Patents
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
01/2006
01/24/2006US6990432 Apparatus and method for performing gas turbine adjustment
01/24/2006US6989610 Electrical system for turbine/alternator on common shaft
01/24/2006US6988872 Turbine moving blade and gas turbine
01/24/2006US6988692 Rear fastening device for aircraft engine
01/24/2006US6988369 Combustion chamber sealing ring, and a combustion chamber including such a ring
01/24/2006US6988368 Method of engine starting in a gas turbine engine
01/24/2006US6988367 Gas turbine engine cooling system and method
01/24/2006US6988357 Nested core gas turbine engine
01/24/2006US6988356 Fuel metering unit with a compensated regulator valve in a turbomachine
01/24/2006CA2383429C Method and device for increasing the pressure of a gas
01/24/2006CA2254885C Turbomachine rotor cooling
01/20/2006CA2507190A1 Methods and apparatus for cooling turbine engine combustor ignition devices
01/19/2006WO2006005319A2 Device for detecting a fractured shaft of a gas turbine and gas turbine
01/19/2006WO2006005199A1 Exhaust-gas turbine for a turbocharger comprising an air-cooled turbine disc
01/19/2006US20060011708 Friction plug welding method, for a hole in a metal part, use of a metal bar and of a bearing supporting part for implementing the method
01/19/2006US20060011408 Acoustic liner for gas turbine engine
01/19/2006US20060011301 Method for repairing loose molded-in bushings
01/19/2006US20060010880 Gas turbine engine with seal assembly
01/19/2006US20060010878 Method of cooling centerbody of premixing burner
01/19/2006US20060010876 Method of operating a gas turbine group
01/19/2006US20060010874 Cooling aft end of a combustion liner
01/19/2006DE19713268B4 Gekühlte Gasturbinenschaufel A cooled gas turbine blade
01/19/2006DE102004030325A1 Gas turbine for airplanes has gas guide that leads exhaust gas to heat exchanger such that heat from exhaust gas is emitted to compressed fresh gas in compressor chamber
01/19/2006CA2573076A1 Cooling arrangement for an accessory gearbox and method of cooling
01/19/2006CA2509788A1 Foreign object damage tolerant nacelle anti-icing system
01/18/2006EP1617053A2 Gas turbine engine bleed air power assist system and method
01/18/2006EP1617042A2 Noise control
01/18/2006EP1617041A1 Turbocharger with air cooled turbine disc
01/18/2006EP1616931A1 Modified fuel burning gas turbine and method of operating the same
01/18/2006CN2752444Y Double working medium combination circulate turbomachine
01/18/2006CN1721670A Improvement of cooling aft end of a combustion liner
01/18/2006CN1721660A Turbine airfoil trailing edge repair and methods therefor
01/18/2006CN1721659A Hot gas path component with a meshed and dimpled cooling structure
01/18/2006CN1237263C Gas turbine controlling apparatus and gas turbine system using same
01/18/2006CN1237262C Device for fixing turbo charger to base
01/18/2006CN1237260C Dimethyl ether fuel and method for producing power in dry low NO2 fuel system
01/18/2006CN1237258C 涡轮叶片 Turbine blades
01/18/2006CN1237197C Method for plasma coating turbine blade and coating device
01/17/2006US6986951 Cobalt-based alloy for the coating of organs subject to erosion by liquid
01/17/2006US6986940 Fiber reinforced composite article, fiber member, and method for making
01/17/2006US6986814 Gas distributor for vapor coating method and container
01/17/2006US6986257 Methods for regulating gas turbine engine fluid flow
01/17/2006US6986256 Gas turbine having a cooling air system and a spray air system
01/17/2006US6986255 Piloted airblast lean direct fuel injector with modified air splitter
01/17/2006US6986254 Method of operating a flamesheet combustor
01/17/2006US6986201 Methods for replacing combustor liners
01/17/2006CA2392384C Operation method for combined plant
01/13/2006CA2511892A1 Cowling for turbine engine nozzle with jet noise reduction patterns
01/12/2006WO2006002523A1 A method of increasing the efficiency of a fuel gas turbine by cooling combustion air
01/12/2006US20060009950 Methods and apparatus for assessing gas turbine engine damage
01/12/2006US20060005547 Cooling arrangement for an accessory gearbox and method of cooling
01/12/2006US20060005546 Modulated flow turbine nozzle
01/12/2006US20060005545 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
01/12/2006US20060005527 Highly supercharged regenerative gas turbine
01/12/2006US20060005526 Combustor controller
01/12/2006DE10393442T5 Verbrennersteuerung Verbrennersteuerung
01/11/2006EP1614880A1 Gas turbine engine
01/11/2006EP1614879A1 Gas turbine cooling system and method
01/11/2006EP1614878A1 Method and apparatus for filtering an air mixture in a gas turbine
01/11/2006EP1614865A1 Stiffener for the low pressure compressor of an aeroengine
01/11/2006EP1614862A1 Gas turbine and gas turbine cooling and sealing method
01/11/2006EP1614858A1 Method and apparatus for monitoring the cooling system of a turbine
01/11/2006EP1614855A1 Turbomachine and method to operate such a turbomachine
01/11/2006CN1236227C Method and device for supplying fuel to a premix burner
01/11/2006CN1236202C 热和电力供给系统及其操作方法 Heat and electric power supply system and method of operation
01/10/2006US6984801 Method of closing a hole in a gas turbine blade top by laser welding
01/10/2006US6984112 Methods and apparatus for cooling gas turbine rotor blades
01/10/2006US6984103 Triple circuit turbine blade
01/10/2006US6983608 Methods and apparatus for assembling gas turbine engines
01/10/2006US6983607 Turbine compartment ventilation control system and method using variable speed fan
01/10/2006US6983606 Integrated gas turbine compressor-rotary fuel injector
01/10/2006US6983599 Combustor member and method for making a combustor assembly
01/10/2006US6983588 Turbofan variable fan nozzle
01/10/2006CA2208154C Method for the combined generation of synthesis gas and power
01/05/2006US20060000944 Aircraft engine with means of suspension from the structure of an aircraft
01/05/2006US20060000220 Acoustically stiffened gas-turbine fuel nozzle
01/05/2006US20060000219 Apparatus for observing combustion conditions in a gas turbine engine
01/05/2006DE102004029696A1 Plattformkühlanordnung für den Leitschaufelkranz einer Gasturbine Platform cooling arrangement for a gas turbine vane ring
01/05/2006DE102004028530A1 Verfahren zum Betrieb einer Kraftwerksanlage Method for operating a power plant
01/05/2006DE102004028224A1 Verfahren zum Betreiben eines Turboladers sowie Turbolader A method of operating a turbocharger and turbocharged
01/04/2006EP1612769A2 High admittance acoustic liner
01/04/2006EP1612375A2 Cooling in a humid air turbine power plant
01/04/2006EP1612371A1 Integrated gearless and non-lubricated auxiliary power unit
01/04/2006EP1611465A2 Method and apparatus for converting or otherwise utilizing radiation pressure to generate mechanical work
01/04/2006EP1611337A1 Anti-detonation fuel delivery system
01/04/2006EP1397588B1 Method for operating an internal combustion engine
01/04/2006EP1062415B1 Apparatus for water injection in a turbine
01/04/2006CN1715626A Method of informing pilot of aircraft of spark detected in gasturbine engine
01/04/2006CN1715625A Passive high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine
01/04/2006CN1714989A Homogeneous welding via pre-heating for high strength superalloy joining and material deposition
01/04/2006CN1234963C Gas turbine and gas turbine generator
01/03/2006US6983199 Vibration measurement and recording system and method
01/03/2006US6981845 Blade for a turbine comprising a cooling air deflector
01/03/2006US6981841 Triple circuit turbine cooling
01/03/2006US6981360 Gas turbine power generator having humidifying and cooling means
01/03/2006US6981359 Centrifugal pump fuel system and method for gas turbine engine
01/03/2006CA2401945C Joint structure of coolant passage, tube seal and gas turbine
12/2005
12/30/2005CA2473033A1 A method of increasing the efficiency of a fuel gas turbine by cooling combustion air
12/29/2005WO2005124125A1 Method for operating a gas turbine compressor while cooling the compressor intake air by evaporation
12/29/2005WO2005106225A3 Fuel controls on apu’s