| 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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| 02/11/2010 | WO2010015500A1 Ignition device for a laser ignition of an internal combustion engine |
| 02/11/2010 | US20100034647 Processes for the formation of positive features on shroud components, and related articles |
| 02/11/2010 | US20100034640 Nested core gas turbine engine |
| 02/11/2010 | US20100034638 Impingement cooling arrangement |
| 02/11/2010 | US20100034635 Predictive Model Based Control System for Heavy Duty Gas Turbines |
| 02/11/2010 | US20100031673 Casing of a gas turbine engine |
| 02/11/2010 | US20100031672 Gas turbine |
| 02/11/2010 | US20100031671 Inner ring with independent thermal expansion for mounting gas turbine flow path components |
| 02/11/2010 | US20100031666 Flow sleeve impingement coolilng baffles |
| 02/11/2010 | US20100031665 Flow sleeve impingement cooling using a plenum ring |
| 02/11/2010 | US20100031663 Turbomachine with a diffuser |
| 02/11/2010 | US20100031662 Turbomachine injection nozzle including a coolant delivery system |
| 02/11/2010 | US20100031660 System and assemblies for pre-heating fuel in a combined cycle power plant |
| 02/11/2010 | US20100031659 Method and Device for Monitoring the Formation of Deposits of Solid Particles, Particularly in a Fuel Line and in the Fuel Valves of a Gas Turbine |
| 02/11/2010 | US20100031658 Gas turbine fuel metering unit |
| 02/11/2010 | US20100031629 Lockable guiding system for a mobile part of a nacelle |
| 02/11/2010 | US20100031624 Fuel heating via exhaust gas extraction |
| 02/11/2010 | DE102009026284A1 System und Anordnungen zur Heißwasserentnahme zum Vorheizen von Brennstoff in einem Kombizykluskraftwerk System and arrangements for hot water supply for preheating of fuel in a combined cycle power plant |
| 02/11/2010 | DE102008036980A1 Stelleinrichtung und mit einer derartigen Stelleinrichtung ausgeführte Ventilanordnung Adjusting device and executed with such a setting device valve assembly |
| 02/11/2010 | DE102008022188B4 Verfahren zum Betreiben einer Dampfturbine A method of operating a steam turbine |
| 02/11/2010 | CA2732801A1 Method for making deicing system on a nacelle panel |
| 02/10/2010 | EP1444658B1 Fault management system for gas turbine engines |
| 02/10/2010 | CN101644193A System and assemblies for pre-heating fuel in a combined cycle power plant |
| 02/10/2010 | CN101644192A System und anordnungen zur heisswasserentnahme zum vorheizen von brennstoff in einem kombizykluskraftwerk |
| 02/09/2010 | US7658078 System for reforming heavy oil, method therefor, and combined cycle power system |
| 02/09/2010 | US7658077 System for deicing an aircraft turbine engine inlet cone |
| 02/09/2010 | US7658062 Gas generator and turbojet fitted with such a generator for starting |
| 02/09/2010 | US7658061 Gas turbine engine provided with a foreign matter removal passage |
| 02/09/2010 | US7658060 Lubricant cooling exchanger dual intake duct |
| 02/05/2010 | CA2668219A1 Turbomachine injection nozzle including a coolant delivery system |
| 02/04/2010 | WO2010013565A1 Welding material for ni-based alloy |
| 02/04/2010 | WO2010013316A1 Hybrid power generation system and its operating method |
| 02/04/2010 | WO2010012900A2 Acoustic attenuation panel for aircraft engine nacelle |
| 02/04/2010 | WO2010012899A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 02/04/2010 | WO2009114205A3 Adsorption-enhanced compressed air energy storage |
| 02/04/2010 | US20100028129 Fan casing for a gas turbine engine |
| 02/04/2010 | US20100024435 Nacelle for turbofan |
| 02/04/2010 | US20100024434 Gas turbine engine arrangement |
| 02/04/2010 | US20100024433 System and method of operating a gas turbine engine with an alternative working fluid |
| 02/04/2010 | US20100024431 Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine |
| 02/04/2010 | US20100024430 Method for operating a firing system |
| 02/04/2010 | US20100024429 Apparatus, system and method for heating fuel gas using gas turbine exhaust |
| 02/04/2010 | US20100024427 Precision counter-swirl combustor |
| 02/04/2010 | US20100024426 Hybrid Fuel Nozzle |
| 02/04/2010 | US20100024425 Turbine engine fuel nozzle |
| 02/04/2010 | US20100024379 Gas Turbine Combustor Exhaust Gas Spray Cooling for NOx Control Using Selective Catalytic Reductions |
| 02/04/2010 | US20100024378 System and method of operating a gas turbine engine with an alternative working fluid |
| 02/04/2010 | DE102009026282A1 Wärmeleitrohr-Zwischenkühler für eine Turbomaschine Heat pipe intercooler for a turbomachine |
| 02/04/2010 | DE102009026240A1 Gasturbinenverbrennungsabgas-Sprühkühlung zur NOx-Steuerung unter Anwendung selektiver katalytischer Reduktionsvorgänge Gas turbine combustion exhaust gas spray cooling for NOx control using selective catalytic reduction processes |
| 02/04/2010 | DE102009026211A1 Verfahren und Systeme zum Betreiben eines Kombikraftwerks Methods and systems for operating a combined cycle power plant |
| 02/04/2010 | DE102009026157A1 Mittelkörperkappe für eine Turbomaschinenbrennkammer und Verfahren Central body cap for a turbo engine combustion chamber and procedures |
| 02/04/2010 | DE102008035880A1 Kühlanordnung eines Kraftfahrzeuges Cooling assembly of a motor vehicle |
| 02/04/2010 | CA2732351A1 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 02/04/2010 | CA2731974A1 Acoustic attenuation panel for aircraft engine nacelle |
| 02/03/2010 | EP2149707A2 Fuel pumping system |
| 02/03/2010 | EP2149690A2 Turbine rotor |
| 02/03/2010 | EP2149681A2 Nested bearing cages |
| 02/03/2010 | CN100586796C Ram air channel for the supply of ambient air in an aircraft and operation method thereof |
| 02/02/2010 | US7656054 Turbine engine with an alternator and method for transmitting movement to an alternator |
| 02/02/2010 | US7654094 Radial turbine and method of cooling nozzle of the same |
| 02/02/2010 | US7654093 Method of adjusting a triggering clearance and a trigger |
| 02/02/2010 | US7654091 Method and apparatus for cooling gas turbine engine combustors |
| 02/02/2010 | US7654088 Dual conduit fuel manifold for gas turbine engine |
| 02/02/2010 | US7654087 Compact compound engine package |
| 02/02/2010 | US7654085 System of an induced flow machine |
| 01/31/2010 | CA2672818A1 Nested bearing cages |
| 01/28/2010 | WO2010009708A1 Engine comprising a core engine and thruster connected downstream |
| 01/28/2010 | US20100023298 Device for determining the distance between a rotor blade and a wall of a turbine engine surrounding the rotor blade |
| 01/28/2010 | US20100021293 Slotted compressor diffuser and related method |
| 01/28/2010 | US20100019496 Method and systems for operating a combined cycle power plant |
| 01/28/2010 | US20100018219 Device for optimizing cooling in gas turbines |
| 01/28/2010 | US20100018211 Gas turbine transition piece having dilution holes |
| 01/28/2010 | US20100018210 Combustor apparatus in a gas turbine engine |
| 01/28/2010 | US20100018209 Integral flow sleeve and fuel injector assembly |
| 01/28/2010 | US20100018208 Turbine engine flow sleeve |
| 01/28/2010 | US20100018181 Centerbody cap for a turbomachine combustor and method |
| 01/28/2010 | US20100018180 Apparatus and method for cooling turbomachine exhaust gas |
| 01/28/2010 | DE102009026237A1 Gasturbinenübergangsstück mit Verdünnungslöchern Gas turbine transition piece with dilution holes |
| 01/28/2010 | DE102009026212A1 Geprägte Endabdeckung und/oder Brennkammergehäusedichtung und zugehöriges Verfahren Embossed end cover and / or combustion chamber housing seal and associated method |
| 01/28/2010 | DE102009026210A1 Geschlitzter Verdichterdiffusor und zugehöriges Verfahren Slotted compressor diffuser and associated method |
| 01/28/2010 | DE102009026156A1 Vorrichtung und Verfahren zur Turbomaschinenabgaskühlung Apparatus and method for turbomachinery exhaust gas cooling |
| 01/28/2010 | DE102009026130A1 Gasturbinenvormischer mit kraterartigen Brennstoffinjektionsstellen Gasturbinenvormischer with crater-like fuel injection sites |
| 01/27/2010 | EP2148066A1 Hybrid power plant and method of controlling such a power plant |
| 01/27/2010 | EP2148065A1 Gas turbine engine |
| 01/27/2010 | EP2148064A2 Gas turbine engine nacelle |
| 01/27/2010 | EP2148063A2 Gas turbine engine nacelle |
| 01/27/2010 | EP2148062A2 Gas turbine engine nacelle |
| 01/27/2010 | EP2146897A1 Articles made from composite materials having toughened and untoughened regions |
| 01/27/2010 | CN101636575A Method for making an acoustic treatment coating and acoustic treatment coating thus obtained |
| 01/27/2010 | CN101634247A Apparatus and method for cooling turbomachine exhaust gas |
| 01/27/2010 | CN100585160C Method of operating a gas engine plant and fuel feeding system of a gas engine |
| 01/26/2010 | US7651023 Nickel-based braze alloy compositions and related processes and articles |
| 01/26/2010 | CA2409579C Discharge means for bypass engines |
| 01/21/2010 | WO2010007220A2 Turbomachine structural casing |
| 01/21/2010 | WO2009014780A3 Noise controlled turbine engine with aircraft engine adaptive noise control tubes |
| 01/21/2010 | US20100014985 Shroud segment cooling configuration |
| 01/21/2010 | US20100014968 Centering device |
| 01/21/2010 | US20100014958 Turbine engine rotor disc with cooling passage |
| 01/21/2010 | US20100012775 Torsionally De-Coupled Engine Mount System |
| 01/21/2010 | US20100011780 Combustor liner support and seal assembly |