| 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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| 12/09/2010 | US20100307165 Gas Turbine Engine Systems Involving I-Beam Struts |
| 12/09/2010 | US20100307161 Flexure seal for fuel injection nozzle |
| 12/09/2010 | US20100307160 Convex Pilot Cone |
| 12/09/2010 | US20100307159 Fuel injector for a gas turbine engine |
| 12/09/2010 | US20100307158 Systems relating to turbine engine control and operation |
| 12/09/2010 | US20100307157 Methods relating to turbine engine control and operation |
| 12/09/2010 | DE202010008725U1 Brennkraftmaschine mit flüssigkeitsgekühlter Turbine Internal combustion engine with liquid-cooled turbine |
| 12/09/2010 | DE102010016999A1 System zum Konditionieren des in eine Turbomaschine eintretenden Luftstroms System to condition the incoming air flow in turbomachinery |
| 12/09/2010 | DE102010016894A1 Aktives Steuerungssystem und Verfahren zur Rotorausrichtung An active control system and method for alignment of rotor |
| 12/09/2010 | CA2764228A1 Hydrodynamic bore seal |
| 12/09/2010 | CA2762301A1 Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
| 12/08/2010 | EP2258934A2 Dual-pump fuel system and method for starting a gas turbine engine |
| 12/08/2010 | EP2258933A1 Gas turbine and method for maintaining and inspecting the same |
| 12/08/2010 | EP2258928A1 Seal member, steam turbine, and method of avoiding resonance |
| 12/08/2010 | EP2258927A2 Shut-down arrangement |
| 12/08/2010 | EP2010429B1 Inlet distortion and recovery control system |
| 12/08/2010 | CN201666187U Airplane engine ignition system |
| 12/08/2010 | CN1670348B Controlled pressure fuel nozzle system |
| 12/08/2010 | CN1664318B Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine |
| 12/08/2010 | CN1616798B Apparatus for distributing fluid into a turbomachine |
| 12/08/2010 | CN101910730A Combustor of gas turbine |
| 12/08/2010 | CN101910564A Cooling structure of turbine blade |
| 12/08/2010 | CN101909999A Locking system for air intake structure for turbojet engine nacelle |
| 12/08/2010 | CN101909998A Aircraft nacelle guidance system installation |
| 12/08/2010 | CN101907022A Methods relating to turbine engine control and operation |
| 12/08/2010 | CN101907020A System for conditioning the airflow entering a turbomachine |
| 12/08/2010 | CN101324206B Cross flame holder for rotor engine |
| 12/08/2010 | CN101245713B 废气涡轮 Turbocharged |
| 12/08/2010 | CN101230988B Operating method for coal gasification combined cycle power plant |
| 12/08/2010 | CN101082345B Bolt-on radial bleed manifold |
| 12/08/2010 | CN101035966B Structure for separating the internal areas of a high pressure and a low pressure turbine |
| 12/07/2010 | US7845159 Heat pipe-based cooling apparatus and method for turbine engine |
| 12/07/2010 | CA2473565C High-temperature protection layer |
| 12/07/2010 | CA2454921C Methods and apparatus for exchanging heat |
| 12/02/2010 | WO2010138677A2 Adsorption-enhanced compressed air energy storage |
| 12/02/2010 | WO2010138507A1 Stabilizing a gas turbine engine via incremental tuning |
| 12/02/2010 | WO2010136454A1 Intake air temperature control device and a method for operating an intake air temperature control device |
| 12/02/2010 | WO2010110833A3 Recuperator for gas turbine engines |
| 12/02/2010 | US20100301161 Acoustic coating for an aircraft incorporating a frost treatment system by joule effect |
| 12/02/2010 | US20100300116 Expansion Hula Seals |
| 12/02/2010 | US20100300115 Process for producing combustor structural member, and combustor structural member, combustor for gas turbine and gas turbine |
| 12/02/2010 | US20100300113 Anti-vortex device for a gas turbine engine compressor |
| 12/02/2010 | US20100300109 Fuel injection method |
| 12/02/2010 | US20100300107 Method and flow sleeve profile reduction to extend combustor liner life |
| 12/02/2010 | US20100300105 Airblast fuel nozzle assembly |
| 12/02/2010 | US20100300102 Method and apparatus for air and fuel injection in a turbine |
| 12/02/2010 | US20100300061 Selective Catalytic Reduction System and Process for Treating NOx Emissions Using a Palladium and Rhodium or Ruthenium Catalyst |
| 12/02/2010 | DE102010016893A1 Verdichterradelement einer Turbomaschine Verdichterradelement a turbomachine |
| 12/02/2010 | DE102010016826A1 Verfahren und Systeme zur Erzeugung von dynamischen Verbrennungsvorgängen Methods and systems for the generation of dynamic combustion processes |
| 12/02/2010 | DE102007036913A1 Turbocharger, particularly supercharger for internal-combustion engine, has turbine, compressor and shaft, on which turbine rotor and compressor rotor are installed in pivoted manner |
| 12/02/2010 | CA2763642A1 Adsorption-enhanced compressed air energy storage |
| 12/02/2010 | CA2763617A1 Stabilizing a gas turbine engine via incremental tuning |
| 12/01/2010 | EP2256319A2 Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup |
| 12/01/2010 | EP2256318A1 Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same |
| 12/01/2010 | EP2256317A1 A process for generating power |
| 12/01/2010 | EP2256316A1 Intake air tempering device and a method for operating same |
| 12/01/2010 | EP2256299A2 Deflector for a gas turbine strut and vane assembly |
| 12/01/2010 | EP2256294A1 Gas turbine, intermediate shaft for gas turbine, and method of cooling gas turbine compressor |
| 12/01/2010 | EP2256221A1 Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine |
| 12/01/2010 | EP2255081A2 System, method and apparatus for lean combustion with plasma from an electrical arc |
| 12/01/2010 | EP2254747A1 Method for joining cellular acoustic panels |
| 12/01/2010 | CN101903241A Ice protection system for a multi-segment aircraft component |
| 12/01/2010 | CN101900032A Gas turbine engine cooling system and method |
| 12/01/2010 | CN101566102B Power generator of rotary-catalytic regenerative-type gas turbine |
| 12/01/2010 | CN101041385B De-icing system for the inlet cone of an aircraft turboengine |
| 11/30/2010 | US7844385 Microserver engine control card |
| 11/30/2010 | US7841187 Turbomachine comprising a system for cooling the downstream face of an impeller of a centrifugal compressor |
| 11/30/2010 | US7841185 Turbine engine and a method of operating a turbine engine |
| 11/30/2010 | US7841184 Start flow measurement |
| 11/30/2010 | US7841183 Method and apparatus for delivering a liquid |
| 11/30/2010 | US7841181 Gas turbine engine combustion systems |
| 11/30/2010 | CA2538899C Passive exhaust suppressor and method |
| 11/30/2010 | CA2371453C A thermodynamic apparatus |
| 11/25/2010 | WO2010135030A2 Aircraft engine starting/generating system and method of control |
| 11/25/2010 | WO2010134570A1 Method for producing impeller applied to supercharger |
| 11/25/2010 | WO2010133483A2 Method of cooling a hydrocarbon stream and apparatus therefor |
| 11/25/2010 | WO2010133482A2 Method and apparatus for cooling a gaseous hydrocarbon stream |
| 11/25/2010 | WO2010094878A3 Engine mounting with an adapted load/deformation curve |
| 11/25/2010 | WO2010089498A3 Turbojet engine nacelle |
| 11/25/2010 | US20100296947 Apparatus and method for providing damper liquid in a gas turbine |
| 11/25/2010 | US20100294882 Aircraft leading edge |
| 11/25/2010 | US20100293973 Combined cycle exhaust powered turbine inlet air chilling |
| 11/25/2010 | US20100293964 Breather duct shielding |
| 11/25/2010 | US20100293961 Gas turbine starting with stepping speed control |
| 11/25/2010 | US20100293960 Gas Turbine Engine Starting Method and Control Device |
| 11/25/2010 | US20100293959 Method for Operating a Gas Turbine Engine, Power Supplying Device for Conducting such Method and Aircraft using such Method |
| 11/25/2010 | US20100293958 Deswirling exhaust mixer |
| 11/25/2010 | US20100293957 System and method for cooling a wall of a gas turbine combustor |
| 11/25/2010 | US20100293956 Turbine fuel nozzle having premixer with auxiliary vane |
| 11/25/2010 | US20100293955 Multi-premixer fuel nozzle support system |
| 11/25/2010 | US20100293954 Method and apparatus for combustor nozzle with flameholding protection |
| 11/25/2010 | US20100293952 Resonating Swirler |
| 11/25/2010 | US20100293919 Dual-pump fuel system and method for starting a gas turbine engine |
| 11/25/2010 | US20100293918 Method and system for use with an integrated gasification combined cycle plant |
| 11/25/2010 | US20100293917 Gas turbine engine having a nacelle and a breather duct |
| 11/25/2010 | DE102010016892A1 Brennstoffdüsenhaltesystem mit vielen Vormisch-Brennstoffdüsen Fuel nozzle support system with many premix fuel nozzle |
| 11/25/2010 | DE102010016890A1 Aktives Regelungssystem und Verfahren zur Gehäuseausrichtung Active control system and method for Body Orientation |
| 11/25/2010 | DE102010016889A1 System und Verfahren zum Kühlen der Wand einer Gasturbinenbrennkammer System and method for cooling the wall of a gas turbine combustor |
| 11/25/2010 | CA2760172A1 Method and apparatus for cooling a gaseous hydrocarbon stream |
| 11/24/2010 | EP2253869A1 Rotary machine and additional ring |