| 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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| 04/15/2010 | US20100089066 Cool flame combustion |
| 04/15/2010 | US20100089065 Fuel delivery system for a turbine engine |
| 04/15/2010 | US20100089023 Intake air heating system of combined cycle plant |
| 04/15/2010 | US20100089021 Method and apparatus of introducing diluent flow into a combustor |
| 04/15/2010 | DE102009044001A1 Deckband für eine Turbomaschine Shroud for a turbomachine |
| 04/15/2010 | DE102009044000A1 Wiederverwendbare Schweissverbindung für Syngas-Brennstoffdüsen Reusable welded joint for syngas fuel nozzles |
| 04/15/2010 | DE102009043891A1 Einrichtung und Verfahren zur Kühlung einer Gasturbine Apparatus and method for cooling a gas turbine |
| 04/15/2010 | DE102009036847A1 Befestigungsanordnung zum Verbinden von Raketentriebwerksdüsen A fastening arrangement for connecting rocket engine nozzle |
| 04/15/2010 | DE102009036657A1 Turboladergehäuse mit fest eingebauten Einlass- und Auslassöffnungen Turbocharger housing with built-inlet and outlet ports |
| 04/15/2010 | DE102008051241A1 Silencer for auxiliary power unit of aircraft, has two groups of outer cells whose volume is greater than volume of inner cells that are surrounded by outer cells and formed in flow channel |
| 04/15/2010 | CA2733602A1 Air intake structure for a turbine engine nacelle |
| 04/14/2010 | EP2175119A2 Combined metering valve and pressure regulating valve |
| 04/14/2010 | EP2175103A1 Turbine blade |
| 04/14/2010 | CN1690389B Rotating seal arrangement for turbine bucket cooling circuits |
| 04/14/2010 | CN101694181A Seal structure of gas turbine combustor |
| 04/14/2010 | CN101693163A Drying device of absorption gas turbine |
| 04/14/2010 | CN101203424B Deicing system for aircraft engine pod and operation and control method thereof |
| 04/13/2010 | US7694523 Control system for gas turbine in material treatment unit |
| 04/13/2010 | CA2539298C Method for efficient, nonsynchronous lng production |
| 04/13/2010 | CA2486237C Method and apparatus for arresting a crack within a body |
| 04/13/2010 | CA2484438C Method for repairing gas turbine compressor rotor blades |
| 04/13/2010 | CA2470699C Gas turbine engine with offset drive |
| 04/13/2010 | CA2469993C Methods and apparatus for injecting cleaning fluids into combustors |
| 04/13/2010 | CA2450975C Methods for replacing a portion of a combustor liner |
| 04/13/2010 | CA2364124C Reduction gearing to counteract axial force generated by the fan of a turbojet engine |
| 04/13/2010 | CA2360775C Improved bushing for a jet engine vane |
| 04/08/2010 | WO2010038528A1 Fuel control method and fuel control system for gas turbine, and gas turbine |
| 04/08/2010 | WO2010038290A1 Gas turbine device |
| 04/08/2010 | WO2010038288A1 Combined cycle electric power generation plant and heat exchanger |
| 04/08/2010 | WO2010037450A2 Turbine cooling system |
| 04/08/2010 | US20100086398 Method for coating sliding surface of high-temperature member, high-temperature member and electrode for electro-discharge surface treatment |
| 04/08/2010 | US20100083664 Method and apparatus for assembling gas turbine engine |
| 04/08/2010 | DE102009026313A1 Vorvermischende Direkteinspritzdüse Vorvermischende Direkteinspritzdüse |
| 04/08/2010 | DE102008050401A1 Bearing arrangement, particularly bearing of rotor for turbocharger, has relatively stationary bearing surface and relatively movable bearing surface that is separated from relatively stationary bearing surface |
| 04/08/2010 | DE102008050325A1 Housing or component e.g. compressor stator, ensemble e.g. exhaust turbo charger, has bearing surfaces arranged at counter-joining piece, turned away from joining plane and extended parallel to joining plane |
| 04/08/2010 | DE102008049250A1 Dichtungssystem für die Verdichterseite eines Turboladers einer Verbrennungskraftmaschine sowie ein Verfahren zur Abdichtung der Verdichterseite eines Turboladers Sealing system for the compressor side of a turbocharger of an internal combustion engine and a method for sealing the compressor side of a turbocharger |
| 04/08/2010 | DE102008049170A1 Vorrichtung und Verfahren zur Lebensdauerüberwachung Apparatus and method for lifetime monitoring |
| 04/08/2010 | DE102008007278B4 Bleedairduct-Segment, Bleedairduct-Anordnung mit solchen Bleedairduct-Segmenten und Bleedairduct-System mit Regulierungsvorrichtung Bleedairduct segment Bleedairduct arrangement with such Bleedairduct segments and Bleedairduct system with regulating device |
| 04/07/2010 | EP2172716A2 Sound attenuation systems |
| 04/07/2010 | EP2172623A2 Sound attenuation system and method |
| 04/07/2010 | EP2172620A1 Stator blade ring and axial flow compressor using the same |
| 04/07/2010 | EP2171239A1 Method for operating a combustion device, and combustion device for carrying out the method |
| 04/07/2010 | EP2171238A1 Continuous-flow or displacement machine with magnetic bearings |
| 04/07/2010 | CN101691848A Rotary engine working radially |
| 04/06/2010 | US7693643 Fault detection system and method for turbine engine fuel systems |
| 04/06/2010 | US7690207 Gas turbine floating collar arrangement |
| 04/06/2010 | US7690205 Gas turbine engine cold start mechanization |
| 04/06/2010 | US7690185 System for driving accessory machines of a double-bodied turbine engine |
| 04/06/2010 | US7690184 Method for treating oil waste in a gas turbine engine |
| 04/06/2010 | US7690112 Process and apparatus for producing a turbine component, turbine component and use of the apparatus |
| 04/06/2010 | CA2353686C Sealing ring for non-hermetic fluid seals |
| 04/01/2010 | WO2010036432A2 System and method of operating gas turbine engine with an alternative working fluid |
| 04/01/2010 | WO2010034922A1 Device for connecting an air inlet with an aircraft nacelle actuator assembly |
| 04/01/2010 | US20100080699 Turbine shroud gas path duct interface |
| 04/01/2010 | US20100080685 Method and Apparatus for Gas Turbine Engine Temperature Management |
| 04/01/2010 | US20100077769 Starter drive assembly and method of starting a gas turbine engine |
| 04/01/2010 | US20100077768 Diffuser with enhanced surge margin |
| 04/01/2010 | US20100077764 Structures with adaptive cooling |
| 04/01/2010 | US20100077763 Combustor with improved cooling holes arrangement |
| 04/01/2010 | US20100077762 Off Center Combustor Liner |
| 04/01/2010 | US20100077761 Impingement cooled combustor seal |
| 04/01/2010 | US20100077759 Tubular Fuel Injector for Secondary Fuel Nozzle |
| 04/01/2010 | US20100077758 Internal fuel manifold having temperature reduction feature |
| 04/01/2010 | US20100077756 Fuel lance for a gas turbine engine |
| 04/01/2010 | US20100077755 Sound attenuation systems and methods |
| 04/01/2010 | US20100077754 Sound attenuation systems and methods |
| 04/01/2010 | DE19940763B4 Im kombinierten Zyklus arbeitender Energieerzeuger mit integrierter Kohlevergasung In combined cycle power generator working with integrated coal gasification |
| 04/01/2010 | DE10259963B4 Wabendichtung Honeycomb seal |
| 04/01/2010 | DE102009044074A1 Gasturbinendichtung Gas turbine seal |
| 04/01/2010 | DE102009044003A1 Verfahren und Vorrichtung zum Temperaturmanagement einer Gasturbinenmaschine Method and apparatus for thermal management of a gas turbine engine |
| 04/01/2010 | DE102009042117A1 Ventilanordnung zum Modulieren einer Brennstoffströmung zu einem Gasturbinenmotor Valve means for modulating a fuel flow to a gas turbine engine |
| 04/01/2010 | CA2732176A1 System and method of operating a gas turbine engine with an alternative working fluid |
| 03/31/2010 | EP2169197A2 Method and system for providing cooling and power for an aircraft |
| 03/31/2010 | EP2167798A2 Turbojet engine for aircraft |
| 03/31/2010 | CN101689362A Panel for acoustic treatment |
| 03/31/2010 | CN101688542A Nonose dome for a turbo machine rotorse dome for a turbo machine rotor |
| 03/31/2010 | CN101688477A System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft |
| 03/31/2010 | CN101688476A Method and system for starting a turboshaft engine by cold weather |
| 03/31/2010 | CN101688474A Integrated gasification combined cycle plant |
| 03/31/2010 | CN101684751A Fuel cut-off valve of reheat fuel control unit of turbofan engine |
| 03/31/2010 | CN101684750A Air filter mounting system and method for fabricating the same |
| 03/31/2010 | CN101684749A Liquefied natural gas power plant and operation method thereof |
| 03/31/2010 | CN101684748A Integrated gas turbine exhaust diffuser and heat recovery steam generation system |
| 03/31/2010 | CN101684736A Shroud for a turbomachine |
| 03/31/2010 | CN101684735A Gas turbine seal |
| 03/30/2010 | US7686580 Turbine element |
| 03/30/2010 | US7685827 Gas turbine cooling systems and methods of assembly |
| 03/30/2010 | US7685822 Rotary cup fuel injector |
| 03/30/2010 | CA2447279C Fuel metering device with compensated regulator valve in a turbine engine |
| 03/30/2010 | CA2441490C Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure |
| 03/30/2010 | CA2406479C Weep plug |
| 03/30/2010 | CA2293076C Fan and compressor noise attenuation |
| 03/25/2010 | WO2010031948A1 Method and system for lubricating a turbine engine |
| 03/25/2010 | WO2010006151A3 Power transmission among shafts in a turbine engine |
| 03/25/2010 | US20100074736 Thermal management system |
| 03/25/2010 | US20100074732 Gas Turbine Sealing Apparatus |
| 03/25/2010 | US20100074731 Gas Turbine Sealing Apparatus |
| 03/25/2010 | US20100074730 Gas turbine sealing apparatus |
| 03/25/2010 | US20100074727 Method and Apparatus for Monitoring Blade Vibration With An Imaging Fiber Optic Ribbon Probe |
| 03/25/2010 | US20100071382 Gas Turbine Transition Duct |