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