| 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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| 06/23/2011 | WO2010103303A3 Turbine engine support arms |
| 06/23/2011 | US20110146299 Annulus filler assembly for a rotor of a turbomachine |
| 06/23/2011 | US20110146298 Retaining member for use with gas turbine engine shaft and method of assembly |
| 06/23/2011 | US20110146294 Airplane engine deflector systems |
| 06/23/2011 | US20110146293 Method for connecting a starting means to a turbomachine |
| 06/23/2011 | US20110146292 Method for starting a turbomachine |
| 06/23/2011 | US20110146291 Method for starting a turbomachine |
| 06/23/2011 | US20110146290 Method of starting a turbomachine |
| 06/23/2011 | US20110146285 Pulse detonation system with fuel lean inlet region |
| 06/23/2011 | US20110146229 Integration of a Surface Heat Exchanger to the Wall of an Aerodynamic Flowpath by a Structure of Reinforcement Rods |
| 06/23/2011 | US20110146227 Apparatus and assembly for a spark igniter |
| 06/23/2011 | US20110146226 Recuperator for gas turbine engines |
| 06/23/2011 | US20110146224 Arrangement for the discharge of oil-venting air on a gas-turbine engine |
| 06/23/2011 | US20110146223 Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine |
| 06/23/2011 | CA2782724A1 Air intake for a plant |
| 06/22/2011 | EP2336525A1 Integration of an air-liquid heat exchanger on an engine |
| 06/22/2011 | EP2336524A2 Gas turbine engine with cooling arrangement |
| 06/22/2011 | EP2336505A2 Lubricant supply filtration system |
| 06/22/2011 | EP2336504A2 Oil cooler |
| 06/22/2011 | EP2336503A2 Arrangement for the discharge of ventilation air separated from the lubricating oil de-aeration system of a gas-turbine engine |
| 06/22/2011 | EP2336501A2 Assembly for removing oil ventilation air in a gas turbine engine |
| 06/22/2011 | EP2336500A2 Aircraft engine inlet having zone of deformation |
| 06/22/2011 | EP2336499A1 Procedure for cold-starting an engine |
| 06/22/2011 | EP2336491A2 Turbofan engine with power extraction system |
| 06/22/2011 | EP2334909A1 Sealing between a combustion chamber and a turbine distributor in a turbine engine |
| 06/22/2011 | EP2334557A1 Device for connecting an air inlet with an aircraft nacelle actuator assembly |
| 06/22/2011 | DE102009060051A1 Anordnung zum Abblasen von aus dem Schmierölentlüftungssystem eines Gasturbinentriebwerks ab getrennter Abluft Arrangement for blowing off from the lubricating oil breather system of a gas turbine engine exhaust from separate |
| 06/22/2011 | DE102009059019A1 Anordnung zum Abführen von Ölentlüftungsluft bei einem Gasturbinentriebwerk An arrangement for discharging oil venting air in a gas turbine engine |
| 06/22/2011 | CN102105260A Welding material for Ni-based alloy |
| 06/22/2011 | CN102102588A Integrated nacelle assembly |
| 06/22/2011 | CN102102586A Peak load power generation device |
| 06/22/2011 | CN102102585A System and method for reducing sulfur compounds within fuel stream for turbomachine |
| 06/22/2011 | CN102101104A Aviation engine sealant sealing thrust increasing method |
| 06/21/2011 | US7963097 Flexible assembly of recuperator for combustion turbine exhaust |
| 06/21/2011 | US7963094 Fragmentor for bird ingestible gas turbine engine |
| 06/21/2011 | CA2726503A1 Integrated nacelle assembly |
| 06/21/2011 | CA2491186C Plate with means of fastening to a support and a sealing joint |
| 06/21/2011 | CA2421117C Process for forming a sector of an inlet lip , system for its implementation and sector thus obtained |
| 06/16/2011 | WO2011070806A1 Structure for connecting a combustor to a turbine unit, and gas turbine |
| 06/16/2011 | WO2011070108A1 Monitoring system for an inner chamber of a machine |
| 06/16/2011 | WO2011005858A3 Compressor cooling for turbine engines |
| 06/16/2011 | US20110140370 Seal Member for Use in a Seal System Between a Transition Duct Exit Section and a Turbine Inlet in a Gas Turbine Engine |
| 06/16/2011 | US20110138819 Gas turbine engine with cooling arrangement |
| 06/16/2011 | US20110138818 Gas turbine and operating method thereof |
| 06/16/2011 | US20110138817 Method of increasing the safety of a power plant, and a power plant suitable for implementing the method |
| 06/16/2011 | US20110138815 Swirler for mixing fuel and air |
| 06/16/2011 | US20110138813 Impurity detection in combustor systems |
| 06/16/2011 | US20110138812 Resonator System for Turbine Engines |
| 06/16/2011 | US20110138772 Turbine detuner for recovering kinetic energy from gas turbine engine exhaust gases |
| 06/16/2011 | US20110138771 Method of Operating a Gas Turbine Power Plant with Auxiliary Power to Reduce Emissions |
| 06/16/2011 | US20110138769 Fan containment case |
| 06/16/2011 | US20110138766 System and method of improving emission performance of a gas turbine |
| 06/16/2011 | DE102009058102A1 Compressor for supercharging device, particularly turbo charger for internal combustion engine, comprises compressor housing and ring element which is held at compressor housing by rod |
| 06/16/2011 | DE102009058068A1 Lagergehäuse einer Ladeeinrichtung Bearing housing of a charging device |
| 06/16/2011 | DE102008051241B4 Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs Silencer for an auxiliary power unit of an aircraft |
| 06/15/2011 | EP2333281A2 Systems and methods for unchoked control of gas turbine fuel gas control valves |
| 06/15/2011 | EP2333280A2 Methods for controlling fuel mixing |
| 06/15/2011 | EP2333248A1 Gas turbine and operating method therefor |
| 06/15/2011 | EP2146897B1 Fan casing made from composite materials having toughened and untoughened regions |
| 06/15/2011 | CN201865772U Vector engine of aerial propeller |
| 06/15/2011 | CN201865771U High-efficiency combustion engine air intake cooling system with mixed cold source |
| 06/15/2011 | CN1826456B Turbine component, gas turbine engine, method of manufacture turbine component, surface processing method, blade component, metal component and steam turbine engine |
| 06/15/2011 | CN1683750B Repairing tenons on turbine buckets |
| 06/15/2011 | CN102099556A Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 06/15/2011 | CN102094850A Design method of circumferential discontinuously distributed entraining grooves of engine air system |
| 06/15/2011 | CN102094713A System and method of reducing heat loss from a gas turbine during shutdown |
| 06/15/2011 | CN102094712A Micro gas turbine system with gas bearing-rotor structure |
| 06/15/2011 | CN102094711A Device for measuring total pressure and total temperature of air flow at inlet of aeromotor |
| 06/15/2011 | CN101592081B Gas turbine generating engine |
| 06/14/2011 | US7958717 Gas turbine power generator plant and silencer for the same |
| 06/14/2011 | CA2660211C Gas turbine engine exhaust duct ventilation |
| 06/09/2011 | US20110131998 Fuel injection in secondary fuel nozzle |
| 06/09/2011 | DE202011004521U1 Gasturbine und Ansaugkrümmer Gas turbine and intake manifold |
| 06/09/2011 | DE202011001957U1 Warmluft-Enteiser Hot air de-icer |
| 06/09/2011 | DE112009001807T5 System und Verfahren zum Betreiben eines Gasturbinenantriebs mit einem alternativen Arbeitsfluid System and method of operating a gas turbine engine with an alternative working fluid |
| 06/09/2011 | DE102010060651A1 Systeme in Bezug auf Erdwärme und den Betrieb von Gasturbinen Systems in terms of geothermal energy and the operation of gas turbines |
| 06/09/2011 | DE102009057100A1 Aggregate for power-heat coupling for small residential units, has gas turbine, compressor and generator, where expander of gas turbine, compressor and generator are arranged on common shaft |
| 06/08/2011 | EP2330350A1 Dual walled combustors with impingement cooled igniters |
| 06/08/2011 | EP2330281A1 Gas turbine device |
| 06/08/2011 | EP2330280A1 Method of operating a gas turbine; a gas turbine system; and a method and system for cooling a hydrocarbon stream |
| 06/08/2011 | EP2330233A1 A method for making a protective coating on a metal substrate |
| 06/08/2011 | EP2329130A2 Active thermal protection for fuel injectors |
| 06/08/2011 | EP2329121A2 Multi passage fuel manifold and methods of construction |
| 06/08/2011 | EP2329112A2 Turbine cooling system |
| 06/08/2011 | CN201858027U Novel edge cooling corrugated unit |
| 06/08/2011 | CN201858026U Novel thermal-edge corrugation device |
| 06/08/2011 | CN1963159B Methods and apparatus for a combustion turbine nitrogen purge system |
| 06/08/2011 | CN102089499A One-stage stator vane cooling structure and gas turbine |
| 06/07/2011 | US7954324 Gas turbine engine |
| 06/07/2011 | US7954310 Fuel oil bi-directional flow divider |
| 06/07/2011 | CA2464188C Passive cooling system for auxiliary power unit installation |
| 06/03/2011 | WO2011066039A1 Thermal energy storage apparatus for an adiabatic compressed air energy storage system and corresponding method of forming this system |
| 06/03/2011 | WO2011007236A4 Gas turbine exhaust gas cooling system |
| 06/03/2011 | CA2781894A1 Thermal energy storage apparatus for an adiabatic compressed air energy storage system and corresponding method of forming this system |
| 06/02/2011 | US20110126549 Ultra low emissions fast starting power plant |
| 06/02/2011 | US20110126548 Method and device for the combustion of hydrocarbon-containing fuels |
| 06/02/2011 | US20110126543 Combustor panel arrangement |
| 06/02/2011 | US20110126510 Pulse detonation combustor |
| 06/02/2011 | US20110126509 Pilot Burner of a Gas Turbine Engine, Combustor, and Gas Turbine Engine |
| 06/02/2011 | US20110126508 Fan case having penetration resistant blanket |