| 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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| 06/25/2008 | EP1936149A1 Gas turbine burner |
| 06/25/2008 | EP1936123A2 Oil scavenge system for a gas turbine engine |
| 06/25/2008 | EP1934528A1 Process and device for monitoring the formation of deposits of solid particles, in particular in a fuel line and in the fuel valves of a gas turbine |
| 06/25/2008 | CN101205968A Gear with built-in overtorque protection |
| 06/25/2008 | CN101205835A Integrated boost cavity ring generator for turbofan and turboshaft engines |
| 06/25/2008 | CN101205834A Moisture removal apparatus and method |
| 06/25/2008 | CN101205833A Thermal barrier coating |
| 06/25/2008 | CN101204863A Thermal barrier coating system and method for coating a component |
| 06/24/2008 | US7390171 High efficiency rotor for the second phase of a gas turbine |
| 06/24/2008 | US7390170 Device for assembling annular flanges together, in particular in a turbomachine |
| 06/24/2008 | US7390163 Radial flow turbine |
| 06/24/2008 | US7389644 Power augmentation of combustion turbines by injection of cold air upstream of compressor |
| 06/22/2008 | CA2613767A1 Variable magnetic coupling of rotating machinery |
| 06/21/2008 | CA2613791A1 Power take-off system and gas turbine engine assembly including same |
| 06/21/2008 | CA2613643A1 Integrated boost cavity ring generator for turbofan and turboshaft engines |
| 06/21/2008 | CA2613606A1 Turbofan engine assembly and method of assembling same |
| 06/20/2008 | CA2613783A1 Turbine engine system with shafts for improved weight and vibration characteristic |
| 06/20/2008 | CA2613770A1 Bearing assembly and method of assembling the same |
| 06/20/2008 | CA2606854A1 Inertial particle separator for compressor shroud bleed |
| 06/19/2008 | WO2008073826A2 Monolithic acoustically-treated engine nacelle inlet panels |
| 06/19/2008 | WO2008072303A1 Friction welding, process for producing centrifugal gas turbine, and process for producing turbo charger |
| 06/19/2008 | WO2008071651A2 Turbine engine lubrication method and system |
| 06/19/2008 | US20080146401 Gear with integral overcouple protection |
| 06/19/2008 | US20080141680 System for ventilating a combustion chamber wall |
| 06/19/2008 | US20080141679 Turbomachine comprising a system for cooling the downstream face of an impeller of a centrifugal compressor |
| 06/19/2008 | US20080141678 System for cooling the impeller of a centrifugal compressor |
| 06/19/2008 | US20080141676 Turbine engine with modulated flow fan and method of operation |
| 06/19/2008 | US20080141651 Ceramic-encased hot surface igniter system for jet engines |
| 06/19/2008 | US20080141648 Fired Heater |
| 06/19/2008 | US20080141645 System and method for low emissions combustion |
| 06/19/2008 | US20080141643 Systems and processes for reducing NOx emissions |
| 06/19/2008 | DE102007060929A1 Verbesserte Systeme und Verfahren zum Verringern von NOx-Emissionen Improved systems and methods for reducing NOx emissions |
| 06/19/2008 | DE102007059980A1 Elektrische Energieerzeugung unter Verwendung einer Arbeitsturbine hinter einer Niederdruckturbine Electric power using a power turbine behind a low-pressure turbine |
| 06/19/2008 | DE102007059488A1 Entfeuchtungsgerät und -verfahren Dehumidifier and procedures |
| 06/19/2008 | DE102006058490A1 Fire detection sensor, for a gas turbine bearing chamber, is of a shape memory alloy |
| 06/19/2008 | DE102006037560B4 Verfahren und Vorrichtung zum vorausschauenden Bestimmen einer Temperaturverteilung in einer Wand einer Turbinenanlage Method and apparatus for determining a predictive temperature distribution in a wall of a turbine plant |
| 06/19/2008 | CA2671839A1 Turbine engine lubrication method and system |
| 06/19/2008 | CA2615038A1 Integrated overboost protection gear |
| 06/19/2008 | CA2615034A1 Electrical connector assembly with pollution protection device |
| 06/19/2008 | CA2615029A1 Deflector for bottom of combustion chamber, combustion chamber equipped with said deflector and turbojet engine containing them |
| 06/19/2008 | CA2613768A1 Method and system for using low btu fuel gas in a gas turbine |
| 06/19/2008 | CA2606121A1 Floatwall dilution hole cooling |
| 06/18/2008 | EP1933077A1 Method and system for lubricating a turbomachine |
| 06/18/2008 | EP1933041A2 Inlet plenum for gas turbine engine |
| 06/18/2008 | EP1933017A2 Variable coupling of turbofan engine spools via open differential or planetary gear set with torque coupling for power extraction and engine operability |
| 06/18/2008 | EP1932659A1 Noise suppression panel with fluid rejection capability and methods of making the same |
| 06/18/2008 | EP1733170B1 Liquid fuel injection with purge air |
| 06/18/2008 | CN101203667A System for defrosting the leading edge sheath of an air inlet hood for a turboengine |
| 06/18/2008 | CN101203424A Anti-icing and deicing system for aircraft engine pod with resistive mat |
| 06/18/2008 | CN101201017A High-speed high-pole count generators |
| 06/18/2008 | CN101201016A Fuel compression system with internal reheat for dew point suppression |
| 06/18/2008 | CN101201015A 旋转喷射器 Rotary injector |
| 06/17/2008 | US7387690 brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy for applying to a crack; brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy and applying to a crack |
| 06/17/2008 | US7387495 High efficiency rotor for the first phase of a gas turbine |
| 06/17/2008 | US7387490 High efficiency stator for the first phase of a gas turbine |
| 06/17/2008 | US7386983 Apparatus for driving an accessory gearbox in a gas turbine engine |
| 06/17/2008 | US7386982 Method and system for detecting ignition failure in a gas turbine engine |
| 06/17/2008 | CA2437758C Thermal barrier coatings with low thermal conductivity |
| 06/17/2008 | CA2416251C Cooling device for the common nozzle of a turbo-jet engine nacelle |
| 06/17/2008 | CA2359342C Electrochemical stripping of turbine blades |
| 06/17/2008 | CA2356766C Method and apparatus for supporting rotor assemblies during unbalances |
| 06/17/2008 | CA2352698C Method of adjusting component airflow |
| 06/15/2008 | CA2612813A1 Electric power generation using power turbine aft of lpt |
| 06/15/2008 | CA2612810A1 Airfoil leading edge end wall vortex reducing plasma |
| 06/15/2008 | CA2612533A1 Plasma induced virtual turbine airfoil trailing edge extension |
| 06/13/2008 | CA2612820A1 High-speed high-pole count generators |
| 06/12/2008 | WO2008069705A1 A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith |
| 06/12/2008 | US20080138196 Exhaust-gas-turbine casing |
| 06/12/2008 | US20080136189 Electromagnetic Variable Transmission |
| 06/12/2008 | US20080134688 Rotatable integrated segmented mid-turbine frames |
| 06/12/2008 | US20080134687 Double U design for mid-turbine frame struts |
| 06/12/2008 | US20080134685 Gas turbine guide vanes with tandem airfoils and fuel injection and method of use |
| 06/12/2008 | US20080134661 Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith |
| 06/12/2008 | US20080134660 Method and system for reducing co2 emissions in a combustion stream |
| 06/12/2008 | US20080134657 Oil Scavenge System for a Gas Turbine Engine |
| 06/12/2008 | DE102006057202A1 Lubricating oil supply system for gas turbines of aircraft engine, has valve device which opens connection line upstream to main oil pump by ventilation line of oil tank to oil line |
| 06/11/2008 | EP1930557A2 Turbine engine with integrated generator having shared lubrication system |
| 06/11/2008 | EP1930554A2 Generator for a turbomachine |
| 06/11/2008 | EP1930553A2 Centrifugal compressor |
| 06/11/2008 | EP1930549A2 Methods and systems for cooling integral turbine shroud assemblies |
| 06/11/2008 | EP1930455A1 Nickel-base superalloy with excellent unsusceptibility to oxidation |
| 06/11/2008 | EP1929208A1 Method for starting a gas turbine equipped with a gas burner, and axial swirler for said burner |
| 06/11/2008 | EP1929128A1 Turbine cleaning |
| 06/11/2008 | EP1928744A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 06/11/2008 | EP1928743A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 06/11/2008 | CN201071756Y Minitype gas turbine |
| 06/11/2008 | CN100394110C Gas turbine |
| 06/11/2008 | CN100393997C Combustion chamber |
| 06/10/2008 | US7384236 Exhaust-gas-turbine casing |
| 06/10/2008 | US7384075 Threaded joint for gas turbine components |
| 06/10/2008 | US7383686 Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines |
| 06/10/2008 | US7383685 Passive exhaust suppressor and method |
| 06/10/2008 | US7383679 Air intake structure for aircraft engine |
| 06/10/2008 | CA2442859C Tortuous path exhaust eductor system |
| 06/10/2008 | CA2361824C Tangentially directed acoustic jet controlling boundary layers |
| 06/07/2008 | CA2612040A1 Double sided starter/generator for aircrafts |
| 06/06/2008 | CA2612041A1 Electromagnetic variable transmission |
| 06/06/2008 | CA2612030A1 Variable coupling of turbofan engine spools via open differential or planetary gear set with torque coupling for power extraction and engine operability |
| 06/05/2008 | WO2008065656A2 Starting turbine engines |
| 06/05/2008 | US20080128475 Nickel-based braze alloy compositions and related processes and articles |