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 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
06/2010
06/10/2010US20100143094 Bearing-chamber pressure system
06/10/2010US20100139900 Gas Turbine Regenerator Apparatus and Method of Manufacture
06/10/2010US20100139288 Heat exchanger to cool turbine air cooling flow
06/10/2010US20100139282 Oxidizing Fuel in Multiple Operating Modes
06/10/2010US20100139280 Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event
06/10/2010US20100139279 Fuel delivery system and method of assembling the same
06/10/2010US20100139238 Combustor Housing for Combustion of Low-BTU Fuel Gases and Methods of Making and Using the Same
06/10/2010DE102008061184A1 Compressor for driving mechanism, particularly for aircraft engines and gas turbines, has compressor housing, where injection nozzle group is arranged in circumferential direction of compressor housing
06/10/2010CA2744474A1 Gas turbine with external combustion, applying a rotating regenerating heat exchanger
06/10/2010CA2688042A1 Heat exchanger to cool turbine air cooling flow
06/09/2010EP2194536A1 Closed cycle plant
06/09/2010EP2194296A2 Lubricating system for gear train
06/09/2010EP2194233A2 Flow splitter for a fan engine
06/09/2010CN201502544U Gas turbine-powered air compressor
06/09/2010CN201502543U Novel air compressor
06/09/2010CN1892000B Igniter tube and method of assembling same
06/09/2010CN1798634B A turbine blade
06/09/2010CN101730791A Turbojet engine for aircraft
06/09/2010CN101725414A System and method for heating a fuel using an exhaust gas recirculation system
06/09/2010CN101725413A Steam cooled direct fired coal gas turbine
06/09/2010CN101725412A A system and method for changing the efficiency of a combustion turbine
06/09/2010CN101725411A Oilway structure of lubricating oil outlet of turbocharger bearing body
06/09/2010CN101725410A Water washing device for gas turbine
06/09/2010CN101392685B Internal waverider hypersonic inlet and design method based on random shock form
06/09/2010CN101333965B Microminiature turbine jet rotor swirling control method
06/09/2010CN101270690B Fuel oil and lubricating oil heat exchanger of light aircraft engine
06/09/2010CN101225769B Power augmentation of combustion turbines by injection of cold air upstream of compressor
06/09/2010CN101189411B Gas turbine with a gap blocking device
06/09/2010CN101126353B 燃气轮机系统和燃气轮机控制方法 Gas turbine and gas turbine system control method
06/08/2010US7730713 Gas turbine power plant
06/08/2010CA2555056C Multi spool gas turbine system
06/08/2010CA2434211C Process and device for gas-phase diffusion coating of metallic components
06/08/2010CA2429414C Metallic cellular structure
06/08/2010CA2398653C Air intake for commercial aircraft jet engine nacelle
06/08/2010CA2394462C Device for the attachment of an engine to an aircraft
06/04/2010CA2686368A1 Torsional mode damping apparatus
06/03/2010WO2010062494A1 Nacelle and method of assembling the same
06/03/2010WO2010062209A1 Oil cooled runner
06/03/2010WO2010060827A1 Device for sealing a bearing housing of an exhaust gas turbocharger
06/03/2010US20100135822 Turbine blade for a gas turbine engine
06/03/2010US20100133832 Aeroengine starter/generator arrangement
06/03/2010US20100133378 Acoustic panel having a variable acoustic characteristic
06/03/2010US20100132378 Hydraulic system for transmission of forces between an aircraft turboprop and an attachment device
06/03/2010US20100132377 Fabricated itd-strut and vane ring for gas turbine engine
06/03/2010US20100132376 Mid turbine frame for gas turbine engine
06/03/2010US20100132375 Attachment structure of combustion oscillation detecting device
06/03/2010US20100132374 Turbine frame assembly and method for a gas turbine engine
06/03/2010US20100132373 Mid turbine frame for gas turbine engine
06/03/2010US20100132372 Mid turbine frame for gas turbine engine
06/03/2010US20100132371 Mid turbine frame system for gas turbine engine
06/03/2010US20100132370 Mid turbine frame system for gas turbine engine
06/03/2010US20100132369 Mid turbine frame system for gas turbine engine
06/03/2010US20100132365 Start-Up Control For a Compact Lightweight Turbine
06/03/2010US20100132363 Turbomachine with separate fuel injection systems, using identical sealing joints
06/03/2010US20100132331 Baffle seal for gas turbine engine thrust reverser
06/03/2010US20100132330 Method and apparatus for suppressing aeroengine contrails
06/03/2010CA2743593A1 Nacelle and method of assembling the same
06/03/2010CA2737118A1 Oil cooled runner
06/03/2010CA2686004A1 System for thermal protection and damping of vibrations and acoustics
06/02/2010EP2192291A2 Aeroengine starter/generator arrangement
06/02/2010EP2192290A1 Damping device and gas turbine combustor
06/02/2010EP2192289A1 Intake silencer for gas turbine
06/02/2010EP2192272A1 Device for sealing a bearing box of a turbocharger
06/02/2010DE19882251B4 Umgehungsluft-Steuerungsvorrichtung zum Steuern des Volumens von Luft, die von der Brennkraftmaschine einer Gasturbine umgeleitet wird Bypass air control means for controlling the volume of air that is diverted from the internal combustion engine of a gas turbine
06/02/2010DE102009044103A1 Turbinengehäuseanordnung und Verfahren für eine Gasturbine Turbine housing assembly and method for a gas turbine
06/02/2010DE102008059598A1 Exhaust gas turbocharger for internal-combustion engine of motor vehicle, has bearing arrangement with cone bearings e.g. hydrodynamic sliding bearings that are axially spaced from each other and have opposite tapers
06/02/2010DE102008058157A1 Bearing bush for hydrodynamic journal bearings for supporting rotor in stator, particularly exhaust gas turbocharger, has radially inner bearing surface, which has porous upper surface structure or forms porous upper surface structure
06/02/2010DE102008049195A1 Shaft sealing for use in steam turbine, has sealing rings fixed at external housing and sealing ring contact at cylinder bearing surfaces of rotor shaft, so that sealing projection touches on surfaces when rotor shaft rotates in housing
06/02/2010DE102005013421B4 Einlaufkonus für ein Gasturbinentriebwerk Inlet cone for a gas turbine engine
06/02/2010CN101718228A Method and system for operating a turbomachine having an unchoked valve
06/02/2010CN101718227A Heat flow turbine
06/02/2010CN101718226A Non-intermittent detonation rotor of engine
06/02/2010CN101418723B Internal waverider-derived hypersonic inlet with ordered inlet and outlet shape and design method
06/02/2010CN101270689B Energy conversion and recovering method of coal gasification supercharging association circulating power generation system
06/02/2010CN101144430B Tower type flame holder for rotor engine
06/01/2010US7726951 Fuel control module
06/01/2010US7726133 Method for operating a burner of a gas turbine and a power plant
06/01/2010US7726022 Method of dismantling a portion of a turbomachine
06/01/2010CA2606580C Improved inlet plenum for gas turbine engine
06/01/2010CA2464209C Turbine engine with air cooled turbine
06/01/2010CA2443352C Gas turbine, vehicle comprising said gas turbine and method for engine-braking a gas turbine
06/01/2010CA2364951C Procedure for manufacturing a protected laminated soundproofing panel and the acoustic panel produced by the procedure
05/2010
05/28/2010CA2672125A1 Mid turbine frame for gas turbine engine
05/27/2010WO2010058356A2 Valves for gas-turbines and multipressure gas-turbines, and gas-turbines therewith
05/27/2010WO2009153478A3 Compressor cover for turbine engine having axial abutment
05/27/2010US20100129226 Axial retention of a platform seal
05/27/2010US20100129202 Gas turbine engine
05/27/2010US20100129197 Method and system for cooling engine components
05/27/2010US20100129196 Cooled gas turbine vane assembly
05/27/2010US20100129195 Castings, Casting Cores, and Methods
05/27/2010US20100129194 Castings, Casting Cores, and Methods
05/27/2010US20100127118 Device for attaching an aircraft engine and aircraft comprising at least one such device
05/27/2010US20100126184 Combustion chamber arrangement for operating a gas turbine
05/27/2010US20100126183 Cmc mixer with structural outer cowling
05/27/2010US20100126182 Flush inlet scoop design for aircraft bleed air system
05/27/2010US20100126181 Method for controlling an exhaust gas recirculation system
05/27/2010US20100126179 Method for the start-up of a gas turbine
05/27/2010US20100126176 Dual swirler
05/27/2010US20100126174 Gas turbine combustion chamber
05/27/2010US20100126137 Combustion Installation
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