| 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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| 05/04/2011 | EP2316911A1 Operating method of a thermal device supplied with aluminium- and titanium-based compounds to reduce corrosion and clogging at high temperatures. |
| 05/04/2011 | EP1827656B1 Method for removing and recovering co2 from an exhaust gas |
| 05/04/2011 | EP1394361B1 Gas turbine |
| 05/04/2011 | CN201818358U Fluid gas-phase working medium compression system |
| 05/04/2011 | CN102046984A Compressor cover for turbine engine having axial abutment |
| 05/04/2011 | CN102046954A Subsonic and stationary ramjet engines |
| 05/04/2011 | CN102042091A System and method for distributing fuel in a turbomachine |
| 05/04/2011 | CN102042090A Reheat gas turbine |
| 05/04/2011 | CN102042089A Low btu fuel injection system |
| 05/04/2011 | CN102042088A Moisture separation system and method of assembling the same |
| 05/04/2011 | CN102042087A Systems and methods for bypassing an inlet air treatment filter |
| 05/04/2011 | CN102042086A Explosion protection, gas turbine and internal combustion engine |
| 05/04/2011 | CN102042048A Exhaust gas diffuser |
| 05/04/2011 | CN102042045A Shroud assembly with discourager |
| 05/04/2011 | CN101566101B Power generation method of rotary-catalytic regenerative-type low-calorific-value gas turbine |
| 05/04/2011 | CA2719626A1 Aircraft starter generator |
| 05/03/2011 | CA2523967C Device for injecting water or water vapor into the working medium of a gas turbine plant |
| 04/30/2011 | CA2718682A1 Planetary gear reduction system |
| 04/28/2011 | WO2011048035A1 A method of operating a multi-fuel combustion system |
| 04/28/2011 | WO2011005438A3 Filter element support assembly, quick installation system, and methods |
| 04/28/2011 | US20110097199 System and method to insulate turbines and associated piping |
| 04/28/2011 | US20110094241 Gas turbine starting process |
| 04/28/2011 | US20110094240 Swirl Generator |
| 04/28/2011 | US20110094239 Low NOx Combustor for Hydrogen-Containing Fuel and its Operation |
| 04/28/2011 | US20110094237 Thermal power plant with co2 sequestration |
| 04/28/2011 | US20110094234 Fuel flexible combustor systems and methods |
| 04/28/2011 | US20110094232 Apparatus for conditioning airflow through a nozzle |
| 04/28/2011 | US20110094229 Adiabatic compressed air energy storage system with combustor |
| 04/28/2011 | US20110094212 Compressed air energy storage system with reversible compressor-expander unit |
| 04/28/2011 | DE102010038134A1 Modellgestützte koordinierte Luft-Brennstoff-Steuerung für eine Gasturbine Model-based coordinated air-fuel control for a gas turbine |
| 04/28/2011 | DE102010038124A1 Brennstoffflexible Brennkammersysteme und Verfahren Flexible fuel combustion systems and methods |
| 04/27/2011 | EP2314883A1 Device for feeding air to a compressor of a gas turbine |
| 04/27/2011 | EP2313617A1 A gas turbine component and a gas turbine engine comprising the component |
| 04/27/2011 | EP1761736B1 Heat exchanger with header tubes |
| 04/27/2011 | CN1676884B Erosion and wear resistant protective structures for turbine engine components |
| 04/27/2011 | CN102032050A Pre-mix catalytic partial oxidation fuel reformer for gas turbine systems |
| 04/27/2011 | CN102032049A Methods and systems involving carbon sequestration and engines |
| 04/27/2011 | CN102032048A Carbon capture cooling system and method |
| 04/27/2011 | CN102032047A Apparatus and method for removing heat from a gas turbine |
| 04/27/2011 | CN102032046A Cooling and tapping system for a gas turbine engine and corresponding operation method |
| 04/27/2011 | CN102032045A System and method for scheduling startup of a combined cycle power generation system |
| 04/27/2011 | CN102032044A Can to can modal decoupling using can-level fuel splits |
| 04/27/2011 | CN102032003A Drain for exhaust gas duct |
| 04/27/2011 | CN102032002A Helical inner diameter groove journal bearing |
| 04/27/2011 | CN101335473B 发电机 Generator |
| 04/26/2011 | US7931828 Gas turbine engine and method including composite structures with embedded integral electrically conductive paths |
| 04/26/2011 | US7930891 Transition duct with integral guide vanes |
| 04/21/2011 | WO2011046580A2 Bird deflector and air replacement system |
| 04/21/2011 | WO2011046063A1 Turbine blade |
| 04/21/2011 | WO2011045373A1 Gas turbine engine air intake in a nacelle |
| 04/21/2011 | WO2011045363A1 Device for filtering the intake air of an internal combustion engine having ventilation means |
| 04/21/2011 | WO2011045128A1 Sealing assembly on a steam turbine housing, comprising a fixable sealing ring |
| 04/21/2011 | WO2011045127A1 Sealing assembly on a steam turbine housing, comprising an adjustable sealing ring |
| 04/21/2011 | WO2010128241A3 Electric generator disposed on a rotating turboprop part |
| 04/21/2011 | US20110089262 Radially outward flowing air-blast fuel injector for gas turbine engine |
| 04/21/2011 | US20110088409 Fuel injector mounting system |
| 04/21/2011 | US20110088408 Fuel injector mounting system |
| 04/21/2011 | US20110088407 Fuel injector mounting system |
| 04/21/2011 | US20110088405 Gas turbine engine temperature modulated cooling flow |
| 04/21/2011 | US20110088404 Reheat gas turbine |
| 04/21/2011 | US20110088401 Mixer assembly for gas turbine engine combustor |
| 04/21/2011 | US20110088400 Gas fuel supply apparatus |
| 04/21/2011 | DE102010038021A1 Hochfester Querverteiler und Verfahren zum Verbinden High-strength transverse distributor and method for connecting |
| 04/21/2011 | DE102010038020A1 Abgasdiffusor Exhaust diffuser |
| 04/21/2011 | DE102010038018A1 Brennstoffdüsen-Lippendichtungen Fuel nozzle-lip seals |
| 04/21/2011 | DE102010037861A1 Gasturbine mit Zwischenüberhitzung Gas turbine with reheat |
| 04/21/2011 | DE102010037844A1 Brennstoffdüsendichtungsabstandhalter und Verfahren zu seinem Einbau Fuel nozzle seal spacer and method for its installation |
| 04/21/2011 | DE102009049841A1 Berstschutz Turbolader (Blech mehrschichtig) Burst protection turbocharger (sheet multi-layer) |
| 04/21/2011 | DE102009048511A1 Bearing unit i.e. dual-row ball bearing, for bearing balancing shaft of four-cylinder engine in turbocharger, has two rows of roller bodies arranged among inner rings and outer ring in axial region that is raised from shaft |
| 04/21/2011 | DE102009043453A1 Wärmedämmung für Turbinengehäuse Thermal insulation for turbine casing |
| 04/21/2011 | CA2776841A1 Gas turbine engine air intake in a nacelle |
| 04/21/2011 | CA2774516A1 Device for filtering the intake air of an internal combustion engine having ventilation means |
| 04/20/2011 | EP2312186A1 Method of manufacturing a fairing with an integrated seal |
| 04/20/2011 | EP2312126A1 Power generation system and corresponding power generating method |
| 04/20/2011 | EP2310652A1 Gas turbine engine and integrated heat exchange system |
| 04/20/2011 | EP2310267A1 Method for making deicing system on a nacelle panel |
| 04/20/2011 | CN201802493U Auxiliary lubricating oil system for aircraft engine |
| 04/20/2011 | CN102022191A Electric startup heater, gas turbine power plant and operation method thereof |
| 04/20/2011 | CN102022190A Integrated ion transport membrane and combustion turbine system |
| 04/20/2011 | CN102022184A Closed circulating water hydrogen energy application |
| 04/20/2011 | CN101586879B Solar thermal utilization system combined with gas-steam combined cycle |
| 04/19/2011 | US7926292 Partial oxidation gas turbine cooling |
| 04/19/2011 | US7926287 Method of operating a gas turbine engine |
| 04/19/2011 | US7926286 Heat shield for a fuel manifold |
| 04/19/2011 | US7926278 Gas-turbine combustion chamber wall for a lean-burning gas-turbine combustion chamber |
| 04/19/2011 | US7926256 Inlet system for an EGR system |
| 04/19/2011 | CA2466568C Method of starting a gas turbine engine |
| 04/19/2011 | CA2465573C Outer and inner cowl-wire wrap to one piece cowl conversion |
| 04/19/2011 | CA2451299C Nickel-base superalloy composition and its use in single-crystal articles |
| 04/19/2011 | CA2416399C Shroud segment and assembly for a turbine engine |
| 04/15/2011 | CA2716237A1 Gas turbine engine temperature modulated cooling flow |
| 04/15/2011 | CA2682818A1 Method of manufacturing a fairing with an integrated seal |
| 04/14/2011 | WO2011043286A1 Turbine |
| 04/14/2011 | WO2011042642A1 Circuit for supplying fuel to an aircraft engine |
| 04/14/2011 | WO2011042641A1 Circuit for supplying fuel to an aircraft engine |
| 04/14/2011 | WO2010136710A3 Fluid-cooling device for a turbine engine propulsive unit |
| 04/14/2011 | US20110083444 Low btu fuel injection system |
| 04/14/2011 | US20110083442 Apparatus and method for cooling nozzles |
| 04/14/2011 | US20110083441 System and method for distributing fuel in a turbomachine |
| 04/14/2011 | US20110083440 High strength crossover manifold and method of joining |