| 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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| 09/25/2008 | WO2008089925A3 Hydrodynamic drive of a high-pressure compressor shaft of a gas turbine engine |
| 09/25/2008 | WO2008087685A3 Open-cycle gas turbine engine system having power and modulation sections |
| 09/25/2008 | WO2008065656A3 Starting turbine engines |
| 09/25/2008 | US20080229757 Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants |
| 09/25/2008 | US20080229756 System and method for passive valving for pulse detonation combustors |
| 09/25/2008 | US20080229755 Humid air turbine, humid air turbine control system, and humid air turbine control method |
| 09/25/2008 | US20080229751 Cooling system for gas turbine engine having improved core system |
| 09/25/2008 | US20080229750 Location ring arrangement |
| 09/25/2008 | DE102008015342A1 Verbundmaterial für Turbinen-Tragestruktur Composite material for turbine support structure |
| 09/25/2008 | DE102007014253A1 Turbine einer Gasturbine Turbine of a gas turbine |
| 09/25/2008 | CA2678405A1 Acoustic panel |
| 09/24/2008 | EP1972774A2 Coated variable area fan nozzle, engine, and corresponding manufacturing method |
| 09/24/2008 | CN101273191A Two-shackle aircraft engine rear attachment |
| 09/24/2008 | CN101270768A Actuator position controller with a servo-valve with position memory in the event of power failure |
| 09/24/2008 | CN101270690A Fuel oil and lubricating oil heat exchanger of light aircraft engine |
| 09/24/2008 | CN101270689A Energy conversion and recovering method of coal gasification supercharging association circulating power generation system |
| 09/24/2008 | CN100420883C Improved brush-seal designs for turbines and smilar rotary apparatus |
| 09/24/2008 | CN100420835C Method for cooling turbomachine and turbomachine for applicating the same method |
| 09/23/2008 | US7426834 “Get home” oil supply and scavenge system |
| 09/23/2008 | US7426833 Gas turbine combustor and fuel supply method for same |
| 09/21/2008 | CA2626724A1 Actuator position controller with a servo-valve with position memory in the event of power failure |
| 09/20/2008 | CA2626119A1 Inter-turbine housing with cooling circuit and jet engine comprising same |
| 09/18/2008 | WO2008111585A1 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE VANE USING THE SAME |
| 09/18/2008 | WO2008111098A1 Air intake for a gas turbine compressor |
| 09/18/2008 | DE202008009449U1 Arretiervorrichtung Locking device |
| 09/18/2008 | DE102007026437A1 Gas turbine system for controlling heat value of gaseous fuel e.g. natural gas, has pressure reduction device with expansion machine for reduction of pressure of gaseous fuel, and mixer to mix air compressed by compressor to gaseous fuel |
| 09/17/2008 | CN101268266A Control system and control method of gas turbine |
| 09/17/2008 | CN101267986A 2387354t engine assembly comprising an engine and a suspension pylon for such an engine |
| 09/17/2008 | CN101265842A Improved system and method for reducing NOx emission |
| 09/17/2008 | CN100419236C Gas turbine brush seal arrangement for cabin air supply |
| 09/17/2008 | CN100419235C Internal anti-icing device of fanjet |
| 09/16/2008 | CA2496621C Cooling construction of transition piece of a gas turbine |
| 09/12/2008 | WO2008109718A1 Integrated cooling, heating, and power systems |
| 09/11/2008 | US20080216873 System and devices for collecting and treating waste water from engine washing |
| 09/11/2008 | US20080216510 Combined Cycle System For Gas Turbines and Reciprocating Engines and a Method for the Use of Air as Working Fluid in Combined Cycle Power Plants |
| 09/11/2008 | US20080216483 Engine Assembly for Aircraft Comprising an Engine as Well as a Device for Locking Said Engine |
| 09/11/2008 | US20080216482 Burner lance |
| 09/10/2008 | EP1967717A1 Gas turbine with a bypass conduit system |
| 09/10/2008 | EP1967716A1 Aircraft engine equipped with heat exchange system |
| 09/10/2008 | EP1967692A2 Turbine blade with microturbine nozzle fixed in blade root |
| 09/09/2008 | US7422611 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s)-centrifuge chamber/manifold particle collector |
| 09/09/2008 | US7422543 Rotation coupling employing torque converter and synchronization motor |
| 09/09/2008 | US7422416 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 09/09/2008 | US7421843 Catalytic combustor having fuel flow control responsive to measured combustion parameters |
| 09/09/2008 | US7421842 Turbine spring clip seal |
| 09/09/2008 | CA2465384C Gas turbine system comprising closed system of fuel and combustion gas using underground coal bed |
| 09/09/2008 | CA2424166C Gas collection pipe carrying hot gas |
| 09/04/2008 | WO2008104716A2 Method for making an acoustic treatment coating and coating thus obtained |
| 09/04/2008 | WO2008104714A2 Coating for acoustic treatment having a hot air icing processing function |
| 09/04/2008 | US20080210340 brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy containing chromium and cobalt for applying to a crack; second alloy sufficient to cause adequate flow during the braze cycle |
| 09/04/2008 | US20080209910 Method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit |
| 09/04/2008 | US20080209909 Gas turbine combustor and fuel supply method for same |
| 09/04/2008 | DE102007010403A1 High-temperature sensor for use in turbocharger overheating safety device, has heat disconnecting wire arranged between measuring resistor and feeder cable, where heat disconnecting wire is clamped at end facing measuring resistor |
| 09/04/2008 | DE102007001026B4 Verfahren zur rechnergestützten Steuerung und/oder Regelung eines technischen Systems Method for computer-aided control and / or regulating a technical system |
| 09/04/2008 | CA2678476A1 Process for producing a coating for acoustic treatment including aclose d cell structure with a complex form and coating for acoustic treatment thus obtained |
| 09/04/2008 | CA2678368A1 Coating for acoustic treatment having a hot air icing processing function |
| 09/03/2008 | EP1965056A1 Method of starting a gas turbine helicopter engine, fuel supply circuit for such an engine, and engine having such a circuit |
| 09/03/2008 | EP1965055A2 Metering demand fuel system |
| 09/03/2008 | EP1965054A2 Gas turbine fuel nozzle apparatus and method of controlling fuel nozzle apparatus |
| 09/03/2008 | EP1965052A2 Mixer for cooling and sealing air system of turbomachinery |
| 09/03/2008 | EP1965042A1 Centring and attaching stator parts |
| 09/03/2008 | EP1965040A1 De-icing System of the nose cone of an airplane jet engine using oil |
| 09/03/2008 | EP1965033A2 Blade outer air seal |
| 09/03/2008 | EP1965032A2 Blade outer air seal |
| 09/03/2008 | EP1963640A1 Rotary combustion device |
| 09/03/2008 | EP1761736A4 Heat exchanger with header tubes |
| 09/03/2008 | EP1628880A4 Aircraft ground run-up enclosure |
| 09/03/2008 | CN101255821A Method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit |
| 09/03/2008 | CN101255820A Mixer for cooling and sealing air system of turbomachinery |
| 09/03/2008 | CN101255801A High back pressure internal combustion steam turbine |
| 09/03/2008 | CN100416142C Seal for a rotating member |
| 09/03/2008 | CN100416063C Fuel injector laminated fuel strip |
| 09/03/2008 | CN100416045C Securing device and disk for the rotor blades of axial flow turbo engines |
| 09/03/2008 | CN100416042C Method and device for monitoring a cooling air system of a turbine |
| 09/03/2008 | CN100416041C Stator for a turbomachine |
| 09/03/2008 | CN100415907C Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 09/02/2008 | US7419364 Nose cone for a turbomachine |
| 09/02/2008 | US7418821 Aircraft gas turbine engines |
| 09/02/2008 | US7418813 Gas turbine engine exhaust nozzle including an infrared suppression system having a plurality of U-shaped blocking fins and method of assembling said exhaut nozzle |
| 09/02/2008 | CA2622113A1 Process for starting a gas turbine helicopter engine, fuel supply system of said engine, and engine with said system |
| 08/28/2008 | WO2008102497A1 Platform cooling structure of gas turbine rotor blade |
| 08/28/2008 | US20080206595 Substrate with protective coating alloy of cobalt, iron or nickel with chromium, aluminum, yttrium alloy |
| 08/28/2008 | US20080206044 Noise reduction assembly for aircraft turbojet |
| 08/28/2008 | US20080202877 Support apparatus and method for ceramic matrix composite turbine bucket shroud |
| 08/28/2008 | US20080202124 Transition support system for combustion transition ducts for turbine engines |
| 08/28/2008 | US20080202094 aeroengine fitted with heat exchanger means |
| 08/28/2008 | US20080202092 Mixer for cooling and sealing air system of turbomachinery |
| 08/27/2008 | EP1961937A2 Wet compression system for a gas turbine engine |
| 08/27/2008 | EP1960266A2 Isentropic compression inlet for supersonic aircraft |
| 08/27/2008 | EP1606502B1 Fuel-conditioning skid |
| 08/27/2008 | CN101249725A Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained thereby |
| 08/27/2008 | CA2621838A1 Aircraft engine equipped with means to transfer heat |
| 08/27/2008 | CA2621837A1 Aircraft engine oil removal system |
| 08/26/2008 | US7416051 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes |
| 08/26/2008 | US7415828 Fuel nozzle sheath retention ring |
| 08/26/2008 | CA2437774C Uniaxial gas turbine system |
| 08/26/2008 | CA2339276C Anti-coking fuel injector purging device |
| 08/21/2008 | WO2008098911A1 Method for operating a power plant |
| 08/21/2008 | WO2008098891A1 Power plant system and method for the operation thereof |
| 08/21/2008 | WO2008098765A1 Insulating system |