Patents for F02C 9 - Controlling gas-turbine plants; Controlling fuel supply in air-breathing jet-propulsion plants (8,382) |
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05/23/2012 | CN102465764A System and method for combustion dynamics control |
05/22/2012 | US8185291 Stall prediction apparatus, prediction method thereof, and engine control system |
05/18/2012 | WO2012064363A2 Ultra low emissions fast starting power plant |
05/17/2012 | US20120119512 Power plant and method of operation |
05/17/2012 | US20120117974 Air flow delivery and fuel consumption control for aircraft air management and auxiliary power systems |
05/17/2012 | US20120117972 Thermal management for fuel injectors |
05/16/2012 | EP2453120A1 Operation control method for gas turbine and operation controller for gas turbine |
05/16/2012 | CN102459850A Combustor systems and methods for using same |
05/16/2012 | CN102459849A Stabilizing a gas turbine engine via incremental tuning |
05/16/2012 | CN102459821A Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
05/16/2012 | CN102454487A System and method for controlling a semi-closed power cycle system |
05/16/2012 | CN102454486A A method and system for preventing combustion instabilities during transient operations |
05/16/2012 | CN102454485A Systems and methods for supplying fuel to a gas turbine |
05/16/2012 | CN102454484A 发电厂 Power plant |
05/16/2012 | CN102454483A Air cooled condenser fogging control system |
05/16/2012 | CA2758545A1 Aircraft and propulsion system |
05/15/2012 | CA2635477C An actuator arrangement and a method of operating an actuator |
05/10/2012 | WO2012059671A2 Method of optimizing the specific fuel consumption of a twin engine helicopter and twin engine architecture with control system for implementing it |
05/10/2012 | WO2012045029A8 Dual fuel aircraft engine control system and method for operating same |
05/10/2012 | CA2814381A1 Method of optimizing the specific fuel consumption of a twin engine helicopter and twin engine architecture with control system for implementing it |
05/09/2012 | EP2450551A2 System and method for compensating fuel composition variations in a gas turbine |
05/09/2012 | CN102444504A Small-temperature-rise and low-thermal-charge mix combustion refrigerating system |
05/08/2012 | US8171717 Model-based coordinated air-fuel control for a gas turbine |
05/03/2012 | WO2012057282A1 Gas turbine and gas turbine plant provided with same |
05/03/2012 | WO2012056144A1 Method of controlling a turbomachine |
05/03/2012 | WO2012056142A2 Control of a fuel metering device for turbomachine |
05/03/2012 | US20120102968 Method for controlling a gas turbine and gas turbine for implementing the method |
05/03/2012 | US20120102967 Method and system for preventing combustion instabilities during transient operations |
05/03/2012 | US20120102966 Operation control method for gas turbine and operation controller for gas turbine |
05/03/2012 | US20120102914 Systems, methods, and apparatus for compensating fuel composition variations in a gas turbine |
05/03/2012 | DE102011054547A1 Verfahren und System zur Verhinderung von Verbrennungsinstabilitäten während transienter Betriebsvorgänge A method and system for the prevention of combustion instabilities during transient operations |
05/03/2012 | CA2815014A1 Method of controlling a turbomachine |
05/03/2012 | CA2814169A1 Control of a fuel metering device for turbomachine |
05/02/2012 | EP2447511A1 Method for controlling a gas turbine and gas turbine for implementing the method |
05/02/2012 | EP2447510A1 Powerplant of an aircraft, aircraft and method for piloting said aircraft |
05/02/2012 | EP2447509A2 Combuster control method and combustor controller |
05/02/2012 | EP2446149A1 Device and method for positioning variable-geometry equipment for a turbomachine, using a relative-measurement jack |
05/02/2012 | CN102439274A Method and device for feeding a turbine engine combustion chamber with a controlled fuel flow |
05/02/2012 | CN102434288A Fuel heating system |
05/02/2012 | CN102434282A Gas turbine circulating device with middle water spray cooling and steam reinjection |
04/29/2012 | CA2756310A1 Aircraft powerplant, aircraft, and process for piloting said aircraft |
04/26/2012 | US20120096829 System and method for controlling a semi-closed power cycle system |
04/26/2012 | DE19902437B4 Verfahren und Vorrichtung zum schnellen Anfahren und zur schnellen Leistungssteigerung einer Gasturbinenanlage Method and apparatus for fast start-up and rapid increase in performance of a gas turbine plant |
04/26/2012 | DE102011113432A1 Turbine for supercharger of e.g. reciprocating piston internal combustion engine of passenger car, has adjusting device including adjusting elements that are adjustable independent of each other for variably adjusting passage area of wheel |
04/26/2012 | DE102011054549A1 System und Verfahren zur Steuerung einer Energieanlage mit halbgeschlossenem Kreislauf System and method for controlling a power plant with semi-closed circuit |
04/25/2012 | EP2444632A1 Method for regulating the flue gas recirculation of a power plant |
04/25/2012 | CN202204613U 一种进气温度传感器 One kind of intake air temperature sensor |
04/24/2012 | CA2661707C Turbofan bypass duct air cooled fluid cooler installation |
04/19/2012 | US20120095663 Fmu mounted eec for small aircraft engine applications |
04/19/2012 | US20120090330 Method of operating an electronic engine control (eec) to compensate for speed changes |
04/19/2012 | US20120090329 Systems and methods involving multiple torque paths for gas turbine engines |
04/19/2012 | US20120090327 Power plant and method for its operation |
04/19/2012 | US20120090326 Power plant |
04/19/2012 | US20120090291 Internal combustion engine |
04/19/2012 | DE102011115364A1 Kraftwerk Power station |
04/19/2012 | DE102011115363A1 Kraftwerk und Verfahren für seinen Betrieb Power plant and method for its operation |
04/18/2012 | EP2441940A2 Method of controlling the operation of a fuel metering unit and such a unit |
04/18/2012 | EP2441939A2 Electronic engine controller mounted on the fuel metering unit for small aircraft engine applications |
04/18/2012 | EP2441938A1 Distributed small engine FADEC |
04/18/2012 | EP2441937A1 Apparatus and method for purging a liquid fuel injection system in a gas turbine |
04/18/2012 | CN102418605A 燃烧基准温度估算 Combustion reference temperature estimate |
04/12/2012 | WO2012045939A1 Thruster for a space launcher, and method for controlling propellant consumption |
04/12/2012 | US20120085101 Method of testing a system for protecting a turbomachine against overspeed while starting |
04/11/2012 | EP2439390A1 Control method for cooling a turbine stage in a gas turbine |
04/11/2012 | EP2439388A1 Solar gas turbine and solar gas turbine power generating device |
04/11/2012 | EP2438281A1 Combustor systems and methods for using same |
04/11/2012 | EP2438274A1 Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
04/11/2012 | CN102410593A Combined cooling and power scheduling system of fuel gas combined cycle unit and scheduling method thereof |
04/05/2012 | WO2012045029A1 Dual fuel aircraft engine control system and method for operating same |
04/05/2012 | WO2012045028A1 Dual fuel aircraft system and method for operating same |
04/05/2012 | WO2012042628A1 Gas turbine power generation device, gas turbine power generation system, and method of controlling the system |
04/05/2012 | US20120079831 Method, apparatus and system for igniting wide range of turbine fuels |
04/05/2012 | DE102011054175A1 Verfahren, Vorrichtung und System zur Zündung eines breiten Spektrums an Turbinenbrennstoffen A method, apparatus and system for igniting a wide range of turbine fuels |
04/05/2012 | CA2812256A1 Dual fuel aircraft engine control system and method for operating same |
04/05/2012 | CA2812250A1 Dual fuel aircraft system and method for operating same |
04/04/2012 | EP2435681A1 Stabilizing a gas turbine engine via incremental tuning |
04/04/2012 | CN102400956A 用于空气流控制的方法和设备 Method and apparatus for the air flow control |
04/04/2012 | CN102400788A Systems and methods for controlling the startup of a gas turbine |
04/02/2012 | DE202012000084U1 Sicherheitsgerichtete fehlertolerante Thermoprozesssteuerung Safety-related fault-tolerant thermal process control |
03/29/2012 | CA2811940A1 System and method for high efficiency power generation using a nitrogen gas working fluid |
03/28/2012 | EP2434132A2 Critical flow nozzle for controlling fuel distribution and burner stability |
03/28/2012 | EP2434131A2 Connection device for data collection device |
03/28/2012 | EP2434127A2 Methods and systems for modeling turbine operation |
03/27/2012 | US8141369 Method of regulation of the temperature of hot gas of a gas turbine |
03/27/2012 | US8141368 Thermal management for fuel injectors |
03/27/2012 | CA2618116C Coated variable area fan nozzle |
03/22/2012 | US20120067053 Combustor system |
03/22/2012 | US20120067022 Gas turbine engine fuel control thrust control override system |
03/22/2012 | DE102011083181A1 Turbine mit variabler Geometrie A variable geometry turbine |
03/21/2012 | EP2431591A2 Bleed valve |
03/21/2012 | EP2431590A2 Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events |
03/21/2012 | CN102383944A Intelligent control system of smoke generator |
03/21/2012 | CN101449039B Gas turbine engine starting method and control device |
03/20/2012 | USRE43252 High efficiency low pollution hybrid Brayton cycle combustor |
03/20/2012 | US8136361 Methods and apparatus for assembling a low noise ejector motive nozzle |
03/20/2012 | US8136360 Method for observing combustion conditions in a gas turbine engine |
03/20/2012 | CA2514435C Flow control in accordance with two separate regulating laws for emergency regulator |
03/15/2012 | US20120060505 Adaptive control for a gas turbine engine |
03/15/2012 | DE112004002348B4 Gasturbinenschutzvorrichtung Gas turbine protection device |
03/15/2012 | DE102005017400B4 Verfahren zur Bestimmung der Turbineneintrittstemperatur einer Gasturbine bei instationären Vorgängen Method for determining the turbine inlet temperature of a gas turbine during transient operations |