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)
04/2013
04/11/2013US20130086906 Heat-exchange architecture built into the exhaust of a turbine engine
04/11/2013US20130086882 Power plant
04/10/2013EP2578844A2 Fuel system of a jet engine
04/10/2013EP2578843A2 Combined pump system for size reduction of thermal management heat exchangers and optimized ventilation to the aircraft cabin
04/10/2013EP2578842A2 Aircraft nacelle comprising a device for supplying hot air to a panel combining acoustic and ice treatments
04/10/2013EP2578841A2 System and method for conditioning air flow to a gas turbine
04/10/2013EP2578814A2 Gas turbine engine anti-icing mounting arrangements
04/10/2013EP2578813A1 Strut rods for structural guide vanes
04/10/2013EP2578810A1 Seal structure, turbine machine equipped with same, and power plant equipped with said turbine machine
04/10/2013EP2578802A1 Vibration damping blade for fluid
04/10/2013EP2578496A2 Acoustic treatment panel including hot-air channels and at least one annular channel
04/10/2013EP2578495A2 Acoustic treatment panel including hot-air channels and at least one stabilising chamber
04/10/2013EP2577024A1 Spark plug preheat
04/10/2013EP2576995A2 Gearbox in a turbomachine
04/10/2013CN202866995U Turbo-supercharger support
04/10/2013CN103038486A Electric power generation plant
04/10/2013CN103038485A Lateral turbojet improved in order to limit the deformation thereof
04/10/2013CN103038484A Multi-layer acoustic treatment panel
04/10/2013CN103032176A Stamping intercooling gas turbine
04/10/2013CN103032175A Method of heating gas turbine inlet
04/10/2013CN103032174A System and method for conditioning air flow to gas turbine
04/10/2013CN103032173A Conformal inlet apparatus for a gas turbine engine
04/10/2013CN103032172A Mist/Moisture removal using fixed bed trickle columns
04/10/2013CN103032171A Exhaust gas diffuser
04/10/2013CN102102586B Peak load power generation device
04/10/2013CN101813027B Bump air inlet method for realizing integration of unequal-strength wave system with forebody
04/09/2013US8413446 Fuel injector arrangement having porous premixing chamber
04/09/2013US8413443 Flow control through a resonator system of gas turbine combustor
04/09/2013CA2776318C Turbofan case and method of making
04/09/2013CA2776254C Turbofan case and method of making
04/09/2013CA2697121C Intentionally mistuned integrally bladed rotor
04/09/2013CA2672818C Nested bearing cages
04/09/2013CA2560561C Methods and apparatuses for assembling a gas turbine engine
04/09/2013CA2507192C Method for coating gas turbine engine components
04/07/2013CA2791024A1 Generator
04/07/2013CA2790958A1 Apparatus for generating power from a turbine engine
04/04/2013WO2013046825A1 Combustor tail pipe, gas turbine with tail pipe, and method for manufacturing tail pipe
04/04/2013WO2013021043A3 Gas turbine with heat exchanger
04/04/2013WO2011157398A3 Noise-reduced turbomachine
04/04/2013US20130084179 Variable vane angular position sensor
04/04/2013US20130084166 Segmented component
04/04/2013US20130084032 Bearing Housing for an Engine with Stress and Stiffness Control
04/04/2013US20130082446 Method of repairing rotating machine components
04/04/2013US20130081408 Method and apparatus for cooling gas turbine rotor blades
04/04/2013US20130081405 Guide and sealing device for a turbine engine, the device having a carbon gasket and an integrated smooth bearing
04/04/2013US20130081375 Conformal inlet apparatus for a gas turbine engine
04/04/2013DE112006001149B4 Verfahren und Vorrichtung für die Nasskompression Method and apparatus for the wet compression
04/04/2013DE10341758B4 Gasturbinenkraftwerk-regelmechanismus Gas turbine power plant-rule mechanism
04/04/2013DE102011083814A1 Segmentiertes Bauteil Segmented component
04/03/2013EP2574759A2 Motor-generator turbomachine starter
04/03/2013EP2574758A2 Conformal inlet apparatus for a gas turbine engine
04/03/2013EP2574731A2 Segmented component
04/03/2013CN202851706U Coupling assembly
04/03/2013CN202851156U Starting equipment of gas turbine engine
04/03/2013CN202851155U Heat-insulation pipe and aeroengine
04/03/2013CN103026031A Low emission triple-cycle power generation systems and methods
04/03/2013CN103026004A Turbine including seal air valve system
04/03/2013CN103016157A Fuel heating in combined cycle turbomachinery
04/03/2013CN103016156A System and method for monitoring the fuel to a gas turbine engine at forwarding skid
04/03/2013CN103016155A Ultrasonic water atomization system for gas turbine inlet cooling and wet compression
04/03/2013CN103016154A Nozzle cooling structure for testing ground gas turbine
04/03/2013CN103016153A Axial force adjusting device for rotor of gas turbine
04/03/2013CN103009024A Components with cooling channels and methods of manufacture
04/02/2013US8408282 Heat exchange device and method
04/02/2013US8408011 Structural reinforcement strut for gas turbine case
04/02/2013US8408010 Combustor wall apparatus with parts joined by mechanical fasteners
04/02/2013CA2776661C Turbofan case and method of making
04/02/2013CA2776404C Turbofan case and method of making
04/02/2013CA2776341C Turbofan case and method of making
04/02/2013CA2776317C Turbofan case and method of making
04/02/2013CA2776316C Turbofan case and method of making
04/02/2013CA2708458C Gas turbine with magnetic shaft forming part of a generator/motor assembly
04/02/2013CA2596805C Method for machining an integrally bladed rotor
04/02/2013CA2593917C Integral heater for fuel conveying member
03/2013
03/30/2013CA2790448A1 Conformal inlet apparatus for a gas turbine engine
03/28/2013WO2013044197A2 A combustor resonator section with an internalthermal barrier coating and method of fabricating the same
03/28/2013WO2013043754A1 Compressed gas energy storage system using turbine
03/28/2013WO2013041198A1 Heat shield for a turbocharger and arrangement of a heat shield between two housing parts of a turbocharger
03/28/2013WO2013007937A3 Method for manufacturing a turbine-engine fan casing having an acoustic coating
03/28/2013US20130078091 Sealing arrangement
03/28/2013US20130075976 Compliant mounting of an axial face seal assembly
03/28/2013US20130074518 Gas turbine engine tie rod retainer
03/28/2013US20130074517 Gas turbine engine mount assembly
03/28/2013US20130074516 Gas turbines
03/28/2013US20130074511 Method of operating a gas turbine and gas turbine
03/28/2013US20130074501 Combustor resonator section with an internal thermal barrier coating and method of fabricating the same
03/28/2013US20130074338 Pre-compressed seal including removable pre-compression member
03/28/2013US20130074334 Rotor centralization for turbine engine assembly
03/28/2013DE102012019477A1 Bearing arrangement for shaft at housing of exhaust gas turbocharger, has bearing elements, which are formed different from each other corresponding to its external dimensions, particularly their axial extensions or their external contours
03/28/2013DE102011114060A1 Hitzeschild für einen Abgasturbolader sowie Anordnung eines Hitzeschilds zwischen zwei Gehäuseteilen eines Abgasturboladers Heat shield for an exhaust gas turbocharger and arrangement of a heat shield between two housing parts of an exhaust gas turbocharger
03/28/2013DE102011053954A1 Abgasturbolader für eine Verbrennungskraftmaschine Exhaust gas turbocharger for an internal combustion engine
03/28/2013DE102009053102B4 Turbolader mit einer Axiallageranordnung für eine Welle des Turboladers Turbocharger with a thrust bearing assembly for a shaft of the turbocharger
03/28/2013CA2849436A1 Compressed gas energy storage system using turbine
03/28/2013CA2790439A1 Noise reduction in a turbomachine, and a related method thereof
03/27/2013EP2573366A2 System and method for monitoring the fuel fed to the fuel supply pumps of a gas turbine engine
03/27/2013EP2573365A2 Gas turbine inlet air cooling system using ultrasonic water atomization, corresponding cooling method and wet compression system
03/27/2013EP2573360A2 Fuel heating in combined cycle turbomachinery
03/27/2013EP2573331A2 Inlet fluid flow and impingement angle control
03/27/2013EP2572093A2 Multi-layer acoustic treatment panel
03/27/2013CN202832797U Start-up system of gas turbine based on frequency changer
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