Patents
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)
09/2012
09/20/2012DE102004016028B4 Verfahren und System zum Vermindern von Turbinenaustrittsturbulenz Method and system for reducing turbine exhaust turbulence
09/20/2012CA2829742A1 Turbine blade
09/19/2012EP2500655A1 Gas turbine combustor and gas turbine
09/19/2012EP2500654A1 Combustion burner for gas turbine
09/19/2012EP2500552A2 Dual pump fuel flow system for a gas turbine engine and method of controlling
09/19/2012EP2500551A2 Fuel flow control system and method for controlling two positive displacement pumps
09/19/2012EP2500549A1 Injection aperture for a steam power plant
09/19/2012EP2500548A1 Method for producing vane
09/19/2012EP2500546A1 System and method for controlling a fuel supply associated with a turbomachine
09/19/2012EP2500528A1 Method for radial column adjustment of an axial turbo engine and axial turbo engine
09/19/2012EP2500527A2 Rotating liquid pumping system
09/19/2012EP2499345A2 Variable performance valve
09/19/2012EP2499341A1 Metal annular connecting structure for an aircraft turbine engine
09/19/2012EP2499332A1 Low emission power generation and hydrocarbon recovery systems and methods
09/19/2012CN202441474U Evaporation cooling device for combustion chamber
09/19/2012CN102686949A Structure for connecting a combustor to a turbine unit, and gas turbine
09/19/2012CN102686864A Contra-rotating propeller system for an aircraft turbine engine
09/19/2012CN102686853A Mitigation of optical signal noise using a multimode transmit fiber
09/19/2012CN102686852A Coil arrangements for air intake system for gas turbine and methods
09/19/2012CN102686833A 航空燃气涡轮机 Aero gas turbine
09/19/2012CN102678387A Rotary-cone blade jet engine and rotary-cone blade combustion engine
09/19/2012CN102678339A Plasma igniter with reusable cathode
09/19/2012CN102678338A Oil supply pressure regulating system for aircraft engine and regulating method thereof
09/19/2012CN102678337A System and method for transitioning between fuel supplies for a combustion system
09/19/2012CN102678336A Machine strap fuel system for gas fuel internal combustion turbine
09/19/2012CN102678335A Turbulated aft-end liner assembly and cooling method
09/19/2012CN102678334A System for cooling and purging exhaust section of gas turbine engine
09/19/2012CN102678333A Imported protective net cover
09/19/2012CN102678332A Reheating vortex combined-type heat engine
09/18/2012US8266914 Heat shield sealing for gas turbine engine combustor
09/18/2012US8266912 Reusable weld joint for syngas fuel nozzles
09/18/2012US8266886 Systems and methods involving multiple torque paths for gas turbine engines
09/18/2012US8266885 Method and systems for adaptive ignition energy
09/18/2012US8266884 Asynchronous combustion system
09/18/2012US8266883 Power plant start-up method and method of venting the power plant
09/18/2012CA2612689C Low cost pressure atomizer
09/18/2012CA2552016C Mistake-proof cable assembly
09/18/2012CA2509791C Shroud and vane segments having edge notches
09/18/2012CA2487841C Mounting structure for mounting a turboprop under an aircraft wing
09/13/2012WO2012121334A1 Guide vane attachment structure and fan
09/13/2012WO2012120555A1 Solar heat utilization gas turbine system
09/13/2012WO2012120229A1 Method for monitoring the change in state of a valve by measuring pressure
09/13/2012WO2012098322A3 Nacelle for an aircraft bypass turbojet engine
09/13/2012WO2012098321A3 Nacelle for an aircraft bypass turbojet engine
09/13/2012WO2010133483A3 Method of cooling a hydrocarbon stream and apparatus therefor
09/13/2012US20120232768 System and method for transitioning between fuel supplies for a combustion system
09/13/2012US20120227415 Positioning arrangement for components of a pressure vessel and method
09/13/2012US20120227414 Gas turbine engine swirled cooling air
09/13/2012US20120227413 igniter
09/13/2012US20120227412 method of operating a multi-fuel combustion system
09/13/2012US20120227409 Aircraft fuel system cooling flow device
09/13/2012US20120227408 Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation
09/13/2012US20120227373 Combustion chamber having a ventilated spark plug
09/13/2012US20120227371 System for cooling and purging exhaust section of gas turbine engine
09/13/2012DE102011005347A1 Turbine mit einem Magnetlager Turbine with a magnetic bearing
09/13/2012CA2824281A1 Guide vane attachment structure and fan
09/12/2012EP2497923A2 Fuel system
09/12/2012EP2497922A2 Systems and methods for cooling a staged airblast fuel injector
09/12/2012EP2497908A2 A conduit for bleed air in a gas turbine engine
09/12/2012EP2497626A1 Cylindrical structure and method for manufacturing same
09/12/2012EP2497625A1 Cylindrical structure and method of production thereof
09/12/2012EP2496810A2 Micro-turbine combustor
09/12/2012EP2496795A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing
09/12/2012CN102667916A Acoustic skin for an aircraft nacelle acoustic panel
09/12/2012CN102667346A Combustion chamber having a ventilated spark plug
09/12/2012CN102667107A Device for changing the transmission ratio between a turbine shaft and a starter/generator shaft of aircraft engine
09/12/2012CN102667106A Adiabatic compressed air energy storage system with liquid thermal energy storage
09/12/2012CN102667072A Dual flow turbine engine for an aircraft including structural means for stiffening the central casing
09/12/2012CN102667068A Turbine for converting energy and method for operating the same
09/12/2012CN102667067A Shaft seal device and rotary machine including shaft seal device
09/12/2012CN102666279A Mounting of accessory casing onto an intermediate housing for a jet engine air blower compartment
09/12/2012CN102665855A Air intake for a plant
09/12/2012CN102661972A Gas turbine heat shield and heat insulating property measurement method thereof
09/12/2012CN102661202A Fireproof systems in aircraft engines
09/12/2012CN102661201A Air entraining structure of engine
09/12/2012CN102661200A Fuel cell/gas turbine hybrid power system with catalytic combustor
09/11/2012US8262344 Thermal management system for a gas turbine engine
09/11/2012US8261556 Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber
09/11/2012US8261528 System for heating an airstream by recirculating waste heat of a turbomachine
09/11/2012US8261527 Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure
09/07/2012WO2012118288A1 Gas turbine
09/07/2012WO2012117792A1 Foil bearing
09/07/2012WO2012116943A1 Turbine comprising a sealing device between the stator blade carrier and the housing
09/07/2012CA2828313A1 Turbine comprising a sealing device between the stator blade carrier and the housing
09/06/2012US20120224960 Gas turbine engine case
09/06/2012DE102011012863A1 Ölversorgungssystem für ein Flugtriebwerk Oil supply system for an aircraft engine
09/06/2012DE102008017962B4 Vorrichtung zur Zuführung von Verbrennungsluft zu einem Triebwerk eines Luftfahrzeuges Device for supplying combustion air to an engine of an aircraft
09/05/2012EP2495417A2 Combustor with a pre-nozzle mixing cap assembly
09/05/2012EP2494184A2 Turbine engine starter/generator, and method for the control thereof
09/05/2012EP2494169A1 Adiabatic compressed air energy storage system with liquid thermal energy storage
09/05/2012EP2494163A1 Reinforced thermal energy storage pressure vessel for an adiabatic compressed air energy storage system
09/05/2012EP2494156A1 Gas turbine starting process
09/05/2012CN202417717U Turbine support framework for aviation turbine engine
09/05/2012CN202417716U Inlet air heating system for gas turbine
09/05/2012CN202417715U Air inlet purifying system for offshore turbine
09/05/2012CN202417640U Detection oil tank
09/05/2012CN102656004A Cylindrical structure and method of production thereof
09/05/2012CN102654080A Method and device for starting and stopping gas turbine
09/05/2012CN102654079A Technical scheme of intermittent inflating turbine engine
09/05/2012CN101915164B Air inlet particle separating device for gas turbine
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