Patents for F02C 3 - Gas-turbine plants characterised by the use of combustion products as the working fluid (9,666)
03/2004
03/24/2004CN1143052C Method of operating power station plant
03/18/2004WO2004022919A1 Rotary vane engine and thermodynamic cycle
03/18/2004US20040050070 Fluid injector and injection method
03/18/2004US20040050069 Power generating apparatus having combustion turbine inlet air flow temperature sensor for sensing a drybulb temperature and related methods
03/18/2004US20040050068 Combustion turbine having inlet air flow temperature sensor and related methods
03/18/2004US20040050067 Low-emission, staged-combustion power generation
03/18/2004US20040050065 Gas compression system and method for microturbine application
03/18/2004US20040050055 Gas turbine power augmenting spray nozzle assembly
03/18/2004US20040050033 Rotary nozzle turbine
03/17/2004EP1398566A2 Fluid injector and injection method
03/17/2004EP1397588A2 Method for operating an internal combustion engine
03/04/2004WO2004018855A1 Power quality system
03/04/2004WO2002080189B1 A nuclear power plant and a method of conditioning its power generation circuit
03/04/2004US20040042909 Compression feed for high humidity fuel gas
03/04/2004US20040042579 Nuclear power plant and method of operating the same
03/04/2004US20040040309 Gas turbine and method for operating a gas turbine
03/04/2004DE10236273A1 'Turax' turbine-type motor with triple action has axial rotor blades with jets and medium flow around radial blades
03/03/2004EP1394386A1 Process for combusting fuels, in particular gas in an oxidizer of high temperature
03/03/2004EP1394385A1 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines
03/03/2004CN1140722C Air jet engine with rotating combustion chamber with specific heat converting effect
02/2004
02/26/2004WO2003002690A8 Process for flash carbonization of biomass
02/26/2004US20040034998 Vane and method of construction thereof
02/25/2004EP1242163B1 Tubular and honeycomb metal fail-safe regenerator filter devices
02/24/2004US6694744 Fuel gas moisturization system level control
02/24/2004US6694743 Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
02/24/2004US6694738 Retrofit equipment for reducing the consumption of fossil fuel by a power plant using solar insolation
02/19/2004US20040031260 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines
02/19/2004DE10249191B3 Jet propulsion system for motor vehicles and agricultural machines has gas acceleration device to generate esp. compressed air, with acceleration turbine, gas guide channel, and gas collection tube, and gas re-circulation device
02/18/2004CN1138961C Turbine/motor (generator) driven booster compressor
02/17/2004US6692222 Micro gas turbine engine with active tip clearance control
02/17/2004US6691504 Gaseous-fuel breathing rocket engine
02/17/2004US6691503 Gas turbine having first and second combustion chambers and cooling system
02/12/2004WO2004013473A2 Vortex turbine engine
02/12/2004US20040025513 Gas turbine engine
02/12/2004US20040025509 Compact rotary ramjet engine generator set
02/12/2004US20040025495 Nested core gas turbine engine
02/12/2004US20040025490 Integrated bypass turbojet engines for air craft and other vehicles
02/11/2004EP1387986A1 Device and method for injecting a liquid fuel in an air flow for a combustion chamber
02/10/2004US6688111 Method for operating a combustion chamber
02/05/2004WO2004011789A1 Microturbine for combustion of volatile organic compounds (vocs)
02/05/2004WO2004011788A1 Single rotor turbine
02/05/2004US20040020211 Trapped vortex combustor
02/05/2004US20040020210 Fuel injection nozzle for gas turbine combustor, gas turbine combustor, and gas turbine
02/05/2004US20040020186 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
02/05/2004US20040020185 Rotary ramjet engine
02/04/2004EP1387060A2 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
02/04/2004CN2602173Y Plasma state water combustion engine
02/03/2004US6684644 Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines
02/03/2004US6684643 Process for the operation of a gas turbine plant
02/03/2004US6684626 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
02/03/2004CA2094975C Gas turbine system for the production of energy and at least one air gas
01/2004
01/29/2004WO2004009979A1 Power system and method
01/29/2004WO2004009225A1 Evaporative duplex counterheat exchanger
01/29/2004US20040016239 Miniature gas turbine engine with unitary rotor shaft for power generation
01/29/2004US20040016236 Software system for verification of gas fuel flow
01/29/2004US20040016235 Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
01/29/2004US20040016226 Radial impulse turbine for rotary ramjet engine
01/22/2004WO2004007928A1 Method for energy transformation in jet-engines
01/22/2004WO2004007927A2 Method for influencing and controlling the oxide layer on metallic components of a hot co2/h2o circulating system
01/22/2004US20040011057 Ultra-low emission power plant
01/22/2004US20040011050 Control system for gas-turbine engine
01/22/2004US20040011048 Method of operating a combustion plant and a combustion plant
01/22/2004US20040011047 Gas turbine and air turbine installation and method of operating a power station installation, in particular a gas turbine and air turbine installation
01/22/2004DE10231879A1 Verfahren zur Beeinflussung und Kontrolle der Oxidschicht auf metallischen Bauteilen heisser CO2/H2O-Kreislaufsysteme A method for influencing and controlling the oxide layer on metallic components hot CO2 / H2O-loop systems
01/22/2004DE10226721A1 Verfahren und Vorrichtung zur Erwärmung eines einer Brennkammer zugeführten Gases Method and apparatus for heating a combustion chamber of a gas supplied
01/20/2004US6679060 Method for operating a premix burner
01/15/2004WO2004005684A1 Rotary impeller driven turbine
01/15/2004US20040007219 Power generation device
01/15/2004US20040006994 Gas turbine engine
01/15/2004US20040006987 Turbine power generation systems and methods using off-gas fuels
01/15/2004US20040006965 Turbo shaft engine with acoustical compression flow amplifying ramjet
01/14/2004EP1379764A1 Gas turbine, vehicle comprising said gas turbine and method for engine-braking a gas turbine
01/08/2004WO2004003362A1 Power fluctuation suppressing method and power generation facility using same
01/08/2004WO2004003357A2 Orbiting combustion nozzle engine
01/08/2004CA2490488A1 Orbiting combustion nozzle engine
01/08/2004CA2487370A1 Power fluctuation suppressing method and power generation facility using same
01/07/2004EP1144916B1 Burner and process for operating gas turbines
01/06/2004US6672070 Gas turbine with a compressor for air
01/06/2004US6672069 Method and device for increasing the pressure of a gas
01/06/2004US6672049 Emergency device for relighting a windmilling turbojet
01/06/2004US6672048 Rotary impeller driven turbine
01/02/2004EP1375865A2 Method and apparatus for generating torque
01/02/2004EP1375864A2 Method and apparatus for lifting and propelling rotorcraft
01/02/2004EP1375822A2 Gas turbine production process
01/02/2004EP1374253A1 A nuclear power plant and method of operating the same
01/02/2004EP1374252A1 A nuclear power plant and a method of conditioning its power generation circuit
01/02/2004EP1373440A2 Process and gas generator for generating fuel gas
01/01/2004US20040000614 Method and apparatus for lifting and propelling rotorcraft
01/01/2004US20040000148 Gas turbine engine
01/01/2004US20040000145 Method and apparatus for generating torque
12/2003
12/31/2003CN1133014C Method for isothermal compression of compressible medium, and atomizing device and nozzle structure thereby
12/30/2003US6669917 Charging fluidized bed reactor with coal and high temperature steam to oxidize coal and form pure hydrogen gas and carbon dioxide; circulating mixture of solids in reactors containing calcium oxide and caclium carboante and iron oxides, reacting
12/30/2003US6668539 Rotary heat engine
12/27/2003CA2432850A1 Method and apparatus for lifting and propelling rotorcraft
12/27/2003CA2432819A1 Method and apparatus for generating torque
12/24/2003WO2003106817A1 Method for operating a gas turbine installation, and gas turbine installation
12/24/2003DE20220621U1 Micro gas turbine for generation of electrical energy and heat has working medium heated by combustion gases from combustion chamber for combustion of biomass
12/23/2003US6666027 Turbine power generation systems and methods using off-gas fuels
12/23/2003US6666017 Counterrotatable booster compressor assembly for a gas turbine engine
12/18/2003WO2003104629A1 Gas turbine group
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