| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 09/11/2013 | EP2636952A2 A fuel nozzle and a combustor for a gas turbine |
| 09/11/2013 | EP2635846A1 Combustion chamber with a wall section and a brim element |
| 09/11/2013 | CN103292356A Beveling main combustion hole rotation aiding low-pollution backflow combustion chamber |
| 09/11/2013 | CN103292355A Gas turbine combustor and method for operating same |
| 09/11/2013 | CN103292354A Fuel nozzle assembly and combustor assembly for use in turbine engines |
| 09/11/2013 | CN103292353A System and method for reducing combustion dynamics in a combustor |
| 09/11/2013 | CN103292352A System and method for reducing combustion dynamics in a combustor |
| 09/11/2013 | CN103292351A Gas turbine combustor |
| 09/11/2013 | CN103292350A Flame holding boundary control |
| 09/11/2013 | CN103292349A Combustor and method for purging a combustor |
| 09/11/2013 | CN101629642B Turbine with fluidically-controlled valve and swirler with a bleed hole |
| 09/10/2013 | US8528337 Lobe nozzles for fuel and air injection |
| 09/06/2013 | WO2013130945A1 Laser clad fuel injector premix barrel |
| 09/06/2013 | WO2013130148A1 Full hoop casing for midframe of industrial gas turbine engine |
| 09/05/2013 | US20130227953 System and method for reducing combustion dynamics in a combustor |
| 09/05/2013 | US20130227928 Fuel nozzle assembly for use in turbine engines and method of assembling same |
| 09/04/2013 | EP2634490A1 Gas turbine combustor |
| 09/04/2013 | EP2634489A1 Fuel nozzle assembly for use in turbine engines and method of assembling same |
| 09/04/2013 | EP2634488A1 System and method for reducing combustion dynamics in a combustor |
| 09/04/2013 | EP2634487A2 System and method for reducing combustion dynamics in a combustor |
| 09/04/2013 | EP2634486A1 Gas turbine combustor and method for operating same |
| 09/04/2013 | EP2634395A1 Gas turbine and gas turbine plant provided with same |
| 09/04/2013 | EP2633238A2 Substrate with shaped cooling holes and methods of manufacture |
| 09/04/2013 | EP2500648B1 Gas turbine combustion chamber |
| 09/04/2013 | CN103277816A Lean oil pre-mixing pre-evaporation low-emission standing vortex combustion chamber |
| 09/04/2013 | CN103277815A Lean oil portion pre-mixing pre-evaporation homogenizing oil feeding device |
| 09/04/2013 | CN103277814A Low-emission trapped-vortex combustor with rich-burn/quick-quench/lean-burn combined with lean pre-mix pre-vaporization |
| 09/04/2013 | CN103277813A Low-pollution combustor for emission reduction through hydrogenation during aviation fuel combustion |
| 09/04/2013 | CN103277812A Rich-burn/quick-quench/lean-burn low-emission trapped-vortex combustor |
| 09/04/2013 | CN103277811A Single-cavity trapped vortex combustor |
| 09/04/2013 | CN101868602B Damping device and gas turbine combustor |
| 09/03/2013 | US8522559 Heat shield element, method and mold for the production thereof, hot-gas lining and combustion chamber |
| 09/03/2013 | US8522558 Multi-lobed cooling hole array |
| 09/03/2013 | US8522555 Multi-premixer fuel nozzle support system |
| 08/29/2013 | WO2013125972A1 A combustor nozzle and method of supplying fuel to a combustor |
| 08/29/2013 | WO2013095951A3 System and method for flame stabilization |
| 08/29/2013 | US20130219903 Gas Turbine Combustor and Method for Operating Same |
| 08/29/2013 | US20130219899 Annular premixed pilot in fuel nozzle |
| 08/29/2013 | US20130219897 Combustor and gas turbine |
| 08/29/2013 | DE112011103722T5 Brennkammer für Gasturbine für niederkalorischen Teibstoff Combustion chamber for gas turbine for low caloric Teibstoff |
| 08/28/2013 | EP2631544A1 Annular Premixed Pilot in Fuel Nozzle |
| 08/28/2013 | EP2631543A2 Combustor and method for purging a combustor |
| 08/28/2013 | EP2631540A2 Flame holding boundary control |
| 08/28/2013 | CN203162988U Two-stage radial lean burn pre-mix type low emission gas nozzle |
| 08/28/2013 | CN103270369A Gas-turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzle |
| 08/28/2013 | CN103266922A Turbine stator blade with interstage combustor |
| 08/28/2013 | CN102393028B Dry-type low-emission combustion chamber of natural gas fuel turbine |
| 08/27/2013 | US8516830 Turbomachine combustion chamber |
| 08/27/2013 | US8516821 Injection element |
| 08/22/2013 | WO2013120558A1 Inclined fuel injection of fuel into a swirler slot |
| 08/22/2013 | US20130213052 Combustion device with pulsed fuel split |
| 08/22/2013 | US20130213047 Combustion liner guide stop and method for assembling a combustor |
| 08/22/2013 | US20130213046 Late lean injection system |
| 08/22/2013 | DE10233805B4 Ringförmige Brennkammer für eine Gasturbine Annular combustor for a gas turbine |
| 08/21/2013 | EP2629018A2 Late lean injection system |
| 08/21/2013 | EP2629017A2 Combustor and method for supplying fuel to a combustor |
| 08/21/2013 | EP2629016A2 Variable angle multi-point injection |
| 08/21/2013 | EP2629015A2 Outer fuel nozzle inlet flow conditioner interface to end cap |
| 08/21/2013 | EP2629014A2 Combustion liner guide stop and method for assembling a combustor |
| 08/21/2013 | EP2629011A1 Fuel nozzle |
| 08/21/2013 | EP2629008A1 Inclined fuel injection of fuel into a swirler slot |
| 08/21/2013 | CN203147824U Annular wall of combustion chamber of turbo engine, combustion chamber of the turbo engine and the turbo engine |
| 08/21/2013 | CN203147823U Annular wall for combustion chamber of turbine set, combustion chamber of turbine set, and turbine set with the combustion chamber |
| 08/21/2013 | CN203147822U Connection structure of flame tube wall, and gas turbine combustion chamber applying the connection structure |
| 08/21/2013 | CN203147821U Fuel gas branched pipeline for gas turbine |
| 08/21/2013 | CN103256633A Low-pollution combustion chamber adopting fuel-grading and three-stage cyclone air inlet |
| 08/21/2013 | CN103256632A Air-cooled head of swirl atomiser |
| 08/21/2013 | CN103256631A Outer fuel nozzle inlet flow conditioner interface to end cap |
| 08/21/2013 | CN103256630A Late lean injection system |
| 08/21/2013 | CN103256629A Combustor and method for supplying fuel to a combustor |
| 08/21/2013 | CN103256628A Combustion liner guide stop and method for assembling a combustor |
| 08/21/2013 | CN102132100B Device for connecting flame-holder arm to afterburner casing |
| 08/21/2013 | CN101169074B Method for detecting onset of uncontrolled fuel in a gas turbine combustor |
| 08/20/2013 | US8511099 Combustor system |
| 08/20/2013 | US8511091 Swirler for a fuel injector |
| 08/20/2013 | US8511089 Relief slot for combustion liner |
| 08/20/2013 | US8511087 Fuel injector and swirler assembly with lobed mixer |
| 08/20/2013 | DE202007019553U1 Brennkammervorrichtung Combustion chamber device |
| 08/15/2013 | WO2013096591A3 Can annular combustion arrangement with flow tripping device |
| 08/15/2013 | US20130205794 Gas turbine engine component with impingement and lobed cooling hole |
| 08/15/2013 | US20130205793 Gas turbine engine component with impingement and diffusive cooling |
| 08/15/2013 | US20130205788 Unknown |
| 08/15/2013 | US20130205787 Tri-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205786 Cooling hole with thermo-mechanical fatigue resistance |
| 08/14/2013 | EP2626636A2 Fuel nozzle end cover, fuel nozzle, and process of fabricating a fuel nozzle end cover |
| 08/14/2013 | EP2626635A2 Combustor assembly with trapped vortex cavity |
| 08/14/2013 | EP2626634A2 Gas turbine premix burner |
| 08/14/2013 | EP2626633A2 Fuel Injection Assembly for use in Turbine Engines and Method of Assembling Same |
| 08/14/2013 | EP2626632A2 Fuel injection assembly for use in turbine engines and method of assembling same |
| 08/14/2013 | EP2626629A2 Detection system and method to detect flame holding event |
| 08/14/2013 | EP2626626A2 Improved liquid fuel swirler |
| 08/14/2013 | DE102012002664A1 Gasturbinenvormischbrenner Gasturbinenvormischbrenner |
| 08/14/2013 | CN103249931A End-fed liquid fuel gallery for a gas turbine fuel injector |
| 08/14/2013 | CN103244968A Combustor assembly with trapped vortex cavity |
| 08/14/2013 | CN103244967A Fuel injection assembly for use in turbine engines and method of assembling same |
| 08/14/2013 | CN103244966A Fuel injection assembly for use in turbine engines and method of assembling same |
| 08/13/2013 | US8505304 Fuel nozzle detachable burner tube with baffle plate assembly |
| 08/08/2013 | WO2013115858A1 Adaptor assembly for removable components |
| 08/08/2013 | WO2013115671A1 Liquid fuel nozzle for gas turbine and method for injecting fuel into a combustor of a gas turbine |
| 08/08/2013 | WO2013115667A1 Gas turbomachine combustor assembly including a liquid fuel start-up system |