| 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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| 11/14/2013 | WO2013167529A1 Energy-optimised jet propulsion method and jet engine for performing same |
| 11/14/2013 | US20130300067 System for sealing a gas path in a turbine |
| 11/14/2013 | US20130298569 Gas turbine and method for operating said gas turbine |
| 11/14/2013 | US20130298567 Method and apparatus for generating motive power |
| 11/14/2013 | US20130298566 Electrical raft with map |
| 11/14/2013 | US20130298562 Fuel Injector With Mixing Circuit |
| 11/14/2013 | US20130298560 System for supplying a working fluid to a combustor |
| 11/14/2013 | DE102012207660A1 Shaft assembly for turbocharger, has turbocharger shaft rotatably mounted by bearing assembly that is provided with water lubrication, where bearing element of bearing assembly is partially coated with amorphous carbon coating |
| 11/13/2013 | EP2662553A2 Cooling medium supply system and method |
| 11/13/2013 | EP2662532A2 Turbine assembly with expansion seal |
| 11/13/2013 | EP2662286A2 Method of supplying auxiliary power from an auxiliary power unit and corresponding architecture |
| 11/13/2013 | EP2661543A1 Expansion turbine |
| 11/13/2013 | CN203289247U Noise reduction casing for generator of gas turbine set |
| 11/13/2013 | CN203285545U Zero-duty fuel operation system for gas turbine |
| 11/13/2013 | CN103392059A Turbomachine comprising a privileged injection device and corresponding injection method |
| 11/13/2013 | CN103388531A Auxiliary power supply process by an auxiliary power group and corresponding architecture |
| 11/13/2013 | CN103388530A Fuel injector with mixing circuit |
| 11/13/2013 | CN103388529A Fixture and method for adjusting workpiece |
| 11/13/2013 | CN102224332B Gas turbine with external combustion, applying a rotating regenerating heat exchanger |
| 11/13/2013 | CN101978197B Rotating machine and additional ring |
| 11/13/2013 | CN101900032B Gas turbine engine cooling system and method |
| 11/12/2013 | US8578720 Particle separator in a gas turbine engine |
| 11/12/2013 | US8578718 Cartridge for the generation of hydrogen for providing mechanical power |
| 11/12/2013 | US8578715 Gas turbine, method of controlling air supply and computer program product for controlling air supply |
| 11/12/2013 | US8578696 Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine |
| 11/12/2013 | CA2729130C Double flow compressor |
| 11/12/2013 | CA2663076C Method and apparatus for production of a cast component |
| 11/12/2013 | CA2637901C Air inlet shroud structure |
| 11/11/2013 | CA2814473A1 Geared fan assembly |
| 11/07/2013 | WO2013166284A1 Shaped rim cavity wing surface |
| 11/07/2013 | WO2013166084A1 Gas turbine and gas turbine afterburner |
| 11/07/2013 | WO2013166060A1 High velocity combustor |
| 11/07/2013 | WO2013165960A1 Water quench for gasifier |
| 11/07/2013 | WO2013165868A1 Gas turbine engine combustor surge retention |
| 11/07/2013 | WO2013165865A1 Hollow fan blade with braided fabric tubes |
| 11/07/2013 | WO2013165790A1 Extraction tool assembly |
| 11/07/2013 | WO2013165771A1 Geared turbofan with distributed accessory gearboxes |
| 11/07/2013 | WO2013165769A1 Manifold for geared turbofan engine |
| 11/07/2013 | WO2013165524A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case |
| 11/07/2013 | WO2013165523A2 Bypass duct with angled drag links |
| 11/07/2013 | WO2013165521A2 Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections |
| 11/07/2013 | WO2013165518A2 Gas turbine engine component with cusped, lobed cooling hole |
| 11/07/2013 | WO2013165517A2 Gas turbine engine component with diffusive cooling hole |
| 11/07/2013 | WO2013165515A2 Gas turbine engine with fan-tied inducer section |
| 11/07/2013 | WO2013165513A2 Counter-rotating low pressure turbine without turbine exhaust case |
| 11/07/2013 | WO2013165512A2 Variable area turbine |
| 11/07/2013 | WO2013165511A2 Edm method for multi-lobed cooling hole |
| 11/07/2013 | WO2013165510A2 Multi-lobed cooling hole and method of manufacture |
| 11/07/2013 | WO2013165509A2 Multi-lobed cooling hole |
| 11/07/2013 | WO2013165508A2 Multi-lobed cooling hole array |
| 11/07/2013 | WO2013165507A2 Cooling hole with asymmetric diffuser |
| 11/07/2013 | WO2013165506A2 Cooling hole with crenellation features |
| 11/07/2013 | WO2013165505A2 Composite fan containment case assembly |
| 11/07/2013 | WO2013165504A2 Manufacturing methods for multi-lobed cooling holes |
| 11/07/2013 | WO2013165503A2 Cooling hole with enhanced flow attachment |
| 11/07/2013 | WO2013165502A2 Cooling hole with thermo-mechanical fatigue resistance |
| 11/07/2013 | WO2013165495A2 Apparatus and method for optically measuring creep |
| 11/07/2013 | WO2013165487A2 Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure |
| 11/07/2013 | WO2012079694A3 Method for operating a small gas turbine assembly and small gas turbine assembly |
| 11/07/2013 | US20130294893 Actuation system for a propulsive unit of an airplane |
| 11/07/2013 | US20130294889 Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations |
| 11/07/2013 | US20130292202 Method for repairing at least a portion of an accoustic panel |
| 11/07/2013 | US20130291553 Integrated thermal protection and leakage reduction in a supersonic air intake system |
| 11/07/2013 | US20130291552 Electrical control of combustion |
| 11/07/2013 | US20130291551 Method for starting a turbomachine |
| 11/07/2013 | US20130291547 Purge method and purge unit for gas turbine combustor |
| 11/07/2013 | US20130291546 Injection device for a turbine engine combustion chamber |
| 11/07/2013 | US20130291545 Method and apparatus for isolating inactive fuel passages |
| 11/07/2013 | US20130291514 Gas turbine engine oil tank |
| 11/07/2013 | US20130291513 Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same |
| 11/07/2013 | DE102011104446B4 Kühlvorrichtung für einen Turbolader eines Motors für ein Fahrzeug Cooling device for a turbocharger of an engine for a vehicle |
| 11/07/2013 | DE102011005347B4 Turbine mit einem Magnetlager und Verfahren zum Betreiben der Turbine Turbine comprising a magnetic bearing, and method of operating the turbine |
| 11/06/2013 | EP2660443A2 Turbine component cooling system |
| 11/06/2013 | EP2660442A2 Integrated thermal protection and leakage reduction in a supersonic air intake system |
| 11/06/2013 | EP2660441A2 Gas turbine air processing system |
| 11/06/2013 | EP2660440A2 Electro-magnetic coupling system |
| 11/06/2013 | EP2660430A1 Shaft sealing device, and rotary machine equipped therewith |
| 11/06/2013 | EP2659111A1 System, propulsion system and vehicle |
| 11/06/2013 | EP2659110A1 Supercritical or mixed phase multi-port fuel injector |
| 11/06/2013 | CN203271955U Energy-saving device of internal/external combustion engine |
| 11/06/2013 | CN103384755A EM energy application for combustion engines |
| 11/06/2013 | CN103384753A Turbine comprising a sealing device between the stator blade carrier and the housing |
| 11/06/2013 | CN103382896A Wear combination for starter air valve |
| 11/06/2013 | CN103382895A 燃气涡轮空气处理系统 Gas turbine air handling system |
| 11/06/2013 | CN103382857A Gas turbine blade and gas turbine equipped with the same |
| 11/06/2013 | CN102257260B System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 11/06/2013 | CN102076941B Gas turbine device |
| 11/06/2013 | CN101978138B Gas turbine |
| 11/06/2013 | CN101970807B Centrifugal oil separator having variable channel section |
| 11/06/2013 | CN101970802B Cover for cooling passage, method of manufacturing the cover, and gas turbine |
| 11/06/2013 | CN101765708B Intake air heating control device for gas turbine |
| 11/06/2013 | CN101646601B Lockable guiding system for a mobile part of a nacelle |
| 11/05/2013 | US8573291 Compact radial counterflow recuperator |
| 11/05/2013 | US8572987 Fuel injector mounting system |
| 11/05/2013 | US8572984 Breather duct shielding |
| 11/05/2013 | US8572982 Diffuser having distribution element for providing part-flow |
| 11/05/2013 | US8572977 Combustor of a gas turbine engine |
| 11/05/2013 | US8572975 Systems relating to turbine engine control and operation |
| 11/05/2013 | US8572943 Fundamental gear system architecture |
| 11/02/2013 | CA2814469A1 Air cooler system for gas turbine engines |