| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 08/15/2007 | EP1818612A1 Annular combustion chamber of a turbomachine |
| 08/15/2007 | EP1817528A1 Thermal shield element, method for the production thereof, hot gas lining, and combustion chamber |
| 08/15/2007 | EP1817147A1 Heat shield element, method and form for the production thereof, hot gas lining and combustion chamber |
| 08/15/2007 | CN101018983A Gas turbine combustor |
| 08/15/2007 | CN101017001A Annular combustion chamber of a turbomachine |
| 08/15/2007 | CN101017000A Turbine engine combustion chamber with tangential slots |
| 08/15/2007 | CN101016999A Transverse wall of a combustion chamber equipped with multi-perforation holes |
| 08/15/2007 | CN101016998A Turbine engine annular combustion chamber with alternating attachments |
| 08/15/2007 | CN101016997A Combustion chamber of a turbomachine |
| 08/14/2007 | CA2409529C Combustor containing fuel nozzle |
| 08/10/2007 | CA2577520A1 Annular combustion chamber of turbine engine |
| 08/10/2007 | CA2577514A1 Annular combustion chamber of turbine engine |
| 08/09/2007 | WO2007087907A1 Method for the operation of a firing plant |
| 08/09/2007 | US20070184287 Environmental barrier coating for silicon-containing substrates and process therefor |
| 08/09/2007 | US20070180834 Transverse wall of a combustion chamber provided with multi-perforation holes |
| 08/09/2007 | US20070180829 Methods and apparatus for fabricating gas turbine engine combustors |
| 08/09/2007 | US20070180828 Combustor liners |
| 08/09/2007 | US20070180827 Gas turbine engine transitions comprising closed cooled transition cooling channels |
| 08/09/2007 | DE10394149T5 Kraftstoffeinspritz-Steuersystem für ein Turbinentriebwerk A fuel injection control system for a turbine engine |
| 08/09/2007 | CA2636412A1 Method for operating a firing plant |
| 08/09/2007 | CA2577595A1 Transverse separator for combustion chamber with multiperforation holes |
| 08/08/2007 | EP1816401A2 Turbomachine |
| 08/08/2007 | EP1816400A2 Gas turbine combustion chamber with fuel injection over the whole combustion chamber ring |
| 08/08/2007 | EP1816399A1 Method of manufacturing a combustion chamber |
| 08/08/2007 | CN101012937A Manufacture of a combustion chamber |
| 08/08/2007 | CA2577527A1 Turbine engine combustion chamber with tangential slots |
| 08/08/2007 | CA2577523A1 Turbine engine annular combustion chamber with alternating attachments |
| 08/08/2007 | CA2577507A1 Turbine engine combustion chamber |
| 08/07/2007 | US7251942 Integrated gearless and nonlubricated auxiliary power unit |
| 08/07/2007 | US7251941 Ablative afterburner |
| 08/07/2007 | US7251940 Air assist fuel injector for a combustor |
| 08/02/2007 | US20070175219 Pilot combustor for stabilizing combustion in gas turbine engines |
| 08/02/2007 | DE102007001835A1 Vergasungsbrenner-Ummantelungen Combustor sheaths |
| 08/01/2007 | EP1813869A2 Wall elements for gas turbine engine combustors |
| 08/01/2007 | EP1813868A2 Wall elements for gas turbine engine combustors |
| 08/01/2007 | EP1813867A2 Wall elements for gas turbine engine combustors |
| 08/01/2007 | EP1813781A1 Part of a turbine, turbine and operation method thereof |
| 08/01/2007 | EP1812756A1 Burner starting method |
| 08/01/2007 | EP1812755A1 Attachment system for ceramic combustor liner |
| 08/01/2007 | CN101008497A Independent pilot fuel control in secondary fuel nozzle |
| 08/01/2007 | CN101008327A Film cooling method and method of manufacturing a hole |
| 08/01/2007 | CA2576704A1 Manufacture of a combustion chamber |
| 07/31/2007 | US7249721 Device and method for injecting a liquid fuel into an air flow for a combustion chamber |
| 07/31/2007 | US7249462 Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine |
| 07/31/2007 | US7249461 Turbine fuel ring assembly |
| 07/31/2007 | CA2575929A1 Multipurpose gas generator ramjet/scramjet cold start system |
| 07/26/2007 | US20070169484 Segmented effusion cooled gas turbine engine combustor |
| 07/26/2007 | US20070169483 Combustion system with low polluting emissions |
| 07/25/2007 | EP1811231A2 Segmented effusion cooled gas turbine engine combustor |
| 07/25/2007 | EP1811229A2 Fuel injector nozzles for gas turbine engines |
| 07/25/2007 | CN1328546C Thermal lump and its application in combustion chamber |
| 07/25/2007 | CN1328493C Orbiting combustion nozzle engine |
| 07/25/2007 | CN1328492C Gas turbine with air compressor |
| 07/25/2007 | CN1328489C Wing structure of air swirling device for internal combustion engine |
| 07/24/2007 | US7246993 Coolable segment for a turbomachine and combustion turbine |
| 07/24/2007 | US7246494 Methods and apparatus for fabricating gas turbine engine combustors |
| 07/24/2007 | US7246493 Gas turbine |
| 07/24/2007 | CA2575277A1 Segmented effusion cooled gas turbine engine combustor |
| 07/24/2007 | CA2379312C Airblast fuel atomization system |
| 07/24/2007 | CA2372070C Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure |
| 07/24/2007 | CA2333932C Impingement and film cooling for gas turbine combustor walls |
| 07/19/2007 | US20070163267 Combustor for a gas turbine and associated operating method |
| 07/19/2007 | US20070163266 Fuel manifold inlet tube |
| 07/19/2007 | US20070163265 Fuel manifold inlet tube |
| 07/19/2007 | DE112005002065T5 Gasturbinen-Brennkammer A gas turbine combustor |
| 07/18/2007 | EP1808644A2 Externally fueled trapped vortex cavity augmentor |
| 07/18/2007 | EP1807652A1 Flexible heat shields and method |
| 07/18/2007 | EP1723369B1 Premix burner and method for combusting a low-calorific gas |
| 07/18/2007 | CN101000145A Combustion chamber of miniature gas turbine with double premixed channel using natural gas |
| 07/18/2007 | CN101000136A Cooling of a multimode injection device for a combustion chamber, particularly for a gas turbine |
| 07/18/2007 | CN101000135A Multimode injection system for a combustion chamber, particularly of a gas turbine |
| 07/17/2007 | US7246002 Method for controlling fuel splits to gas turbine combustor |
| 07/17/2007 | US7243496 Electric flame control using corona discharge enhancement |
| 07/17/2007 | US7243426 Method for the manufacture of a combustion chamber of a gas-turbine engine |
| 07/17/2007 | CA2172862C Dome assembly for a multiple annular combustor |
| 07/12/2007 | WO2007078267A1 Rich catalytic injection |
| 07/12/2007 | US20070157624 Pilot fuel flow tuning for gas turbine combustors |
| 07/12/2007 | US20070157620 Method for controlling fuel splits to gas turbine combustor |
| 07/12/2007 | US20070157618 Methods and apparatus for assembling gas turbine engines |
| 07/12/2007 | DE102007002231A1 Verfahren und Einrichtung zum Zusammenbau von Gasturbinentriebwerken Method and apparatus for assembling gas turbine engines |
| 07/12/2007 | DE102005062079A1 Magervormischbrenner mit einer Zerstäuberlippe Lean premix burner with an atomizer |
| 07/12/2007 | DE102005061486A1 Brennkammer mit Brenner und zugehöriges Betriebsverfahren Combustion chamber with burner and operating method thereof |
| 07/12/2007 | CA2567533A1 Externally fueled trapped vortex cavity augmentor |
| 07/11/2007 | EP1806536A1 Cooling of a multimode injection device for a combustion chamber, particularly for a gas turbine |
| 07/11/2007 | EP1806535A1 Multimode injection system for a combustion chamber, particularly of a gas turbine |
| 07/11/2007 | EP1806534A2 Combustion turbine engine and methods of assembly |
| 07/11/2007 | EP1805459A1 Method of optimum controlled outlet, impingement cooling and sealing of a heat shield and a heat shield element |
| 07/11/2007 | EP1504222B1 Premix burner |
| 07/11/2007 | CN1995826A Combustion turbine engine and methods of assembly |
| 07/11/2007 | CN1325840C Combustion chamber intermediate part for a gas turbine |
| 07/11/2007 | CN1325769C Method for operating a burner of a gas turbine and a power plant |
| 07/10/2007 | US7241138 Burner with stepped fuel injection |
| 07/10/2007 | CA2393863C Pilot burner, premixing combustor, and gas turbine |
| 07/09/2007 | CA2572857A1 Cooling of a multimode injection apparatus for combustion chambers, namely a turbojet engine |
| 07/09/2007 | CA2572852A1 Multimode injection apparatus for combustion chambers, namely a turbojet engine |
| 07/05/2007 | WO2007074033A1 Combustion chamber with burner and associated operating method |
| 07/05/2007 | WO2007073593A1 Reduced thermal stress assembly and process of making same |
| 07/05/2007 | US20070151481 Thermal barrier coating material |
| 07/05/2007 | US20070151260 Crossfire tube assembly for gas turbines |
| 07/05/2007 | US20070151259 Combustor assembly |