| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 07/05/2007 | US20070151255 Combustion turbine engine and methods of assembly |
| 07/05/2007 | US20070151251 Counterflow injection mechanism having coaxial fuel-air passages |
| 07/05/2007 | US20070151250 Gas turbine combustor having counterflow injection mechanism |
| 07/05/2007 | US20070151249 Heat shield |
| 07/05/2007 | US20070151248 Gas turbine engine premix injectors |
| 07/04/2007 | EP1803999A1 Device to attach an augmentor arm to a post-combustion chamber wall and equipment including such a device |
| 07/04/2007 | EP1802915A2 Gas turbine burner |
| 07/04/2007 | EP1488086A4 Dry low combustion system with means for eliminating combustion noise |
| 07/04/2007 | EP1334307A4 Method of thermal nox reduction in catalytic combustion systems |
| 07/03/2007 | US7238247 Method of making a multi-perforated part out of ceramic matrix composite material |
| 07/03/2007 | US7237389 Attachment system for ceramic combustor liner |
| 07/03/2007 | US7237388 Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle |
| 07/03/2007 | US7237387 Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine |
| 07/03/2007 | US7237385 Method of using a combustion chamber for a gas turbine |
| 07/03/2007 | US7237384 Counter swirl shear mixer |
| 06/29/2007 | CA2568371A1 Valve assembly for modulating fuel flow to a gas turbine engine |
| 06/28/2007 | WO2007040909A3 Fuel nozzle having swirler-integrated radial fuel jet |
| 06/28/2007 | US20070144180 Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engine |
| 06/28/2007 | US20070144178 Dual wall combustor liner |
| 06/28/2007 | US20070144177 Combustor turbine interface |
| 06/28/2007 | DE102006060669A1 Catalytic evaporation of liquid fuels involves air quantity fed to evaporation being no more than 25 per cent of that needed for full oxidation of supplied fuel quantity; heat transfer from catalyzer to fuel takes place mainly by radiation |
| 06/28/2007 | DE102005060704A1 Gasturbinenbrennkammer A gas turbine combustor |
| 06/27/2007 | EP1801504A2 Lean-burn premix burner with an atomising lip |
| 06/27/2007 | EP1801503A2 Combustor nozzle |
| 06/27/2007 | EP1801502A2 Dual wall combustor liner |
| 06/27/2007 | EP1801500A2 Device and method to attenuate thermo-acoustic resonance in combustion chambers |
| 06/27/2007 | EP1800062A1 Burner for combustion of a low-calorific fuel gas and method for operating a burner |
| 06/27/2007 | EP1800061A1 Burner for fluid fuels and method for the operation of such a burner |
| 06/27/2007 | EP1800060A1 Method for operation of a burner in particular a burner for a gas turbine and device for carrying out said method |
| 06/27/2007 | EP1799970A1 Gas turbine casing for enclosing a gas turbine component |
| 06/27/2007 | CN1987205A Combustor nozzle |
| 06/27/2007 | CN1987204A Hot gas machine burner |
| 06/26/2007 | US7234306 Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members |
| 06/26/2007 | US7234305 Gas turbine control apparatus and gas turbine system using the same |
| 06/26/2007 | CA2499908C Gas turbine combustor cooling stucture |
| 06/21/2007 | WO2007069309A1 Gas turbine |
| 06/21/2007 | US20070141519 Method and device for the combustion of fuel |
| 06/21/2007 | US20070137220 Combustion Chamber for a Gas Turbine |
| 06/21/2007 | US20070137212 Combustor nozzle |
| 06/21/2007 | US20070137208 Combustor swirler and method of manufacturing same |
| 06/21/2007 | US20070137207 Pilot fuel injector for mixer assembly of a high pressure gas turbine engine |
| 06/20/2007 | EP1798475A2 Fuel spraying apparatus of gas turbine engine |
| 06/20/2007 | EP1798474A2 Local cooling hole pattern |
| 06/20/2007 | EP1798473A2 Axial flow positive displacement gas generator with combustion extending into an expansion section |
| 06/20/2007 | EP1798472A2 Gas turbine combustion chamber |
| 06/20/2007 | CN1982784A Swirler assembly |
| 06/20/2007 | CA2569299A1 Combustor nozzle |
| 06/19/2007 | US7232308 Method and device for affecting thermoacoustic oscillations in combustion systems |
| 06/14/2007 | WO2007067085A1 Method and apparatus for combustion of a fuel |
| 06/14/2007 | US20070130958 Combustor flow sleeve attachment system |
| 06/14/2007 | US20070130956 Rich catalytic clean burn for liquid fuel with fuel stabilization unit |
| 06/14/2007 | US20070130955 Independent pilot fuel control in secondary fuel nozzle |
| 06/14/2007 | US20070130954 Swirler Assembly |
| 06/14/2007 | US20070130953 Local cooling hole pattern |
| 06/14/2007 | US20070130951 Combustor |
| 06/14/2007 | DE102005059502A1 Heißkammer Hot chamber |
| 06/13/2007 | EP1795809A2 Gas turbine combustor |
| 06/13/2007 | EP1795808A2 Drilled and integrated secondary fuel nozzle and manufacturing method |
| 06/13/2007 | EP1795807A2 Swirler assembly |
| 06/13/2007 | EP1795806A2 Warm chamber |
| 06/13/2007 | EP1795805A2 Rich catalytic clean burn for liquid fuel with fuel stabilization unit |
| 06/13/2007 | EP1795802A2 Independent pilot fuel control in secondary fuel nozzle |
| 06/13/2007 | EP1794503A1 Heat shield-less combustor and cooling of combustor liner |
| 06/13/2007 | EP1458563B1 Foam wall combustor construction |
| 06/13/2007 | CN1981159A Combustion chamber for a gas turbine |
| 06/08/2007 | CA2570633A1 Methods and apparatus for assembling turbine engines |
| 06/08/2007 | CA2570631A1 Methods and apparatus for assembling turbine engines |
| 06/08/2007 | CA2558165A1 Rich catalytic clean burn for liquid fuel with fuel stabilization unit |
| 06/07/2007 | US20070128564 Burner |
| 06/07/2007 | US20070128093 Catalyzer |
| 06/07/2007 | US20070128002 Sealing arrangement |
| 06/07/2007 | US20070125093 Gas turbine combustor |
| 06/07/2007 | US20070125091 System for vaporization of liquid fuels for combustion and method of use |
| 06/07/2007 | US20070125089 Method of suppressing combustion instabilities using a resonator adopting counter-bored holes |
| 06/07/2007 | US20070125088 Method and apparatus for actuating fuel trim valves in a gas turbine |
| 06/07/2007 | US20070125085 Device for injecting a mixture of air and fuel, and a combustion chamber and turbomachine provided with such a device |
| 06/06/2007 | EP1793170A2 Opposed flow combustor |
| 06/06/2007 | EP1793169A2 Turbine engine fuel nozzles and methods of assembling the same |
| 06/06/2007 | EP1793168A1 Device for the injection of mixture of fuel and air, turbomachine and combustor with such a device |
| 06/06/2007 | EP1793097A1 Apparatus for assembling a gas turbine engine |
| 06/06/2007 | EP1793096A1 Apparatus for assembling a gas turbine engine |
| 06/06/2007 | EP1793095A1 Apparatus for assembling a gas turbine engine |
| 06/06/2007 | EP1792124A1 Combustor exit duct cooling |
| 06/06/2007 | EP1792123A1 Combustion chamber, in particular for a gas turbine, with at least two resonator devices |
| 06/06/2007 | CN1975259A Low emission combustor and method of operation |
| 06/06/2007 | CN1975144A Augmentor pilot nozzle |
| 06/06/2007 | CN1320314C Gas turbine |
| 06/06/2007 | CN1320313C Gas turbine |
| 06/06/2007 | CN1320312C Cylinder combustion chamber irrelevant on dynamic |
| 06/05/2007 | US7226672 Turbine components with thermal barrier coatings |
| 06/05/2007 | US7225996 Fuel supply method and fuel supply system for fuel injection device |
| 06/05/2007 | US7225623 Trapped vortex cavity afterburner |
| 06/05/2007 | CA2494251C Flow guiding body for a gas turbine combustion chamber |
| 05/31/2007 | WO2007060216A1 A combustion apparatus |
| 05/31/2007 | US20070119183 Gas turbine engine combustor |
| 05/31/2007 | US20070119182 Methods and apparatuses for assembling a gas turbine engine |
| 05/31/2007 | US20070119181 Methods and apparatuses for assembling a gas turbine engine |
| 05/31/2007 | US20070119180 Methods and apparatuses for assembling a gas turbine engine |
| 05/31/2007 | US20070119179 Opposed flow combustor |
| 05/31/2007 | US20070119177 Turbine engine fuel nozzles and methods of assembling the same |