| 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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| 03/13/2013 | EP2566757A1 Unit for an aircraft thruster |
| 03/13/2013 | CN202789128U Noise control device |
| 03/13/2013 | CN202789127U Aeroengine accelerating system |
| 03/13/2013 | CN202789126U High-temperature-resistant structure |
| 03/13/2013 | CN102971510A Air recovery-type cooling structure for air-cooled gas turbine combustor |
| 03/13/2013 | CN102971508A Low emission power generation systems and methods |
| 03/13/2013 | CN102971493A Turbine blade and engine component |
| 03/13/2013 | CN102971217A Airflow-straightening structure for the nacelle of an aircraft engine |
| 03/13/2013 | CN102966439A Aeroengine chamber cold backheating device |
| 03/13/2013 | CN101975122B Stabilized knocking engine with magnetic fluid energy bypath system |
| 03/13/2013 | CN101688476B Method and system for starting a turboshaft engine by cold weather |
| 03/13/2013 | CN101235753B Distributed architecture for a gas turbine starter/generator |
| 03/12/2013 | US8393159 Gas turbine combustor and fuel supply method for same |
| 03/12/2013 | US8393154 Fuel delivery system with reduced heat transfer to fuel manifold seal |
| 03/12/2013 | US8393138 Oxygen-enriched air assisting system for improving the efficiency of cogeneration system |
| 03/12/2013 | CA2709573C Effluent collection unit for engine washing |
| 03/12/2013 | CA2683945C Surge detection in a gas turbine engine |
| 03/12/2013 | CA2607674C Dual interstage cooled engine |
| 03/12/2013 | CA2577770C Hybrid burner lance |
| 03/12/2013 | CA2525283C Methods and apparatus for cooling gas turbine engine components |
| 03/12/2013 | CA2524113C Gas turbine engine and method of assembling same |
| 03/12/2013 | CA2522950C Methods and apparatus for cooling gas turbine engines |
| 03/12/2013 | CA2518355C Retention of centring keys of the rings under the variable setting stator blades of a gas turbine engine |
| 03/12/2013 | CA2517180C System and method for improving thermal efficiency of dry low emissions combustor assemblies |
| 03/12/2013 | CA2511892C Cowling for turbine engine nozzle with jet noise reduction patterns |
| 03/12/2013 | CA2508391C Methods and apparatus for fabricating a turbine nozzle assembly |
| 03/12/2013 | CA2502793C High efficiency rotor for the second phase of a gas turbine |
| 03/12/2013 | CA2455673C Methods and apparatus for assessing gas turbine engine damage |
| 03/08/2013 | CA2788303A1 Method and apparatus for extracting electrical power from a gas turbine engine |
| 03/07/2013 | WO2013030988A1 Gas turbine plant and combined cycle plant |
| 03/07/2013 | WO2013029914A1 Bypass steam line |
| 03/07/2013 | WO2013029911A1 Cooling for a fluid flow machine |
| 03/07/2013 | WO2012080332A3 Cooling device for a jet engine |
| 03/07/2013 | WO2011144567A3 Method and device for supplying cooling air to an engine, in particular an aircraft engine, gas turbine, or the like |
| 03/07/2013 | US20130058778 Fabricated intermediate case with engine mounts |
| 03/07/2013 | US20130055725 Gas duct for a gas turbine and gas turbine having such a gas duct |
| 03/07/2013 | US20130055723 Apparatus and Method for Separating Ice from Fuel in a Gas Turbine Engine |
| 03/07/2013 | US20130055722 Pin fin arrangement for heat shield of gas turbine engine |
| 03/07/2013 | US20130055721 Method and apparatus for segregated oil supply and scavenge in a gas turbine engine |
| 03/07/2013 | US20130055720 Interface ring for gas turbine nozzle assemblies |
| 03/07/2013 | US20130055719 Fuel supply device of gas turbine engine |
| 03/07/2013 | US20130055718 Device for reducing the noise emitted by the jet of an aircraft propulsion engine |
| 03/07/2013 | DE102012108283A1 Kriechanzeigesystem und Verfahren zum Bestimmen eines Kriechbetrags Kriechanzeigesystem and method for determining a Kriechbetrags |
| 03/07/2013 | DE102011112255A1 Hilfsgerätegetriebeeinrichtung für ein Triebwerk Accessory gearbox means for an engine |
| 03/07/2013 | DE102011112254A1 Jet engine for aircraft, has accessory gearbox that is coupled to auxiliary units for maintaining temperature of lubrication and cooling agent in tank device integrated in intermediate housing |
| 03/07/2013 | DE102011112253A1 Baueinheit für ein Triebwerk eines Luftfahrzeugs Assembly for an engine of an aircraft |
| 03/07/2013 | DE102011112252A1 Generator und Hilfsgerätegetriebeeinrichtung mit einem Generator Generator and accessory gearbox device with a generator |
| 03/07/2013 | DE102011112250A1 Hilfsgerätegetriebeeinrichtung für ein Triebwerk Accessory gearbox means for an engine |
| 03/07/2013 | DE102011081962A1 Brennkammer für eine Gasturbinenanlage Combustor for a gas turbine plant |
| 03/06/2013 | EP2565538A1 Diversion steam line |
| 03/06/2013 | EP2565424A2 Torque frame and asymmetric journal bearing for fan drive gear system |
| 03/06/2013 | EP2565423A2 Accessory gearbox buffer cooling air pump system and method of providing cooling air |
| 03/06/2013 | EP2565422A2 Auxiliary geared drive for a jet engine |
| 03/06/2013 | EP2565421A2 Accessory gearbox device with a generator for a turbine engine |
| 03/06/2013 | EP2565420A2 Accessory gearbox device for a turbine engine |
| 03/06/2013 | EP2565419A1 Flow machine cooling |
| 03/06/2013 | EP2565400A2 Exhaust gas duct for a gas turbine with heat resistant liner and gas turbine having such a gas duct |
| 03/06/2013 | EP2565396A2 Distributed lubrication system |
| 03/06/2013 | EP2565394A2 Annular bearing support dampers, gas turbine engines including the same, and methods for the manufacture thereof |
| 03/06/2013 | EP2565389A1 Method of starting a turbo machine |
| 03/06/2013 | EP2564045A1 Turbomachine fueling system with jet pump |
| 03/06/2013 | CN202768152U Gas turbine module with fire protection, heat insulation, ventilation and sound insulation functions |
| 03/06/2013 | CN102959206A System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor |
| 03/06/2013 | CN102959205A Heat-exchange architecture built into the exhaust of turbine engine |
| 03/06/2013 | CN102959204A Shroud segment producing method and shroud segment |
| 03/06/2013 | CN102953836A Method for operating gas turbine plant and gas turbine plant for implementing the method |
| 03/06/2013 | CN102953831A Seal end attachment |
| 03/06/2013 | CN102953830A Power plant start-up method |
| 03/06/2013 | CN102953829A Variable temperature chiller coils |
| 03/06/2013 | CN102953828A Component with cooling channel and method of manufacture |
| 03/06/2013 | CN102953827A Pulse filtration apparatus |
| 03/06/2013 | CN102953826A Pneumatic supersonic velocity/hypersonic velocity adjustable air inlet passage for forebody-inner passage circulation |
| 03/06/2013 | CN102953825A Pneumatic supersonic velocity/hypersonic velocity adjustable air inlet passage for self-circulation of forebody |
| 03/06/2013 | CN102953824A Hot gas path measurement |
| 03/06/2013 | CN102953818A Power plant and method of operation |
| 03/06/2013 | CN102003284B Hydrogen-blended gas fuel engine |
| 03/06/2013 | CN101959759B Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing |
| 03/06/2013 | CN101675227B Cooling structure for gas-turbine combustor |
| 03/06/2013 | CA2818108A1 Cable-actuated variable area fan nozzle with elastomeric seals |
| 03/06/2013 | CA2776530A1 Pin fin arrangement for heat shield of gas turbine engine |
| 03/05/2013 | US8388309 Gas turbine sealing apparatus |
| 03/05/2013 | US8387897 Vaporization water distribution plant |
| 03/05/2013 | US8387401 Cooling passage cover, manufacturing method of the cover, and gas turbine |
| 03/05/2013 | US8387392 Fuel injection system and burner using the same |
| 03/05/2013 | US8387359 Electrolytic igniter for rocket engines using monopropellants |
| 03/05/2013 | US8387358 Gas turbine engine steam injection manifold |
| 03/05/2013 | US8387357 Recuperated bypass turbine engine |
| 03/05/2013 | US8387354 Oil varnish mitigation systems |
| 03/05/2013 | CA2788264A1 Method and apparatus for segregated oil supply and scavenge in a gas turbine engine |
| 03/05/2013 | CA2527352C Turbine engine with a decoupling device common to the first and second drive shaft bearings, compressor including the decoupling device and the decoupling device |
| 02/28/2013 | WO2013028562A1 Split control unit |
| 02/28/2013 | WO2013028561A1 Staged cooling flow nozzle valve |
| 02/28/2013 | WO2013028557A1 Air inlet arrangement and method of making the same |
| 02/28/2013 | WO2012082813A3 Multi-event corona discharge ignition assembly and method of control and operation |
| 02/28/2013 | US20130054108 System and method for predicting turbine rub |
| 02/28/2013 | US20130051994 Retractable gas turbine inlet coils |
| 02/28/2013 | US20130051992 Turbine Disc Sealing Assembly |
| 02/28/2013 | US20130051985 Assembly and method preventing tie shaft unwinding |
| 02/28/2013 | US20130051984 Torque frame and asymmetric journal bearing for fan drive gear system |
| 02/28/2013 | US20130048781 Aircraft including an electric starter-generator for the or each turbojet and an undercarriage fitted with an electric motor for taxiing |