion cooled gas turbine engine combustor |
| 06/11/2013 | CA2568818C Methods and apparatuses for assembling a gas turbine engine |
| 06/11/2013 | CA2566789C Methods and apparatus for injecting fluids into a turbine engine |
| 06/11/2013 | CA2534213C Inboard radial dump venturi for combustion chamber of a gas turbine |
| 06/11/2013 | CA2528808C Method and apparatus for decreasing combustor acoustics |
| 06/11/2013 | CA2512417C Method for repair and replacement of combustor liner panel |
| 06/11/2013 | CA2502813C Improved fuel injector head |
| 06/07/2013 | CA2776539A1 Two-stage combustor for gas turbine engine |
| 06/07/2013 | CA2776528A1 Two-stage combustor for gas turbine engine |