Patents
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)
03/2014
03/05/2014EP2702251A1 Casing cooling duct
03/05/2014CN203464331U Dual-sealing connecting structure for flame tube and transition section of gas turbine combustion chamber
03/05/2014CN203463193U Miniature turbojet engine
03/05/2014CN203463192U Novel micro gas turbine supporting system
03/05/2014CN103620165A Turbomachine fan case
03/05/2014CN103615321A Method for preventing foreign body from entering enclosed chamber of engine case
03/05/2014CN103615320A Turbulent flow ring structure with uniform fuel gas temperature field
03/05/2014CN102518517B Design method of bistable air inlet
03/05/2014CN102414522B Transcritical thermally activated cooling, heating and refrigerating system
03/04/2014US8666633 Engine systems with efficient start control logic
03/04/2014US8666568 Method and a device for performing a health check of a turbine engine of an aircraft having at least one such engine
03/04/2014US8661835 Bushing for torque load transfer attachment hardware
03/04/2014US8661834 Method and apparatus for starting engine
03/04/2014US8661832 Surge margin regulation
03/04/2014US8661825 Pegless secondary fuel nozzle including a unitary fuel injection manifold
03/04/2014US8661822 Acoustically stiffened gas turbine combustor supply
03/04/2014US8661781 Counter rotating fan design and variable blade row spacing optimization for low environmental impact
03/04/2014US8661780 Gas turbine plant with exhaust gas recirculation and also method for operating such a plant
03/04/2014CA2826127A1 Systems and methods for driving an oil cooling fan of a gas turbine engine
03/04/2014CA2493500C Methods and apparatus for operating gas turbine engines
02/2014
02/27/2014WO2014031629A2 High efficiency power generation system and system upgrades
02/27/2014WO2014031502A1 Annular turbomachine seal and heat shield
02/27/2014WO2014031275A1 Gas turbine engine airfoil internal cooling features
02/27/2014WO2014031205A2 Seal land for static structure of a gas turbine engine
02/27/2014WO2014031198A2 Variable blade outer air seal
02/27/2014WO2014031194A2 Direct feed auxiliary oil system for geared turbofan engine
02/27/2014WO2014031160A1 Compliant cantilevered airfoil
02/27/2014WO2014030011A1 Sensor apparatus, corresponding turbocharger and method of measuring a mass flow rate
02/27/2014WO2014029580A1 Fluid dynamics machine comprising a rotor and a housing
02/27/2014WO2014007893A3 Geared turbofan with three turbines with first two counter-rotating, and third co-rotating with the second turbine
02/27/2014WO2013172893A3 Composite airfoil with local tailoring of material properties
02/27/2014WO2013162672A3 Gas turbine engine sump pressurization system
02/27/2014US20140053574 System for remote vibration detection on combustor basket and transition in gas turbines
02/27/2014US20140053573 Hot gas expander inlet casing assembly and method
02/27/2014US20140053571 Seal for a perforated plate
02/27/2014US20140053566 Method for mixing a dilution air in a sequential combustion system of a gas turbine
02/27/2014US20140053564 Liner bracket for gas turbine engine
02/27/2014US20140053563 Method for assembling a nozzle and an exhaust case of a turbomachine
02/27/2014US20140053562 Press-fitting corrosion resistant liners in nozzles and casings
02/27/2014US20140053561 Aircraft fuel cell system, aircraft and use of a synthetic fuel
02/27/2014US20140053560 High efficiency power generation system and system upgrades
02/27/2014US20140053532 Nacelle scoop inlet
02/27/2014US20140053530 Fuel metering system electrically servoed metering pump
02/27/2014US20140053529 System and method for high efficiency power generation using a carbon dioxide circulating working fluid
02/27/2014DE102013109114A1 Turbolader und Eindämmungssystem für den Fall des Berstens eines Verdichterrads Turbocharger and control system in the event of bursting of a compressor
02/27/2014DE102013108985A1 System for reducing combustion dynamics in gas turbine utilized for e.g. industrial operations, has fuel injection device extending through pipes, where fourth axial spacing in burner is different from fourth axial spacing in another burner
02/27/2014DE102012016493A1 Gasturbinenbrennkammer mit prallgekühlten Bolzen der Brennkammerschindeln Gas turbine combustor with impingement cooled bolts of the combustion chamber shingles
02/27/2014DE102010034766B4 Lageranordnung für die Verdichterseite eines Turboladers einer Verbrennungskraftmaschine Bearing arrangement for the compressor side of a turbocharger of an internal combustion engine
02/26/2014EP2700798A1 Turbomachine comprising a rotor and a casing
02/26/2014EP2700789A1 Turbine stator vane and gas turbine
02/26/2014EP2700787A1 Vane member and rotary machine
02/26/2014EP2700068A1 Multi-degree of freedom resonator array
02/26/2014EP2699780A1 Closed gas generator and micro power unit including the same
02/26/2014EP2699769A1 Hydraulic bearing for a stationary gas turbine
02/26/2014CN203454467U Multi-renewable-energy-complementary distribution-type energy system
02/26/2014CN103608567A Gas turbine arrangement for a locomotive
02/26/2014CN103608566A Gas turbine, and method for repairing gas turbine
02/26/2014CN103608565A Aircraft engine fuel system and method of operating the same
02/26/2014CN103603877A 锁紧装置 Locking device
02/26/2014CN103603696A Novel Brandon brush steam seal
02/25/2014US8657569 Breather duct shielding
02/25/2014US8657566 Turbine engine including a reversible electric machine
02/25/2014US8656724 Aluminium combustion power system
02/25/2014US8656699 Combustion burner
02/25/2014CA2487911C Method and apparatus for detecting rub in a turbomachine
02/20/2014WO2014028421A1 Gas turbine engine airfoil profile
02/20/2014WO2014028419A1 Thermal barrier coating having outer layer
02/20/2014WO2014028418A1 Platform cooling circuit for a gas turbine engine component
02/20/2014WO2014028294A1 Gas turbine engine component having platform trench
02/20/2014WO2014028270A1 Synchronizing ring surge bumper
02/20/2014WO2014028180A1 Harness support and mount
02/20/2014WO2014028157A1 Rotor keyhole fillet for a gas turbine engine
02/20/2014WO2014028138A1 Trailing edge cooling configuration for a gas turbine engine airfoil
02/20/2014WO2014028056A1 Contoured flowpath surface
02/20/2014WO2014027157A1 Tool for degritting a turbomachine
02/20/2014WO2013176727A3 Structures and methods for intercooling aircraft gas turbine engines
02/20/2014US20140050559 Gas turbine and method for operating a gas turbine
02/20/2014US20140048166 Pivoting ball stop for exhaust duct liner hanger
02/20/2014US20140047850 Assembly for mounting a turbine engine to an airframe
02/20/2014US20140047849 Spherical button washer for exhaust duct liner hanger
02/20/2014US20140047848 Adjustable cable for exhaust duct liner hanger
02/20/2014US20140047846 Turbine component cooling arrangement and method of cooling a turbine component
02/20/2014US20140047845 Combustor liner cooling assembly
02/20/2014US20140047843 Platform cooling circuit for a gas turbine engine component
02/20/2014US20140047842 Suction side turbine blade tip cooling
02/20/2014US20140047813 Exhaust collector with radial and circumferential flow breaks
02/20/2014DE102013108609A1 Kappensystem für Turbinenöffnungen Cap system for turbine openings
02/20/2014DE102012214444A1 Gas- und Dampfturbinenanlage mit Naturzugkühlturm Gas and steam turbine plant with natural draft cooling tower
02/20/2014CA2823368A1 High temperature resistive temperature detector for exhaust as temperature measurement
02/19/2014EP2697493A1 Fuel circuit comprising means for controlling a pump
02/19/2014CN203441604U System for reducing backpressure in gas turbine system
02/19/2014CN103597171A Turbine engine comprising a floating bearing for guiding a shaft of the turbine engine
02/19/2014CN103597170A Casing cooling duct
02/19/2014CN103590907A Temperature-changing internal combustion turbine
02/19/2014CN103590906A Utilization of fuel gas for purging a dormant fuel gas circuit
02/19/2014CN102705081B Binary hypersonic variable geometrical inlet channel, design method and work mode
02/19/2014CN101936219B Power augmentation system for engine and method of humidifying air
02/18/2014US8651925 Ventilating air intake arrangement with mobile closing device
02/18/2014US8650885 Retaining member for use with gas turbine engine shaft and method of assembly
02/18/2014US8650880 Active combustion control for turbine engine
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