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)
10/2014
10/28/2014US8870530 Gas turbine engine
10/28/2014US8870523 Method for manufacturing a hot gas path component and hot gas path turbine component
10/28/2014US8869539 Arrangement for connecting a duct to an air-distribution casing
10/28/2014US8869538 Gas turbine engine flow path member
10/28/2014US8869537 Apparatus and method of operating a gas turbine engine
10/28/2014US8869536 Liner stop for turbine system combustor
10/28/2014US8869533 Combustion system for a gas turbine comprising a resonator
10/28/2014US8869509 Accessory flow recovery system and method for thermal efficient pump and control system
10/28/2014US8869504 Geared turbofan engine gearbox arrangement
10/23/2014US20140314546 Turbine engine gearbox mount with multiple fuse joints
10/23/2014US20140311585 Filter bypass valve
10/23/2014US20140311580 Air intake and a method of controlling the same
10/23/2014US20140311162 Connection structure of exhaust chamber, support structure of turbine, and gas turbine
10/23/2014US20140311161 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element
10/23/2014US20140311160 Hybrid turbomachine enclosure
10/23/2014US20140311159 Variable nozzle mechanism
10/23/2014US20140311158 Heat and power plant with a waste gasification system
10/23/2014US20140311157 Vane carrier temperature control system in a gas turbine engine
10/23/2014US20140311156 Combustor cap for damping low frequency dynamics
10/21/2014US8868262 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
10/21/2014US8866318 Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
10/21/2014US8864956 Multi-component deposition
10/21/2014US8864461 Turbine for the expansion of gas/vapour
10/21/2014US8864458 Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such fixed vane assembly
10/21/2014US8863894 Silencer and rotating machine equipped therewith
10/21/2014US8863531 Cooling apparatus for a mid-turbine frame
10/21/2014US8863530 Toroidal boundary layer gas turbine
10/21/2014US8863528 Ceramic combustor can for a gas turbine engine
10/21/2014US8863523 System for supplying a working fluid to a combustor
10/21/2014US8863495 Ignition/chemical reaction promotion/flame holding device, speed-type internal combustion engine, and furnace
10/21/2014US8863494 Turbine outlet frozen gas capture apparatus and method
10/16/2014US20140305136 Mounting arrangement
10/16/2014US20140305135 Fuel drain valve for a turbine engine
10/16/2014US20140305134 Rigid raft for a gas turbine engine
10/16/2014US20140305129 Gas turbine engine support strut assembly
10/16/2014US20140305128 Method for operating a combustion chamber and combustion chamber
10/16/2014US20140305126 Flow velocity distribution equalizing apparatus
10/14/2014US8862364 Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup
10/14/2014US8858388 Gas turbine engine gear train
10/14/2014US8858223 Glycerin fueled afterburning engine
10/14/2014US8858180 Annulus filler element for a rotor of a turbomachine
10/14/2014US8858163 Ventilation inlet
10/14/2014US8858087 Bearing assembly
10/14/2014US8857193 Intermediate casing for a gas-turbine engine
10/14/2014US8857192 Accessory gearbox with a starter/generator
10/14/2014US8857191 Hybrid propulsive engine including at least one independently rotatable propeller/fan
10/14/2014US8857189 Gas turbine combustion burner
10/14/2014US8857150 Monitoring of a high-pressure pump in a turbine engine fuel supply circuit
10/14/2014US8857149 Torque connector lubrication scuppers
10/14/2014US8857055 Process and system for forming shaped air holes
10/09/2014WO2014165467A1 Engine component having support with intermediate layer
10/09/2014WO2014165364A1 Bifurcated air inlet housing for a gas turbine engine
10/09/2014WO2014165182A1 Assembly for sealing a gap between components of a turbine engine
10/09/2014WO2014165138A1 Oil transfer passage arrangement for a shaft of a gas turbine engine
10/09/2014WO2014165084A1 A sensor housing
10/09/2014WO2014164888A1 Low pressure loss cooled blade
10/09/2014WO2014164586A1 Engine mounting system
10/09/2014WO2014164483A1 Structural guide vane outer diameter k gussets
10/09/2014WO2014164426A1 Turbine engine adaptive low leakage air seal
10/09/2014WO2014164252A1 Damper mass distribution to prevent damper rotation
10/09/2014WO2014164238A1 Gas turbine engine hydraulically operated nacelle latch
10/09/2014WO2014164189A1 Heat shield mount configuration
10/09/2014WO2014164128A1 Automatic coalescer replacement system and method
10/09/2014WO2014164095A1 Turbine cylinder cavity heated recirculation system
10/09/2014WO2014163708A2 Rotor noise suppression
10/09/2014WO2014163675A1 Geared architecture to protect critical hardware during fan blade out
10/09/2014WO2014162767A1 Rotating machine
10/09/2014WO2014162617A1 Gas turbine generation system
10/09/2014WO2014161661A1 Method and combined heat and power generation system comprising an internal combustion engine for carrying out said method
10/09/2014WO2014081493A9 Low profile compressor bleed air-oil coolers
10/09/2014US20140301829 Engine Bearing Support
10/09/2014US20140301820 Turbine engine shutdown temperature control system with nozzle injection for a gas turbine engine
10/09/2014US20140300058 Sealing of turbine engine enclosures produced by brush seal and labyrinth
10/09/2014US20140300057 Fluid transfer seal assemblies, fluid transfer systems, and methods for transferring process fluid between stationary and rotating components using the same
10/09/2014US20140298821 Gas turbine engine provided with heat exchanger, and method for starting same
10/09/2014US20140298820 Gas turbine engine and method for starting same
10/09/2014US20140298819 Turbine engine comprising an electrically activated fuel supply pump, and turbine engine fuel supply method
10/09/2014US20140298818 Control method and control device for lean fuel intake gas turbine
10/09/2014US20140298817 Arrangement for preparation of liquid fuel for combustion and a method of preparing liquid fuel for combustion
10/09/2014US20140298816 Simple cycle gas turbomachine system having a fuel conditioning system
10/09/2014US20140298814 Catalytic combustion air heating system
10/09/2014DE102014104454A1 Turbomaschinensystem mit einfachem Kreisprozess und Kraftstoffkondfitionierungssystem Turbomachinery system with simple cycle and Kraftstoffkondfitionierungssystem
10/09/2014DE102014104317A1 Lufterhitzungssystem mit katalytischer Verbrennung Air heating system with catalytic combustion
10/09/2014DE102014004782A1 Vorschmier- und nachschmiersystem für eine maschine Prelubrication and re-lubrication system for a machine
10/09/2014DE102013206245A1 Flüssigkeitsgekühlte Turbine Liquid-cooled turbine
10/09/2014DE102013205922A1 Vorrichtung und Verfahren zur Befestigung von Dichtungselementen Device and method for attaching sealing members
10/09/2014DE102013205911A1 Mischvorrichtung und Turbofantriebwerk mit einer derartigen Mischvorrichtung Mixer and turbofan engine with such a mixing device
10/09/2014DE102013005764A1 Verfahren und Kraft-Wärme-Kopplungssystem mit einer Verbrennungskraftmaschine zur Ausführung des Verfahrens Procedures and Cogeneration system with an internal combustion engine for executing the method
10/09/2014DE102010006143B4 Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs Silencer for an auxiliary power unit of an aircraft
10/08/2014EP2787198A2 Contamination free reverse flow fitting
10/08/2014EP2787173A1 Turbine blade
10/08/2014EP2786827A1 Bonded component
10/08/2014EP2785981A1 Turbine engine comprising an electrically activated fuel supply pump, and turbine engine fuel supply method
10/07/2014US8855952 Ram air turbine with flux regulated permanent magnet generator and testing method
10/07/2014US8851830 Harmonization of multiple gear train configurations
10/07/2014US8851416 Aircraft nacelle including at least one radial partition between two conducts
10/07/2014US8851151 Method and apparatus for production of a cast component
10/07/2014US8851054 Apparatus for providing diluted fugitive gases as a fuel to an engine
10/07/2014US8850828 Cooling hole with curved metering section
10/07/2014US8850826 Carbon capture with power generation
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