| 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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| 01/31/2007 | CN1297735C High temperature gas seal structure with heat insulating and cooling action |
| 01/30/2007 | US7169241 Ni-based superalloy having high oxidation resistance and gas turbine part |
| 01/30/2007 | US7168916 Welded rotor for a thermal machine, and process for producing a rotor of this type |
| 01/30/2007 | US7168913 Twin-spool turbojet with means for driving ancillary machines |
| 01/30/2007 | US7168254 Control logic for fuel controls on APUs |
| 01/30/2007 | US7168253 Monobloc flameholder arm for an afterburner device of a bypass turbojet |
| 01/30/2007 | US7168235 Highly supercharged regenerative gas turbine |
| 01/29/2007 | CA2554106A1 Mounting of a labyrinth seal support on a turbine engine rotor |
| 01/29/2007 | CA2553245A1 Pto assembly for a gas turbine engine |
| 01/25/2007 | WO2007009874A1 Gas and steam turbine installation and method for operating the same |
| 01/25/2007 | US20070021899 Method and system for operating a multi-stage combustor |
| 01/25/2007 | US20070017958 Method for coating a substrate and articles coated therewith |
| 01/25/2007 | US20070017227 Advanced humid air turbine power plant |
| 01/25/2007 | US20070017226 Generator assembly |
| 01/25/2007 | US20070017208 Turbine engine with interstage heat transfer |
| 01/25/2007 | US20070017206 Ejector pump for a fuel system for a gas turbine engine |
| 01/25/2007 | DE102005033860A1 Protective ring for gas turbine engine collector housing has cylinder of welded, prefabricated sheet metal bands, stiffening ribs as vertically protruding first sheet metal ring welded to cylinder, second ring coaxial to cylinder end |
| 01/25/2007 | DE102005033660A1 Guiding tube for receiving an oil-level gauge/dip stick on an internal combustion engine is removable for observing a wetting marker created by the oil-level |
| 01/24/2007 | EP1746523A2 Method of designing a hypersonic inlet for an aircraft and system therefor |
| 01/24/2007 | EP1746270A1 Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine |
| 01/24/2007 | EP1746257A2 Vehicle and corresponding operating method |
| 01/24/2007 | EP1746252A2 Structural strut and shroud element |
| 01/24/2007 | EP1206384B1 Supersonic external-compression diffuser and method for designing same |
| 01/24/2007 | CN1902389A 混合式发动机附件动力系统 Hybrid engine accessory power system |
| 01/24/2007 | CN1902380A Heat shield for gas turbine engine |
| 01/24/2007 | CN1902094A Ram air channel for the supply of ambient air in an aircraft |
| 01/24/2007 | CN1902093A Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding |
| 01/24/2007 | CN1900500A 退耦套筒 Decoupling sleeve |
| 01/24/2007 | CN1899661A Fuel deoxygenation for improved combustion performance |
| 01/24/2007 | CN1296611C Exhaust diffuser for axial-flow turbine |
| 01/24/2007 | CN1296173C Method for removing coating material from a cooling hole of a gas turbine engine component |
| 01/23/2007 | US7166380 Power generating system |
| 01/23/2007 | US7166372 creep resistance and high strength overcoatings comprising alloys of chromium, aluminum, yttrium and nickel, cobalt, iron or hafnium having discrete nitride particles, used on substrates such as blades and vanes for gas turbine engines |
| 01/23/2007 | US7165935 Axial compressor |
| 01/23/2007 | US7165325 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle |
| 01/23/2007 | CA2363895C Air inlet and outlet silencer structures for turbine |
| 01/23/2007 | CA2226441C Turboprop engine with an air-oil cooler |
| 01/23/2007 | CA2226424C Aircraft gas turbine engine with a liquid-air heat exchanger |
| 01/23/2007 | CA2145633C Multiple passage cooling circuit for gas turbine fuel injector nozzle |
| 01/18/2007 | US20070012046 Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure |
| 01/18/2007 | US20070012042 Low smoke and emissions fuel nozzle |
| 01/18/2007 | US20070012026 Nested core gas turbine engine |
| 01/18/2007 | CA2551600A1 System and method for trending exhaust gas temperature in a turbine engine |
| 01/17/2007 | EP1744034A2 An arrangement for sealing a steam-cooled gas turbine |
| 01/17/2007 | EP1744033A2 Acoustic liner assembly |
| 01/17/2007 | EP1744032A1 Combined gas and steam turbine installation and method of operating same |
| 01/17/2007 | EP1743092A2 Two-displacement setting variable displacement pump used as engine over-thrust protection with fuel system thermal benefit |
| 01/17/2007 | EP1656295B1 Device for stabilizing the engine inlet flow in static tests of engines |
| 01/17/2007 | EP1402152B1 Securing system for the rotor blades of axial flow turbo engines |
| 01/17/2007 | EP1301695B1 Method for operating a turbomachine and corresponding turbomachine |
| 01/17/2007 | EP0990780B1 Gas turbine equipment |
| 01/16/2007 | US7163747 Turbine component having masking layer which can very easily be removed following coating of the components |
| 01/16/2007 | US7163375 Lightened interblade platform for a turbojet blade support disc |
| 01/16/2007 | US7162876 Ejector for cooling air supply pressure optimization |
| 01/16/2007 | US7162859 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 01/16/2007 | CA2220892C Closure system for an air intake port in the combustion chamber of a ramjet |
| 01/16/2007 | CA2162079C Integral disc seal |
| 01/15/2007 | CA2551408A1 Multi-material turbine engine shaft |
| 01/13/2007 | CA2548719A1 Impact resistance acoustic treatment |
| 01/11/2007 | WO2007003587A2 Molding compound for producing a refractory lining |
| 01/11/2007 | WO2006015857A9 Compressed-air generating system |
| 01/11/2007 | US20070006596 Flashback-detecting equipment, flashback-detecting method and gas turbine |
| 01/11/2007 | US20070006591 Fuel deoxygenation for improved combustion performance |
| 01/11/2007 | US20070006569 Turbomachine with contrarotating fans |
| 01/11/2007 | US20070006565 Purification works for thermal power plant |
| 01/10/2007 | EP1741902A2 Variable jet mixer for improving the performance of a fixed displacement fuel pump |
| 01/10/2007 | EP1741900A2 Gas turbine equipment utilizing high humidity |
| 01/10/2007 | EP1740919A1 Apparatus and method of balancing a shaft of an aircraft engine |
| 01/10/2007 | EP1740806A1 Method and device for transporting a liquid |
| 01/10/2007 | CN1892000A Igniter tube and method of assembling same |
| 01/10/2007 | CN1891999A System for fixing an injection system to the dome of turbine combustion chamber and method of fixation |
| 01/10/2007 | CN1891843A Pipe for steam turbine, manufacturing process of same, and steam turbine power plant using those pipes |
| 01/09/2007 | US7162354 Apparatus and method for determining date of gas turbine washing |
| 01/09/2007 | US7160345 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 |
| 01/09/2007 | CA2422553C Valve assembly for gas turbine engine |
| 01/09/2007 | CA2333934C Fluid deflecting and straining system |
| 01/08/2007 | CA2551219A1 Systems and methods for power generation with carbon dioxide isolation |
| 01/04/2007 | WO2007000390A1 Method for increasing aerodynamic stability of a working fluid of a compressor |
| 01/04/2007 | WO2005096769A3 Highly supercharged regenerative gas turbine |
| 01/04/2007 | US20070000349 Drive arrangement |
| 01/04/2007 | US20070000229 Water treatment and pressurization system for the adiabatic cooling of comburent |
| 01/03/2007 | EP1739356A1 Moulding composition for making a refractory lining |
| 01/03/2007 | EP1425502B1 Sealing method and device for a gas turbine shaft |
| 01/03/2007 | EP1381481B1 Multi-wall core and process |
| 01/03/2007 | EP1352161A4 Main propulsion engine system integrated with secondary power unit |
| 01/03/2007 | CN1890475A Bearing device for turbocharger |
| 01/03/2007 | CN1888405A Realizing method for efficient gas turbine |
| 01/02/2007 | US7155897 Combustion temperature high speed detection device |
| 01/02/2007 | US7155896 Combustor drain valve |
| 01/02/2007 | CA2381490C Laser cladding a turbine engine vane platform |
| 12/30/2006 | CA2545149A1 Augmentor spray bar mounting |
| 12/30/2006 | CA2545113A1 Augmentor fuel conduit bushing |
| 12/28/2006 | WO2006136680A1 System for defrosting the leading edge sheath of an air inlet hood for a tirboengine |
| 12/28/2006 | US20060288707 Support system for transition ducts |
| 12/28/2006 | US20060288706 Method for operating a reduced center burner in multi-burner combustor |
| 12/28/2006 | US20060288705 Modified fuel burning gas turbine and method of operating the same |
| 12/28/2006 | US20060288703 System for detecting and compensating for aerodynamic instabilities in turbo-jet engines |
| 12/28/2006 | DE102005028296A1 Exhaust gas turbocharger for internal combustion engine has washer nozzle which is arranged on a line or straight line coinciding with rotational axis of turbine rotors |
| 12/28/2006 | DE102005027890A1 Exhaust gas turbocharger for internal combustion engine has inlet casing and line which is integrated into inlet casing for cooling air whereby line guides cooling air on rotor disk of turbine rotors |
| 12/28/2006 | DE102004050644B4 System zur Verdichtung von Gasen System for compressing gases |