| 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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| 04/12/2006 | CN1250864C Brush seal |
| 04/12/2006 | CN1250361C Method for making turbine vanes |
| 04/11/2006 | US7025802 Filter control method, and filter controlled by the method |
| 04/11/2006 | US7025579 Bearing system for high-speed rotating machinery |
| 04/11/2006 | US7025565 Gas turbine engine component having bypass circuit |
| 04/11/2006 | US7025562 Device for cooling turbine disks |
| 04/11/2006 | US7025559 Methods and systems for operating rotary machines |
| 04/11/2006 | US7024861 Fully premixed pilotless secondary fuel nozzle with improved tip cooling |
| 04/11/2006 | US7024860 Gas-turbine installation |
| 04/11/2006 | CA2402947C Gas turbine and operation method of gas turbine combined electric generating plant, gas turbine combined electric generating plant, and computer product |
| 04/11/2006 | CA2285449C Combined cycle power generation plant |
| 04/06/2006 | US20060073019 Axial-flow thermal turbomachine |
| 04/05/2006 | EP1643575A1 Fuel cell/constant pressure turbine/hybrid system |
| 04/05/2006 | EP1643114A2 Multiflow jet engine, system and method of operating the same |
| 04/05/2006 | EP1643113A2 Multiflow jet engine, system and method of operating the same |
| 04/05/2006 | EP1643099A1 Electric power supply equipment |
| 04/05/2006 | EP1643084A1 Turbine engine shroud segment, hanger and assembly |
| 04/05/2006 | EP1642014A2 Air turbine starter with angular contact thrust bearing |
| 04/05/2006 | EP1642008A1 Turbine shroud segment |
| 04/05/2006 | EP1322844B1 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 04/05/2006 | CN1755081A Spark detecting sensor of igniter in gas turbine engine |
| 04/05/2006 | CN1755080A Nose cone for a turbomachine |
| 04/04/2006 | US7022168 Device for removing carbon dioxide from exhaust gas |
| 04/04/2006 | US7021899 Lightened turbomachine blade and its manufacturing process |
| 04/04/2006 | US7021893 Fanned trailing edge teardrop array |
| 04/04/2006 | US7021892 Method for assembling gas turbine engine components |
| 04/04/2006 | US7021061 Heat shield arrangement for a hot-gas conducting component, in particular for structural pieces of gas turbines and method for production of said arrangement |
| 04/04/2006 | US7021058 Supercharging air compressor for an internal combustion engine, internal combustion engine and method for that purpose |
| 04/04/2006 | US7021042 Geartrain coupling for a turbofan engine |
| 04/04/2006 | CA2220213C Fuel injection device with a liquid-cooled injection nozzle for a combustion chamber of a gas turbine |
| 03/30/2006 | US20060064988 Turbine power plant having minimal-contact brush seal augmented labyrinth seal |
| 03/30/2006 | US20060064985 Power plant and operating method |
| 03/30/2006 | US20060064982 Valve for dynamic control of fuel flow rate in gas turbine power plant, power plant and components thereof employing such valve, and method of constructing such valve |
| 03/30/2006 | US20060064959 Device for indicating a residual power margin of aircraft turbine engines |
| 03/30/2006 | DE102004028125B3 Bearing for shaft of vehicle exhaust turbocharger has disk-shaped base, slide blocks being mounted in seatings near its center which swivel so that wedges of lubricant are formed between them and shaft |
| 03/30/2006 | CA2521983A1 Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor |
| 03/29/2006 | EP1640587A1 Cooling system for gas turbine, compressor stator vane and method for cooling a gas turbine |
| 03/29/2006 | EP1640586A1 Method of enhancing the power output of an already existing stationary gas turbine |
| 03/29/2006 | EP1640565A2 Swirl-enhanced aerodynamic fastener shield for turbomachine |
| 03/29/2006 | EP1640563A2 Heat transfer augmentation in a compact heat exchanger pedestral array |
| 03/29/2006 | EP1446556B1 Turbine unit |
| 03/29/2006 | EP1153157B1 Thermal barrier coating resistant to sintering |
| 03/28/2006 | US7018176 Cooled turbine airfoil |
| 03/28/2006 | US7018168 Method and apparatus for fabricating gas turbine engines |
| 03/28/2006 | US7017793 Repair process |
| 03/28/2006 | US7017706 Turbine noise absorber |
| 03/28/2006 | US7017350 Combustion chamber having a flexible connection between a chamber end wall and a chamber side wall |
| 03/28/2006 | US7017349 Gas turbine and bleeding method thereof |
| 03/28/2006 | US7017330 Water and sulfur removal from combustion turbine exhaust |
| 03/23/2006 | WO2006029888A1 Structure for separating the internal areas of a high pressure and a low pressure turbine |
| 03/23/2006 | WO2006014300A3 Acoustically stiffened gas-turbine fuel nozzle |
| 03/23/2006 | WO2005016748A3 Dual action inlet door and method for use thereof |
| 03/23/2006 | US20060063637 Coated journals |
| 03/23/2006 | US20060062674 Axial-flow thermal turbomachine |
| 03/23/2006 | US20060059919 System and method for improving thermal efficiency of dry low emissions combustor assemblies |
| 03/23/2006 | US20060059917 Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine |
| 03/23/2006 | US20060059915 Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber |
| 03/23/2006 | US20060059914 Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber |
| 03/23/2006 | US20060059913 Combustion chamber for a gas turbine with at least two resonator devices |
| 03/23/2006 | US20060059891 Quiet chevron/tab exhaust eductor system |
| 03/23/2006 | US20060059885 Two piece jet engine igniter assembly |
| 03/23/2006 | DE4424597B4 Verbrennungsvorrichtung Combustor |
| 03/23/2006 | DE102004037356A1 Wandstruktur zur Begrenzung eines Heißgaspfads Wall structure for defining a hot gas path |
| 03/23/2006 | CA2580476A1 Structure for separating the internal areas of a high pressure and a low pressure turbine |
| 03/23/2006 | CA2579929A1 A method and a washing system for washing turbines |
| 03/23/2006 | CA2519692A1 Lubricant distribution weir for lubricating moving machine elements |
| 03/22/2006 | EP1637713A2 Gas turbine electric power generation equipment |
| 03/22/2006 | EP1637711A2 High thrust gas turbine engine with modified core system |
| 03/22/2006 | EP1636476A2 Constant bypass flow controller for a variable displacement pump |
| 03/22/2006 | EP1635955A2 Water distribution and vaporization assembly |
| 03/22/2006 | CN1749620A Hingeless flapper valve for flow control |
| 03/22/2006 | CN1246638C Combustion chamber in particularly of gas turbine |
| 03/21/2006 | US7015698 Sensor for detection of spark in igniter in gas turbine engine |
| 03/21/2006 | US7014533 Method for smoothing the surface of a gas turbine blade |
| 03/21/2006 | US7014424 Turbine element |
| 03/21/2006 | US7014419 Passive improved air turbine starter lubrication system |
| 03/21/2006 | US7014145 Variable position intake for an aircraft mounted gas turbine engine |
| 03/21/2006 | US7014144 Dual action inlet door and method for use thereof |
| 03/21/2006 | US7013652 Gas turbo set |
| 03/21/2006 | US7013651 Compact quick attach starter-generator installation |
| 03/21/2006 | US7013649 Gas turbine engine combustor mixer |
| 03/21/2006 | US7013647 Outer casing covering gas turbine combustor |
| 03/21/2006 | US7013634 Sealing arrangement |
| 03/21/2006 | CA2393282C Turbine blade and method of repair |
| 03/17/2006 | CA2479985A1 Enhanced energy conversion system from a fluid heat stream |
| 03/16/2006 | WO2006027989A1 Gas turbine combustor |
| 03/16/2006 | US20060057059 System for reforming heavy oil, method therefor, and combined cycle power system |
| 03/16/2006 | US20060056977 Nose cone for a turbomachine |
| 03/16/2006 | US20060056963 Retaining of centring keys for rings under variable angle stator vanes in a gas turbine engine |
| 03/16/2006 | US20060053804 Gas turbine engine having improved core system |
| 03/16/2006 | US20060053803 Metering demand fuel system for gas turbine engines |
| 03/16/2006 | US20060053802 Ignition detecting method for gas turbine |
| 03/16/2006 | US20060053801 Cooling system for gas turbine engine having improved core system |
| 03/16/2006 | US20060053800 High thrust gas turbine engine with improved core system |
| 03/16/2006 | US20060053799 Recuperator and turbine support adapter for recuperated gas turbine engines |
| 03/16/2006 | US20060053796 Method and apparatus for adding a secondary fluid flow to a gas turbine engine control fuel line |
| 03/16/2006 | US20060053768 Aerodynamic fastener shield for turbomachine |
| 03/16/2006 | US20060053767 Method and device for reducing engine noise |
| 03/16/2006 | DE102004045049A1 Protection layer application, involves applying undercoating with heat insulating layer, and subjecting diffusion layer to abrasive treatment, so that outer structure layer of diffusion layer is removed by abrasive treatment |
| 03/15/2006 | EP1635066A2 Gas supply apparatus and associated method of operation for a gas turbine |