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)
08/2006
08/17/2006US20060179845 Extended operability aircraft fuel delivery system
08/17/2006US20060179816 Cooled dual wall liner closeout
08/17/2006US20060179815 Passive exhaust suppressor and method
08/17/2006CA2596805A1 Method for machining an integrally bladed rotor
08/16/2006EP1691056A1 Bypass turbofan engine with means to drive the gearbox
08/16/2006EP1691055A2 Intercooling in gas turbine engines
08/16/2006EP1691054A1 Gas Turbine
08/16/2006EP1689992A2 Method and apparatus for actuating fuel trim valves in a gas turbine
08/16/2006EP1386070B1 Method for cooling a gas turbine and gas turbine installation
08/16/2006EP0974737B1 Combined cycle power plant
08/16/2006CN1819874A Water distribution and vaporization assembly.
08/16/2006CN1818527A Heat shield
08/16/2006CN1818362A Inboard radial dump venturi for combustion chamber of a gas turbine
08/16/2006CN1818361A Multiple venturi tube gas fuel injector for a combustor
08/16/2006CN1270066C Gas turbine and method for operating gas turbine
08/16/2006CN1270065C Installation for generation of energy
08/16/2006CN1269995C Fin stripping system with feedback control of water treatment and acid reusing system
08/15/2006US7090459 Hybrid seal and system and method incorporating the same
08/15/2006US7090224 Seal device
08/15/2006US7090165 Aeroengine nacelle
08/15/2006US7089748 Combustion chamber, in particular of a gas turbine
08/15/2006US7089745 System for vaporization of liquid fuels for combustion and method of use
08/15/2006US7089744 Onboard supplemental power system at varying high altitudes
08/15/2006US7089743 Method for operating a power plant by means of a CO2 process
08/15/2006US7089741 Gas turbine combustor
08/15/2006US7089728 Single-piece turbine rotor and pinion gear and manufacturing technique for same
08/15/2006US7089727 Gas turbine plant with an exhaust gas chimney
08/11/2006CA2536129A1 Two-spool turboshaft engine with means of power take-off on the low pressure and high pressure rotors, power take-off module for the turboshaft engine and process for mounting theturboshaft engine
08/11/2006CA2535094A1 Methods and apparatus for operating gas turbine engines
08/10/2006WO2006081676A1 Low cost pressure atomizer
08/10/2006WO2006081675A1 Variable arc gap plasma igniter element
08/10/2006US20060174627 Gas turbine cycle
08/10/2006CA2612687A1 Variable arc gap plasma igniter element
08/09/2006EP1688669A1 Integral heater for fuel conveying member
08/09/2006EP1688024A1 Control arrangement
08/09/2006EP1687518A1 Power generation
08/09/2006EP1570566B1 Gas turbine engine starter generator with multiple windings on each exciter stator pole
08/09/2006EP1252370B1 Chemical cleaning solution for gas turbine blades
08/09/2006CN1816934A Fuel cell/constant pressure turbine/hybrid system
08/09/2006CN1816684A Electrical power generation system and method
08/09/2006CN1816683A Turbine shroud segment
08/09/2006CN1816682A Turbine shroud segment
08/09/2006CN1816681A Turbine shroud segment
08/08/2006US7086830 Tube-type vortex reducer with retaining ring
08/08/2006US7086235 Cascade ignition of catalytic combustors
08/08/2006US7086234 Gas turbine combustion chamber with defined fuel input for the improvement of the homogeneity of the fuel-air mixture
08/08/2006US7086232 Multihole patch for combustor liner of a gas turbine engine
08/08/2006US7086231 Thermal and compressed air storage system
08/08/2006US7086219 Cowl structure for a gas turbine engine
08/08/2006CA2496697A1 Differential power transmission for expander driven compressor machines
08/08/2006CA2408881C Thermal barrier coating material, gas turbine parts and gas turbine
08/08/2006CA2222607C A liquefied natural gas (lng) fueled combined cycle power plant and an lng fueled gas turbine plant
08/04/2006CA2532605A1 Tube heat shield and method of making same
08/03/2006WO2006080386A1 Turbofan engine
08/03/2006WO2006080057A1 Gas turbine apparatus, apparatus for supplying fuel gas and method for suppressing calorie elevation of fuel gas
08/03/2006WO2006080055A1 Turbofan engine
08/03/2006WO2006080054A1 Gas calorie variation suppressing device, fuel gas supply facility, gas turbine facility, and boiler facility
08/03/2006WO2006079438A1 Intercooled turbo-compressor
08/03/2006WO2006044291A3 Wirelless terminal location using apparatus and methods employing carrier diversity
08/03/2006US20060168968 Systems and methods for starting aircraft engines
08/03/2006US20060168966 Self-Purging Pilot Fuel Injection System
08/03/2006DE102005003853A1 Gas turbine for aircraft engine has generator which is used as an engine to drive the rotor of respective turbine after gas turbine is switched off for certain period of time and through this it cause uniform cooling to rotor
08/02/2006EP1686058A1 Aircraft inlet assembly for reducing auxiliary power unit noise
08/02/2006EP1685310A1 Sealing arrangement in a compressor
08/02/2006CN1811148A Alcohol fuel cracking device for gas turbine
08/01/2006US7083389 Compressor for gas turbines
08/01/2006US7082771 Combustion chamber
08/01/2006US7082769 Helicopter turbine engine protection system
08/01/2006US7082768 Method for injecting a fuel-air mixture into a combustion chamber
08/01/2006US7082748 Gas turbine installation
07/2006
07/31/2006CA2534213A1 Inboard radial dump venturi for combustion chamber of a gas turbine
07/27/2006WO2006077670A1 Method for local application of diffusion aluminide coating
07/27/2006WO2006077642A1 Method of correcting balance of gas turbine
07/27/2006WO2006076809A1 Evacuation of hot gases accumulated in an inactive gas turbine engine
07/27/2006US20060166014 Formation of corrosion-resistant coating
07/27/2006US20060165893 Thermal barrier coating protected by alumina and method for preparing same
07/27/2006US20060162339 Gas turbine engine component having bypass circuit
07/27/2006US20060162338 Evacuation of hot gases accumulated in an inactive gas turbine engine
07/27/2006US20060162316 Atmospheric pressure combustion turbine system
07/27/2006DE19736276B4 Optisches Pyrometer für Gasturbinen Optical pyrometer for gas turbines
07/27/2006DE19646527B4 Vorrichtung zur Abdichtung von zwei Räumen unterschiedlichen Druckes Device for sealing two spaces of different pressure
07/27/2006DE102004031783B4 Gas turbine for aircraft engine has fuel supply system which exhibits wave-channel in which turbine shaft is swivel mounted and part of fuel supply takes place through shaft alley, which exhibits fuel outlets at its outer circumference
07/27/2006CA2595471A1 Evacuation of hot gases accumulated in an inactive gas turbine engine
07/26/2006EP1683947A2 Method to control starter/generator cooling fuel flow during engine starting
07/26/2006EP1683742A1 Valve for dewatering of freight containers
07/26/2006EP1682758A1 Hybrid engine accessory power system
07/26/2006EP1682750A1 Power plant
07/26/2006EP1423647B1 Combustion chamber arrangement
07/26/2006EP1336036B1 Fuel gas moisturization system level control
07/26/2006CN2799870Y Charge air cooler of gas turbine unit
07/26/2006CN1808858A Turbine generator
07/26/2006CN1807861A Fuel gas heating control equipment and gas turbine power generation facility provided with the fuel gas heating control equipment
07/26/2006CN1266708C Nuclear power plant and method for adjusting its generation circuit
07/26/2006CN1266419C Coolable segment for a turbine set and combustion turbine
07/26/2006CN1266375C 燃气轮机 Gas turbine
07/25/2006US7080514 High frequency dynamics resonator assembly
07/25/2006US7080513 Seal element for sealing a gap and combustion turbine having a seal element
07/20/2006WO2006075441A1 Process quantity measurement method and device
07/20/2006WO2006074552A1 Integral heater for fuel conveying member
07/20/2006US20060156733 Integral heater for fuel conveying member