F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants

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)
08/2013
08/14/2013	CN103249930A Monitoring of a filter of the fuel-supply system of an aircraft engine
08/14/2013	CN103244278A Gas turbine engine fuel return valve and system
08/14/2013	CN103244277A Fuel heating system for power plant
08/14/2013	CN103244276A Squirrel-cage SMA (shape memory alloy) driving variable rigidity rotor supporting device
08/14/2013	CN103244275A System and method for gas turbine nox emission improvement
08/14/2013	CN103244274A System and method for gas turbine inlet air heating
08/14/2013	CN103244273A Method and apparatus to control part-load performance of a turbine
08/14/2013	CN103244271A Compact microscale thermal energy power system
08/14/2013	CN101737169B Fuel control system for gas turbine and feed forward control method
08/14/2013	CN101493048B Starting-up control method for aviation fan engine in escape status
08/14/2013	CN101487421B Oil seal control device for aviation turbofan engine in deplaning state
08/13/2013	US8510013 Gas turbine shutdown
08/13/2013	US8505311 Turbomachine with separate fuel injection systems, using identical sealing joints
08/13/2013	US8505310 Gas turbine ejector and method of operation
08/13/2013	US8505303 Impurity detection in combustor systems
08/13/2013	US8505302 Multiple tube premixing device
08/13/2013	US8505275 Fuel injection systems in a turbomachine combustion chamber
08/13/2013	US8505274 Gas turbine
08/13/2013	DE202013005040U1 Das Schutzstab-Gitter bietet einen Schutz, für Flugzeuge mit Strahltriebwerk und einem zusätzlichen Sicherheit für den Flugverkehr The protection bar grille provides protection for aircraft jet engine and an additional security for air travel
08/13/2013	CA2675904C Filtration system for gas turbines
08/13/2013	CA2624005C Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine
08/13/2013	CA2513076C Bypass duct fluid cooler
08/13/2013	CA2509798C Modulated current gas turbine engine starting system
08/10/2013	CA2803342A1 Vane assemblies for gas turbine engines
08/08/2013	WO2013116034A1 Gas turbine engine variable area fan nozzle control
08/08/2013	WO2013116028A1 Geared turbofan engine with counter-rotating shafts
08/08/2013	WO2013115994A2 Gas turbine engine with variable area fan nozzle positioned for starting
08/08/2013	WO2013115921A1 Speed sensor probe location in gas turbine engine
08/08/2013	WO2013113324A1 Gas turbine with rotating casing
08/08/2013	US20130204506 Engine systems with efficient start control logic
08/08/2013	US20130202433 Seal assembly for turbine coolant passageways
08/08/2013	US20130202420 Turbine Shell Having A Plate Frame Heat Exchanger
08/08/2013	US20130200625 Sweep-Based Membrane Gas Separation Integrated With Gas-Fired Power Production And CO2 Recovery
08/08/2013	US20130200571 Seal mechanism for use with turbine rotor
08/08/2013	US20130200569 Leaf seal
08/08/2013	US20130199624 Gas turbine engine nacelle
08/08/2013	US20130199206 Speed sensor probe location in gas turbine engine
08/08/2013	US20130199204 Method and a device for performing a check of the health of a turbine engine of an aircraft provided with at least one turbine engine
08/08/2013	US20130199202 System and method for gas turbine inlet air heating
08/08/2013	US20130199201 Main engine start by means of an aircraft air conditioning system
08/08/2013	US20130199200 Fuel distribution within a gas turbine engine combustor
08/08/2013	US20130199199 Drive for a turbine and drive method
08/08/2013	US20130199194 Combustor head arrangement
08/08/2013	US20130199193 Tungsten carbide inserts and method
08/08/2013	US20130199192 System and method for gas turbine nox emission improvement
08/08/2013	US20130199189 Fuel injection assembly for use in turbine engines and method of assembling same
08/08/2013	US20130199187 Gas-turbine combustion chamber having non-symmetrical fuel nozzles
08/08/2013	US20130199152 Turbine engine heat recuperator plate and plate stack
08/08/2013	DE102012201650A1 Hitzeschild mit äußerer Faserwicklung Heat shield with outer fiber winding
08/07/2013	EP2623745A2 Gas turbine engine fuel return valve and system
08/07/2013	EP2623744A1 Air recovery-type cooling structure for air-cooled gas turbine combustor
08/07/2013	EP2623743A1 Water injection device for a by-pass steam system of a power plant
08/07/2013	EP2623742A1 Gas turbine system, control device for gas turbine system, and control method for gas turbine system
08/07/2013	EP2623741A1 Combined cycle power generation plant utilzing solar heat
08/07/2013	EP2623740A2 Method for transferring fuel
08/07/2013	EP2623726A2 Turbofan engine fan case and corresponding turbofan engine
08/07/2013	EP2622278A1 Gas turbine assembly and method therefor
08/07/2013	EP2622193A1 Dual fuel aircraft engine control system and method for operating same
08/07/2013	EP2622192A2 Aircraft engine systems and methods for operating same
08/07/2013	EP2622191A1 Dual fuel aircraft system and method for operating same
08/07/2013	EP2622181A1 Gas turbine engine comprising means for axially retaining a fan of the engine
08/07/2013	CN203114428U Sealing suspension ring connecting structure of gas turbine engine
08/07/2013	CN203114354U Turbine guide vane tube bundle cooling structure
08/07/2013	CN103237970A Adiabatic compressed air energy storage process
08/07/2013	CN103233821A Air temperature adjusting system
08/07/2013	CN101892910B Cold-heat compatible aircraft ignition circuit
08/07/2013	CA2804675A1 Interface and mounting process between an item of equipment and a rotary drive source for an engine group equiping a rotorcraft
08/06/2013	US8499567 Hybrid fuel tank inerting system
08/06/2013	US8499566 Combustor liner cooling system
08/06/2013	US8499564 Pilot burner for gas turbine engine
08/06/2013	CA2799933A1 Method and device for implementing a fitness monitor for a turbine engine in an aircraft equipped with at least one turbine engine
08/06/2013	CA2799712A1 Device and control method for a drive installation including at least one turbine engine, and aircraft
08/06/2013	CA2649087C Torque transmission for an aircraft engine
08/06/2013	CA2560633C Air/oil separation system and method
08/03/2013	CA2804108A1 Fastening system for fan and shaft interconnection
08/03/2013	CA2803638A1 Turbine engine heat recuperator plate and plate stack
08/02/2013	CA2803711A1 Segmented rings with captive nuts for fan bolts
08/02/2013	CA2803706A1 Fan and boost joint
08/01/2013	WO2013113038A1 Heat exchanger
08/01/2013	WO2013111825A1 Mixing turbine power generation device
08/01/2013	US20130195647 Gas turbine engine bearing arrangement including aft bearing hub geometry
08/01/2013	US20130195604 Turbomachine geared architecture support assembly
08/01/2013	US20130195392 Bearing assembly
08/01/2013	US20130193688 Bevel gear arrangement for axial accessory gearbox
08/01/2013	US20130192267 Internally cooled spoke
08/01/2013	US20130192261 Gas turbine engine mid turbine frame bearing support
08/01/2013	US20130192260 Gas turbine engine seal carrier
08/01/2013	US20130192259 Turbine engine monitoring system
08/01/2013	US20130192258 Geared turbofan gas turbine engine architecture
08/01/2013	US20130192257 Turbine shroud hanger with debris filter
08/01/2013	US20130192256 Geared turbofan engine with counter-rotating shafts
08/01/2013	US20130192255 Fixture assembly for repairing a shroud tile of a gas turbine
08/01/2013	US20130192248 Gas turbine engine buffer system
08/01/2013	US20130192247 Gas turbine engine variable area fan nozzle with ice management
08/01/2013	US20130192244 Hybrid apu start fuel system
08/01/2013	US20130192243 Fuel nozzle for a gas turbine engine and method of operating the same
08/01/2013	US20130192242 Speed sensor probe location in gas turbine engine
08/01/2013	US20130192241 Gas turbine engine variable area fan nozzle control
08/01/2013	US20130192240 Buffer system for a gas turbine engine
08/01/2013	US20130192239 Gas turbine engine buffer system

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