Patents for F02C 9 - Controlling gas-turbine plants; Controlling fuel supply in air-breathing jet-propulsion plants (8,382)
03/2002
03/14/2002US20020029557 Gas turbine system
03/13/2002EP1186761A2 Energy recovery from compressor discharge bleed air in gas turbine plants
03/13/2002EP0866915B1 A power plant
03/07/2002US20020027213 Extended range proportional valve method
03/07/2002US20020026786 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
03/07/2002US20020026785 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
03/07/2002US20020026784 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
03/07/2002DE10040868A1 Verfahren zur Reduzierung thermoakustischer Schwingungen in Strömungskraftmaschinen mit einem Brennersystem A method of reducing thermoacoustic oscillations in the flow engine with a burner system
03/06/2002EP1184623A2 Liquid fuel and water injection purge system and method for a gas turbine
03/05/2002US6353790 Gas turbine aeroengine control system
03/05/2002CA2270672C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system
02/2002
02/28/2002US20020023425 Method and apparatus for the rapid startup and rapid increase in output of a gas turbine plant
02/27/2002EP1182399A2 Process for reducing the thermoacoustic oscillations in a turbo-engine using a combustion system
02/21/2002WO2002014695A1 Method and system of pulsed or unsteady ejector
02/20/2002EP1180577A2 Cooling method for a turbine rotor
02/14/2002WO2002012795A2 Control method for pilot and premix fuel flow split for a gas turbine combustor
02/14/2002WO2002012692A1 Compressor starting torque converter
02/14/2002WO2002012691A1 Gas turbine engine and method of operation at idle speed
02/14/2002WO2001048574A3 Device and method for adjusting the power of a power pack driving a helicopter rotor
02/13/2002EP1179788A2 Method and system for exporting flight data for long term storage
02/12/2002US6345495 Gas turbine system for flameless combustion of fuel gases
02/12/2002CA2077842C Gas turbine engine case counterflow thermal control
02/07/2002WO2002010569A1 Proportional bypass valve for a fuel control system
02/07/2002US20020016654 Method of monitoring and displaying health performance of an aircraft engine
02/06/2002EP1178196A2 Methods and apparatus for trimming engine control systems
01/2002
01/31/2002US20020011063 Gas turbine plant and method of controlling gas turbine plant
01/29/2002US6343251 Method and system for monitoring the operation of and predicting part life consumption for turbomachinery
01/29/2002CA2199875C Combined bleed valve and annular diffuser for gas turbine inter compressor duct
01/24/2002US20020007820 Apparatus and method for determining the status of a valve arrangement forming part of a fuelling system
01/23/2002EP1174606A2 Method of controlling a gas turbine plant
01/22/2002US6340289 Single lever power controller for manned and unmanned aircraft
01/17/2002WO2002005046A2 Extended range proportional flow valve method
01/17/2002WO2002004797A1 Valve control logic
01/17/2002US20020006329 Nozzle airfoil having movable nozzle ribs
01/15/2002US6338240 Control method for gas turbine load
01/10/2002WO2002002920A1 System and method for gaseous fuel control for a turbogenerator/motor
01/10/2002WO2002002919A1 Pulse width modulated valve transition control logic
01/10/2002US20020002819 Apparatus and methods for supplying auxiliary steam in a combined cycle system
01/10/2002US20020002818 Apparatus for fuel nozzle staging for gas turbine engines
01/10/2002US20020002817 Pulse width modulated valve transition control logic
01/09/2002EP1169557A1 Biomass combustion chamber for gas turbine
01/03/2002WO2002001055A1 Method and apparatus for providing shutoff, overspeed protection, and directional control of a bypass flow in a fuel delivery system
01/02/2002EP1168121A2 Data acquisition for remote monitoring system and method for remote monitoring
01/02/2002EP1167698A2 Integrated operation instructing system for operating power generation plants
12/2001
12/27/2001US20010054290 Low-cost general aviation fuel control system
12/26/2001CN1328617A Turbomachine
12/26/2001CN1076785C Power plant
12/20/2001WO2001096785A1 Method for operating a burner and burner with stepped premix gas injection
12/19/2001EP1164282A2 Stand alone multi stage fuel pump
12/18/2001CA2119246C Closed loop fuel control system and method
12/18/2001CA2048829C High pressure compressor flowpath bleed valve extraction slot
12/13/2001CA2350297A1 Stand alone multi stage fuel pump
12/12/2001EP1161622A1 Method of operation of a gas turbine engine power plant and a gas turbine engine power plant
12/11/2001US6328526 Gas turbine starting method
12/11/2001US6328056 Proportional bypass valve with dual variable orifice
12/06/2001WO2001092702A1 Integrated gas compressor
12/06/2001WO2001092701A1 Heat engines and associated methods of producing mechanical energy and their application to vehicles
12/06/2001US20010047650 Method of operating a gas-turbine chamber with gaseous fuel
12/06/2001CA2410952A1 Heat engines and associated methods of producing mechanical energy and their application to vehicles
12/05/2001EP1160551A1 Sensors and methodology for improved turbine exhaust gas temperature measurements
12/04/2001US6325142 Turbogenerator power control system
12/04/2001US6324828 Gas turbine engine and a method of controlling a gas turbine engine
11/2001
11/29/2001US20010045088 Surge detection system of gas turbine aeroengine
11/27/2001US6321527 Bi-level fuel pressurizing system
11/27/2001US6321525 Overspeed detection techniques for gas turbine engine
11/27/2001CA2048988C Dual independent input hydraulic shutoff
11/22/2001WO2001088355A1 Method for remote monitoring of gas turbine
11/22/2001US20010042368 Bleed valve of a compressor, in particular a compressor of a bypass aero-engine
11/21/2001EP1156190A1 Gas turbine controller of single-shaft combined cycle power generating plant and gas turbine output calculating method
11/21/2001EP0900351B1 Fuel injection method for a stepped gas turbine combustion chamber
11/15/2001US20010039796 Method of and apparatus for generating power
11/15/2001US20010039794 Methods for operating gas turbine engines
11/14/2001EP1154137A2 Monitoring arrangement to determine the status of a valve in a fuel supply system
11/13/2001US6314737 Internal combustion engine having an activatable boost air delivery capacity adjusting
11/08/2001WO2001084053A1 Controller for combustion system
11/08/2001WO2001083965A1 Fuel injection system for a gas turbine
11/06/2001US6312154 Method for on-line measurement of fuel heat content of fuel in a combustion turbine system
11/06/2001CA2215276C Method and apparatus for detecting burner blowout
10/2001
10/31/2001EP1096122A4 Method for detecting sensor failures and for controlling the operation conditions of an object
10/31/2001CN1074085C Exhaust recirculation type combined plant
10/30/2001US6308740 Method and system of pulsed or unsteady ejector
10/24/2001EP1147458A2 Smooth transfer between main and back-up fuel control
10/18/2001DE10018137A1 Verfahren und Vorrichtung zur Zumessung von Kraftstoffen Method and apparatus for metering of fuels
10/18/2001DE10005246C1 Exhaust gas turbocharger for IC engine has force acting on compressor shaft supported by magnetic bearing detected for controlling variable turbine geometry
10/17/2001EP1146214A2 System and device for controlled fuel supply
10/17/2001CN1317634A Method and appts. for reducing discharge of gas turbine
10/11/2001US20010027641 Fluid apparatus and method of using the same
10/11/2001US20010027639 Fuel injection for a staged gas turbine combustion chamber
10/11/2001US20010027638 Method and apparatus for minimizing thermoacoustic vibrations in gas-turbine combustion chambers
10/11/2001US20010027637 Gas-turbine engine combustion system
10/10/2001EP1143319A1 Device and method of flow and pressure regulation of the fuel actuating a servovalve unit
10/10/2001EP1143199A1 Methods and apparatus for reducing gas turbine engine emissions
10/10/2001EP1143128A2 Fuel supply system
10/04/2001EP1137873A1 Turbine engine control system, aircraft, and fuel delivery system for an engine
10/03/2001CN1072305C Starting method for combined device
09/2001
09/27/2001WO2001071172A2 Method and installation for generating energy
09/27/2001US20010023578 Method of operating a burner and burner configuration
09/25/2001US6293088 Gas turbine with steam cooling and fuel atomization
09/25/2001US6293085 Shaft decouple logic for gas turbine engine
09/20/2001US20010022079 Device and process for controlling the pressure and delivery of a fuel feed to a servovalve unit
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