| 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) |
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| 02/11/2009 | EP1576267B1 Gas turbine power plant |
| 02/11/2009 | EP1407120B1 Method for operating a burner of a gas turbine and a power plant |
| 02/11/2009 | CN101365870A Infrared suppression system |
| 02/11/2009 | CN101363367A Method and apparatus for supplying pressure for spray inlet temperature suppressor of gas turbines |
| 02/11/2009 | CN100460644C Method for operating a turbine group |
| 02/11/2009 | CN100460630C Turbine nozzle segment cantilevered mounted |
| 02/10/2009 | US7488154 Intake housing for axial fluid flow engines |
| 02/10/2009 | US7487642 Methods and apparatus for operating gas turbine engines |
| 02/10/2009 | CA2638814A1 Multipoint injector for turbine engine |
| 02/10/2009 | CA2284384C Thermal barrier coating with low thermal conductivity, metal part protected by said coating, process for depositing said coating |
| 02/07/2009 | CA2638808A1 Turbojet including a current generator mounted in the fan and a process for mounting the said generator in the fan |
| 02/05/2009 | WO2009017015A1 Turbine blade |
| 02/05/2009 | WO2009016744A1 Wing for turbine |
| 02/05/2009 | WO2009016363A1 A turbocharger bearing assembly and lubrication thereof |
| 02/05/2009 | WO2008142287A3 Method and system for starting a turboshaft engine by cold weather |
| 02/05/2009 | US20090037036 Automatic Control Systems for Aircraft Auxiliary Power Units, and Associated Methods |
| 02/05/2009 | US20090035128 Cooled turbine blade for a gas turbine and use of such a turbine blade |
| 02/05/2009 | US20090035125 Impingement cooled structure |
| 02/05/2009 | US20090035124 Hot-Gas-Ducting Housing Element, Protective Shaft Jacket and Gas Turbine System |
| 02/05/2009 | US20090031731 Wobbe control and enhanced operability through in-line fuel reforming |
| 02/05/2009 | US20090031696 Power Plant |
| 02/05/2009 | US20090031695 Methods and apparatus for mixing fluid in turbine engines |
| 02/04/2009 | EP2020500A2 Heat exchanger assembly for gas turbine engines |
| 02/04/2009 | EP2020499A2 Heat exchanger assembly for gas turbine engines |
| 02/04/2009 | CN201190607Y Preposition air cleaner |
| 02/04/2009 | CN201190596Y Side-combusting type roter internal combustion engine |
| 02/04/2009 | CN101360900A Fuel ratio control in a combustion apparatus with multiple fuel supply lines |
| 02/04/2009 | CN100458122C Methods and apparatus for assessing gas turbine damage |
| 02/04/2009 | CN100458121C Atmospheric pressure combustion turbine system |
| 02/04/2009 | CN100458106C Methods for optimizing turbine engine shell radial clearances |
| 02/04/2009 | CN100458104C Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method |
| 02/03/2009 | US7484928 Repaired turbine nozzle |
| 02/03/2009 | US7484369 Apparatus for observing combustion conditions in a gas turbine engine |
| 02/03/2009 | US7484354 Aircraft engine arrangement |
| 02/03/2009 | US7484352 Combustor for a gas turbine |
| 02/03/2009 | CA2383463C Methods and apparatus for cooling gas turbine engine combustors |
| 01/30/2009 | CA2632487A1 Methods and apparatus for mixing fluid in turbine engines |
| 01/30/2009 | CA2632469A1 Methods and apparatus for mixing fluid in turbine engines |
| 01/29/2009 | WO2009013119A1 Continuous-flow or displacement machine with magnetic bearings |
| 01/29/2009 | WO2009012556A1 Method for manufacturing of fuel nozzle floating collar |
| 01/29/2009 | US20090028699 Static gas turbine component and method for repairing such a component |
| 01/29/2009 | US20090025397 Method of Optimizing the Energy of a Site Comprising a Cogeneration System and a Thermal Power Plant |
| 01/29/2009 | US20090025393 Auxiliary power unit assembly |
| 01/29/2009 | US20090025363 Vent for the lubricating oil system of a jet engine |
| 01/29/2009 | US20090025362 Infrared suppression system with spiral septum |
| 01/29/2009 | DE102008002940A1 Fuel injector arrangement for gas turbine, has opening plate arranged inside injector body in removable manner, retaining ring holding opening plate in place, and connecting mechanism connecting ring with body in removable manner |
| 01/29/2009 | DE102008002934A1 Secondary fuel nozzle arrangement for use in gas-turbine engine, has nozzle section with central passage and passages, and head section with set of inlets in flow-connection with nozzle passages |
| 01/29/2009 | CA2694163A1 Method for manufacturing of fuel nozzle floating collar |
| 01/28/2009 | CN100455781C Wet compression-rear surface cooling-regenerative cycle combustion turbine |
| 01/27/2009 | US7482710 Power generation system and control method |
| 01/27/2009 | US7481102 Method and apparatus for determining the extent of internal wear in a fuel pump of a fuel system |
| 01/27/2009 | US7481061 Fuel control for starting a gas turbine engine |
| 01/27/2009 | US7481060 Method for operating a power plant |
| 01/27/2009 | US7481037 Cooling structure of gas turbine tail pipe |
| 01/27/2009 | CA2446771C Abradeable seal system |
| 01/27/2009 | CA2360885C Fuel-saving circuit |
| 01/23/2009 | CA2635171A1 Pre-loaded internal fuel manifold support |
| 01/23/2009 | CA2595061A1 Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor |
| 01/22/2009 | WO2009009864A1 Preloading brace for gas turbine engine transportation |
| 01/22/2009 | US20090022579 Burn resistant organic matrix composite material |
| 01/22/2009 | US20090019858 Tip turbine engine with aspirated compressor |
| 01/22/2009 | US20090019855 Low emissions gas turbine combustor |
| 01/22/2009 | US20090019854 APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR |
| 01/22/2009 | DE102008002931A1 Vorrichtung/Verfahren zur Kühlung einer Brennkammer/Venturi-Düse in einem Brenner mit niedrigen NOx-Emissionen The apparatus / method for cooling a combustion chamber / venturi nozzle in a burner having low NOx emissions |
| 01/22/2009 | DE102007032933A1 Turbomaschine Turbomachine |
| 01/22/2009 | DE102007032702A1 Exhaust-gas turbocharger comprises housing, compressed wheel and turbine carrying shaft, which is mounted in housing by multiple bearings |
| 01/22/2009 | CA2692712A1 Preloading brace for gas turbine engine transportation |
| 01/21/2009 | EP2017435A2 Turbo engine with electric machine and magnetic bearings |
| 01/21/2009 | EP2017077A2 Process for manufacturing a sound-absorbing panel for aircrafts |
| 01/21/2009 | EP2016267A1 Gas turbine engine |
| 01/21/2009 | EP2016266A2 Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 01/21/2009 | EP1492941B1 Steam and gas turbine installation |
| 01/21/2009 | CN101349197A Contrarotating rotary spraying engine |
| 01/20/2009 | US7478534 Arrangement with a twist-lock coupling for a turbomachine combustion chamber |
| 01/20/2009 | US7478525 System and method for controlling the temperature and infrared signature of an engine |
| 01/15/2009 | WO2009008743A1 Circular run gear-piston engine |
| 01/15/2009 | WO2009008524A1 Ignition and chemical reaction accelerator and flame stabilizer, speed-type internal combustion engine, and furnace |
| 01/15/2009 | WO2009007564A2 Turbojet engine for aircraft |
| 01/15/2009 | WO2008091502A3 Power augmentation of combustion turbines by injection of cold air upstream of compressor |
| 01/15/2009 | US20090016886 Apparatus and method for retaining bladed rotor disks of a jet engine |
| 01/15/2009 | US20090013696 Gas turbine engine mixing duct and method to start the engine |
| 01/15/2009 | US20090013693 Integrated fuel nozzle with feedback control for a gas turbine engine |
| 01/15/2009 | DE102007032760A1 Hot gas chamber device e.g. for rocket engines, has hot gas chamber and probe with air-conditioning device provided for cooling of probe which has cooling fluid for chamber |
| 01/15/2009 | DE102007032600A1 Vorrichtung und Verfahren zur Verbesserung der Dämpfung von akustischen Wellen Apparatus and method for improving the damping of acoustic waves |
| 01/15/2009 | CA2690601A1 Turboreacteur pour aeronef |
| 01/15/2009 | CA2636805A1 Components capable of transporting liquids manufactured using injection molding |
| 01/14/2009 | EP2014901A2 Gas turbine engine with dual fans driven about a central core axis |
| 01/14/2009 | EP2014877A2 Systems and methods for monitoring gas turbine engines |
| 01/14/2009 | EP2014551A1 Device and method for protecting an aircraft component from collision with flying objects |
| 01/14/2009 | EP2014395A1 A machining method and a blocking tool of an oil retainer seal of an exhaust case of a turbine |
| 01/14/2009 | CN101344037A Method and apparatus for actuating fuel trim valves in a gas turbine |
| 01/14/2009 | CN101344036A Turbo engine |
| 01/14/2009 | CN100450581C Improved configuration and process for carbonyl removal |
| 01/13/2009 | US7476703 In-situ method and composition for repairing a thermal barrier coating |
| 01/13/2009 | US7475550 Method and device for reducing engine noise |
| 01/13/2009 | US7475549 Thermal management system for a gas turbine engine |
| 01/13/2009 | CA2404187C Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine |
| 01/13/2009 | CA2380779C Discharge system for simplified control turbojet or turboprop engine |
| 01/08/2009 | WO2009005146A1 Blast furnace gas burning facility and its operation method |
| 01/08/2009 | WO2009004133A1 System for producing power, particularly electrical power, with a gas turbine and a rotary regenerative heat exchanger. |