| 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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| 09/25/2014 | WO2014152101A1 Turbofan engine bearing and gearbox arrangement |
| 09/25/2014 | WO2014151785A1 Turbofan engine bearing and gearbox arrangement |
| 09/25/2014 | WO2014151685A1 Gas turbine engine with air-oil cooler oil tank |
| 09/25/2014 | WO2014151673A1 Aerodynamic track fairing for a gas turbine engine fan nacelle |
| 09/25/2014 | WO2014151470A1 Fan axial containment system |
| 09/25/2014 | WO2014151425A1 Instrumentation transfer strut |
| 09/25/2014 | WO2014151356A1 Geared architecture turbofan engine thermal management system and method |
| 09/25/2014 | WO2014151299A1 Gas turbine engine turbine vane rail seal |
| 09/25/2014 | WO2014151275A1 Nacelle mounted latching system |
| 09/25/2014 | WO2014151239A1 Gas turbine engine component cooling channels |
| 09/25/2014 | WO2014151176A1 Turbofan engine main bearing arrangement |
| 09/25/2014 | WO2014151101A1 Turbine blade tip treatment for industrial gas turbines |
| 09/25/2014 | WO2014151099A1 Structural guide vane leading edge |
| 09/25/2014 | WO2014151097A1 Reinforced composite case |
| 09/25/2014 | WO2014151036A1 Radial pleat design and collapsible filter element |
| 09/25/2014 | WO2014150954A1 Gas turbine engine stator vane assembly with split shroud |
| 09/25/2014 | WO2014150681A1 Gas turbine engine component having shaped pedestals |
| 09/25/2014 | WO2014150490A1 Additive manufacturing method for the addition of features within cooling holes |
| 09/25/2014 | WO2014150489A1 Gas turbine engine with low fan noise |
| 09/25/2014 | WO2014150420A1 Speed sensor probe location in gas turbine engine |
| 09/25/2014 | WO2014150377A1 Electrically coupled counter-rotation for gas turbine compressors |
| 09/25/2014 | WO2014150353A1 Low leakage duct segment using expansion joint assembly |
| 09/25/2014 | WO2014150335A1 Multiple coating configuration |
| 09/25/2014 | WO2014150187A1 Turbine engine face seal arrangement including anti-rotation features |
| 09/25/2014 | WO2014150182A1 Interlocking rotor assembly with thermal shield |
| 09/25/2014 | WO2014149604A1 Apu exhaust system |
| 09/25/2014 | WO2014149366A1 Injection molded composite fan platform |
| 09/25/2014 | WO2014149354A1 Geared turbofan engine having a reduced number of fan blades and improved acoustics |
| 09/25/2014 | WO2014149353A1 Cyclonic dirt separating turbine accelerator |
| 09/25/2014 | WO2014149292A1 Titanium aluminide turbine exhaust structure |
| 09/25/2014 | WO2014149260A1 Fan blade root integrated sealing solution |
| 09/25/2014 | WO2014149253A1 Knife edge with increased crack propagation life |
| 09/25/2014 | WO2014149121A2 Clutch coupled to gas turbine engine and method for cooling |
| 09/25/2014 | WO2014149110A2 Seals for a gas turbine engine |
| 09/25/2014 | WO2014149105A1 Compartment shielding |
| 09/25/2014 | WO2014149104A1 Lock for retaining minidisks with rotors of a gas turbine engine |
| 09/25/2014 | WO2014149100A1 Heat exchanger integrated with a gas turbine engine and adaptive flow control |
| 09/25/2014 | WO2014148166A1 Combustor and gas turbine |
| 09/25/2014 | WO2014146955A1 Sealing element for sealing a gap |
| 09/25/2014 | WO2014146954A1 Sealing element for sealing a gap |
| 09/25/2014 | WO2014146866A1 Sealing element for sealing a gap and corresponding gas turbine |
| 09/25/2014 | WO2014146854A1 Gas turbine and method for operating the gas turbine |
| 09/25/2014 | US20140287367 Method for Operating a Combustor |
| 09/25/2014 | US20140286764 Composite panel having a built-in sampling scoop |
| 09/25/2014 | US20140286763 Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavity |
| 09/25/2014 | US20140286760 Seal assembly including grooves in an inner shroud in a gas turbine engine |
| 09/25/2014 | US20140286755 Ring gear mounting arrangement with oil scavenge scheme |
| 09/25/2014 | US20140286754 Elongated Geared Turbofan With High Bypass Ratio |
| 09/25/2014 | US20140283529 Supporting device for gas turbine and gas turbine with the same |
| 09/25/2014 | US20140283528 Aftertreatment Module and Method of Assembly |
| 09/25/2014 | US20140283524 Nozzle system and method for starting and operating gas turbines on lowbtu fuels |
| 09/25/2014 | US20140283519 Rotary wing aircraft with a hybrid power plant |
| 09/25/2014 | DE102014100571A1 Düsensystem und Verfahren zum Start und Betrieb von Gasturbinen mit niedrigenergetischen Kraftstoffen Nozzle system and method for starting and operating gas turbines with low-energy fuels |
| 09/25/2014 | DE102008031986B4 Gasturbine mit gegenläufigen Verdichtermodulen Gas turbine with counter-rotating compressor modules |
| 09/24/2014 | EP2781838A1 Gas turbine combustor |
| 09/24/2014 | EP2781720A1 Power plant assembly and method for generating electric energy and network supply |
| 09/24/2014 | EP2781700A2 Supporting device for gas turbine |
| 09/24/2014 | EP2781698A1 Gas turbine and method for operating the gas turbine |
| 09/24/2014 | EP2780570A1 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
| 09/24/2014 | EP2780554A1 Device and method for slow turning of an aeroderivative gas turbine |
| 09/23/2014 | US8840061 Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut |
| 09/23/2014 | US8840059 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 09/23/2014 | US8839805 Passive boundary layer bleed system for nacelle inlet airflow control |
| 09/23/2014 | US8839628 Methods for operating a gas turbine engine apparatus and assembling same |
| 09/23/2014 | US8839625 Gas turbine engine diffuser having air flow channels with varying widths |
| 09/23/2014 | US8839624 Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators |
| 09/23/2014 | US8839600 Igniter for a rocket engine, method for ignition of a rocket engine |
| 09/23/2014 | CA2720387C Gasification power generation system provided with carbon dioxide separation and recovery device |
| 09/23/2014 | CA2597938C Aircraft engine fuel supply |
| 09/18/2014 | WO2014144023A1 Engine wash collector |
| 09/18/2014 | WO2014143934A1 Floating blade outer air seal assembly for gas turbine engine |
| 09/18/2014 | WO2014143874A1 Vibration damping for structural guide vanes |
| 09/18/2014 | WO2014143831A1 Coated articles and manufacture methods |
| 09/18/2014 | WO2014143785A1 Coated articles and manufacture methods |
| 09/18/2014 | WO2014143372A1 Power-generating apparatus and method |
| 09/18/2014 | WO2014143305A1 Low speed fan for gas turbine engines |
| 09/18/2014 | WO2014143296A1 Splitter for air bleed manifold |
| 09/18/2014 | WO2014143294A1 Distributed engine accessory drive |
| 09/18/2014 | WO2014143293A1 Sequencing of multi-pass laser shock peening applications |
| 09/18/2014 | WO2014143292A1 Fan airfoil shrouds with area ruling in the shrouds |
| 09/18/2014 | WO2014143290A1 Off-cambered vanes for gas turbine engines |
| 09/18/2014 | WO2014143288A1 Modular mount assembly |
| 09/18/2014 | WO2014143286A1 Fan blade lubrication |
| 09/18/2014 | WO2014143284A1 Vibration damping apparatus for hydrostatic seal of gas turbine engine |
| 09/18/2014 | WO2014143283A1 Airfoil with thickened root and fan and engine incorporating same |
| 09/18/2014 | WO2014143282A1 Air-oil heat exchangers with minimum bypass flow pressure loss |
| 09/18/2014 | WO2014143281A1 Asymmetric fan nozzle in high-bpr separate-flow nacelle |
| 09/18/2014 | WO2014143280A1 Gas turbine blade array with reduced acoustic output |
| 09/18/2014 | WO2014143268A1 T-shaped platform leading edge anti-rotation tabs |
| 09/18/2014 | WO2014143267A1 Gas turbine engine with low fan noise |
| 09/18/2014 | WO2014143266A1 Turbine engine component with vibration damping |
| 09/18/2014 | WO2014143265A1 Hybrid fan blade biscuit construction |
| 09/18/2014 | WO2014143264A1 Engine inlet total air temperature sensor |
| 09/18/2014 | WO2014143263A1 Multi-airfoil split and rejoin method |
| 09/18/2014 | WO2014143262A1 Locally extended leading edge sheath for fan airfoil |
| 09/18/2014 | WO2014143256A1 Frangible sheath for a fan blade of a gas turbine engine |
| 09/18/2014 | WO2014143255A1 De-icing by integral electric heat generation |
| 09/18/2014 | WO2014143248A1 Ultra high bypass ratio turbofan engine |
| 09/18/2014 | WO2014143224A1 Turbine engine repair methods |
| 09/18/2014 | WO2014143219A1 Engine health monitoring and power allocation control for a turbine engine using electric generators |