| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 08/02/2007 | DE102007001835A1 Vergasungsbrenner-Ummantelungen Combustor sheaths |
| 08/02/2007 | DE102006002130A1 Twin-Scroll Abgasturbolader Twin-scroll turbocharger exhaust |
| 08/02/2007 | DE102004025142B4 Dichtungsanordnung Seal assembly |
| 08/02/2007 | CA2576683A1 Aircraft auxiliary gas turbine engine and method for operating |
| 08/01/2007 | EP1813792A1 Engine shaft linking system with retractable nut |
| 08/01/2007 | EP1813775A2 Film cooling method and method of manufacturing a hole in gas turbine engine part |
| 08/01/2007 | EP1813770A1 Fastening system for an engine shaft with a clamping nut |
| 08/01/2007 | EP1813769A1 Assembly with reduced radial dimensions between a turbine shaft and a compressor shaft journal in a turbomachine |
| 08/01/2007 | EP1813529A1 Air intake of a turbofan engine |
| 08/01/2007 | EP1812769A1 Aspherical dimples for heat transfer surfaces and method |
| 08/01/2007 | EP1812756A1 Burner starting method |
| 08/01/2007 | EP1812699A1 Gas turbine apparatus |
| 08/01/2007 | EP1446565B1 Turbine engine with air cooled turbine |
| 08/01/2007 | EP1152851B1 Die casting of high temperature material |
| 08/01/2007 | CN1329680C Rotary machine with seal |
| 08/01/2007 | CN1329648C Gas turbine plant |
| 08/01/2007 | CN1329647C Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 08/01/2007 | CN101008351A Method and apparatus for enabling engine turn down |
| 08/01/2007 | CN101008350A Gas turbine engine assembly and methods of assembling same |
| 07/31/2007 | US7249721 Device and method for injecting a liquid fuel into an air flow for a combustion chamber |
| 07/31/2007 | US7249463 Aerodynamic fastener shield for turbomachine |
| 07/31/2007 | US7249461 Turbine fuel ring assembly |
| 07/30/2007 | CA2576701A1 Engine shaft linkage system using retractable nut |
| 07/30/2007 | CA2576036A1 Welding shielding dam for automated welding of impellors and blisks |
| 07/27/2007 | CA2576700A1 Bypass engine air inlet |
| 07/27/2007 | CA2576698A1 Radially compact bearing assembly between a turbine shaft and a turbine engine compressor shaft |
| 07/26/2007 | WO2007083088A1 Method and apparatus for delivering liquid in droplet form |
| 07/26/2007 | WO2007083027A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | WO2007083026A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | WO2007082608A1 Fuel ratio control in a combustion apparatus with multiple fuel supply lines |
| 07/26/2007 | US20070172351 Repaired turbine nozzle |
| 07/26/2007 | US20070169990 Jet engine |
| 07/26/2007 | US20070169486 Multimode fuel injector for combustion chambers, in particular of a jet engine |
| 07/26/2007 | DE102004019970B4 Anordnung und Verfahren zum Einbringen eines Fluids in ein Arbeitsmedium einer Gasturbinenanlage mit einem Verdichter Apparatus and method for introducing a fluid into a working medium of a gas turbine engine having a compressor |
| 07/26/2007 | CA2635049A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | CA2631849A1 Dual flow turbine engine equipped with a precooler |
| 07/25/2007 | EP1811143A2 Acoustic liner with bypass cooling |
| 07/25/2007 | EP1811132A1 Turbomachine with integrated generator-starter |
| 07/25/2007 | EP1811129A2 Aerofoils for gas turbine engines |
| 07/25/2007 | EP1810529A2 Wirelless terminal location using apparatus and methods employing carrier diversity |
| 07/25/2007 | EP1809891A1 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
| 07/25/2007 | EP1688024B1 Control arrangement |
| 07/25/2007 | EP1061237B1 Seal ring for steam turbine |
| 07/25/2007 | CN1328493C Orbiting combustion nozzle engine |
| 07/25/2007 | CN1327997C Method for renewing cooling path in turbine wing surface |
| 07/25/2007 | CN101004147A Microcircuit cooling for a turbine blade tip |
| 07/25/2007 | CN101004141A Microcircuit cooling for a turbine blade tip |
| 07/25/2007 | CN101004140A Microcircuit cooling for a turbine blade tip |
| 07/24/2007 | US7247212 Orthogonal weaving for complex shape preforms |
| 07/24/2007 | US7246994 Spacing arrangement |
| 07/24/2007 | US7246993 Coolable segment for a turbomachine and combustion turbine |
| 07/24/2007 | US7246493 Gas turbine |
| 07/24/2007 | US7246482 Gas turbine engine bleed air power assist system and method |
| 07/24/2007 | US7246480 System for heating an air intake of turbine engine |
| 07/24/2007 | CA2575343A1 Turbomachine with integrated starter-generator |
| 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 | WO2006085943A3 Improved heat exchanger performance |
| 07/19/2007 | US20070163682 Ni-based superalloy having high oxidation resistance and gas turbine part |
| 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 | US20070163264 Method for operating a gas turbine group |
| 07/19/2007 | US20070163263 System and method for cooling a staged airblast fuel injector |
| 07/19/2007 | US20070163229 Gas turbine engine inlet with noise reduction features |
| 07/19/2007 | DE19807563B4 Kühlkonstruktion zum Kühlen der Plattform einer Turbinenschaufel Cooling structure for cooling the platform of a turbine blade |
| 07/19/2007 | DE112005002065T5 Gasturbinen-Brennkammer A gas turbine combustor |
| 07/18/2007 | EP1808588A1 Augmentation of power output and efficiency in gas turbine and combined cycle plants |
| 07/18/2007 | EP1807616A1 Acoustic absorber for aircraft engines |
| 07/18/2007 | CN1327124C Turbine engine with semi-fixed turbine |
| 07/18/2007 | CN1327109C Turbo-blade and gas turbine |
| 07/18/2007 | CN1327018C Cobalt-base alloy for coating element corroded by fluid |
| 07/17/2007 | US7246024 Sensor malfunction detection system for gas-turbine engine |
| 07/17/2007 | US7246002 Method for controlling fuel splits to gas turbine combustor |
| 07/17/2007 | CA2574145A1 Squeeze film damper using low pressure oil |
| 07/17/2007 | CA2232166C Brush seal having bristles tilted in the circumferential direction |
| 07/12/2007 | WO2007078267A1 Rich catalytic injection |
| 07/12/2007 | WO2005107382A3 Method and device for reducing engine noise |
| 07/12/2007 | US20070157616 Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine |
| 07/12/2007 | DE102007002231A1 Verfahren und Einrichtung zum Zusammenbau von Gasturbinentriebwerken Method and apparatus for assembling gas turbine engines |
| 07/11/2007 | EP1806492A2 Method and apparatus for reducing or eliminating oscillations in a gas turbine fuel control system |
| 07/11/2007 | EP1806491A2 Squeeze film damper bearing assembly |
| 07/11/2007 | EP1806478A2 Gas turbine engine and cooling system therefor |
| 07/11/2007 | EP1595058B1 Sealing arrangement, particularly for the blade segments of gas turbines |
| 07/11/2007 | EP1296796A4 Welding superalloy articles |
| 07/11/2007 | CN1325840C Combustion chamber intermediate part for a gas turbine |
| 07/11/2007 | CN1325770C Device and method for preheating combustibles in combined gas and turbine installations |
| 07/11/2007 | CN1325769C Method for operating a burner of a gas turbine and a power plant |
| 07/11/2007 | CN1325765C Gas turbine stator housing |
| 07/11/2007 | CN1325762C Heat-insulating coating material and gas turbine component and gas turbine |
| 07/11/2007 | CN1325760C Method for providing turbulence structure on internal surface of middle hole of workpiece and relative workpiece |
| 07/10/2007 | US7242195 Integral spark detector in fitting which supports igniter in gas turbine engine |
| 07/10/2007 | US7241112 Turbomachine blade, in particular a fan blade, and its method of manufacture |
| 07/10/2007 | US7241109 Seal system |
| 07/10/2007 | US7241108 Cantilevered stator stage |
| 07/10/2007 | US7240493 Method and device for reducing engine noise |
| 07/10/2007 | US7240478 Highly supercharged regenerative gas turbine |
| 07/05/2007 | WO2007073593A1 Reduced thermal stress assembly and process of making same |