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)
11/2011
11/22/2011	CA2599113C Fuel injection valve, combustor using the fuel injection valve, and fuel injection method for the fuel injection valve
11/22/2011	CA2444929C A process for removing aluminosilicate material from a substrate, and related compositions
11/17/2011	WO2011142270A1 Method for fabricating shaft sealing device and jig for fabricating shaft sealing device, and rotary machine provided with shaft sealing device
11/17/2011	WO2011084941A3 Dual-pump supply system with by-pass-controlled flow regulator
11/17/2011	WO2011056928A4 Micro-turbine combustor
11/17/2011	US20110280735 Ventilation of a high-pressure turbine in a turbomachine
11/17/2011	US20110277484 System and method for ventilating a turbine
11/17/2011	US20110277483 Gas turbine engine with ejector
11/17/2011	US20110277481 Late lean injection injector
11/17/2011	US20110277480 System and method for washing and purging the liquid fuel system of a turbine with water
11/17/2011	US20110277442 Seal for Gas Turbine Filter
11/17/2011	US20110277441 Method and apparatus for an air filter cartridge replacement assembly
11/17/2011	DE102010020363A1 Air turbine, has round wavy panes connected firmly with one another and driven by drive motor based on change of energy supplied from external power source and temperature of surrounding air, and drive axle present in middle of panes
11/17/2011	DE102010020213A1 Ladevorrichtung, insbesondere Abgasturbolader für ein Kraftfahrzeug Charging device, in particular exhaust gas turbocharger for a motor vehicle
11/17/2011	CA2739210A1 Gas turbine engine compressor components comprising thermal barriers, thermal barrier systems, and methods of using the same
11/16/2011	EP2386344A2 Seal for gas turbine filter
11/16/2011	CN202039954U Gas fuel starting nozzle and igniter provided with same
11/16/2011	CN202039908U Container type gas turbine generating set and container housing thereof
11/16/2011	CN102245861A Power plant comprising a turbine unit and a generator
11/16/2011	CN102242673A Turbomachine nozzle
11/15/2011	US8057163 Gas turbine engine cooling system and method
11/15/2011	US8056346 Combustor
11/15/2011	US8056344 Gas turbine engine and method for reducing turbine engine combustor gaseous emission
11/15/2011	CA2498663C Property recovering method for nickel superalloy
11/15/2011	CA2492149C Nozzle flap cooling air supply system
11/15/2011	CA2470928C Turbomachine annular combustion chamber
11/15/2011	CA2439555C Acoustically resistive layer for a sound attenuation panel, panel using such a layer
11/10/2011	WO2011139741A2 Brush ring seal
11/10/2011	WO2011139567A1 Selecting and applying to fuel-flow splits bias values to correct for elevated inlet air humidity
11/10/2011	WO2011139317A2 Gas turbine engine and heat exchange system
11/10/2011	WO2011139314A2 Gas turbine engine component construction
11/10/2011	WO2011139311A2 Gas turbine engine and cooling system
11/10/2011	WO2011139310A2 Gas turbine engine and high speed rolling element bearing system
11/10/2011	WO2011138952A1 Heat-resistant nickel-based superalloy containing annealing twins and heat-resistant superalloy member
11/10/2011	WO2011138571A1 Unit for an aircraft thruster
11/10/2011	WO2011107682A3 Turbojet engine nacelle provided with a cooling assembly for cooling a component
11/10/2011	US20110276247 Method and a system for monitoring vibratory phenomena that occur in an aviation gas turbine engine in operation
11/10/2011	US20110272533 Jet engine nacelle intended to equip an aircraft
11/10/2011	US20110271689 Gas turbine cooling
11/10/2011	US20110271688 Reduced Pressure Loss Transition Support
11/10/2011	US20110271686 Exhaust silencer convection cooling
11/10/2011	US20110271683 Turbomachine injection nozzle assembly
11/10/2011	US20110271680 Lean premix burner of a gas-turbine engine provided with a concentric annular central body
11/10/2011	US20110271679 Liquid Fuel System and Method
11/10/2011	US20110271655 Separate cooling plate for aircraft engine electric control
11/10/2011	DE102010019605A1 Fliehkraft-Ölabscheider für ein Flugzeugtriebwerk Centrifugal oil separator for an aircraft engine
11/10/2011	DE102010019604A1 Zentrifugal-Ölabscheider für ein Flugzeugtriebwerk Centrifugal oil separator for an aircraft engine
11/10/2011	DE102010019285A1 Vorrichtung zur Drehlagerung einer Welle, insbesondere zur Verwendung in einer Dampfturbine Apparatus for rotatably supporting a shaft, in particular for use in a steam turbine
11/10/2011	CA2793080A1 Brush ring seal
11/10/2011	CA2785895A1 Gas turbine engine component construction
11/10/2011	CA2738312A1 Gas turbine engine combustor with cmc heat shield and methods therefor
11/09/2011	EP2385275A1 A fireseal
11/09/2011	EP2385234A2 Gas turbine cooling configuration
11/09/2011	EP2385220A2 Labyrinth seal for a turbo engine
11/09/2011	EP2384397A2 Method and systems for an engine starter/generator
11/09/2011	EP1853805B1 Aircraft engine fuel supply
11/09/2011	CN202031663U Air inlet shell, sound eliminator, suction connecting pipe, compressor and exhaust-gas turbo charger of compressor
11/09/2011	CN1849483B Partitioned exciter system
11/09/2011	CN102235267A Gas turbine engine modified by using exservice turbofan engine through low-pressure crest truncation
11/09/2011	CN102235266A Exhaust silencer convection cooling
11/09/2011	CN102235246A Accessory gearbox with a starter/generator
11/09/2011	CN102235245A Fluid cooled injection nozzle assembly for a gas turbomachine
11/09/2011	CN102235244A Pocketed air and fuel mixing tube
11/09/2011	CN102235243A Gas turbine cooling configuration
11/09/2011	CN102235242A Hot gas path component cooling system
11/09/2011	CN102235241A Low-pressure turbine structure with big expanding path at inlet
11/09/2011	CN102235239A System for heating an airstream by recirculating waste heat of a turbomachine
11/09/2011	CN102233218A Filter
11/09/2011	CN102233213A Filter assembly
11/08/2011	US8051952 Deoiling device and turbomachine comprising this device
11/08/2011	US8051664 Pre-loaded internal fuel manifold support
11/08/2011	US8051654 Reheat gas and exhaust gas regenerator system for a combined cycle power plant
11/08/2011	US8051638 Systems and methods for exhaust gas recirculation (EGR) for turbine engines
11/08/2011	CA2495982C Turbojet with fan connected to a drive shaft supported by a first and second level
11/08/2011	CA2459473C Turbomachine with cooled ring segments
11/05/2011	CA2736454A1 Exhaust silencer convection cooling
11/03/2011	WO2011137110A1 Dynamically auto-tuning a gas turbine engine
11/03/2011	WO2011137107A1 Employing fuel properties to auto-tune a gas turbine engine
11/03/2011	WO2011135240A1 Turbomachine fueling system with jet pump
11/03/2011	WO2011134730A2 Turbine including seal air valve system
11/03/2011	WO2011112108A3 Bullgear gas turbine with intercooler and reheat
11/03/2011	WO2011100663A3 Coil arrangements for air intake system for gas turbine and methods
11/03/2011	US20110265491 Combustor connection structure, combustor transition piece, designing method of combustor transition piece, and gas turbine
11/03/2011	US20110265486 Combustion system with variable pressure differential for additional turndown capability of a gas turine engine
11/03/2011	US20110265485 Fluid cooled injection nozzle assembly for a gas turbomachine
11/03/2011	US20110265482 Pocketed air and fuel mixing tube
11/03/2011	US20110265445 Method for Reducing CO2 Emissions in a Combustion Stream and Industrial Plants Utilizing the Same
11/03/2011	US20110265443 System and method for adjusting compressor inlet fluid temperature
11/03/2011	DE102011050011A1 System zum Erwärmen eines Luftstroms durch Rückführung von Abwärme einer Gasturbine System for heating a stream of air by recycling waste heat from a gas turbine
11/02/2011	EP2383451A2 Alternate method for diluent injection for gas turbine NOx emissions control
11/02/2011	EP2383442A2 Gas turbine engine
11/02/2011	EP2383441A2 A Gas Turbine Engine
11/02/2011	EP2383440A1 Turbine including seal air valve system
11/02/2011	EP2382424A1 Device for large-scale media conditioning
11/02/2011	EP2382386A1 Method and systems for adaptive ignition energy
11/02/2011	EP2382026A1 Inlet particle separator system for a gas turbine engine
11/02/2011	CN1626629B Method of inhibiting deposit formation in a jet fuel at high temperatures
11/02/2011	CN102230848A Method for acquiring optimal classification surface of hypersonic speed air inlet starting/non-starting mode
11/02/2011	CN102230420A Low-temperature gas exhausting engine
11/02/2011	CN102229360A Aviation kerosene high-temperature combustion gas flow generating device

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