| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 10/03/2007 | CN101046297A Combustor of gas turbine and combustion control method for gas turbine |
| 09/30/2007 | CA2582796A1 Improved combustor |
| 09/30/2007 | CA2582634A1 Configuration of dilution inlets in a turbine engine combustion chamber wall |
| 09/30/2007 | CA2582629A1 Apparatus to inject a mixture of air and fuel, combustion chamber and turbine engine equipped with such an apparatus |
| 09/30/2007 | CA2582624A1 Flame-retention arm of a post-combustion chamber |
| 09/27/2007 | WO2007106983A1 Calibration of optical patternator spray parameter measurements |
| 09/27/2007 | WO2007106982A1 Method of computing spray parameters from optical patternation |
| 09/27/2007 | US20070220891 Augmentor pilot nozzle |
| 09/27/2007 | CA2643374A1 Calibration of optical patternator spray parameter measurements |
| 09/27/2007 | CA2643373A1 Method of computing spray parameters from optical patternation |
| 09/26/2007 | EP1837597A2 Burner for combustion chamber and combustion method |
| 09/26/2007 | EP1837596A2 Calibration of optical patternator spray parameter measurements |
| 09/26/2007 | EP1836443A1 Rich catalytic injection |
| 09/26/2007 | EP1836442A1 Heat shield element |
| 09/26/2007 | EP1334309B1 Method for supplying fuel to a premix burner |
| 09/26/2007 | CN101044355A Burner for a gas turbine |
| 09/26/2007 | CN101042242A Secondary fuel nozzle with improved fuel pegs and fuel dispersion method |
| 09/26/2007 | CN101042071A Systems and methods of reducing NOx emissions in gas turbine systems and internal combustion engines |
| 09/25/2007 | US7272931 Method and apparatus to decrease combustor acoustics |
| 09/20/2007 | WO2007106087A1 Crack resistant combustor |
| 09/20/2007 | WO2007104615A1 Combustor and method of operating a combustor |
| 09/20/2007 | WO2007104599A1 Burner, in particular for a gas turbine combustor, and method of operating a burner |
| 09/20/2007 | WO2007104587A2 Method for mounting a mixing housing in a gas turbine, and adjusting device therefor |
| 09/20/2007 | WO2007001512A3 Attachment device for removable components in hot gas paths in a turbine engine |
| 09/19/2007 | EP1835231A1 Burner in particular for a gas turbine combustor, and method of operating a burner |
| 09/19/2007 | EP1835230A2 Supporting structure for spray bars |
| 09/19/2007 | EP1835229A1 Combustor and method of operating a combustor |
| 09/19/2007 | EP1835148A2 Component for fuel supply |
| 09/19/2007 | EP1834133A1 Improved gas turbines |
| 09/19/2007 | EP1754003B1 Premix burner with a staged liquid fuel supply system |
| 09/19/2007 | CN101040149A Burner for combustion of a low-calorific fuel gas and method for operating a burner |
| 09/19/2007 | CN101040148A Method for operation of a burner in particular a burner for a gas turbine and device for carrying out said method |
| 09/18/2007 | US7270890 Conductor can be operatively connected to a power source to form an electrical circuit, resistance across the conductor can be measured, as component contacts a second component, the component can begin to wear, once the wear progresses to the conductor, changes in the measured resistance can result |
| 09/18/2007 | US7270175 Extended impingement cooling device and method |
| 09/18/2007 | US7269958 Combustor exit duct |
| 09/18/2007 | US7269957 Combustion liner having improved cooling and sealing |
| 09/18/2007 | CA2567432C Gas turbine combustor |
| 09/13/2007 | WO2007102807A1 Angled flow annular combustor for turbine engine |
| 09/13/2007 | DE102006011248A1 Gas turbine combustion chamber wall has damping recesses for inner wall, with respective center axis arranged perpendicularly to inner wall, and cooling recesses, with respective center axis inclined at angle to inner wall |
| 09/13/2007 | DE102006011247A1 Gas turbine combustion chamber wall has damping recesses for inner wall, with respective center axis arranged perpendicularly to inner wall, and cooling recesses, with respective center axis inclined at angle to inner wall |
| 09/12/2007 | EP1832812A2 Gas turbine combustion chamber wall with absorption of combustion chamber vibrations |
| 09/12/2007 | EP1831520A1 Tip turbine engine and corresponding operating method |
| 09/12/2007 | CN101033858A Methods and apparatus for assembling turbine engines |
| 09/11/2007 | US7266945 Fuel injection apparatus |
| 09/07/2007 | WO2007099046A1 Gas turbine burner and method of operating a gas turbine burner |
| 09/06/2007 | DE102007008995A1 Brennkammer Combustion chamber |
| 09/06/2007 | DE102007008993A1 Brenner Burner |
| 09/05/2007 | EP1830129A2 Method and apparatus for assembling gas turbine engine |
| 09/05/2007 | EP1828684A1 Premix burner comprising a mixing section |
| 09/05/2007 | EP1828683A1 Combustor for turbine engine |
| 09/05/2007 | CN101029743A Arrangement for a combustion chamber of a turbine engine |
| 09/05/2007 | CN101029742A Combustor |
| 09/05/2007 | CN101029741A Combustor |
| 09/05/2007 | CN101029740A Combustor |
| 09/05/2007 | CN101029739A Method and apparatus for assembling gas turbine engine |
| 09/05/2007 | CN101029599A Methods and apparatus for assembling gas turbine engines |
| 09/04/2007 | US7263833 Fuel injector |
| 09/04/2007 | US7263772 Foam wall combustor construction |
| 08/30/2007 | WO2007096294A1 A swirler for use in a burner of a gas turbine engine |
| 08/30/2007 | US20070199328 System for identification of hot and cold chambers in a gas turbine combustor |
| 08/30/2007 | US20070199327 Combustor |
| 08/30/2007 | US20070199326 Combustor |
| 08/30/2007 | US20070199325 Combustor |
| 08/30/2007 | US20070199324 Combustor |
| 08/30/2007 | DE102007009285A1 Main-combustion chamber for gas turbine, has ribs with plate unit installed on central axis of casing such that unit stays in close contact with casing and is installed at distance in circumferential direction of outer cylinder |
| 08/30/2007 | DE102007009282A1 Combustion chamber e.g. gas turbine-combustion chamber, has notches formed at tips on side of base surfaces of main nozzles by providing slot having different level to position corresponding to intermediate position between nozzles |
| 08/30/2007 | DE102006004785A1 Strömungsmaschine Flow machine |
| 08/29/2007 | EP1826492A1 Arrangement for a combustion chamber of a turbine engine |
| 08/29/2007 | EP1826491A1 Annular combustion chamber with removable combustor dome |
| 08/29/2007 | EP1826490A2 Method and apparatus for gas turbine engines |
| 08/29/2007 | CN101025272A Multi-stage efficient enzironment-protection turbine gas-fuel staged burning method and system |
| 08/29/2007 | CN101025115A Aircraft auxiliary gas turbine engine and method for operating |
| 08/29/2007 | CN100334327C 涡轮机 Turbines |
| 08/28/2007 | US7260937 Method and apparatus for actuating fuel trim valves in a gas turbine |
| 08/28/2007 | US7260935 Method and apparatus for reducing gas turbine engine emissions |
| 08/27/2007 | CA2578711A1 Layout of a turbojet engine combustion chamber |
| 08/27/2007 | CA2578701A1 Annular combustion chamber with removable bottom section |
| 08/23/2007 | WO2007093248A1 Gas turbine burner and method of mixing fuel and air in a swirling area of a gas turbine burner |
| 08/23/2007 | US20070193273 Method and apparatus for gas turbine engines |
| 08/23/2007 | DE102007002422A1 System und Verfahren zur Kühlung einer gestuften Luftstrom- Kraftstoffeinspritzvorrichtung System and method for cooling an airflow stepped fuel injector |
| 08/23/2007 | DE102006004840A1 Gasturbinenbrennkammer mit Kraftstoffeinspritzung über den gesamten Brennkammerring Gas turbine combustion chamber with fuel injection throughout the entire combustion chamber ring |
| 08/23/2007 | CA2578565A1 Method and apparatus for gas turbine engines |
| 08/22/2007 | EP1821037A2 Low emission combustor assembly for gas turbine engines |
| 08/22/2007 | EP1821035A1 Gas turbine burner and method of mixing fuel and air in a swirling area of a gas turbine burner |
| 08/22/2007 | EP1819964A2 Low emissions combustion apparatus and method |
| 08/22/2007 | EP1819905A1 Coating system, use and method of manufacturing such a coating system |
| 08/22/2007 | EP1651841B1 Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 08/22/2007 | EP1358401A4 Bulkhead for dual fuel industrial and aeroengine gas turbines |
| 08/22/2007 | CN1333201C Device for increasing heat power of gas burner |
| 08/22/2007 | CN1333161C Gas turbine combustor |
| 08/22/2007 | CN101023302A Gas turbine combustor |
| 08/21/2007 | CA2421802C Hollow structure with flange |
| 08/16/2007 | US20070186559 Annular combustion chamber of a turbomachine |
| 08/16/2007 | US20070186558 Annular combustion chamber of a turbomachine |
| 08/16/2007 | DE102006007711A1 Combustion chamber, especially for rockets, has at least one resonator which by overtone is matched to eigenmode, wherein matching is achieved by adjustment of geometric dimensions of resonance chamber of resonator |
| 08/15/2007 | EP1818617A1 Transverse wall of a combustion chamber equipped with multi-perforation holes |
| 08/15/2007 | EP1818616A1 Turbomachine combustion chamber with tangential slots |
| 08/15/2007 | EP1818615A1 Annular combustion chamber of a turbomachine |
| 08/15/2007 | EP1818614A1 Annular combustion chamber of a turbomachine with alternating mountings |
| 08/15/2007 | EP1818613A1 Combustion chamber of a turbomachine |