| 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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| 01/31/2014 | CA2822511A1 Electric heater for integration into an aircraft acoustic panel |
| 01/30/2014 | WO2014018963A1 Turbine engine combustor and stator vane assembly |
| 01/30/2014 | WO2014018385A1 Gas turbine engine exhaust duct |
| 01/30/2014 | WO2014018383A1 Top hat bearing retainer for variable vane actuator |
| 01/30/2014 | WO2014018382A1 Geared fan with inner counter rotating compressor |
| 01/30/2014 | WO2014018277A1 Flexible combustor bracket |
| 01/30/2014 | WO2014018199A1 Integrated nacelle inlet and metallic fan containment case |
| 01/30/2014 | WO2014018138A2 Airfoil cooling circuits |
| 01/30/2014 | WO2014018137A2 Aircraft engine driveshaft vessel assembly and method of assembling the same |
| 01/30/2014 | WO2014018126A2 High pressure muffling devices |
| 01/30/2014 | WO2014017585A1 Engine duct, and aircraft engine |
| 01/30/2014 | WO2014017217A1 System for low-concentration-methane gas oxidation equipped with multiple oxidizers |
| 01/30/2014 | WO2014016498A1 Internal and/or external combustion turbine engine |
| 01/30/2014 | WO2013007937A8 Method for manufacturing a turbine-engine fan casing having an acoustic coating |
| 01/30/2014 | US20140031163 Fan drive gear system torque frame pin retainer |
| 01/30/2014 | US20140030087 Thrust reverser-integrated track beam and inner fixed structure |
| 01/30/2014 | US20140026974 Process of manufacturing a turbojet engine nacelle part |
| 01/30/2014 | US20140026700 Accessory gearbox device for a jet engine |
| 01/30/2014 | US20140026592 Assembly for a jet engine of an aircraft |
| 01/30/2014 | US20140026591 Axial retention for fasteners in fan joint |
| 01/30/2014 | US20140026590 Flexible combustor bracket |
| 01/30/2014 | US20140026589 Aircraft engine |
| 01/30/2014 | US20140026587 Gas turbine controller and a method for controlling a gas turbine |
| 01/30/2014 | US20140026585 Ceramic-to-metal turbine volute attachment for a gas turbine engine |
| 01/30/2014 | US20140026562 Turbine for an internal combustion engine |
| 01/30/2014 | DE102012106354A1 Method for manufacturing e.g. hollow-profiled rotationally-symmetrical component used in e.g. jet engine, involves depositing and simultaneous pressing the molten semi-finished material onto tool to wrap the material around tool |
| 01/29/2014 | EP2690365A1 Acoustic damper, combustor, and gas turbine |
| 01/29/2014 | EP2247906B1 Heat accumulator |
| 01/29/2014 | EP2034159B1 Active flow control for nacelle air intake |
| 01/29/2014 | EP2000648B1 Cooling device for a gas turbine engine and corresponding gas turbine engine |
| 01/29/2014 | CN203412665U Air treatment device for improving efficiency of gas turbine |
| 01/29/2014 | CN103547779A Method for rationalising a chain of electric components of an aircraft, implementation architecture and corresponding aircraft |
| 01/29/2014 | CN103547402A Friction bonding method and bonding structure |
| 01/29/2014 | CN103541832A Engine fuel supplying system |
| 01/29/2014 | CN102678339B Plasma igniter with reusable cathode |
| 01/29/2014 | CN102606313B 冷却装置 Cooling device |
| 01/29/2014 | CN102518516B Integral compressed air energy storage and coal gasification power generation system and integrated power generation method |
| 01/29/2014 | CN102434286B Efficient compact primary surface heat regenerator with low pressure loss |
| 01/29/2014 | CN101952171B Aircraft propulsion assembly comprising hot air bleed systems |
| 01/29/2014 | CN101846101B 进口空气加热和冷却系统 The inlet air heating and cooling system |
| 01/29/2014 | CN101832181B Novel film cooling hole with anti-whorl hole branch structure |
| 01/29/2014 | CN101749116B Low-grade heat recovery system for air inlet of turbine |
| 01/28/2014 | US8635876 Gas turbine for a thermal power plant, and method for operating such a gas turbine |
| 01/28/2014 | US8635874 Gas turbine combustor including an acoustic damper device |
| 01/28/2014 | US8635849 Method and system for introducing fluid into an airstream |
| 01/28/2014 | CA2607245C Bearing arrangement of a rotating shaft and turbojet equipped with such an arrangement |
| 01/28/2014 | CA2564488C Device for extracting mechanical power between the hp and lp shafts of a twin-spool turbine engine |
| 01/28/2014 | CA2557073C Device for heating a cylindrical part, to be used in the assembly of an inter-shaft bearing in a turbine engine |
| 01/28/2014 | CA2544784C Turbine module for gas turbine starter |
| 01/24/2014 | CA2794646A1 Turbinaltm apparatus for purging hydrogen cooling gas from a turbine and high flow co2 delivery system |
| 01/23/2014 | WO2014015142A1 Bayoneted anti-rotation turbine seals |
| 01/23/2014 | WO2014014872A1 Clearance control for gas turbine engine seal |
| 01/23/2014 | WO2014014870A1 Damped egt probe |
| 01/23/2014 | WO2014014773A1 First stage compressor disk configured for balancing the compressor rotor assembly |
| 01/23/2014 | WO2014014762A1 Blade outer air seal with cooling features |
| 01/23/2014 | WO2014014760A1 Blade outer air seal having inward pointing extension |
| 01/23/2014 | WO2014014750A1 Joint between airfoil and shroud |
| 01/23/2014 | WO2014014675A1 Gas turbine engine outer case with contoured bleed boss |
| 01/23/2014 | WO2014014598A1 Radial position control of case supported structure |
| 01/23/2014 | WO2014014596A1 Gearbox for gas turbine engine |
| 01/23/2014 | WO2014014550A1 Pmc laminate embedded hypotube lattice |
| 01/23/2014 | WO2014014539A2 Blade dovetail bottom |
| 01/23/2014 | WO2014014538A2 Manifold for gas turbine engine |
| 01/23/2014 | WO2014014536A2 Systems and methods for preventing fuel leakage in a gas turbine engine |
| 01/23/2014 | WO2014014535A2 Air accelerator on tie rod within turbine disk bore |
| 01/23/2014 | WO2014013741A1 Turbine and electric power generation system |
| 01/23/2014 | WO2014013201A1 Device for the transfer of heat between a lubrication pipe and a turbomachine blade pitch actuator control hydraulic pipe |
| 01/23/2014 | WO2014013170A1 Cooling of an oil circuit of a turbomachine |
| 01/23/2014 | WO2013180797A3 Shark-bite tip shelf cooling configuration |
| 01/23/2014 | WO2013180789A3 Pump system for hpc ecs parasitic loss elimination |
| 01/23/2014 | WO2013180788A3 Constant speed pump system for engine ecs loss elimination |
| 01/23/2014 | WO2013165523A3 Bypass duct with angled drag links |
| 01/23/2014 | WO2013165515A3 Gas turbine engine with fan-tied inducer section |
| 01/23/2014 | WO2013165495A3 Apparatus and method for optically measuring creep |
| 01/23/2014 | WO2013158192A3 Internally cooled spoke |
| 01/23/2014 | US20140023787 Thermal barrier coating method, masking pin and combustor transition piece |
| 01/23/2014 | US20140023489 Seal assembly and gas turbine having the same |
| 01/23/2014 | US20140023480 Radial position control of case supported structure |
| 01/23/2014 | US20140021325 Transport securing device of an aircraft gas turbine |
| 01/23/2014 | US20140020404 Fundamental gear system architecture |
| 01/23/2014 | US20140020401 Method for conditioning a power supply for starting a jet engine |
| 01/23/2014 | US20140020394 System and method for turbomachine housing ventilation |
| 01/23/2014 | DE102012014109A1 Washer seal for use in gas turbine engine, has sealing ring, which is arranged between radially outer sections of rotor disks and is clamped between rotor disks in axial direction, where sealing elements are arranged on sealing ring |
| 01/22/2014 | EP2687703A2 Turbine using CO2 as working fluid |
| 01/22/2014 | EP2686522A1 System and method for operating a precooler in an aircraft |
| 01/22/2014 | CN103534531A Combustor for gas turbine engine and gas turbine |
| 01/22/2014 | CN103527714A Integrated drive generator gear alignment |
| 01/22/2014 | CN103527321A Transition duct for a combustor of a gas turbine |
| 01/22/2014 | CN102227545B Turbine blade including seal pocket |
| 01/21/2014 | US8631656 Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities |
| 01/21/2014 | US8631655 Gas turbine engine including apparatus to transfer power between multiple shafts |
| 01/21/2014 | US8631654 Burner system and method for damping such a burner system |
| 01/21/2014 | US8631639 System and method of cooling turbine airfoils with sequestered carbon dioxide |
| 01/21/2014 | US8631638 Method, system and apparatus for providing water to a heat engine via a dammed water source |
| 01/21/2014 | US8631637 Auxiliary power unit fire enclosure |
| 01/21/2014 | US8631557 Laser drilling methods of shallow-angled holes |
| 01/19/2014 | CA2817298A1 Gas turbine |
| 01/16/2014 | WO2014011983A1 Vane insertable tie rods with keyed connections |
| 01/16/2014 | WO2014011982A1 Mid-turbine frame with oil system mounts |
| 01/16/2014 | WO2014011979A1 Mid-turbine frame with threaded spokes |