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)
05/2010
05/11/2010US7712317 Flow control systems
05/11/2010US7712316 Turbine blade with reverse cooling air film hole direction
05/11/2010US7712302 Crossfire tube assembly for gas turbines
05/11/2010US7712301 System and method for augmenting turbine power output
05/11/2010US7712300 Water treatment and pressurization system for the adiabatic cooling of comburent air
05/11/2010CA2676773A1 Fuel injector
05/11/2010CA2464414C High pressure turbine blade cooling scoop
05/11/2010CA2460662C Methods and apparatus for assembling gas turbine engines
05/11/2010CA2357942C System and method for direct non-intrusive measurement of corrected airflow
05/06/2010WO2010051453A2 Turbine blade including a seal pocket
05/06/2010WO2010051011A1 Systems and methods for thermal management in a gas turbine powerplant
05/06/2010WO2010050609A1 Fluid valve drive mechanism
05/06/2010WO2010050248A1 Method for manufacturing turbine wheel
05/06/2010WO2009075721A3 Sequential combustion firing system for a fuel system of a gas turbine engine
05/06/2010US20100111691 Turbine engine components
05/06/2010US20100111681 Bearing device of gas turbine power generation equipment and gas turbine power generation equipment
05/06/2010US20100111679 Asymmetrical gas turbine cooling port locations
05/06/2010US20100111670 Shroud hanger with diffused cooling passage
05/06/2010US20100109338 Method for providing auxiliary power to an electric power plant using fischer tropsch technology
05/06/2010US20100107653 Nozzle tip assembly with secondary retention device
05/06/2010US20100107652 Hybrid propulsive engine including at least one independently rotatable compressor rotor
05/06/2010US20100107651 Hybrid propulsive engine including at least one independently rotatable compressor stator
05/06/2010US20100107649 Gas Turbine Engine With Fuel Booster
05/06/2010US20100107648 Method and System for Starting a Turboshaft Engine by Cold Weather
05/06/2010US20100107647 Toroidal boundary layer gas turbine
05/06/2010US20100107645 Combustor liner cooling flow disseminator and related method
05/06/2010US20100107644 Combustion pre-chamber
05/06/2010US20100107641 Method and apparatus for affecting a recirculation zone in a cross flow
05/06/2010US20100107640 Air cooling apparatus for a purge valve
05/06/2010US20100107639 Fuel nozzle assembly for use with a gas turbine engine and method of assembling same
05/06/2010US20100107603 Systems and methods for thermal management in a gas turbine powerplant
05/06/2010US20100107594 Turbine integrated bleed system and method for a gas turbine engine
05/06/2010US20100107593 Integrated Cooling, Heating, and Power Systems
05/06/2010US20100107592 System and method for reducing corrosion in a gas turbine system
05/06/2010DE19645322B4 Kombinierte Kraftwerksanlage mit einem Zwangsdurchlaufdampferzeuger als Gasturbinen-Kühlluftkühler Combined power plant with a once-through steam generator as the gas turbine cooling air cooler
05/06/2010DE102008037513A1 Baffle seal for deflector flap arrangement of thrust-reverser for gas turbine, has sealing edge including outer peripheral area that extends-out over outer peripheral area of central section, in order to define exposed sealing surface
05/05/2010EP2182290A1 Gas turbine combustor
05/05/2010EP2182195A1 Gas turbine combustor
05/05/2010EP2182178A2 Particle separator and separating method for gas turbine engine
05/05/2010EP2182086A1 Ni-BASE ALLOY-HIGH CHROMIUM STEEL STRUCTURE AND PROCESS FOR PRODUCING THE NI-BASE ALLOY-HIGH CHROMIUM STEEL STRUCTURE
05/05/2010CN1965154B Absorber silencer for compressors
05/05/2010CN101023256B Gas turbine apparatus, low calorie content gas feeding apparatus, and method of suppressing rise of calorie content of the gas
05/05/2010CN101023255B Gas turbine apparatus, low calorie content gas feeding apparatus, and method of suppressing rise of calorie content of the gas
05/04/2010US7710058 Motor drive architecture for high frequency AC bus
05/04/2010US7707818 Exhaust stacks and power generation systems for increasing gas turbine power output
05/04/2010CA2683382A1 Bearing support structure for turbine
05/04/2010CA2642777A1 Baffle seal for gas turbine engine thrust reverser
05/04/2010CA2598276C Gas turbine fuel preparation and introduction method
05/04/2010CA2371763C Concentricity ring
04/2010
04/29/2010WO2010046553A1 Ventilation of a high-pressure turbine in a turbomachine
04/29/2010US20100104901 Gasification equipment
04/29/2010US20100104426 Turbine engine ring seal
04/29/2010US20100101234 Evaporative Cooler and Use Thereof and Gas Turbine System Featuring an Evaporative Cooler
04/29/2010US20100101233 Cooling Temperature Ladder and Applications Thereof
04/29/2010US20100101232 Compliant metal support for ceramic combustor liner in a gas turbine engine
04/29/2010US20100101229 Flame Holding Tolerant Fuel and Air Premixer for a Gas Turbine Combustor
04/29/2010US20100101205 Device for deflection and retention of aircraft engine debris
04/29/2010DE10344843B4 Integrierte Rotations-Messerkanten-Injektionsanordnung Integrated rotary knife-edge injection assembly
04/29/2010DE10329849B4 Anlage mit kombiniertem Zyklus vom 1-Achsen-Typ Combined cycle plant from the 1-axis type
04/29/2010DE102009043830A1 Flammenhaltungs-toleranter Brennstoff/Luft-Vormischer für eine Gasturbinenbrennkammer Flames entertainment tolerant fuel / air pre-mixer for a gas turbine combustor
04/29/2010CA2739219A1 Ventilation of a high-pressure turbine in a turbomachine
04/28/2010EP2180166A1 Ignition and chemical reaction accelerator and flame stabilizer, speed-type internal combustion engine, and furnace
04/28/2010EP2180165A2 A system and method for changing the efficiency of a combustion turbine
04/28/2010EP2180164A1 Method and system for altering engine air intake geometry
04/28/2010EP2180161A2 A system and method for heating a fuel using an exhaust gas recirculation system
04/28/2010CN1510415B Method for selecting adhesive, product and system thereof
04/28/2010CN1497148B Method and device for controlling fluid flow of gas turbine engine
04/27/2010US7703289 Internal fuel manifold having temperature reduction feature
04/27/2010US7703272 System and method for augmenting turbine power output
04/27/2010CA2454278C Method for operating a burner of a gas turbine, and power plant installation
04/27/2010CA2428167C Device to join two tubular parts from an aircraft turbojet engine
04/24/2010CA2682865A1 A system and method for changing the efficiency of a combustion turbine
04/24/2010CA2673139A1 Diffuser case removal apparatus and method
04/22/2010WO2010044958A1 Methods and systems for controlling the products of combustion
04/22/2010WO2010043778A1 Sealing between a combustion chamber and a turbine distributor in a turbine engine
04/22/2010WO2010024989A3 Multi passage fuel manifold and methods of construction
04/22/2010US20100095683 Gas turbine engine and system for servicing a gas turbine engine
04/22/2010US20100095682 Removing Particulate Matter From Air
04/22/2010US20100095679 Dual wall structure for use in a combustor of a gas turbine engine
04/22/2010US20100095678 Heat Shield Sealing for Gas Turbine Engine Combustor
04/22/2010US20100095676 Multiple Tube Premixing Device
04/22/2010US20100095649 Staged combustion systems and methods
04/22/2010DE202009014217U1 Einteilige Triebwerk-Frontschutzabdeckung One-piece engine-Front cover
04/22/2010DE102009026400A1 Systeme und Verfahren für gestufte Verbrennung Systems and methods for staged combustion
04/22/2010DE102008052321A1 Turbocharger i.e. exhaust gas turbocharger, for motor vehicle, has rotor shaft comprising magnetic bearing arrangement with axial bearing device with pole, where shaft is positioned such that gravitational force works against magnetic force
04/22/2010DE102008052261A1 Exhaust gas turbocharger for internal combustion engine, particularly motor vehicle, has shaft, which rotates compressor and turbine wheel
04/22/2010CA2737133A1 Methods and systems for controlling the products of combustion
04/21/2010EP2178191A2 Free-piston unit
04/21/2010EP2177831A2 Method and apparatus of fuel nozzle diluent introduction
04/21/2010EP2177735A2 Turbofan
04/21/2010CN1816683B Turbine shroud segment
04/20/2010USRE41229 Methods and apparatus for regulating gas turbine engine fluid flow
04/20/2010US7698884 Power transmission arrangement
04/15/2010WO2010041552A1 Gas turbine and operating method therefor
04/15/2010WO2010040907A1 Air intake structure for a turbine engine nacelle
04/15/2010WO2010021807A3 Fuel injector sans support/stem
04/15/2010WO2010012899A3 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
04/15/2010US20100092281 Turbine ring assembly for gas turbine
04/15/2010US20100092280 Steam Cooled Direct Fired Coal Gas Turbine
04/15/2010US20100089068 Combustion liner damper