Patents for F02C 3 - Gas-turbine plants characterised by the use of combustion products as the working fluid (9,666)
09/2011
09/29/2011DE112009001834T5 System und Verfahren zum Betreiben eines Energieerzeugungssystems mit einem alternativen Arbeitsfluid System and method for operating a power generation system with an alternative working fluid
09/28/2011EP2368030A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
09/28/2011EP2368022A2 Power plant with co2 capture
09/28/2011CN201991616U 超燃双工质汽轮机 Supersonic combustion turbine duplex quality
09/28/2011CN102200057A System and method for cooling gas turbine component
09/28/2011CN102200053A Method and apparatus for radial exhaust gas turbine
09/27/2011CA2483380C Discrete passage diffuser
09/22/2011WO2011056928A3 Micro-turbine combustor
09/22/2011US20110225973 Combustor with Pre-Mixing Primary Fuel-Nozzle Assembly
09/22/2011US20110225947 System and methods for altering air flow in a combustor
09/21/2011EP2366874A1 Turbine system with several independent compressors and turbines
09/21/2011EP2366062A2 Method for stabilization of the network frequency of an electrical power network
09/21/2011CN102192508A Axially staged premixed combustion chamber
09/21/2011CN102192013A Mixed combustion type engine
09/21/2011CN102192011A 涡轮系统 Turbine system
09/20/2011US8020388 Method for increasing the efficiency of a combined gas/steam power station with integrated gasification combined cycle
09/20/2011CA2739420A1 Systems and methods for generating electricity from carbonaceous material with substantially no carbon dioxide emissions
09/20/2011CA2475148C Lateral deflection interblade platform for a turbojet blade support
09/20/2011CA2458417C Turbojet engine arrow blade
09/15/2011WO2011112146A1 Gas turbine power generation plant and method for operating such a plant
09/15/2011US20110223026 Gas turbine engine compressor and turbine section assembly utilizing tie shaft
09/15/2011US20110219784 Compressor section with tie shaft coupling and cantilever mounted vanes
09/15/2011US20110219780 Processing fuel and water
09/15/2011US20110219779 Low emission combustion systems and methods for gas turbine engines
09/15/2011US20110219778 Power generation process with partial recycle of carbon dioxide
09/15/2011US20110219777 Power generation process with partial recycle of carbon dioxide
09/15/2011US20110219776 Aerodynamic flame stabilizer
09/15/2011US20110219773 Systems and methods for producing hydrogen from cellulosic and/or grain feedstocks for use as a vehicle fuel, use in the production of anhydrous ammonia, and to generate electricity
09/15/2011US20110219741 Determining fan parameters through pressure monitoring
09/14/2011EP2364400A2 Ultra-low sulfur fuel and method for reduced contrail formation
09/14/2011CN102182558A System and method of improving emission performance of a gas turbine
09/13/2011US8015821 Apparatus and method for a gas turbine entrainment system
09/09/2011WO2011109008A1 Methods of oxy-combustion power generation using low heating value fuel
09/09/2011CA2792061A1 Methods of oxy-combustion power generation using low heating value fuel
09/08/2011US20110214429 Angled vanes in combustor flow sleeve
09/08/2011US20110214428 Hybrid venturi cooling system
09/07/2011CN101725410B Water washing device for gas turbine
09/07/2011CN101652546B Rotary mechanically reciprocated sliding metal vane air pump and boundary layer gas turbines integrated with a pulse gas turbine engine system
09/01/2011WO2011106073A2 Damper seal and vane assembly for a gas turbine engine
09/01/2011WO2011104685A2 Rotary type internal combustion engine
09/01/2011WO2011016945A3 Coannular ducted fan
09/01/2011US20110209482 Tangential combustor with vaneless turbine for use on gas turbine engines
09/01/2011US20110209481 Turbine Combustor End Cover
09/01/2011CA2786153A1 Damper seal and vane assembly for a gas turbine engine
08/2011
08/31/2011EP1825111B1 Counter-rotating compressor case for a tip turbine engine
08/31/2011CN201953481U 涡旋空气内能利用装置 The air inside the vortex energy utilization device
08/31/2011CN102170957A Treatment of CO2-depleted flue gases
08/30/2011US8006499 Humid air turbine, humid air turbine control system, and humid air turbine control method
08/26/2011CA2732464A1 Aircraft gas turbine engine
08/25/2011WO2011101711A1 Engine for thrust or shaft output and corresponding operating method
08/25/2011US20110203287 Combustor liner for a turbine engine
08/25/2011US20110203282 Assembly for directing combustion gas
08/24/2011CN1854486B Double reverse turbine engine, and method for assembling the same
08/24/2011CN102162396A Gas auto-rotating-type motor
08/24/2011CN101368510B Cut-spraying type engine
08/23/2011US8001788 Method and apparatus for preparing pulverized coal used to produce synthesis gas
08/23/2011CA2731914A1 Epicyclic gearbox
08/23/2011CA2495624C Turbojet having a large bypass ratio
08/23/2011CA2433991C Power generating system
08/18/2011US20110197590 Burner inserts for a gas turbine combustion chamber and gas turbine
08/18/2011US20110197586 Systems and Methods of Providing High Pressure Air to a Head End of a Combustor
08/18/2011DE102004058760B4 Verfahren zum Betreiben eines Gas- und Dampfturbinenkraftwerkes mit integrierter Kohlevergasung Method for operating a gas and steam turbine power plant with integrated coal gasification
08/17/2011CN102155299A Combination system of stirling engine and combustion gas turbine utilizing liquefied natural gas
08/17/2011CN102155298A Ejector/mixer nozzle for noise reduction
08/17/2011CN102155297A Secondary combustion fuel supply systems
08/16/2011US7998227 Method for utilizing gas reserves with low methane concentrations for fueling gas turbines
08/16/2011US7997082 Turbine engine arrangement
08/16/2011CA2579057C Heat shield-less combustor and cooling of combustor liner
08/11/2011WO2011001311A3 Hybrid cycle sofc - inverted gas turbine with co2 separation
08/11/2011WO2011000548A3 Method for operating a power plant using a gas turbine system
08/11/2011US20110192168 Method and system for reducing power plant emissions
08/10/2011EP2354495A2 Integrated exhaust gas cooling system and corresponding method
08/10/2011EP2354492A2 Ejector in an Overboard Bleed scheme for a gas turbine
08/10/2011EP2354491A2 Gas turbine engine steam injection manifold
08/10/2011EP1706620B1 Gas turbine engine architecture
08/10/2011CN102149915A Gas turbine operation-controlling device
08/04/2011US20110189557 Aero-thermal energy technology platform using recycled energy with endothermic decomposition
08/04/2011US20110185736 Gas turbine combustor with variable airflow
08/04/2011US20110185735 Gas turbine combustor with staged combustion
08/04/2011US20110185701 Turbine equipment and power generating plant
08/03/2011EP2350444A1 Gas turbine engine accessory system
08/03/2011CN201916074U 喷气轮发动机 Jet turbine engine
08/03/2011CN102140963A Methods and apparatus for diluent nitrogen saturation
08/02/2011CA2672457C Heat shield sealing for gas turbine engine combustor
07/2011
07/28/2011WO2011091424A1 Carbon dioxide capture interface and power generation facility
07/28/2011US20110179801 Methods and apparatus for diluent nitrogen saturation
07/28/2011US20110179799 System and method for high efficiency power generation using a carbon dioxide circulating working fluid
07/28/2011US20110179797 Burner and method for operating a burner
07/28/2011CA2786010A1 Carbon dioxide capture interface and power generation facility
07/27/2011CN102135034A Bled diffuser fed secondary combustion system for gas turbines
07/21/2011WO2011031983A3 Rayleigh-taylor assisted combustion and combustors adapted to exploit rayleigh-taylor instability for increasing combustion rates therein
07/21/2011WO2010142440A3 Method for generating mechanical power
07/21/2011DE112009001835T5 System und Verfahren zum Betreiben eines Gasturbinenantriebs mit einem alternativen Arbeitsfluid System and method of operating a gas turbine engine with an alternative working fluid
07/21/2011DE102010004936A1 Compressor e.g. multistage axial compressor operating method for fluid-flow machine, involves impinging angle of attack of turbo-compressor stages with fluid such that front stages are more heavily loaded in relation to dry operation
07/20/2011CN102128101A Jet engine with parallel combustion chambers
07/20/2011CN102128084A Thermal power device for turbine fan engine
07/14/2011WO2011084551A2 Gas turbine generator
07/14/2011WO2011083137A1 Contra-rotating propeller system for an aircraft turbine engine
07/14/2011US20110167831 Adaptive core engine
07/14/2011US20110167783 Gas turbine device
1 ... 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 ... 97