Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 9 - Controlling gas-turbine plants; Controlling fuel supply in air-breathing jet-propulsion plants
Patents for F02C 9 - Controlling gas-turbine plants; Controlling fuel supply in air-breathing jet-propulsion plants (8,382)
01/2013
01/02/2013CN102859148A Energy recovery system and method
01/02/2013CN102852647A Control system and method for small-size turbojet engine
01/02/2013CN102852644A Gas turbine inlet heating system
12/2012
12/27/2012WO2012177372A1 Phase and amplitude matched fuel injector
12/27/2012US20120324900 Phase and amplitude matched fuel injector
12/27/2012DE102011077908A1 Gasturbine mit Pyrometer Gas turbine with pyrometer
12/26/2012CN102844547A Method and device for formulating setpoint signal
12/26/2012CN102840035A Novel throttle actuator
12/26/2012CN102840034A Fluid leak detection system
12/26/2012CN102840033A Systems and methods for use in monitoring operation of a rotating device
12/26/2012CN102840031A Improved structure of rotary engine
12/25/2012US8336315 Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine
12/20/2012WO2012173651A1 Aircraft engine fuel system and method of operating the same
12/20/2012DE102011077723A1 Temperatursensoranordnung Temperature sensor array
12/20/2012CA2838561A1 Aircraft engine fuel system and method of operating the same
12/19/2012EP2535643A2 Systems and methods for combustor emissions control
12/19/2012EP2535543A1 Method for operating a fuel supply for a heat engine
12/19/2012EP2534351A1 Method of determining a combustor exit temperature and method of controlling a gas turbine
12/19/2012CN102828833A Method for operating a fuel supply system for heat engine
12/13/2012US20120312027 Flow discharge device
12/13/2012US20120312024 Late lean injection with adjustable air splits
12/12/2012EP2532859A1 Fuel supply device for gas turbine engine
12/12/2012EP2531709A2 Cooling of turbine components using combustor shell air
12/12/2012CN202596900U Servo control system for gas turbine trial
12/06/2012WO2012164224A1 Turbomachine with blow‑off valves located at the intermediate case
12/06/2012WO2012163667A1 Adiabatic compressed air storage power plant
12/06/2012US20120304666 Aircraft control system
12/05/2012EP2530283A1 Adiabatic pressurised air storage power plant
12/05/2012EP2529096A1 Energy recovery system and method
12/05/2012CN101479678B Device and method for performing a functional test on a control element of a turbo engine
12/05/2012CN101265842B Improved system and method for reducing NOx emission
11/2012
11/29/2012US20120297788 Method of determining a combustor exit temperature and method of controlling a gas turbine
11/29/2012DE102011102359A1 Gas turbine for use in gas turbine engine i.e. turbo-engine, of aircraft, has guide tracks extending in axial direction with respect to axis, and blades moved along curved tracks by piston-cylinder that has front piston and rear piston
11/28/2012EP2527618A2 A bleed flow discharge device of a gas turbine engine
11/28/2012CN102803735A Device and method for positioning variable-geometry equipment for a turbomachine, using a relative-measurement jack
11/28/2012CN102798150A System and method for flow control in gas turbine engine
11/28/2012CN102797565A Vortex composite heat engine
11/27/2012US8321119 Methods and systems to facilitate over-speed protection
11/27/2012US8316630 Flow equalizing override assembly for fuel divider system
11/27/2012CA2724083C Fan blade retention and variable pitch system
11/22/2012DE102008029227B4 Oberflächenstrukturierter Temperaturfühler und Verfahren zur Herstellung Structured surface temperature sensor and methods for preparing
11/21/2012CN202545060U Low-temperature-rise low-entropy multifuel-fired refrigeration system
11/20/2012US8313324 Fuel ratio control in a combustion apparatus with multiple fuel supply lines
11/15/2012WO2012107467A3 Method for controlling a gas turbine
11/15/2012US20120285174 Systems and Methods for Optimized Gas Turbine Shutdown
11/15/2012DE102011101302A1 Producing a housing, with a tempering line, preferably a housing of a digital electronic regulating and control unit of an aircraft engine, comprises layer-by-layer building of housing with tempering line by generative manufacturing method
11/14/2012EP2522908A1 Control method for controlling the pilot gas supply to at least one burner assembly of a gas turbine plant and gas turbine plant
11/14/2012EP2522833A2 Gas turbine engine with bleed air removal device
11/14/2012EP2522813A2 A controller, for use in a power plant having a liquid cooling system and an air cooling system
11/14/2012CN102777935A Burner and method for regulating a gas turbine with such a burner
11/14/2012CN102777264A Systems and methods for optimized gas turbine shutdown
11/13/2012US8307627 Method and device for monitoring the formation of deposits of solid particles, particularly in a fuel line and in the fuel valves of a gas turbine
11/13/2012CA2608042C Method and device for regulating the operating line of a gas turbine combustion chamber
11/08/2012US20120279230 Exhaust temperature based threshold for control method and turbine
11/08/2012US20120279229 Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting the method
11/08/2012US20120279198 Gas turbine engine with bypass mixer
11/07/2012EP2520863A1 Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting said method
11/07/2012EP2519862A1 Process optimization method and system for a power plant
11/07/2012CN102767431A Method for operating a gas turbine power plant with exhaust gas recirculation
11/01/2012US20120277969 Passing from a non-synchronized state between an engine and a rotor to a synchronized state
10/2012
10/31/2012EP2518273A2 Axial compressor with arrangement for bleeding air from variable stator vane stages
10/31/2012CN102762840A Method of determining a combustor exit temperature and method of controlling a gas turbine
10/30/2012US8297060 Apparatus, system and method for observing combustion conditions in a gas turbine engine
10/30/2012US8297036 Method and apparatus for determining failures of gas shutoff valves in gas turbines
10/24/2012EP2514926A1 Hybrid control system
10/24/2012CN102748137A Fuel control system of gas turbine
10/23/2012US8291713 Method of operating a gas turbine power plant
10/23/2012US8291712 Method for determining sensor locations
10/20/2012CA2769809A1 Distributed aircraft engine fuel system
10/18/2012WO2012141252A1 Gaseous-fuel analyzer and system for controlling gas turbine
10/18/2012WO2012140373A1 Fuel circuit comprising means for controlling a pump
10/18/2012DE102011007386A1 Abgasnutzturbine, Abwärmerückgewinnungssystem und Verfahren zum Betreiben eines Abwärmerückgewinnungssystems The exhaust gas turbine, waste heat recovery system and method of operating a waste heat recovery system
10/18/2012CA2832098A1 Fuel circuit comprising means for controlling a pump
10/17/2012EP2511499A2 Fuel flow divider and ecology system for a gas turbine engine fuel flow control system
10/17/2012EP2511497A2 Methods and systems for loading a steam turbine
10/17/2012CN102733869A 联合循环发电设备 Combined cycle power plant
10/16/2012CA2586885C Device for issuing authorization to act on the operating conditions of an aircraft engine and engine control system comprising same
10/11/2012WO2012138672A1 Quiet bleed valve for gas turbine engine
10/11/2012US20120259528 Control of compression system with independently actuated inlet guide and/or stator vanes
10/11/2012US20120259483 Actuation control system
10/10/2012EP2508801A2 Apparatus, system and method for observing combustion conditions in a gas turbine
10/10/2012EP2508735A1 Method and device for controlling the operating speed of the engines of an aircraft during the take-off phase
10/10/2012EP2508734A2 Combustor with integrated control valve system
10/10/2012EP2508732A2 System and method for air extraction from gas turbine engines
10/10/2012CN202483722U Air bleed valve structure
10/10/2012CN102725498A Exhaust temperature based mode control method for gas turbine and gas turbine
10/10/2012CN102720590A Starting control method and device of combustion gas turbine
10/10/2012CN101126352B Methods and systems for gas turbine engine control
10/08/2012CA2736720A1 System for diverting exhaust gases to actuate auxiliary features of an aircraft
10/06/2012CA2773964A1 Flow device and method and system using the flow device
10/04/2012WO2012132062A1 Method for operating gas compressor, and gas turbine provided with gas compressor
10/04/2012US20120247122 Powerplant and related control system and method
10/04/2012US20120247119 Active pattern factor control for gas turbine engines
10/04/2012US20120247116 Method for switching over a gas turbine burner operation from liquid to gas fuel and vice-versa
10/04/2012US20120247115 Gas compressor operating method and gas turbine equipped with gas compressor
10/03/2012EP2504672A1 Method and device for checking a system for measuring a flow of fuel in real time
10/03/2012EP2504548A2 Exhaust temperature versus turbine pressure ratio based turbine control method and device
10/03/2012EP2504547A1 Exhaust temperature based mode control method for gas turbine and gas turbine
10/03/2012EP2504546A1 Exhaust temperature based mode control method for gas turbine and gas turbine
10/03/2012EP2504545A1 Exhaust temperature based threshold for control method and turbine
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