| 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) |
|---|
| 03/04/2010 | DE102009043871A1 System und Verfahren zur Wärmesteuerung eines Gasturbineneinlasses System and method for thermal control of a gas turbine inlet |
| 03/04/2010 | DE102009043856A1 Verfahren und Vorrichtung zum Zusammenbau von Gasturbinen Method and apparatus for assembling gas turbine |
| 03/04/2010 | DE102009026329A1 Strahlpumpen mit lösbar befestigen Düsen, Düsen mit einstellbarer Grösse oder Mischrohren mit einstellbarer Größe Jet pumps with detachable mount nozzles, nozzle with adjustable size or mixing tubes with adjustable size |
| 03/04/2010 | DE102008045546A1 Fluggasturbinen-Einlaufkonus Aircraft gas turbine inlet cone |
| 03/04/2010 | DE102008045229A1 Axial bearing for shaft of exhaust gas turbo-charger utilized for increasing efficiency of motor vehicle, has oil- supply channels, discharge channels and wedge surfaces provided as negative contours in surfaces of axial bearing washer |
| 03/04/2010 | DE102008031887A1 Abgasanlage Exhaust system |
| 03/04/2010 | CA2735321A1 Multi passage fuel manifold and methods of construction |
| 03/04/2010 | CA2734289A1 Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine including at least one such fixed vane assembly |
| 03/03/2010 | EP2159399A1 Method for pre-heating a fuel to be burned up in a gas turbine and gas turbine with a fuel supply system |
| 03/03/2010 | EP2159398A2 Separation-resistant inlet duct for mid-turbine frames |
| 03/03/2010 | EP2159397A2 Filtration system for gas turbines |
| 03/03/2010 | EP2159396A2 Filtration system for gas turbines |
| 03/03/2010 | EP2159383A2 Gas turbine engine fan bleed heat exchanger system |
| 03/03/2010 | EP2159377A1 Stator vane support for a gas turbine and corresponding gas turbine plant |
| 03/03/2010 | EP2158404A1 Nose dome for a turbomachine rotor |
| 03/03/2010 | EP2158391A1 System for producing power, particularly electrical power, with a gas turbine and a rotary regenerative heat exchanger. |
| 03/03/2010 | CN101660452A Heat pipe intercooler for a turbomachine |
| 03/03/2010 | CN101660451A System and method for thermal management of a gas turbine inlet |
| 03/03/2010 | CN101660450A Filtration system for gas turbines |
| 03/03/2010 | CN101660449A Filtration system for gas turbines |
| 03/02/2010 | US7669425 Closed loop turbine cooling fluid reuse system for a turbine engine |
| 03/02/2010 | US7669424 Combustor assembly |
| 03/02/2010 | US7669423 Operating method for CAES plant using humidified air in a bottoming cycle expander |
| 03/02/2010 | CA2402522C Method and arrangement for cleaning the intake air of a gas turbine |
| 02/28/2010 | CA2675908A1 Filtration system for gas turbines |
| 02/28/2010 | CA2675904A1 Filtration system for gas turbines |
| 02/25/2010 | WO2010021807A2 Fuel injector sans support/stem |
| 02/25/2010 | WO2010021573A1 A gas turbine engine structure |
| 02/25/2010 | WO2010021358A1 Heat exchanging partition wall |
| 02/25/2010 | US20100049417 Dual ECU for aftermarket conversions of vehicles and boats to oxy-hydrogen or hybrid fuels |
| 02/25/2010 | US20100047077 Ferry Flight Engine Fairing Kit |
| 02/25/2010 | US20100047075 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same |
| 02/25/2010 | US20100047061 Grid ceramic matrix composite structure for gas turbine shroud ring segment |
| 02/25/2010 | US20100047056 Duplex Turbine Nozzle |
| 02/25/2010 | US20100043450 System for attaching an engine to the structure of an aircraft, such as a sail wing aircraft |
| 02/25/2010 | US20100043449 Device for attaching a combustion chamber |
| 02/25/2010 | US20100043448 Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor |
| 02/25/2010 | US20100043444 Starting turbine engines |
| 02/25/2010 | US20100043443 Method and apparatus for suppressing aeroengine contrails |
| 02/25/2010 | US20100043441 Method and apparatus for assembling gas turbine engines |
| 02/25/2010 | US20100043440 Gas Turbine Burner and Method of Operating a Gas Turbine Burner |
| 02/25/2010 | US20100043391 Injector assembly having multiple manifolds for propellant delivery |
| 02/25/2010 | US20100043390 Controlling ice buildup on aircraft engine and nacelle static and rotating components |
| 02/25/2010 | US20100043388 Gas turbine engine arrangement |
| 02/25/2010 | US20100043387 Methods and systems for operating gas turbine engines |
| 02/25/2010 | US20100043386 Methods and apparatus for mixing fluid in turbine engines |
| 02/25/2010 | DE102009037713A1 Mehrstufenabsperrventil Mehrstufenabsperrventil |
| 02/25/2010 | DE102009026315A1 Übergangskanal-Hinterrahmen-Kühlung und diesbezügliches Verfahren Transition channel rear frame-cooling and related method |
| 02/25/2010 | DE102008014607A1 Vorrichtung zum Auffangen von Waschflüssigkeit aus einer Strahltriebwerkswäsche Device for collecting the washing liquid from a jet engine wash |
| 02/25/2010 | CA2733916A1 Fuel injector sans support/stem |
| 02/25/2010 | CA2731373A1 Heat exchange bulkhead |
| 02/25/2010 | CA2675400A1 Gas turbine engine fan bleed heat exchanger system |
| 02/24/2010 | EP2157299A1 Nacelle assembly for a gas turbine engine with variable shape inlet section, corresponding gas turbine engine and operating method |
| 02/24/2010 | EP2157298A2 A method for detecting overpressure inside a compartment associated with a gas turbine nacelle |
| 02/24/2010 | EP2155555A1 A mounting element for a gas turbine engine, and a structure and an aircraft with such a mounting element |
| 02/24/2010 | EP1999022B1 Air inlet shroud structure |
| 02/24/2010 | CN101655035A Dimpled serrated fin tube structure |
| 02/23/2010 | US7665968 Cooled rotor blade |
| 02/23/2010 | US7665694 Dual action inlet door and method for use thereof |
| 02/23/2010 | US7665310 Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl |
| 02/23/2010 | US7665309 Secondary fuel delivery system |
| 02/23/2010 | US7665293 Low speed rotor shaft for a small twin spool gas turbine engine |
| 02/23/2010 | US7665291 Method and system for heat recovery from dirty gaseous fuel in gasification power plants |
| 02/23/2010 | CA2586518C Thermal barrier coating material, method of production thereof, and gas turbine member and gas turbine applying the thermal barrier coating material |
| 02/18/2010 | WO2010018338A2 Fuel flow metering valve |
| 02/18/2010 | WO2010018314A1 Inner wall for the nacelle of a turbine engine |
| 02/18/2010 | US20100040482 Ejectors with separably secured nozzles, adjustable size nozzles, or adjustable size mixing tubes |
| 02/18/2010 | US20100040462 Separation-resistant inlet duct for mid-turbine frames |
| 02/18/2010 | US20100038476 Device that makes it possible to improve the effectiveness of the acoustic treatments in a pipe of an aircraft power plant |
| 02/18/2010 | US20100037622 Contoured Impingement Sleeve Holes |
| 02/18/2010 | US20100037621 Thermal Machine |
| 02/18/2010 | US20100037620 Impingement and effusion cooled combustor component |
| 02/18/2010 | US20100037619 Canted outlet for transition in a gas turbine engine |
| 02/18/2010 | US20100037618 Transition with a linear flow path for use in a gas turbine engine |
| 02/18/2010 | US20100037617 Transition with a linear flow path with exhaust mouths for use in a gas turbine engine |
| 02/18/2010 | US20100037616 Diffuser for Decelerating a Compressed Fluid |
| 02/18/2010 | US20100037615 Multi-stage check valve |
| 02/18/2010 | US20100037613 Fuel injector and method of assembling the same |
| 02/18/2010 | US20100037612 Fuel divider system for gas turbine engine |
| 02/18/2010 | US20100037586 Method and system for feeding a gas-turbine engine with liquid fuel |
| 02/18/2010 | DE202009014270U1 Druckluftstartgerät für ein Luftfahrzeug Compressed air boot device for an aircraft |
| 02/18/2010 | DE102009026379A1 Durch Prallkühlung und Effusionskühlung gekühlte Brennkammerkomponente By impingement and effusion-cooled combustion chamber component |
| 02/18/2010 | DE102006053277B4 Resonatorvorrichtung und Brennkammervorrichtung Resonator and combustion chamber device |
| 02/18/2010 | CA2733094A1 Inner wall for the nacelle of a turbine engine |
| 02/17/2010 | EP2154434A1 Combustion oscillation detection device mounting structure |
| 02/17/2010 | EP2154351A2 Inlet air conditioning system for a turbomachine |
| 02/17/2010 | EP2154350A1 Method of preparing through holes in tube body wall surfaces, and tube body structure |
| 02/17/2010 | EP2152937A1 Coating |
| 02/17/2010 | CN201407103Y Soft-starting gas turbine system with redundancy design |
| 02/17/2010 | CN201407102Y Turbine combination pulse detonation engine |
| 02/16/2010 | US7661273 Turbomachine with annular combustion chamber |
| 02/16/2010 | US7661271 Integrated electric gas turbine |
| 02/16/2010 | US7661267 System for damping thermo-acoustic instability in a combustor device for a gas turbine |
| 02/16/2010 | CA2528878C Turbine component, gas turbine engine, production method of turbine component, surface treatment method thereof, blade component, metal component and steam turbine engine |
| 02/16/2010 | CA2430444C Simplified support device for nozzles of a gas turbine stage |
| 02/16/2010 | CA2430441C System for control and regulation of the flame temperature for single-shaft gas turbines |
| 02/16/2010 | CA2422827C Multi-component hybrid turbine blade |
| 02/16/2010 | CA2405472C Fuel ratio control method and device in a gas turbine combustor |
| 02/11/2010 | WO2010016159A1 Gas turbine |
| 02/11/2010 | WO2010015758A1 Method for making deicing system on a nacelle panel |