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)
12/2013
12/03/2013	CA2611983C System for defrosting the leading edge sheath of an air inlet hood for a turboengine
11/2013
11/28/2013	WO2013177263A1 Engine inlet
11/28/2013	WO2013177050A1 Airfoil mateface sealing
11/28/2013	WO2013177030A1 Method and device for modifying a secondary air system in a gas turbine engine
11/28/2013	WO2013176920A1 Shield system for gas turbine engine
11/28/2013	WO2013176919A1 Debris discourager
11/28/2013	WO2013176876A1 Liquid-gas mixer and turbulator therefor
11/28/2013	WO2013176863A1 Passive thermostatic valve
11/28/2013	WO2013176727A2 Structures and methods for intercooling aircraft gas turbine engines
11/28/2013	WO2013176717A2 Pressure balanced area control of high aspect ratio nozzle
11/28/2013	WO2013175563A1 Liquid spray method and spray device
11/28/2013	US20130315714 Method for pulling a bearing body off the rotor of a gas turbine and tubular shaft extension
11/28/2013	US20130315657 Unit for an aircraft thruster
11/28/2013	US20130313039 Method for repairing a sound attenuation panel
11/28/2013	US20130312425 Passive thermostatic valve
11/28/2013	US20130312423 Method of detecting shaft break
11/28/2013	DE202013010098U1 Abgasturbolader Exhaust gas turbocharger
11/28/2013	DE102012208744A1 Wälzlager Rolling bearings
11/28/2013	DE102012208673A1 Device for discharging oil ventilation air from lubrication oil venting system of dual flow jet engine, has air outlet formed at suction side and at pressure side such that oil ventilation air is exhausted over air outlet into flow channel
11/27/2013	EP2666991A2 Apparatus and system for changing temperature of vane separators in a power generating system
11/27/2013	EP2666970A1 Gas turbine system having a plasma actuator flow control arrangement
11/27/2013	EP2665909A2 Nacelle for an aircraft bypass turbojet engine
11/27/2013	EP2665908A2 Nacelle for an aircraft bypass turbojet engine
11/27/2013	EP2665904A1 Sound absorber for a gas turbine exhaust cone, and method for the production thereof
11/27/2013	EP2665898A2 Gas turbine exhaust cone
11/27/2013	EP2665896A1 Intermediate housing of a gas turbine with an outer bounding wall, having upstream of a supporting rib a contour that changes in the circumferential direction, for reducing secondary flow losses
11/27/2013	EP2553244B1 Method for increasing the efficiency of a power plant equipped with a gas turbine, and power plant for carrying out the method
11/27/2013	CN203308586U Device for balancing liquid levels of lubricating oil tanks of gas turbine and gas compressor
11/27/2013	CN103415684A 燃气涡轮机 Gas turbines
11/27/2013	CN103410617A Method for determining position of hoops on engine pipelines
11/27/2013	CN103410616A High-capacity compressed air energy storage efficient power generating system
11/27/2013	CN102953826B Pneumatic supersonic velocity/hypersonic velocity adjustable air inlet passage for forebody-inner passage circulation
11/27/2013	CN101821481B Turbomachine
11/27/2013	CN101772628B Fuel control method and fuel control apparatus for gas turbine and gas turbine
11/26/2013	US8590492 Cartridge for the generation of hydrogen for providing mechanical power
11/26/2013	US8590317 Gas turbine engine starting method and control device
11/26/2013	US8590285 Three-point fixing arrangement of ignition electrodes of a burner
11/25/2013	CA2815478A1 Apparatus and system for changing temperature of vane separators in a power generating system
11/21/2013	WO2013173220A1 Turbocharger with journal bearing
11/21/2013	WO2013173089A1 Detachable fan blade platform and method of repairing same
11/21/2013	WO2013173055A1 Shaft sealing system for a turbocharger
11/21/2013	WO2013173054A1 Flinger oil seal and turbocharger incorporating the same
11/21/2013	WO2013173006A1 Method for making metal plated gas turbine engine components
11/21/2013	WO2013172905A2 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame
11/21/2013	WO2013172903A2 Tapered thermal coating for airfoil
11/21/2013	WO2013172899A2 Gas turbine engine systems involving tip fans
11/21/2013	WO2013172893A2 Composite airfoil with local tailoring of material properties
11/21/2013	WO2013126122A3 Bleed air and hot section component cooling air system of a gas turbine and method
11/21/2013	WO2010030441A3 System for enhanced gas turbine performance in a liquefied natural gas facility
11/21/2013	US20130306403 Method for the production of a sound absorber, especially for a gas turbine exhaust cone
11/21/2013	US20130306402 Method for the production of a sound absorber, especially for a gas turbine exhaust cone
11/21/2013	US20130305740 Method and apparatus for gas turbine engine temperature management
11/21/2013	US20130305739 Fuel nozzle cap
11/21/2013	US20130305738 System and method for producing hydrogen rich fuel
11/21/2013	US20130305737 System and method for heat recovery in a gas turbine engine
11/21/2013	US20130305736 Method and apparatus for increasing combustion efficiency and reducing particulate matter emissions in jet engines
11/21/2013	US20130305733 Apparatus and method for providing damper liquid in a gas turbine engine
11/21/2013	US20130305732 Mixing element for gas turbine units with flue gas recirculation
11/21/2013	US20130305731 Methods and apparatus for providing fluidic inserts into an exhaust stream to reduce jet noise from a nozzle
11/21/2013	US20130305730 Method for preheating fuels in a gas turbine engine
11/21/2013	US20130305729 Turbomachine combustor and method for adjusting combustion dynamics in the same
11/21/2013	US20130305728 Systems and Methods for Minimizing Coking in Gas Turbine Engines
11/21/2013	US20130305684 Debris discourager
11/21/2013	US20130305668 Debris Intrusion Shield for Jet Engine Applications
11/21/2013	DE102012009732A1 Schaltarmaturanordnung Switching valve arrangement
11/20/2013	EP2664767A1 Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor
11/20/2013	EP2664766A2 A heat exchanger
11/20/2013	EP2664765A2 System and method for heat recovery in a gas turbine engine
11/20/2013	EP2664748A2 Cooling system and method for turbine system
11/20/2013	EP2664747A2 Engine wash optimisation
11/20/2013	EP2664410A2 Methods of fabricating fuel injectors using laser additive deposition
11/20/2013	EP2663777A1 Turbofan engine
11/20/2013	EP2663759A1 Method for starting a turbomachine
11/20/2013	EP2216530B1 Aircraft electric generation system
11/20/2013	CN103403300A Axial brush seal
11/20/2013	CN103403299A Turbine blade
11/20/2013	CN103398398A Double-seal connection structure of flame tube and transition section of combustion gas turbine combustion chamber
11/20/2013	CN103397943A Fuel gas-steam combined cycle inlet air dehumidifying and cooling system and method
11/20/2013	CN103397911A Compound nozzle cooled engine
11/20/2013	CN102297026B Dust collector and ground gas turbine
11/20/2013	CN102124198B Fuel injector sans support/stem
11/20/2013	CN101922353B Feeding film cooling hole from seal slot
11/19/2013	US8584470 Tri-lobed cooling hole and method of manufacture
11/19/2013	US8584469 Cooling fluid pre-swirl assembly for a gas turbine engine
11/19/2013	US8584467 Method of controlling a combustor for a gas turbine
11/19/2013	US8584465 Method for increasing the efficiency of a power plant which is equipped with a gas turbine, and power plant for carrying out the method
11/19/2013	CA2714809C System for washing an aero gas turbine engine
11/19/2013	CA2682570C Gas turbine engine
11/19/2013	CA2498486C Rotating shaft scavenging scoop
11/19/2013	CA2478750C Thermal barrier compound, superalloy mechanical part coated with such a compound, ceramic coating, and process for manufacturing the said coating
11/18/2013	CA2815845A1 Inner bypass duct wall attachment
11/15/2013	CA2813216A1 Engine wash optimisation
11/14/2013	WO2013169711A1 Non-axisymmetric rim cavity features to improve sealing efficiencies
11/14/2013	WO2013169604A1 Blade tip having a recessed area
11/14/2013	WO2013169495A1 Gas turbine engine oil tank
11/14/2013	WO2013169322A1 Convective shielding cooling hole pattern
11/14/2013	WO2013167639A1 Dispensing device for cryogenic liquids
11/14/2013	WO2013167638A1 Supplying a pump with cryogenic liquid
11/14/2013	WO2013167637A1 Supplying a pump with cryogenic liquid
11/14/2013	WO2013167636A1 Method and system for retrofitting an aircraft

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