| 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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| 01/08/2013 | US8347598 Apparatus for starting up combined cycle power systems and method for assembling same |
| 01/08/2013 | CA2713168C Exhaust washed structure and associated composite structure and method of fabrication |
| 01/08/2013 | CA2657252C Gas turbine aircraft engine with power variability |
| 01/08/2013 | CA2606854C Inertial particle separator for compressor shroud bleed |
| 01/08/2013 | CA2526717C Multiform film cooling holes |
| 01/08/2013 | CA2499575C A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines |
| 01/08/2013 | CA2488436C "get home" oil supply and scavenge system |
| 01/08/2013 | CA2486500C Attachment device linking an engine and an aircraft wing |
| 01/08/2013 | CA2206885C Acoustic chamber |
| 01/03/2013 | WO2013003411A1 Acoustic panel and associated assembly method |
| 01/03/2013 | WO2013002950A1 System and method for driving a pump |
| 01/03/2013 | WO2013001246A1 Arrangement for connecting a duct to an air-distribution casing |
| 01/03/2013 | WO2013001238A1 Improved housing for the accessory relay of a gas turbine |
| 01/03/2013 | WO2012017247A3 Gas turbine apparatus with improved exergy recovery |
| 01/03/2013 | US20130004306 Chordal mounting arrangement for low-ductility turbine shroud |
| 01/03/2013 | US20130000323 Differential gear system with carrier drive |
| 01/03/2013 | US20130000318 Ecology system for draining the manifold of a gas turbine engine |
| 01/03/2013 | US20130000317 Mechanism for turbine engine start from low spool |
| 01/03/2013 | US20130000313 Hydraulic fluid transfer coupling |
| 01/03/2013 | US20130000312 Turbomachine combustor assembly including a vortex modification system |
| 01/03/2013 | US20130000311 Gas turbine engine staged fuel injection |
| 01/03/2013 | US20130000310 Flow sleeve impingement cooling baffles |
| 01/03/2013 | US20130000308 Diffuser Pipe and Assembly for Gas Turbine Engine |
| 01/03/2013 | US20130000307 Swirler for gas turbine engine fuel injector |
| 01/03/2013 | US20130000306 Gas turbine combustion burner |
| 01/03/2013 | US20130000305 Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine |
| 01/03/2013 | DE102012105681A1 Verdrehsichere Biegeaufhängungen von Dichtungsanordnungen Twist-bending suspensions of sealing arrangements |
| 01/03/2013 | DE102012105504A1 Turbomaschine mit Flussabweisungssystem Turbomachinery flow rejection system |
| 01/03/2013 | DE102010045712B4 Turbomaschinengehäuse Turbo machine housing |
| 01/03/2013 | CA2839985A1 Improved housing for the accessory relay of a gas turbine |
| 01/03/2013 | CA2838345A1 Acoustic panel and associated assembly method |
| 01/02/2013 | EP2541180A1 Heat exchanger |
| 01/02/2013 | EP2541024A2 APU fuel system and method |
| 01/02/2013 | EP2541023A2 Ecology valve for draining a manifold of a gas turbine engine, fuel system and method for draining fuel |
| 01/02/2013 | EP2541022A2 Gas turbine inlet heating system |
| 01/02/2013 | EP2541020A2 System for ventilating a gas turbine enclosure |
| 01/02/2013 | EP2540993A1 Aircraft gas turbine |
| 01/02/2013 | EP2540991A2 Mechanism for turbine engine start from low spool |
| 01/02/2013 | EP2540990A2 Seal assembly for a rotational fluid metering valve |
| 01/02/2013 | EP2539547A1 Turbomachine comprising a vertical shaft |
| 01/02/2013 | CN202645738U Plasma igniter and combustion gas turbine |
| 01/02/2013 | CN202645737U Fuel oil adjusting device |
| 01/02/2013 | CN202645736U APU core machine |
| 01/02/2013 | CN202645735U Transmission device and gas turbine with same |
| 01/02/2013 | CN102859242A Method for fabricating shaft sealing device and jig for fabricating shaft sealing device, and rotary machine provided with shaft sealing device |
| 01/02/2013 | CN102859147A Method for removal of entrained gas in a combined cycle power generation system |
| 01/02/2013 | CN102858634A Unit for an aircraft thruster |
| 01/02/2013 | CN102858632A Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means |
| 01/02/2013 | CN102852646A Multifunctional gas turbine module with functions of fire fighting, heat insulating, ventilating and sound insulating |
| 01/02/2013 | CN102852645A System for fuel gas moisturization and heating |
| 01/02/2013 | CN102852644A Gas turbine inlet heating system |
| 01/02/2013 | CN102851633A Method of maintaining surface-related properties of gas turbine combustor components |
| 01/01/2013 | US8342444 Fail safe extended torque box strut-to-wing mount |
| 12/27/2012 | WO2012177372A1 Phase and amplitude matched fuel injector |
| 12/27/2012 | WO2012176759A1 Gas turbine, and method for repairing gas turbine |
| 12/27/2012 | WO2012176662A1 Fuel generation system and power generation system |
| 12/27/2012 | WO2012176373A1 Rotor for turbine, process for producing same, method for bonding ni-based superalloy material to steel material, and structure |
| 12/27/2012 | WO2012176257A1 Closed-cycle gas turbine |
| 12/27/2012 | WO2012175884A1 Accessory relay having an extended service life |
| 12/27/2012 | WO2012175883A1 Ventilation of an accessory gear box, and turbojet engine comprising such a gear box |
| 12/27/2012 | WO2012175850A1 Turbomachine casing acoustic panels fitted with improved attachment devices |
| 12/27/2012 | US20120328427 Fireshield fastener hood |
| 12/27/2012 | US20120325325 Supersonic engine inlet diffuser with deployable vortex generators |
| 12/27/2012 | US20120324907 Mounting assembly |
| 12/27/2012 | US20120324906 Heat protection system |
| 12/27/2012 | US20120324905 Apu fuel system and method |
| 12/27/2012 | US20120324902 Method of maintaining surface-related properties of gas turbine combustor components |
| 12/27/2012 | US20120324900 Phase and amplitude matched fuel injector |
| 12/27/2012 | US20120324899 Oil bypass channel deaerator for a geared turbofan engine |
| 12/27/2012 | US20120324896 Premixer fuel nozzle for gas turbine engine |
| 12/27/2012 | US20120324895 Fuel supply device of gas turbine engine |
| 12/27/2012 | US20120324863 Cooling scheme for an increased gas turbine efficiency |
| 12/27/2012 | US20120324859 Heat exchanger |
| 12/27/2012 | DE102011003905B4 Abgasturbolader mit gekühltem Turbinengehäuse und gekühltem Lagergehäuse und gemeinsamer Kühlmittelzufuhr Exhaust gas turbocharger with cooled turbine housing and cooled bearing housing and common coolant supply |
| 12/27/2012 | DE102010049541B4 Laufschaufel für eine Strömungsmaschine Blade for a turbomachine |
| 12/27/2012 | CA2834753A1 Turbine engine rotor, method of producing the same, method of joining ni-based superalloy member and steel member, and junction structure of ni-based superalloy member and steel member |
| 12/26/2012 | EP2538199A2 Signal processing for inlet debris monitoring system to distinguish particulates |
| 12/26/2012 | EP2538057A2 Gearbox comprising a fail-safe manual rotator cover |
| 12/26/2012 | EP2538056A2 A heat protection assembly |
| 12/26/2012 | EP2538055A2 Oil bypass channel deaerator for a geared turbofan engine |
| 12/26/2012 | EP2538054A1 Structure for gas turbine casing |
| 12/26/2012 | EP2538023A2 Pressure and temperature actuation system |
| 12/26/2012 | EP2538022A2 Non-mechanically fastened TOBI heat shield |
| 12/26/2012 | EP2537754A1 Method for producing an acoustic treatment panel including channels adjacent to a cellular structure |
| 12/26/2012 | EP2537753A1 Method for producing an acoustic treatment panel including the function of de-icing with hot air |
| 12/26/2012 | EP2536935A2 Coil arrangements for air intake system for gas turbine and methods |
| 12/26/2012 | CN202628279U Binary hypersonic speed-variable geometric air inlet channel |
| 12/26/2012 | CN202628278U Miniature turbojet engine starting system |
| 12/26/2012 | CN202620786U Oil treating sledge for double-fuel turbine power station in oil and gas field |
| 12/26/2012 | CN202620785U Gas treating sledge for double-fuel turbine power station in oil and gas field |
| 12/26/2012 | CN102840034A Fluid leak detection system |
| 12/26/2012 | CN102840032A Inlet air pulse filtration system |
| 12/26/2012 | CN102839992A Component with cooling channels and manufacturing method |
| 12/26/2012 | CN101796304B Fluid intake assembly |
| 12/26/2012 | CN101135250B Heat pipe-based cooling apparatus and method for turbine engine |
| 12/25/2012 | US8340886 System and method for transitioning between fuel supplies for a combustion system |
| 12/25/2012 | US8336812 Engine attachment for an assembly system mounted between an attachment strut and an aircraft engine |
| 12/25/2012 | US8336317 Ventilation for a turbine wheel in a turbine engine |
| 12/25/2012 | US8336313 Fuel distributor |
| 12/25/2012 | US8336312 Attenuation of combustion dynamics using a Herschel-Quincke filter |