| 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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| 06/25/2013 | US8468831 Lean direct injection for premixed pilot application |
| 06/25/2013 | CA2558897C Redundant fuel manifold sealing arrangement |
| 06/25/2013 | CA2502810C Turbine shroud cooling system |
| 06/25/2013 | CA2491437C Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 06/22/2013 | CA2799018A1 Gas turbine engine systems |
| 06/22/2013 | CA2799004A1 Electrical grounding plane |
| 06/22/2013 | CA2799000A1 Method of servicing a gas turbine engine |
| 06/22/2013 | CA2798998A1 Electrical harness |
| 06/21/2013 | CA2798787A1 Variable area fan nozzle with drive system health monitoring |
| 06/21/2013 | CA2792586A1 Gas turbine engine particle separator |
| 06/20/2013 | WO2013089251A1 Turbine blade |
| 06/20/2013 | WO2013089250A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089218A1 Heat-resistant nickel-based superalloy |
| 06/20/2013 | WO2013089173A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089139A1 Turbine |
| 06/20/2013 | WO2013088088A1 Fluid discharge vibration damping strips for acoustic protection of aircraft turbomachine fan casing |
| 06/20/2013 | WO2013088033A1 Air intake structure for turbojet engine nacelle |
| 06/20/2013 | WO2013034829A9 Oil and fuel circuits in a turbomachine and method for managing heat exchanges |
| 06/20/2013 | WO2012071166A3 Integrated variable geometry flow restrictor and heat exchanger |
| 06/20/2013 | US20130158831 Detection of the ingress of water or hail into a turbine engine |
| 06/20/2013 | US20130157000 Component and turbomachine having a component |
| 06/20/2013 | US20130156557 Shaping apparatus and method of shaping a workpiece |
| 06/20/2013 | US20130154199 Leaf seal |
| 06/20/2013 | US20130152602 Controller |
| 06/20/2013 | US20130152600 Shaft break detection |
| 06/20/2013 | US20130152599 Hydrocarbon film protected refractory carbide components and use |
| 06/20/2013 | US20130152597 System and method for flame stabilization |
| 06/20/2013 | US20130152591 System of integrating baffles for enhanced cooling of cmc liners |
| 06/20/2013 | DE102012003902A1 Inlet for gas turbine, has inlet wall, bypass-channel formed at inner side of inlet wall, and bypass flow-stator arranged at end of bypass-channel, where inner side of bypass-channel is limited by bypass-channel wall that has drain holes |
| 06/20/2013 | DE102011088872A1 Gas turbine used in gas and steam power plant, has compressor connected with heat exchanger that is coupled with combustion chamber or expander in order to supply heated air to combustion chamber or expander |
| 06/20/2013 | DE102011088524A1 Verfahren zum Stabilisieren einer Netzfrequenz mit einer Gasturbine im Brennstoffmischbetrieb A method for stabilizing a power frequency to a gas turbine in the fuel mixing operation |
| 06/20/2013 | CA2858503A1 Air intake structure for turbojet engine nacelle |
| 06/20/2013 | CA2858165A1 Fluid discharge vibration damping strips for acoustic protection of aircraft turbomachine fan casing |
| 06/20/2013 | CA2858020A1 Turbine blade |
| 06/20/2013 | CA2798746A1 Spring assembly |
| 06/20/2013 | CA2770858A1 Fuel manifold with jumper tubes |
| 06/19/2013 | EP2605238A2 Acoustic absorber |
| 06/19/2013 | EP2604827A2 Gas turbine engine transient assist using a starter-generator |
| 06/19/2013 | EP2604826A2 System and Method for Warming up a Steam Turbine |
| 06/19/2013 | EP2604825A2 Controller for cooling the turbine section of a gas turbine engine |
| 06/19/2013 | EP2604808A1 An apparatus for driving a load, a method of offline washing and a method of rolling a multi-shaft gas turbine |
| 06/19/2013 | EP2604426A1 Manufacturing method for a sound attenuating panel |
| 06/19/2013 | EP2603684A2 Adiabatic compressed air energy storage process |
| 06/19/2013 | CN203009045U Control device for baffle plate door of gas turbine air intake channel |
| 06/19/2013 | CN203009044U Baffle plate door device for gas turbine air intake channel |
| 06/19/2013 | CN103161578A Gas turbine engine part retention |
| 06/19/2013 | CN103161577A Hydrocarbon film protected refractory carbide components and use |
| 06/19/2013 | CN103161576A Turning gear for gas turbine arrangements |
| 06/19/2013 | CN103161575A Method and system for separating co2 from n2 and o2 in a turbine engine system |
| 06/19/2013 | CN103161523A Dynamic load reduction system |
| 06/19/2013 | CN101915128B System comprising multiple spool generators |
| 06/19/2013 | CN101806247B Optimization of low-btu fuel-fired combined-cycle power plant by performance heating |
| 06/19/2013 | CN101619677B Vortex air-oil separator system |
| 06/19/2013 | CN101372902B Gas turbine shroud support apparatus |
| 06/19/2013 | CN101230800B Holding device and system for turbine rotor |
| 06/19/2013 | CN101153559B Gas turbine engine assembly and method of assembling same |
| 06/19/2013 | CN101144429B Thermoelectrically cooled components for distributed electronics control system for gas turbine engines |
| 06/19/2013 | CN101135268B Heat pipe-based cooling apparatus and method for turbine engine |
| 06/18/2013 | US8464541 Closing system for an aircraft fan shroud |
| 06/18/2013 | US8464536 Gas turbine combustion chamber |
| 06/18/2013 | CA2672125C Mid turbine frame for gas turbine engine |
| 06/18/2013 | CA2665303C Starting and generating apparatus for engine |
| 06/18/2013 | CA2642505C Cooling structure |
| 06/18/2013 | CA2521983C Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor |
| 06/18/2013 | CA2499379C Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft |
| 06/16/2013 | CA2798269A1 System of integrating baffles for enhanced cooling of cmc liners |
| 06/16/2013 | CA2798257A1 System and method for active clearance control |
| 06/13/2013 | WO2013085641A1 Gas turbine engine with variable overall pressure ratio |
| 06/13/2013 | WO2013085435A1 Gas turbine engine component |
| 06/13/2013 | WO2013084763A1 Lean fuel sucking gas turbine |
| 06/13/2013 | WO2013084308A1 Installation boss and fan case |
| 06/13/2013 | WO2013084135A1 Element for sound absorption mounted on aircraft components |
| 06/13/2013 | WO2013083937A1 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element |
| 06/13/2013 | WO2013083917A1 System for sealing an oil chamber from an adjoining exterior volume and turbo-machine provided with such a sealing system |
| 06/13/2013 | WO2013083271A1 Method for thermal ignition of a pulsed combustion engine, and thermoreactor with thermal ignition |
| 06/13/2013 | US20130151039 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same |
| 06/13/2013 | US20130149139 Dynamic load reduction system |
| 06/13/2013 | US20130147123 Air riding seal arrangement |
| 06/13/2013 | US20130145774 Accessory gearbox with tower shaft removal capability |
| 06/13/2013 | US20130145773 Method and system for separating co2 from n2 and o2 in a turbine engine system |
| 06/13/2013 | US20130145770 Substitution device for aircraft engine |
| 06/13/2013 | US20130145769 Gas Turbine Engine with Variable Overall Pressure Ratio |
| 06/13/2013 | US20130145765 System for aerodynamically enhanced premixer for reduced emissions |
| 06/13/2013 | US20130145744 System for directing air flow to a plurality of plena |
| 06/13/2013 | US20130145741 Two-stage combustor for gas turbine engine |
| 06/13/2013 | DE102011088032A1 Ladeeinrichtung Loader |
| 06/13/2013 | CA2858158A1 System for sealing an oil chamber from an adjoining exterior volume and turbo-machine provided with such a sealing system |
| 06/13/2013 | CA2857938A1 Attachment boss and fan case |
| 06/13/2013 | CA2856105A1 Element for sound absorption mounted on aircraft components |
| 06/13/2013 | CA2798309A1 System for aerodynamically enhanced premixer for reduced emissions |
| 06/12/2013 | EP2602458A2 Multiple turboshaft engine control method and system for helicopters |
| 06/12/2013 | EP2602457A2 Fuel driven actuation systems for thrust reverser |
| 06/12/2013 | EP2602456A2 Fuel or hydraulic fluid driven actuation systems for variable area fan nozzles |
| 06/12/2013 | EP2602455A1 Wind energy assembly rotor blade with an electrical heating element |
| 06/12/2013 | EP2602442A1 Cranking pad interlock |
| 06/12/2013 | EP2602441A1 Exhaust gas housing for a gas turbine and gas turbine having an exhaust gas housing |
| 06/12/2013 | EP2602439A1 Coolable hot gas component for a gas turbine |
| 06/12/2013 | EP2601395A2 Oil supply system for a stationary turbomachine |
| 06/12/2013 | EP2601394A2 Gas turbine apparatus with improved exergy recovery |
| 06/12/2013 | EP2601388A1 Multi-piece turbocharger casing |