Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › 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)
06/2014
06/18/2014CN102016265B Casing comprising a peripheral shroud for a turbomachine rotor
06/18/2014CN101612823B Multilayer thermal barrier coating
06/18/2014CA2835584A1 Gas turbine engine mounting ring
06/17/2014US8752583 Multi-way valve of a fuel system of a gas turbine
06/17/2014US8752395 Combustor liner support and seal assembly
06/17/2014US8752392 Device and a method for starting a turbine engine fitted to a helicopter, making use of an electrical energy source that includes discharge booster members
06/17/2014US8752386 Air/fuel supply system for use in a gas turbine engine
06/17/2014CA2836008A1 Circuit and method for allocating power among generators
06/17/2014CA2764664C Ni-based single crystal superalloy and turbine blade
06/17/2014CA2549091C Durable thermal barrier coating having low thermal conductivity
06/12/2014WO2014088929A1 A method of fabricating a rotor of a turbofan engine
06/12/2014WO2014088925A1 Gas turbine engine with a low speed spool driven pump arrangement
06/12/2014WO2014088671A2 Gas turbine engine two degree of freedom variable bleed valve for ice extraction
06/12/2014WO2014088608A1 Windback device for a circumferential seal
06/12/2014WO2014087316A1 Electric redundant circuit
06/12/2014WO2014058483A3 Corrugated mid-turbine frame thermal radiation shield
06/12/2014US20140161592 Guidance of turbine engine shafts
06/12/2014US20140161591 Lubricant system
06/12/2014US20140157791 System for controlling a cooling flow from a compressor section of a gas turbine
06/12/2014US20140157788 Fuel nozzle for gas turbine
06/12/2014US20140157787 Fuel nozzle for gas turbine
06/12/2014US20140157779 SYSTEM FOR REDUCING COMBUSTION DYNAMICS AND NOx IN A COMBUSTOR
06/12/2014US20140157596 Free-state seal plate functional gage tool
06/12/2014DE102013225464A1 Kühlmittelmantel für einen Turbolader-Ölablass Coolant jacket for a turbocharger oil drain
06/12/2014DE102013001507A1 Lagergehäuse eines Abgasturboladers An exhaust gas turbocharger bearing housing
06/12/2014DE102012222671A1 Device for utilizing waste heat of combustion engine in e.g. passenger car, has starting channel arranged within turbine housing, bypassed according to type of bypass on turbine unit and connecting intake port with exhaust opening
06/11/2014EP2740905A1 Separator llip of an axial turbomachine with de-icing device, corresponding compressor and turbomachine
06/11/2014EP2740903A2 A system for controlling a cooling flow from a compressor section of a gas turbine
06/11/2014EP2739905A2 A combustor resonator section with an internal thermal barrier coating and method of fabricating the same
06/11/2014CN203640837U 燃气轮机的辅助支撑装置 Gas turbine auxiliary support means
06/11/2014CN103857891A Lean fuel intake gas turbine
06/11/2014CN103850801A Gas turbine part comprising a near wall cooling arrangement
06/11/2014CN103850800A Air inlet anticer and civil turbofan engine
06/11/2014CN103850797A Combustible gas direct power machine
06/11/2014CN103850733A Centering device
06/11/2014CN102414422B One-piece mounting for aeronautical apparatuses
06/11/2014CN102272428B Engine
06/11/2014CN101903241B Ice protection system for a multi-segment aircraft component
06/11/2014CN101779002B Turbine blade
06/11/2014CN101709673B Device and method used for cooling gas turbine
06/11/2014CN101029598B Methods and systems of variable extraction for gas turbine control
06/10/2014US8745991 Turbine system
06/10/2014US8745987 Late lean injection manifold
06/10/2014CA2575343C Turbomachine with integrated starter-generator
06/10/2014CA2527641C Gas turbine engine assembly and method of assembling same
06/10/2014CA2424363C A novel method for chromatographic finger printing and standardization of single medicines and formulations
06/07/2014CA2833987A1 Splitter nose of an axial turbomachine with a de-icing device
06/06/2014CA2833754A1 Operations support systems and methods for calculating and evaluating turbine temperatures and health
06/05/2014WO2014085636A1 Geared architecture gas turbine engine with improved lubrication and misalignment tolerant roller bearing system
06/05/2014WO2014085292A1 Turbofan with optical diagnostic capabilities
06/05/2014WO2014085031A2 Lubrication system for gas turbine engines
06/05/2014WO2014085020A1 Trailing edge and tip cooling
06/05/2014WO2014084969A1 Engine compressor wash system
06/05/2014WO2014084965A1 Cooled combustor seal
06/05/2014WO2014083270A1 Method for creating a power transmission casing using friction stir welding
06/05/2014WO2014083256A1 Turbine engine cowl capable of covering a fan cone
06/05/2014US20140154062 System and method for sealing a gas path in a turbine
06/05/2014US20140154054 Oil baffle for gas turbine fan drive gear system
06/05/2014US20140154053 Carbon seal assembly
06/05/2014US20140150452 Transition piece for a gas turbine system
06/05/2014US20140150450 Exhaust component mounting structure
06/05/2014US20140150449 Air cooling shaft at bearing interface
06/05/2014US20140150447 Load ramp and start-up system for combined cycle power plant and method of operation
06/05/2014US20140150446 Battery current regulation
06/05/2014US20140150441 Power plant and method for generating electrical power
06/05/2014US20140150440 Gas turbine engine with a low speed spool driven pump arrangement
06/05/2014US20140150439 Lubrication System for Gas Turbine Engines
06/05/2014US20140150434 Fuel nozzle for a combustor of a gas turbine engine
06/05/2014US20140150433 Exhaust gas collector for an exhaust aftertreatment system
06/05/2014US20140150402 System and method for burning vanadium-containing fuels
06/05/2014US20140150401 Geared compressor for gas turbine engine
06/05/2014US20140150400 Fluid system with gravity controlled valve
06/05/2014US20140150399 Diverter damper
06/05/2014US20140150261 Trip cup for overspeed control
06/05/2014DE102013106228A1 Zwei-stufen-turbolader Two-stage-turbocharger
06/05/2014DE102012206126B4 Laufschaufel sowie Strömungsmaschine Blade and flow machine
06/05/2014DE102012111847A1 High speed gear assembly for powertrain of motor vehicle, has drive shaft and second shaft that are indirectly supported in housing pot, and storage unit provided in housing pot for storage of third shaft
06/05/2014DE102012023802A1 Exhaust gas turbocharger for use with internal combustion engine, has adjusting device with several mutually operatively connected valve elements that are in sealing engagement with associated valve seat in closed position
06/04/2014EP2738358A1 Turbomachine component including a seal member
06/04/2014EP2737933A1 Inlet particle separator system with air injection
06/04/2014EP2737191A1 Turbo - compressor train with rolling bearings and related assembly method
06/04/2014CN203626968U 用于涡轮组件的装置 Means for a turbine assembly
06/04/2014CN103842695A Shaft sealing device and rotating machine comprising same
06/04/2014CN103842626A Liquefied gas treatment system, control method therefor, liquefied gas carrier provided therewith, and liquefied gas storage facility provided therewith
06/04/2014CN103842251A System and method for mounting an aircraft engine
06/04/2014CN103836127A Starting device for two-level speed changing gas turbine
06/04/2014CN103835811A Insert element for closing an opening inside a wall of a hot gas path component of a gas turbine
06/04/2014CN103835810A Acoustic liner for air-inlet nacelle of aircraft engine and aircraft engine
06/04/2014CN103835773A Air cylinder supporting assembly
06/04/2014CN102720587B Variable cross-section high supersonic speed inward rotation type air inlet with consistency of local contraction ratio
06/04/2014CN102278204B Powdery solid fuel combustion and work application method and device
06/04/2014CN102057194B Multi-way valve of a fuel system of a gas turbine
06/04/2014CN101929387B Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith
06/04/2014CN101684749B Liquefied natural gas power plant and operation method thereof
06/04/2014CN101625028B Gasket for providing a seal between two objects
06/04/2014CN101280726B Power output system and gas turbine assembly including same
06/03/2014USH2292 Materials of construction for a gas turbine
06/03/2014US8739811 Direct metering fuel system with constant servo flow
06/03/2014US8739550 Two stage combustor with reformer
06/03/2014US8739545 Burner for a gas turbine engine
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