| 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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| 03/03/2011 | US20110048019 Turbine enhancement system |
| 03/03/2011 | US20110048017 Method of depositing protective coatings on turbine combustion components |
| 03/03/2011 | DE102010037078A1 Akustisch versteifte Gasturbinenbrennkammerzuführung Acoustically stiffened gas turbine combustor feed |
| 03/03/2011 | DE102010037048A1 Zwischenstufen-Dichtungsring Interstage seal ring |
| 03/03/2011 | DE102009038772A1 Abgasnutzturbine für ein Turbo-Compound-System Exhaust gas turbine for a turbo-compound system |
| 03/02/2011 | EP2290207A2 Cambered aero-engine inlet |
| 03/02/2011 | EP2290199A2 A turbomachine casing assembly |
| 03/02/2011 | EP2288798A1 Casing comprising a peripheral shroud for a turbomachine rotor |
| 03/02/2011 | EP2288797A1 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/02/2011 | EP1910168B1 Control of engine intake door |
| 03/02/2011 | EP1825128B1 Regenerative turbine blade and vane cooling for a tip turbine engine |
| 03/02/2011 | EP1504488B1 Gas turbine power generating system with fuel cell |
| 03/01/2011 | US7896962 Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles |
| 03/01/2011 | US7896620 Integral gas turbine compressor and rotary fuel injector |
| 03/01/2011 | US7895822 Systems and methods for power generation with carbon dioxide isolation |
| 02/27/2011 | CA2713802A1 Lubrication system with porous element |
| 02/27/2011 | CA2712113A1 Sealing and cooling at the joint between shroud segments |
| 02/24/2011 | WO2011022155A1 Self-regulating cooling water system for intercooled gas turbine engines |
| 02/24/2011 | WO2011021693A1 Turbine cooling structure and turbine |
| 02/24/2011 | WO2011020768A1 Method and device for converting thermal energy from biomass into mechanical work |
| 02/24/2011 | WO2010138677A3 Adsorption-enhanced compressed air energy storage |
| 02/24/2011 | WO2010077766A3 Method and systems for an engine starter/generator |
| 02/24/2011 | US20110044795 Turbine vane platform leading edge cooling holes |
| 02/24/2011 | US20110041511 Gas turbine engine |
| 02/24/2011 | US20110041510 Fuel control apparatus for gas turbine engine |
| 02/24/2011 | US20110041508 Burner |
| 02/24/2011 | DE102009038323A1 Verfahren und Vorrichtung zur Verwertung von Biomasse Method and apparatus for utilizing biomass |
| 02/24/2011 | DE102009038322A1 Verfahren und Vorrichtung zur Umwandlung thermischer Energie aus Biomasse in mechanische Arbeit Method and apparatus for converting thermal energy from biomass into mechanical work |
| 02/24/2011 | DE102009037877A1 Method for mounting compressor wheel of turbocharger on exhaust turbocharger shaft, involves applying force on compressor-side end of exhaust turbocharger shaft with application of torque on mounting nut |
| 02/24/2011 | CA2771146A1 Method and device for converting thermal energy from biomass into mechanical work |
| 02/23/2011 | EP2287504A2 System and method for locking retention of valve components |
| 02/23/2011 | EP2287449A2 Gas turbine engine oil consumption monitoring system and method |
| 02/23/2011 | EP2286065A2 Compressor rotor for a turbomachine including centripetal air bleeding means |
| 02/23/2011 | EP2285681A2 Offset ambient level fuel feed system |
| 02/23/2011 | CN101981382A Gas turbine and method of forming insertion hole for combustor of gas turbine |
| 02/23/2011 | CN101981381A Cooling structure for gas turbine combustor |
| 02/23/2011 | CN101981292A Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same |
| 02/23/2011 | CN101981277A Device and method for balancing pressure in a turbojet bearing housing |
| 02/23/2011 | CN101981276A Turbine engine including a reversible electric machine |
| 02/23/2011 | CN101981275A Gas turbine, intermediate shaft for gas turbine, and method of cooling gas turbine compressor |
| 02/22/2011 | US7891193 Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine |
| 02/22/2011 | US7891191 Combustor, gas turbine combustor, and air supply method for same |
| 02/21/2011 | CA2713479A1 Staged compressor water wash system |
| 02/18/2011 | CA2713284A1 Blade outer air seal cooling |
| 02/18/2011 | CA2712952A1 Blade outer air seal support |
| 02/18/2011 | CA2712758A1 Blade outer air seal support cooling air distribution system |
| 02/18/2011 | CA2712756A1 Blade outer air seal anti-rotation |
| 02/17/2011 | WO2011019755A1 Mitigation of optical signal noise using a multimode transmit fiber |
| 02/17/2011 | WO2011019018A1 Ni-BASED MONOCRYSTALLINE SUPERALLOY AND TURBINE BLADE |
| 02/17/2011 | WO2011018299A1 Turbo engine having steam tapping |
| 02/17/2011 | US20110038709 Turbine Vane for a Gas Turbine Engine Having Serpentine Cooling Channels |
| 02/17/2011 | US20110036098 Self-regulating cooling water system for intercooled gas turbine engines |
| 02/17/2011 | US20110036092 Methods and Systems for Dry Low NOx Combustion Systems |
| 02/17/2011 | DE10297340B4 Steuerventil mit integriertem elektrohydraulischen Aktuator Control valve with integrated electro-hydraulic actuator |
| 02/17/2011 | DE102010036872A1 Turbinenendwandkühlungsanordnung Turbinenendwandkühlungsanordnung |
| 02/17/2011 | DE102010036805A1 Verfahren und Systeme für Dry-Low-NOx-Verbrennungssysteme Methods and systems for dry low NOx combustion systems |
| 02/17/2011 | DE102010036525A1 System und Verfahren zur Rotordruckkraft-Modifizierung System and method for rotor thrust modifier |
| 02/17/2011 | CA2764664A1 Ni-based single crystal superalloy and turbine blade |
| 02/16/2011 | EP2283262A1 Multi-way valve of a fuel system of a gas turbine |
| 02/16/2011 | EP2283218A2 Thermal insulation structure for structural member, and scroll structure |
| 02/16/2011 | CN201747464U Signal matching box for aircraft engines |
| 02/16/2011 | CN101978197A Rotating machine and additional ring |
| 02/16/2011 | CN101978150A System of counter-rotating propellers with a feathering device for propeller blades |
| 02/16/2011 | CN101978138A Gas turbine |
| 02/16/2011 | CN101975122A Stabilized knocking engine with magnetic fluid energy bypath system |
| 02/16/2011 | CN101972749A Spray device for washing aircraft gas turbine engine and washing system |
| 02/15/2011 | US7887610 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 |
| 02/15/2011 | US7886516 Combined cycle integrated combustor and nozzle system |
| 02/15/2011 | CA2673721C Power augmentation of combustion turbines by injection of cold air upstream of compressor |
| 02/15/2011 | CA2528693C Internally cooled gas turbine airfoil and method |
| 02/10/2011 | US20110030387 Mid-turbine frame torque box having a concave surface |
| 02/10/2011 | US20110030386 Mid-turbine frame |
| 02/10/2011 | US20110030385 propulsion unit |
| 02/10/2011 | US20110030378 Combustor tile mounting arrangement |
| 02/10/2011 | US20110030376 Gas injection in a burner |
| 02/10/2011 | US20110030375 Aerodynamic pylon fuel injector system for combustors |
| 02/10/2011 | US20110030334 System for purging a device |
| 02/10/2011 | US20110030332 System and method for liquid air production, power storage and power release |
| 02/10/2011 | US20110030331 Ammonia Injection System |
| 02/10/2011 | DE102008023052B4 Brennkammerwand bzw. Heißgaswand einer Brennkammer und Brennkammer mit einer Brennkammerwand Combustion chamber wall or hot gas wall of a combustion chamber and combustion chamber with a combustion chamber wall |
| 02/10/2011 | DE10196104B4 Graphitkörper imprägniert mit einer Leichtmetall-Legierung, Verfahren zu dessen Herstellung und seine Verwendung Graphite body impregnated with a light metal alloy, process for its preparation and its use |
| 02/09/2011 | EP2282123A1 Turbine engine fuel injector |
| 02/09/2011 | EP2282031A1 Filtering device with integrated bypass for an air inlet |
| 02/09/2011 | EP2282030A2 Spray system, power augmentation system for engine containing spray system and method of humidifying air |
| 02/09/2011 | EP2281110A2 Device and method for balancing pressure in a turbojet bearing housing |
| 02/09/2011 | EP2281109A1 Turbine engine including a reversible electric machine |
| 02/09/2011 | CN201739008U Aircraft ignition circuit with cold and hot ignition combination |
| 02/09/2011 | CN101970833A Adsorption-enhanced compressed air energy storage |
| 02/09/2011 | CN101970807A Centrifugal oil separator having variable channel section |
| 02/09/2011 | CN101970802A Cover for cooling passage, method of manufacturing the cover, and gas turbine |
| 02/09/2011 | CN101970298A Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method |
| 02/09/2011 | CN101970296A Air intake lip for turbojet nacelle |
| 02/09/2011 | CN101968007A Oxyfuel gas turbine system and method |
| 02/08/2011 | US7882704 Flame stability enhancement |
| 02/08/2011 | CA2457892C Gas turbine stator housing |
| 02/03/2011 | WO2011012985A2 Method and assembly for supplying fuel to a combustion chamber of a gas turbine plant |
| 02/03/2011 | WO2011012982A1 Flow rate measuring device and method |
| 02/03/2011 | WO2011011963A1 Full steam-driven intaernal combustion engine |
| 02/03/2011 | WO2010018314A8 Inner wall for the nacelle of a turbine engine |
| 02/03/2011 | US20110027064 System and method for modifying rotor thrust |