Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
10/2012
10/04/2012WO2012133123A1 Turbine exhaust structure and gas turbine
10/04/2012WO2012132898A1 Combustor and gas turbine provided with same
10/04/2012WO2012132787A1 Gas turbine
10/04/2012WO2012131209A1 Anti-fire seal assembly and nacelle comprising such a seal
10/04/2012WO2012129631A1 Method for generating propulsion, and engine
10/04/2012US20120251309 Cmc turbine nozzle adapted to support a metallic turbine internal casing by an axial contact
10/04/2012US20120247125 Communicating structure between combustor and turbine portion and gas turbine
10/04/2012US20120247124 Continuous ring composite turbine shroud
10/04/2012US20120247123 Securing system
10/04/2012US20120247121 Aircraft gas turbine
10/04/2012US20120247120 Apparatus and method for cooling a combustor
10/04/2012US20120247118 Combustor crossfire tube
10/04/2012US20120247114 Water Cooling System For Intercooled Turbines
10/04/2012US20120247109 Gas turbine and air intake manifold
10/04/2012DE102012102730A1 Ansaugflächendichtung und zugehöriges Verfahren Ansaugflächendichtung and associated method
10/04/2012DE102012006329A1 Gasturbine und Ansaugkrümmer Gas turbine and intake manifold
10/04/2012DE102011015703A1 Method for integrating intercooler in compression process of thermal turbomachine e.g. turbofan engine, involves redirecting and rerouting compressor air in fan housing into engine after air is flowed through fan stator
10/04/2012DE102011006358A1 Exhaust gas turbocharger for internal combustion engine, particularly for motor vehicle, comprises bearing housing for mounting turbine wheel, and sprial housing, which has spiral chamber enclosing turbine wheel
10/04/2012CA2831281A1 Combustor for gas turbine engine and gas turbine
10/04/2012CA2829267A1 Anti-fire seal assembly and nacelle comprising such a seal
10/03/2012EP2505879A1 Gearbox and oil spreader thereof
10/03/2012EP2505808A2 Device for mixing fuel and air of a turbojet engine
10/03/2012EP2505789A1 Gaseous flow separator with device for thermal-bridge defrosting
10/03/2012EP2505782A1 Plasma actuated vortex generators
10/03/2012EP2504832A1 Acoustic skin for an aircraft nacelle acoustic panel
10/03/2012EP2504564A1 Laser spark plug
10/03/2012CN202468101U Oil fuel pipeline control system of micro turbine generator of automobile
10/03/2012CN202468091U Air circuit system of electric vehicle turbine generator
10/03/2012CN102713303A Turbo compressor and compressor system comprising said turbo compressor
10/03/2012CN102713206A Dual-pump supply system with by-pass-controlled flow regulator
10/03/2012CN102713205A Turbojet engine nacelle component cooling assembly
10/03/2012CN102713164A Method for operating a steam turbine, steam turbine and atomizer
10/03/2012CN102705083A Seal for a turbine engine
10/03/2012CN102705082A Windward pressure differential plasma ignition nozzle
10/03/2012CN102705081A Binary hypersonic variable geometrical inlet channel, design method and work mode
10/03/2012CN101672483B 燃气轮机 Gas turbine
10/03/2012CN101652809B Method for producing an acoustically resistive structure, resulting acoustically resistive structure and skin using one such structure
10/02/2012US8276391 Combustor liner cooling at transition duct interface and related method
10/02/2012US8276386 Apparatus and method for a combustor
10/02/2012US8276359 Gas turbine plant
10/02/2012CA2471259C Nacelle inlet lip anti-icing with engine oil
09/2012
09/30/2012CA2772720A1 Gas flow separator with a thermal bridge de-icer
09/30/2012CA2769811A1 Connection device for drive assembly
09/27/2012WO2012128778A1 Protecting aircraft and aircraft engines against icing by burning fuel
09/27/2012WO2012127959A1 Acoustic damper, combustor, and gas turbine
09/27/2012US20120242045 Combustor interface sealing arrangement
09/27/2012US20120241561 Method and apparatus for protecting aircraft and aircraft engines against icing
09/27/2012US20120240593 Fuel system for gas turbine engine
09/27/2012US20120240592 Combustor with Fuel Nozzle Liner Having Chevron Ribs
09/27/2012US20120240591 Method for shutting down a generator to prepare the generator for restart
09/27/2012US20120240586 Low emission and flashback resistant burner tube and apparatus
09/27/2012DE112009002724T5 System und Verfahren zum Waschen und Spülen der Flüssigbrennstoffleitung einer Turbine mit Wasser System and method for washing and rinsing the liquid fuel line of a turbine with water
09/27/2012DE102012102365A1 Einsätze für einen Turbinenkühlkreislauf Inserts for a turbine cooling circuit
09/27/2012DE102010041066B4 Trägergehäuse und Brennkraftmaschine Support housing and internal combustion engine
09/26/2012EP2503131A2 Hybrid slinger combustion system
09/26/2012EP2503106A1 Gas turbine power plant with flue gas recirculation and oxygen-depleted cooling gas
09/26/2012EP2503104A2 Turbo engine
09/26/2012EP2503103A2 Steam turbine
09/26/2012EP2503013A1 Heat-resistant superalloy
09/26/2012EP2501996A1 Combustion chamber having a ventilated spark plug
09/26/2012EP2501914A1 Device for changing the transmission ratio between a turbine shaft and a starter/generator shaft of aircraft engine
09/26/2012EP2501613A1 Mounting of accessory casing onto an intermediate housing for a jet engine air blower compartment
09/26/2012CN202451282U Small efficient reheater
09/26/2012CN102695919A Combustion burner for gas turbine
09/26/2012CN102695918A Guiding of a spark plug into a turbine engine combustion chamber
09/26/2012CN102695862A Fluid-cooling device for a turbine engine propulsive unit
09/26/2012CN102691578A System and method for controlling fuel supply associated with turbomachine
09/26/2012CN102691577A Integrated gasification combined cycle system with vapor absorption chilling
09/26/2012CN102691576A Power transmission mechanism of gas compressor and turbine
09/26/2012CN102691575A Transmission device and gas turbine provided with same
09/26/2012CN102691533A Components with cooling channels formed in coating and methods of manufacture
09/26/2012CN102691532A System for regulating a cooling fluid within a turbomachine
09/25/2012US8272224 Apparatus and methods for fuel nozzle frequency adjustment
09/25/2012US8272219 Gas turbine engine combustor having trapped dual vortex cavity
09/25/2012US8272201 Means for cooling a bearing assembly
09/25/2012CA2771562A1 Hybrid slinger combustion system
09/25/2012CA2735299A1 Airfoil and method of a repair the same
09/25/2012CA2533425C Turbofan case and method of making
09/25/2012CA2500762C Ring-shaped turbine engine combustion chamber with improved internal attachment clamp
09/24/2012CA2771922A1 Turbomachine
09/22/2012CA2770913A1 Fuel system for gas turbine engine
09/20/2012WO2012125895A1 System and method for operating a precooler in an aircraft
09/20/2012WO2012124578A1 Turbine blade
09/20/2012WO2012123684A1 Method for optimizing the speed of a twin-spool turbojet engine fan, and architecture for implementing same
09/20/2012WO2012123194A1 Injection aperture for a steam power plant
09/20/2012WO2012097997A3 Gas turbine exhaust cone
09/20/2012US20120237333 Cooled gas turbine engine component
09/20/2012US20120234019 Tapered bearings
09/20/2012US20120234018 Aft frame and method for cooling aft frame
09/20/2012US20120234017 Gas turbine engine compressor arrangement
09/20/2012US20120234016 Small gas turbine engine with multiple burn zones
09/20/2012US20120234015 Dual pump fuel flow system for a gas turbine engine and method of controlling
09/20/2012US20120234013 Recirculating product injection nozzle
09/20/2012US20120234011 Gas turbine combustor having a fuel nozzle for flame anchoring
09/20/2012US20120234009 Gas turbine combustion chamber
09/20/2012US20120233982 Gas turbine engine compressor arrangement
09/20/2012US20120233977 Rotating fluid pumping system
09/20/2012DE102012202530A1 Kühlstruktur für ein Lagergehäuse eines Turboladers Cooling structure for a bearing housing of a turbocharger
09/20/2012DE102012202387A1 Lageraufbau eines Turboladers Bearing structure of a turbocharger
09/20/2012DE102011014292A1 Intermediate level sealing ring for gas turbine engine, is made of metal foam, and has element, which is made of wear-resistant material that is arranged in metal foam, where inner platform is provided for supporting guide vanes
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