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)
03/2009
03/10/2009US7500349 Power plant and operating method
03/10/2009US7500347 Variable geometry combustor
03/05/2009WO2009028475A1 Gas turbine combustor
03/05/2009WO2009028474A1 Gas turbine combustor
03/05/2009WO2008091502A4 Power augmentation of combustion turbines by injection of cold air upstream of compressor
03/05/2009US20090061369 Multi-response time burner system for controlling combustion driven pulsation
03/05/2009US20090056343 Engine mounting configuration for a turbofan gas turbine engine
03/05/2009US20090056337 Turbomachine with annular combustion chamber
03/05/2009US20090056335 Gas turbine engine combustor assembly having integrated control valves
03/05/2009US20090056306 Gas turbine engine front architecture
03/05/2009US20090056303 Cooling apparatus, gas turbine system using cooling apparatus, heat pump system using cooling system, cooling method, and method for operating cooling apparatus
03/05/2009DE102008044478A1 Support system for rotor and stator of rotary machine, has pedestal, which is connected operationally with bearing of rotor and support base
03/05/2009DE102008044476A1 Verfahren und Systeme für Turbinenteillast-Betriebsbedingungen Methods and systems for turbine part load operating conditions
03/04/2009EP2030892A1 Suspension pylon for an engine beneath an aircraft wing
03/04/2009CN201202537Y Oil seal control device of aviation turbo fan engine under off-machine state
03/04/2009CN201202536Y Reutilization apparatus of natural gas pipe network pressure energy in gas turbine working field
03/04/2009CN201202535Y Turbine type single-stage centrifugal rotor engine
03/04/2009CN101377134A Rotor-stator-support system of gas turbinen
03/03/2009US7497300 Noise reduction tubes
03/03/2009US7497220 Method and apparatus for cleaning a turbofan gas turbine engine
03/03/2009US7497083 Fuel supply system
02/2009
02/28/2009CA2639217A1 Electricity generation in a turbine engine
02/28/2009CA2639209A1 Ventilation and pressurization of components in a turbomachine
02/28/2009CA2632589A1 Systems for supplying oil from an oil source to a bearing assembly
02/26/2009WO2008132009A3 Sound absorption device for a jet engine or a turbine
02/26/2009US20090053424 Method for repairing high temperature articles
02/26/2009US20090053055 Seal assembly
02/26/2009US20090053046 Method, system and apparatus for turbine diffuser sealing
02/26/2009US20090053045 Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud
02/26/2009US20090049840 Optimizing an anti-coke film in an injector system
02/26/2009US20090049839 Jet aircraft engine with ionized throughflow
02/26/2009US20090049838 Turbine fuel delivery apparatus and system
02/26/2009US20090049837 Gas turbine engine air valve assembly
02/26/2009US20090049836 Thermally powered turbine inlet air chiller heater
02/26/2009DE4034012A1 Schmiersystem für Flugzeugtriebwerke Lubrication system for aircraft engines
02/26/2009DE102008044442A1 Systeme und Verfahren zur Erweiterung des Emissionseinhaltungsbereichs bei Gasturbinen Systems and methods for extending the range of emission compliance for gas turbines
02/26/2009DE102008044436A1 Verfahren zur Versorgung einer Gasturbine mit Kühlmedien Process for supplying a gas turbine with cooling media
02/26/2009DE102008044435A1 Vorrichtung und Verfahren zur Reduzierung von Unrundlauf und Unwucht in Turbinen Apparatus and method for reducing runout and unbalance in turbines
02/26/2009DE102008044434A1 Schallhaube für eine Gasturbine und Verfahren zum Umschliessen derselben Acoustic enclosure for a gas turbine and method for enclosing the same
02/25/2009EP2028422A2 Variable amplitude double binary valve system for active fuel control
02/25/2009EP2028375A2 Nose cone for an airplane turbine engine with integrated balancing ring
02/25/2009EP2028352A1 Gas turbine engine with means of driving the turbine accessory drive gearbox assembly and method of assembling said engine
02/25/2009EP1831530B1 Compressor variable stage remote actuation for turbine engine
02/25/2009EP1699698B1 Ram air channel for the supply of ambient air in an aircraft
02/25/2009CN101374723A Dual flow turbine engine equipped with a precooler
02/25/2009CN101374722A Dual flow turbine engine equipped with a precooler
02/25/2009CN101373753A Switching assembly for an aircraft ignition system
02/25/2009CN101372915A Single element miniature turbogenerating system
02/25/2009CN101372903A Enclosure for a gas turbine and method for enclosing the same
02/25/2009CN101372902A Gas turbine shroud support apparatus
02/25/2009CN101372900A Combustion turbine cooling media supply method
02/24/2009US7495354 Gas turbine, particularly an aircraft engine
02/24/2009US7494619 High temperature alloys, and articles made and repaired therewith
02/24/2009US7494522 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) - centrifuge chamber/manifold particle collector
02/24/2009US7493771 Methods and apparatuses for assembling a gas turbine engine
02/24/2009US7493767 Method and apparatus for cooling combustor liner and transition piece of a gas turbine
02/23/2009CA2639171A1 Gas turbine engine with means for driving the accessory drive and mounting process of said motor
02/22/2009CA2638585A1 Fuel nozzle for a gas turbine engine
02/19/2009WO2009022449A1 Combustor
02/19/2009US20090044543 Jet engine with compressor air circulation and method for operating the jet engine
02/19/2009US20090044539 Fuel lance for a gas turbine installation and a method for operating a fuel lance
02/19/2009US20090044536 Gas turbine power generator plant and silencer for the same
02/19/2009US20090044512 Dirt separator for compressor diffuser in gas turbine engine
02/19/2009DE102008002981A1 Brennkammereinsatzanschlag in einer Gasturbine Combustor liner stop in a gas turbine
02/19/2009DE102007036995A1 Ausführung und Schnittstellen eines wassergekühlten Turbinengehäuse für einen Abgasturbolader Implementation and interfaces of a water-cooled turbine housing for an exhaust gas turbocharger
02/19/2009DE102007036916A1 Turbocharger, particularly exhaust gas turbocharger for combustion engine, has turbine, which has turbine rotor, compressor, which has compressor rotor and shaft on which turbine rotor and compressor rotor are mounted in torque proof manner
02/19/2009DE102007036912A1 Turbocharger for use in internal-combustion engine of motor vehicle, has pair of starting units approaching surfaces of central disk, and radial bearing arranged on both sides of axial bearing
02/18/2009EP2026006A1 Turbomachine with diffuser
02/18/2009EP2025901A2 Fuel metering system with minimal heat input
02/18/2009EP2025899A2 An engine arrangement
02/18/2009EP2025898A2 Engine mounting configuration for a turbofan gas turbine engine
02/18/2009EP2025895A2 Counter-rotatable fan gas turbine engine
02/18/2009EP2025881A2 Electric motor driven lubrication pump and lubrication system prognostic and health management system and method
02/18/2009EP2025876A2 Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
02/18/2009EP2025875A2 Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
02/18/2009EP2024620A1 Method of operating a gas turbine, application of the method in a combined cycle power plant, and combined cycle power plant for carrying out the method
02/18/2009EP1781915B1 Compressed-air generating system
02/18/2009CN101368515A Apparatus and method for monitoring compressor clearance and controlling a gas turbine
02/18/2009CN101368512A Turbine engine diffuser
02/18/2009CN101368510A Cut-spraying type engine
02/18/2009CN100462531C System and method for improving efficiency of combined cycle electric power plant
02/17/2009US7491253 Engine intake system with accessible, interchangeable air filters
02/17/2009US7490472 Efficient combined cycle power plant with CO2 capture and a combustor arrangement with separate flows
02/17/2009CA2413637C Improved liquid fuel injector for burners of gas turbines
02/17/2009CA2382493C Play measuring sensor by multiple depth abrasion
02/17/2009CA2357583C Process for producing a protective coating that forms a thermal barrier with an underlying binding layer on a superalloy substrate and the resulting item
02/16/2009CA2597846A1 Pilot fuel injector for mixer assembly of a high pressure gas turbine engine
02/12/2009WO2008152259A3 Acoustic panel having a variable acoustic characteristic
02/12/2009WO2008132400A3 System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft
02/12/2009US20090042070 Barometric thermal trap and collection apparatus and method thereof for combining multiple exhaust streams into one
02/12/2009US20090041610 Gas turbine honeycomb seal
02/12/2009US20090038315 Ion pump and an electrochemical engine using same
02/12/2009US20090038313 Method and apparatus for supplying pressure for spray inlet temperature suppressor of gas turbines
02/12/2009US20090038312 Multipoint injector for turbomachine
02/12/2009DE102008000050A1 Brenner für eine Brennkammer einer Turbogruppe Burner for a combustor of a turbine group
02/11/2009EP2022965A1 Axial flow fluid device
02/11/2009EP2022962A2 High humidity gas turbine equipment
02/11/2009EP2022947A2 Deicing method and device for variable inlet guide vanes of a compressor
02/11/2009EP2021602A1 Modular fuel supply device for a gas turbine
02/11/2009EP2021601A1 Gas turbine engine starting method and control device