Patents for F02C 3 - Gas-turbine plants characterised by the use of combustion products as the working fluid (9,666)
07/2013
07/31/2013CN103228872A Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
07/31/2013CN103225544A Turbomachine passage cleaning system
07/30/2013US8495882 integrated gasification combined cycle (IGCC) power plants with high temperature membrane separation of carbon dioxide from syngas; many advantages for an integrated coal-to-hydrogen and electricity power process such as reduced energy cost for CO2 capture, lower capital cost, and a smaller footprint
07/25/2013WO2013109581A1 Method of electricity distribution including grid energy storage, load leveling, and recirculating c02
07/25/2013WO2013107966A1 Bearing bracket for a turbine engine
07/25/2013US20130186100 Small engine cooled cooling air system
07/25/2013US20130186097 Liquid Fuel Heating System
07/25/2013US20130186095 Gas turbine with motive fluid driven jet-compressor
07/25/2013US20130186057 Naphtha and process gas/syngas mixture firing method for gas turbine engines
07/24/2013CN203081581U Internal combustion wave rotor with pressurization function based on nonsteady combustion
07/24/2013CN103221660A System and method for high efficiency power generation using a nitrogen gas working fluid
07/24/2013CN103221640A High efficiency power production methods, assemblies, and systems
07/24/2013CN103216337A 液体燃料加热系统 Liquid fuel heating system
07/24/2013CN103216333A Countercurrent tangential type micro turbojet engine
07/24/2013CN103216275A Near flow path seal for a turbomachine
07/23/2013US8490407 System and method for generation of high pressure air in an integrated gasification combined cycle system
07/23/2013CA2556485C Compressor with multiple dividers creating an annular volume separating the flow in a turbine engine
07/23/2013CA2538223C Multi-spool turbogenerator system and control method
07/23/2013CA2498459C Gas turbine inlet flow straightener
07/18/2013US20130183531 Article including ceramic structure
07/18/2013US20130180259 System and method for generating power using a supercritical fluid
07/18/2013US20130180256 Turbine fuel nozzle assembly and method for operating a turbine
07/18/2013DE102009059330B4 Verfahren und Vorrichtung zur Kühlung eines Übergangsstücks Method and apparatus for cooling a transition piece
07/17/2013EP2615289A1 Turbofan with gear-driven compressor and fan-driven core
07/17/2013EP2614241A1 Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine
07/17/2013EP2614240A2 An energy generation system and method thereof
07/17/2013EP2614239A1 Screw shaft turbine compressor and system
07/17/2013CN101915162B Discrete load fins for individual stator vanes
07/17/2013CN101761390B Method and systems for operating a combined cycle power plant
07/11/2013WO2013103977A2 Rotational engine
07/11/2013WO2012164371A3 Flue gas recirculation system and method
07/11/2013WO2012079694A8 Method for operating a small gas turbine assembly and small gas turbine assembly itself
07/11/2013US20130174566 Method for removing carbon dioxide, and also gas turbine installation with carbon dioxide removal
07/11/2013US20130174533 Magnetically coupled contra-rotating propulsion stages
07/10/2013EP2613034A1 Method for operating a gas turbine
07/10/2013EP2613033A2 Magnetically coupled contra-rotating propulsion stages
07/10/2013EP2612008A1 Flushing the exhaust gas recirculation lines of a gas turbine
07/10/2013CN203050891U Turbine engine
07/10/2013CN103201461A Method for attaching the cover of a centrifugal compressor of a turbine engine, compressor cover implementing same and compressor assembly provided with such a cover
07/10/2013CN103195581A Method for operating a gas turbine
07/10/2013CN103195570A Method and apparatus for operating a gas turbine engine
07/10/2013CN101652549B 旋转装置 Rotating device
07/09/2013US8479487 Hybrid multichannel porous structure for hydrogen separation
07/09/2013CA2562588C Axial flow positive displacement worm gas generator
07/04/2013WO2013102171A2 Blade track assembly, components, and methods
07/04/2013WO2013102135A2 Gas turbine engine and turbine blade
07/04/2013WO2013102113A2 Gas turbine engine with variable speed turbines
07/04/2013US20130171532 Conversion of c-o-h compounds into hydrogen for power or heat generation
07/04/2013US20130170982 Turbine and method for separating particulates from a fluid
07/04/2013US20130167555 Aluminum fan blade construction with welded cover
07/03/2013EP2610464A2 Gas turbine engine lubrication
07/03/2013EP2610463A2 Gas turbine engine gear train
07/03/2013EP2610462A2 Gas turbine engine with low stage count low pressure turbine
07/03/2013EP2610461A2 Dual fan gas turbine engine and gear train
07/03/2013EP2610460A2 Gas turbine engine compressor arrangement
07/02/2013CA2553574C Delivery apparatus
06/2013
06/27/2013WO2013094381A1 Method for operating lean-fuel suction gas turbine engine, and gas turbine electricity generation device
06/27/2013WO2013094379A1 Control method and control device for lean-fuel suction gas turbine
06/27/2013WO2013092563A1 Vent for a gaseous fuel supply circuit of a gas turbine, and associated method
06/27/2013WO2013092411A1 Control of the gas composition in a gas turbine power plant with flue gas recirculation
06/27/2013WO2013091222A1 Optimized design method for radial-flow-type hydraulic turbine
06/27/2013DE102011122013A1 Method of operating gas turbine, involves producing gas mixture from recycled exhaust gas and gas stream, and supplying gas mixture from compressor unit with pressure lower than atmospheric pressure so that gas turbine is operated
06/26/2013EP2607655A2 Intake liner for a gas turbine engine
06/26/2013EP2607649A2 System and method for controlling oxygen emissions from a gas turbine
06/26/2013CN103180551A Exhaust gas treatment of gas turbine engines
06/26/2013CN103174518A System and method for controlling oxygen emissions from gas turbine
06/26/2013CN103174517A Cold-source-acting impeller Stirling hot-air engine
06/25/2013US8468832 Combustor, method of supplying fuel to same, and method of modifying same
06/25/2013US8468830 Inlet air heating and cooling system
06/25/2013CA2491437C Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed
06/25/2013CA2479235C Gas turbine engine system
06/20/2013WO2013087347A1 Method for stabilising a network frequency with a gas turbine in mixed-fuel operation
06/20/2013WO2013086625A1 Rotary pulse detonation engine
06/20/2013WO2012071166A3 Integrated variable geometry flow restrictor and heat exchanger
06/20/2013US20130152598 System and method for thermal control in a gas turbine engine
06/20/2013US20130152543 Radial inflow gas turbine engine with advanced transition duct
06/20/2013DE102011089242A1 Combustion system for gas turbine, has two annular combustion chambers, which are arranged parallel to each other relative to flow direction of combustion gas in coaxial manner
06/20/2013DE102011088872A1 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
06/20/2013CA2857377A1 Rotary pulse detonation engine
06/19/2013EP2604824A1 Method and Device for producing electrical energy
06/19/2013EP2604823A2 Method and system for separating CO2 from N2 and O2 in a turbine engine system
06/19/2013EP2604822A1 Jet engine with sliding vane compressor
06/19/2013CN103161575A Method and system for separating co2 from n2 and o2 in a turbine engine system
06/19/2013CN101806247B Optimization of low-btu fuel-fired combined-cycle power plant by performance heating
06/19/2013CN101457694B Method and system for controlling an exhaust gas recirculation system
06/18/2013CA2521983C 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
06/16/2013CA2798269A1 System of integrating baffles for enhanced cooling of cmc liners
06/16/2013CA2798199A1 Hydrocarbon film protected refractory carbide components and use
06/13/2013WO2013085641A1 Gas turbine engine with variable overall pressure ratio
06/13/2013WO2013084763A1 Lean fuel sucking gas turbine
06/13/2013WO2012013289A3 Method and device for storing electricity
06/13/2013WO2011163192A3 Fluidization device for solid fuel particles
06/13/2013US20130145771 System and method using low emissions gas turbine cycle with partial air separation
06/13/2013US20130145769 Gas Turbine Engine with Variable Overall Pressure Ratio
06/13/2013US20130145741 Two-stage combustor for gas turbine engine
06/13/2013DE102011120704A1 Steam-/work process system for electric power generation in cyclic process, has axial compressor, where work fluid i.e. water vapor, coming from axial compressor flows into external heater and heated fluid flows into internal heater
06/12/2013EP2601393A1 Systems and methods for optimizing stoichiometric combustion
06/12/2013CN101978150B System of counter-rotating propellers with a feathering device for propeller blades
06/12/2013CN101368512B Turbine engine diffuser
06/12/2013CA2797229A1 Turning gear for gas turbine arrangements
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