| 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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| 08/28/2013 | CN102505991B Power generation device for condensed steam type double-working-medium gas turbine circulation system |
| 08/28/2013 | CN102410088B Adjustable guide vane system of gas turbine power turbine |
| 08/28/2013 | CN101815853B Turbocharger bearing assembly and lubrication thereof |
| 08/27/2013 | US8518160 Turbine inlet heat transfer system |
| 08/27/2013 | US8517663 Method and apparatus for gas turbine engine temperature management |
| 08/27/2013 | US8516830 Turbomachine combustion chamber |
| 08/27/2013 | US8516820 Integral flow sleeve and fuel injector assembly |
| 08/27/2013 | US8516819 Forward-section resonator for high frequency dynamic damping |
| 08/24/2013 | CA2806785A1 Fuel air heat exchanger |
| 08/24/2013 | CA2806342A1 Thermal expansion joint connection for sheet metal assembly |
| 08/24/2013 | CA2806068A1 Air-cooled oil cooler for turbofan engine |
| 08/22/2013 | WO2013123195A1 Case with ballistic liner |
| 08/22/2013 | WO2013123172A1 Adjustable blade outer air seal apparatus |
| 08/22/2013 | WO2013123121A1 Gas turbine engine component with multi-lobed cooling hole |
| 08/22/2013 | WO2013123120A1 Gas turbine engine component with impingement and lobed cooling hole |
| 08/22/2013 | WO2013123115A1 Gas turbine engine component with impingement and diffusive cooling |
| 08/22/2013 | WO2013123012A1 Gas turbine engine component with compound cusp cooling configuration |
| 08/22/2013 | WO2013123008A1 Gas turbine engine component with converging/diverging cooling passage |
| 08/22/2013 | WO2013123006A1 Gas turbine engine component with cusped cooling hole |
| 08/22/2013 | WO2013122913A1 Cooling hole with curved metering section |
| 08/22/2013 | WO2013122910A1 Multi-lobed cooling hole |
| 08/22/2013 | WO2013122908A1 Multiple diffusing cooling hole |
| 08/22/2013 | WO2013122906A1 Tri-lobed cooling hole and method of manufacture |
| 08/22/2013 | WO2013122878A1 Anti-rotation stator segments |
| 08/22/2013 | US20130213733 Silencer and rotating machine equipped therewith |
| 08/22/2013 | US20130213051 Combustor and method for supplying fuel to a combustor |
| 08/22/2013 | US20130213045 Coated Porous Metallic Mat |
| 08/22/2013 | US20130213044 Architecture for feeding fuel to a power plant for driving a rotary wing of a rotorcraft |
| 08/22/2013 | US20130213004 Multi-electrode igniter for a gas turbine engine |
| 08/22/2013 | US20130213003 Retractable bird and debris deflector for an aircraft jet engine |
| 08/22/2013 | US20130213002 Gas turbine start/stop apparatus |
| 08/22/2013 | DE102012202341A1 Radial bearing for supercharger for motor car, has non-intersecting grooves which are helically formed around outer surface of shaft, so as to enhance lubrication oil supply by hole of floating socket |
| 08/22/2013 | DE102012202272A1 Rotor Rotor |
| 08/22/2013 | DE102012003348A1 Micro gas turbine plant for peripheral power supply of building, has recuperator into which exhaust gas stream is flowed through radial outlets and radial inlets of recuperator that transfers heat between exhaust stream and air flow |
| 08/22/2013 | DE102012003347A1 Annular recuperator for transferring heat from warmer fluid stream to cold fluid stream for micro gas turbine plant, has two passages that are separated from each other by wall, and fluid streams comprising filling arranged in passages |
| 08/21/2013 | EP2628920A2 Fuel heating system for power plant |
| 08/21/2013 | EP2628919A2 An aircraft propulsion system nacelle |
| 08/21/2013 | EP2628904A2 Turbine assembly and method for reducing fluid flow between turbine components |
| 08/21/2013 | EP2627883A1 Method for operating a gas turbine in the case of load shedding, a device for controlling the operation of a gas turbine and a power plant |
| 08/21/2013 | EP2627882A2 Generating power using an ion transport membrane |
| 08/21/2013 | EP2627870A2 Connecting module between a drive shaft of an engine fan and a rolling element bearing |
| 08/21/2013 | CN203146115U Electric heating anti-icing system of engine lip |
| 08/21/2013 | CN103261675A Multi-event corona discharge ignition assembly and method of control and operation |
| 08/21/2013 | CN103261632A Integrated method and apparatus for compressing air and producing carbon dioxide-ich fluid |
| 08/21/2013 | CN103261631A Flow path structure and gas turbine exhaust diffuser |
| 08/21/2013 | CN103261585A Buffer air for a labyrinth seal |
| 08/21/2013 | CN103259361A High altitude and high voltage rear terminal block assembly |
| 08/21/2013 | CN103256122A Seal for a variable area fan nozzle |
| 08/21/2013 | CN103256121A Cooling of a shroud hanger assembly of a gas turbine engine |
| 08/21/2013 | CN103256120A Gas turbine inlet system with solid-state heat pump |
| 08/21/2013 | CN103256119A Integration system for religion architecture |
| 08/21/2013 | CN101845997B Apparatus for turbine engine cooling air management |
| 08/21/2013 | CN101652535B Assistance device for transient acceleration and deceleration phases |
| 08/21/2013 | CN101629878B System for sampling the airflow entering the compressor of a turbomachine |
| 08/21/2013 | CN101446235B Rotor decoupler system for a gas turbine |
| 08/21/2013 | CN101169074B Method for detecting onset of uncontrolled fuel in a gas turbine combustor |
| 08/21/2013 | CN101169073B Turbine inlet air treatment apparatus |
| 08/20/2013 | US8511987 Engine bearing support |
| 08/20/2013 | US8511972 Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine |
| 08/20/2013 | US8511099 Combustor system |
| 08/20/2013 | US8511098 Slideable liner link assembly |
| 08/20/2013 | US8511097 Gas turbine combustor and ignition method of igniting fuel mixture in the same |
| 08/20/2013 | US8511096 High bleed flow muffling system |
| 08/20/2013 | US8511094 Combustion apparatus using pilot fuel selected for reduced emissions |
| 08/20/2013 | US8511088 Gas turbine fuel injector mounting system |
| 08/20/2013 | US8511087 Fuel injector and swirler assembly with lobed mixer |
| 08/20/2013 | US8511057 Lubricant scavenge arrangement |
| 08/20/2013 | US8511056 Gas turbine engine having a nacelle and a breather duct |
| 08/20/2013 | US8511055 Apparatus and method for providing damper liquid in a gas turbine |
| 08/20/2013 | CA2601027C Method and apparatus for utilising fugitive gases as a supplementary fuel source |
| 08/15/2013 | WO2013119652A1 Electroformed sheath |
| 08/15/2013 | WO2013119645A1 Turbine engine shaft coupling |
| 08/15/2013 | WO2013119535A1 Gas turbine engine with modular cores and propulsion unit |
| 08/15/2013 | WO2013119527A1 Gas turbine engine with separate core and propulsion unit |
| 08/15/2013 | WO2013119520A1 Customer bleed air pressure loss reduction |
| 08/15/2013 | US20130211690 Detection System and Method to Detect Flame Holding Event |
| 08/15/2013 | US20130207351 Seal arrangement for sealling a gap; and sealing element for this purpose |
| 08/15/2013 | US20130205803 Multi-lobed cooling hole array |
| 08/15/2013 | US20130205802 Cooling hole with crenellation features |
| 08/15/2013 | US20130205801 Multi-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205797 Fuel heating system for power plant |
| 08/15/2013 | US20130205795 Turbomachine flow improvement system |
| 08/15/2013 | US20130205794 Gas turbine engine component with impingement and lobed cooling hole |
| 08/15/2013 | US20130205793 Gas turbine engine component with impingement and diffusive cooling |
| 08/15/2013 | US20130205792 Cooling hole with asymmetric diffuser |
| 08/15/2013 | US20130205791 Cooling hole with curved metering section |
| 08/15/2013 | US20130205790 Multi-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205789 Fuel nozzle end cover, fuel nozzle, and process of fabricating a fuel nozzle end cover |
| 08/15/2013 | US20130205787 Tri-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205754 Oxidizer compound for rocket propulsion |
| 08/15/2013 | CA2795647A1 Thermoelectric generator in turbine engine nozzles |
| 08/14/2013 | EP2626636A2 Fuel nozzle end cover, fuel nozzle, and process of fabricating a fuel nozzle end cover |
| 08/14/2013 | EP2626536A2 Acoustic panel and method of forming |
| 08/14/2013 | EP2626535A2 System and method for gas turbine inlet air heating |
| 08/14/2013 | EP2626533A1 Method for operating a gas turbine |
| 08/14/2013 | EP2626523A1 Assembly interface and method between a device and a rotating power source of an engine unit provided on a rotorcraft |
| 08/14/2013 | CN203130259U Axial force adjusting device of gas turbine rotor |
| 08/14/2013 | CN203130257U Intermediate and turbocharger |
| 08/14/2013 | CN203130256U Intermediate and turbocharger |
| 08/14/2013 | CN103249931A End-fed liquid fuel gallery for a gas turbine fuel injector |