Patents for F02C 3 - Gas-turbine plants characterised by the use of combustion products as the working fluid (9,666)
12/2013
12/05/2013US20130318942 Flame detection in no-flame region of gas turbine
12/04/2013EP2669490A2 Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
12/04/2013EP2669489A2 Axial compressor and gas turbine having axial compressor
12/04/2013EP2668387A1 Mixing element for gas turbine units with flue gas recirculation
12/04/2013CN103429852A Determining fan parameters through pressure monitoring
12/04/2013CN103429848A 气体和蒸汽涡轮装置 Gas and steam turbine unit
12/04/2013CN103422993A System and method for producing hydrogen rich fuel
12/04/2013CN103421544A Gasification and generation system of carbon fuel
12/04/2013CN102691576B Power transmission mechanism of gas compressor and turbine
12/04/2013CN101037960B High pressure ratio aft fan
12/03/2013US8596076 Variable pressure ratio gas turbine engine
12/03/2013US8596071 Method and apparatus for assembling a gas turbine engine
12/03/2013US8596069 Rational late lean injection
11/2013
11/28/2013WO2013177030A1 Method and device for modifying a secondary air system in a gas turbine engine
11/28/2013WO2013176876A1 Liquid-gas mixer and turbulator therefor
11/28/2013WO2013176709A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case
11/28/2013WO2012112889A3 Fluid flow devices with vertically simple geometry and methods of making the same
11/28/2013US20130312425 Passive thermostatic valve
11/28/2013US20130312424 Renewable Combined Cycle Low Turbine Boost
11/28/2013US20130312384 Flex-Fuel Hydrogen Generator for IC Engines and Gas Turbines
11/26/2013CA2545618C Cooled support boss for a combustor in a gas turbine engine
11/21/2013WO2013173006A1 Method for making metal plated gas turbine engine components
11/21/2013WO2013172906A2 Counter rotating low pressure turbine with splitter gear system
11/21/2013WO2013172902A1 Geared turbofan architecture for improved thrust density
11/21/2013US20130305729 Turbomachine combustor and method for adjusting combustion dynamics in the same
11/21/2013DE102012208263A1 Compressor device for turbomachine of jet engine, has secondary compressor that is designed such that air withdrawn after last compressor stage is supplied to secondary compressor, which is driven by gearbox of auxiliary device carrier
11/20/2013EP2664764A2 System and method for producing hydrogen rich fuel
11/20/2013EP2663756A1 Systems and methods for improved combustion operations
11/14/2013WO2013167639A1 Dispensing device for cryogenic liquids
11/14/2013WO2013167638A1 Supplying a pump with cryogenic liquid
11/14/2013WO2013167636A1 Method and system for retrofitting an aircraft
11/14/2013WO2013167328A1 Rotor for a steam turbine
11/14/2013WO2013126125A3 Radial inflow gas turbine engine with advanced transition duct
11/14/2013US20130298570 Method for producing liquid hydrogen and electricity
11/14/2013US20130298522 Geared fan assembly
11/13/2013EP2662535A1 Rotor for a steam turbine and corresponding steam turbine
11/13/2013CN102562302B Gas-steam combined cycle inert gas protection control system
11/12/2013CA2729130C Double flow compressor
11/12/2013CA2571167C Axial flow positive displacement gas generator with combustion extending into an expansion section
11/07/2013WO2013166284A1 Shaped rim cavity wing surface
11/07/2013WO2013166084A1 Gas turbine and gas turbine afterburner
11/07/2013WO2013165960A1 Water quench for gasifier
11/07/2013WO2013165868A1 Gas turbine engine combustor surge retention
11/07/2013WO2013165771A1 Geared turbofan with distributed accessory gearboxes
11/07/2013WO2013165769A1 Manifold for geared turbofan engine
11/07/2013WO2013165495A2 Apparatus and method for optically measuring creep
11/07/2013WO2012079694A3 Method for operating a small gas turbine assembly and small gas turbine assembly
11/07/2013US20130291544 Gas turbine engine combustor surge retention
11/06/2013EP2660440A2 Electro-magnetic coupling system
11/06/2013EP2659108A1 Engine liquid injection
11/06/2013EP2659107A1 Engine and combustion system
11/06/2013CN203271919U Gas turbine with multiple independent combustion chambers
11/06/2013CN103382856A Housing movable vane wheel mechanism
11/06/2013CN102257260B System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
11/06/2013CN102076941B Gas turbine device
11/05/2013US8572980 Cooling scheme for an increased gas turbine efficiency
11/05/2013US8572944 Prime mover for an exhaust gas recirculation system
10/2013
10/31/2013WO2013163045A1 System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine
10/31/2013WO2013162887A1 Airfoil with break-way, free-floating damper member
10/31/2013WO2013162752A1 Thermal management system for a gas turbine engine
10/31/2013WO2010093512A3 System and method for operating power generation systems
10/31/2013US20130284123 Energy recovery system for a mobile machine
10/31/2013US20130283821 Gas turbine engine and nacelle noise attenuation structure
10/31/2013US20130283820 Hollow fan bladed with braided fabric tubes
10/31/2013US20130283810 Combustion nozzle and a related method thereof
10/31/2013US20130283809 Fuel injector with purged insulating air cavity
10/31/2013US20130283808 System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine
10/31/2013US20130283761 Co2 separation and recovery equipment, and a coal gasification combined power plant comprising co2 separation and recovery equipment
10/30/2013EP2657457A2 Electricity generation system
10/30/2013EP2655832A2 Method for operating a small gas turbine assembly and small gas turbine assembly
10/30/2013CN203257540U Oxygen-containing gas liquefied product engine
10/30/2013CN103375812A Gas turbine combustor and a method for controlling air flow in the gas turbine combustor
10/30/2013CN103375265A Turboshaft engine and use method thereof
10/30/2013CN103375258A Method and system for controlling an extraction pressure and temperature of a stoichiometric EGR system
10/30/2013CN103375257A Systems and apparatus relating to combustion turbine engines with exhaust gas recirculation
10/30/2013CN103375256A Systems and apparatus relating to combustion turbine engines with exhaust gas recirculation
10/30/2013CN103375255A Method and system for controlling a powerplant during low-load operations
10/30/2013CN103375254A Methods relating to reheat combustion turbine engines with exhaust gas recirculation
10/30/2013CN103375253A Method and system for controlling a secondary flow system
10/30/2013CN102022193B Systems and methods for closed loop emissions control
10/29/2013US8567199 Method and apparatus of introducing diluent flow into a combustor
10/29/2013US8567178 Positive displacement rotary vane engine
10/29/2013US8567176 Rotating device
10/24/2013WO2013158191A1 Geared turbofan gas turbine engine architecture
10/24/2013WO2013158179A2 Turbine engine gearbox
10/24/2013WO2013156611A1 System and method for ecologically generating and storing electricity
10/24/2013US20130276461 Airfoil having internal lattice network
10/24/2013US20130276460 Airfoil having minimum distance ribs
10/24/2013US20130276459 Resistive band for turbomachine blade
10/24/2013US20130276458 Gas turbine inlet system and method
10/24/2013US20130276457 Airfoil including loose damper
10/24/2013US20130276456 Airfoil including member connected by articulated joint
10/24/2013US20130276455 Airfoil with break-way, free-floating damper member
10/24/2013US20130276424 Low Noise Compressor Rotor for Geared Turbofan Engine
10/24/2013DE102012007832A1 Verfahren zum Betrieb einer Gasturbineneinheit A method of operating a gas turbine unit
10/24/2013CA2857351A1 Geared turbofan gas turbine engine architecture
10/23/2013EP2653698A1 Method for operating a gas turbine unit
10/23/2013EP2652269A1 Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
10/23/2013CN103362648A System and method of improving emission performance of a gas turbine
10/23/2013CN103362647A Gas turbine and gas turbine power facilities
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