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)
07/2012
07/04/2012CN102536463A Cutoff valve
07/04/2012CN102536462A Filter assembly for use in a turbine system
07/04/2012CN102536461A Filter cartridge assembly for use with turbine engine systems
07/04/2012CN102536413A Evaporative cooling device for combustion chamber
07/04/2012CN102536335A Combustion gas turbine wheel-disc broaching combination key and processing and using method thereof
07/04/2012CN102536332A Components with re-entrant shaped cooling channels and methods of manufacture
07/04/2012CN102528413A Method of modifying a substrate for passage hole formation therein, and related articles
07/04/2012CN101718226B Non-intermittent detonation rotor of engine
07/04/2012CN101652534B Stator blade ring and axial flow compressor using the same
07/04/2012CN101283221B Process and device for monitoring the formation of deposits of solid particles, in particular in a fuel line and in the fuel valves of a gas turbine
07/03/2012US8210825 Heated engine nose cone using spiral channels
07/03/2012US8210316 Oil scavenge system for a gas turbine engine
07/03/2012US8209951 Power generation system having an exhaust attemperating device
07/03/2012CA2680650C Ni-based single crystal superalloy and turbine blade incorporating the same
07/03/2012CA2671242C Hybrid drive installation and control method therefor
07/03/2012CA2481932C Target designed to be vaporized by an electron beam, the process for manufacturing the said target, thermal barrier and coating obtained from the use of such a target, and mechanical parts on which such a coating is used
07/03/2012CA2478793C Device used to estimate mass fuel flow
06/2012
06/30/2012CA2762849A1 Variable cycle gas turbine engine
06/30/2012CA2762835A1 Gas turbine engine flange assembly including flow circuit
06/30/2012CA2762613A1 Structural low-ductility turbine shroud apparatus
06/30/2012CA2762609A1 Mounting apparatus for low-ductility turbine shroud
06/30/2012CA2762598A1 Integration of a surface heat-exchanger with regulated air flow in an airplane engine
06/30/2012CA2762289A1 Vane with spar mounted composite airfoil
06/30/2012CA2762288A1 Vane with spar mounted composite airfoil
06/29/2012CA2762393A1 Method and system for powering a vehicle
06/28/2012WO2012088499A1 Gas turbine engine flow path member
06/28/2012WO2012087952A2 Method and tooling for partial disassembly of a bypass turbofan engine
06/28/2012WO2012087420A2 Method for balancing rotating assembly of gas turbine engine
06/28/2012WO2012086044A1 Flow path structure and gas turbine exhaust diffuser
06/28/2012WO2012084892A1 Filtering chamber and method for maintaining same
06/28/2012US20120159966 Gearbox assembly
06/28/2012US20120159964 Accessory gearbox with a starter/generator
06/28/2012US20120159963 Cartridge for the generation of hydrogen for providing mechanical power
06/28/2012US20120159962 Water self-sufficient turbine system
06/28/2012US20120159960 Turbomachine drive arrangement
06/28/2012US20120159958 Gas turbine engine flow path member
06/28/2012US20120159957 Water self-sufficient turbine system
06/28/2012US20120159956 Top cycle power generation with high radiant and emissivity exhaust
06/28/2012US20120159954 Transition piece and gas turbine
06/28/2012US20120159953 Fuel Staging System
06/28/2012DE102011056905A1 Kühlkanalsysteme für mit Beschichtungen überzogene Hochtemperaturkomponenten und zugehörige Verfahren Cooling duct systems with coatings plated high-temperature components and associated methods
06/28/2012DE102011056643A1 System und Verfahren zur Online-Überwachung einer Rotationsmaschine System and method for on-line monitoring of a rotary machine
06/28/2012CA2762774A1 Gas turbine engine and airfoil
06/28/2012CA2762701A1 Accessory gearbox with a starter/generator
06/27/2012EP2469214A2 Surface cooler having channeled fins
06/27/2012EP2469057A1 Fuel staging system
06/27/2012EP2469056A1 Enclosure for thermal equipment and installation method.
06/27/2012EP2467589A1 Method and device for converting thermal energy from biomass into mechanical work
06/27/2012EP2118471B1 Coating for acoustic treatment having a hot air icing processing function
06/27/2012CN102518518A Fuel conveying system and method for substituting main fuel for pilot fuel in combustion engine
06/27/2012CN102518517A Bistable air inlet, its application as aircraft air inlet and design method of bistable air inlet
06/27/2012CN102518516A Integral compressed air energy storage and coal gasification power generation system and integrated power generation method
06/27/2012CN102518499A Silencer
06/27/2012CN101681616B Acoustic septum cap honeycomb
06/27/2012CN101050726B System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine
06/26/2012US8205597 Aircraft engine fuel supply
06/26/2012US8205457 Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor
06/26/2012US8205452 Apparatus for fuel injection in a turbine engine
06/26/2012US8205451 System and assemblies for pre-heating fuel in a combined cycle power plant
06/26/2012US8205427 Interdependent lubrication systems in a turbine engine
06/26/2012CA2535700C Device for stabilizing the engine inlet flow in static tests of engines
06/26/2012CA2491666C Improvements to the device to control the play in a gas turbine
06/26/2012CA2484944C Miniature gas turbine engine with unitary rotor shaft for power generation
06/26/2012CA2472935C Device for reducing jet noise from a turbine engine
06/24/2012CA2762694A1 Gas turbine engine flow path member
06/21/2012WO2012082221A1 Buffer air for a labyrinth seal
06/21/2012WO2012080633A1 Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
06/21/2012WO2012080601A1 Integrated method and apparatus for compressing air and producing carbon dioxide-rich fluid
06/21/2012US20120156061 Flow Sensing Dual Pump Switching System and Method
06/21/2012US20120156039 Electric generator disposed on a rotating turboprop part
06/21/2012US20120156005 Buffer air for a labyrinth seal
06/21/2012US20120151937 Method for balancing rotating assembly of gas turbine engine
06/21/2012US20120151935 Gas turbine engine and method of operating thereof
06/21/2012US20120151934 Recuperator with wire mesh
06/21/2012US20120151933 Method and system for feeding and ventilating with air a plant of an aircraft auxiliary power unit
06/21/2012US20120151932 Trapped vortex combustor and method of operating thereof
06/21/2012US20120151930 Fuel atomization dual orifice fuel nozzle
06/21/2012US20120151929 Aerodynamically enhanced fuel nozzle
06/21/2012US20120151928 Cooling flowpath dirt deflector in fuel nozzle
06/21/2012US20120151927 Pegless secondary fuel nozzle
06/21/2012US20120151895 Hot gas path component cooling for hybrid pulse detonation combustion systems
06/21/2012DE102011056566A1 Gasturbine und Verfahren für ihren Betrieb Gas turbine and method for its operation
06/21/2012DE102010063391A1 Lageranordnung für schnelldrehende Wellen von Maschinen Bearing assembly for high-speed shafts of machines
06/21/2012DE102010063197A1 Verdichter für die Aufladung einer Brennkraftmaschine Compressor for charging an internal combustion engine
06/21/2012DE102010054996A1 Lagereinheit für einen Turbolader Bearing unit for turbocharger
06/21/2012DE102010054939A1 Lageranordnung für einen Turbolader und Turbolader Bearing assembly for a turbocharger and turbocharger
06/21/2012DE102010054937A1 Lageranordnung für einen Turbolader Bearing assembly for a turbocharger
06/21/2012DE102010054926A1 Lagereinheit für einen Turbolader Bearing unit for turbocharger
06/21/2012DE102010054905A1 Lagereinheit für einen Turbolader Bearing unit for turbocharger
06/21/2012DE102010054904A1 Lagerkartusche für einen Turbolader Bearing cartridge for a turbocharger
06/21/2012DE102009053238B4 Turboladergehäuse mit einer Dichtungseinrichtung Turbocharger housing with a sealing device
06/21/2012CA2817189A1 Integrated method and apparatus for compressing air and producing carbon dioxide-rich fluid
06/21/2012CA2816512A1 Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
06/21/2012CA2762710A1 Gas turbine for aeronautic engines
06/21/2012CA2762496A1 Gas turbine bladed rotor for aeronautic engines and method for cooling said bladed rotor
06/20/2012EP2466097A1 Clustered inlet particle selector
06/20/2012EP2466096A1 Plant for the production of electric power and method for operating said plant
06/20/2012EP2466095A2 An acoustic liner
06/20/2012EP2465957A1 Ni-BASED MONOCRYSTALLINE SUPERALLOY AND TURBINE BLADE
06/20/2012EP2464846A1 Mitigation of optical signal noise using a multimode transmit fiber
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