| 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) |
|---|
| 09/15/2011 | US20110219781 Gas turbine engine with tie shaft for axial high pressure compressor rotor |
| 09/15/2011 | US20110219779 Low emission combustion systems and methods for gas turbine engines |
| 09/15/2011 | US20110219776 Aerodynamic flame stabilizer |
| 09/15/2011 | US20110219774 Circumferentially varied quench jet arrangement for gas turbine combustors |
| 09/15/2011 | US20110219773 Systems and methods for producing hydrogen from cellulosic and/or grain feedstocks for use as a vehicle fuel, use in the production of anhydrous ammonia, and to generate electricity |
| 09/14/2011 | EP2365199A2 Aerodynamically shaped support and/or cladding element in the bypass of a gas turbine engine |
| 09/14/2011 | EP2365198A2 Preferential cooling of gas turbine nozzles |
| 09/14/2011 | EP2365197A1 Accelerated cooling of a gas turbine |
| 09/14/2011 | EP2364796A2 Casting mold |
| 09/14/2011 | CN102187062A Ventilation of a high-pressure turbine in a turbomachine |
| 09/14/2011 | CN102187061A 燃气轮机 Gas turbine |
| 09/14/2011 | CN102183040A Combustor assembly for a turbine engine that mixes combustion products with purge air |
| 09/14/2011 | CN102182560A Tunable transition piece aft frame |
| 09/14/2011 | CN102182559A Anti-icing passage system with functions of precooling and backheating |
| 09/14/2011 | CN101163869B Mechanism and method for removing steam remaining in steam cooling piping of gas turbine |
| 09/13/2011 | US8019522 Method and system for providing cooling and power |
| 09/13/2011 | US8015828 Power take-off system and gas turbine engine assembly including same |
| 09/13/2011 | US8015823 Endothermic cracking aircraft fuel system |
| 09/13/2011 | US8015814 Turbine engine having folded annular jet combustor |
| 09/13/2011 | US8015813 Fuel injector for injecting fuel into a turbomachine combustion chamber |
| 09/13/2011 | US8015793 Fuel heating via exhaust gas extraction |
| 09/13/2011 | US8015789 Anti-icing apparatus and method for aero-engine nose cone |
| 09/13/2011 | US8015788 Heat transfer system for turbine engine using heat pipes |
| 09/13/2011 | CA2509934C An improved mounting system for installing a starter-generator to an accessory housing on a gas turbine engine |
| 09/13/2011 | CA2475404C Exchanger on turbine ventilation system |
| 09/13/2011 | CA2475083C Cooling circuits for gas turbine blades |
| 09/13/2011 | CA2475081C Device to control the play in a gas turbine |
| 09/13/2011 | CA2472301C Pin and nut attachment device |
| 09/13/2011 | CA2442509C Method and system for detecting precursors to compressor stall and surge |
| 09/09/2011 | WO2011108440A1 Rotor blade for gas turbine, method for manufacturing same, and gas turbine using rotor blade |
| 09/09/2011 | WO2011108216A1 Gas turbine engine |
| 09/09/2011 | WO2011108164A1 Rotor blade for gas turbine, method for manufacturing same, and gas turbine using rotor blade |
| 09/09/2011 | WO2011107733A2 Seamless acoustic liner |
| 09/09/2011 | CA2791633A1 Seamless acoustic liner |
| 09/09/2011 | CA2791191A1 Gas turbine engine |
| 09/08/2011 | US20110217159 Preferential cooling of gas turbine nozzles |
| 09/08/2011 | US20110217158 Cooled turbine rim seal |
| 09/08/2011 | US20110217155 Cooling gas turbine components with seal slot channels |
| 09/08/2011 | US20110214747 Nacelle with an adaptable outlet section |
| 09/08/2011 | US20110214433 Strain tolerant bound structure for a gas turbine engine |
| 09/08/2011 | US20110214431 Turbine guide vane support for a gas turbine and method for operating a gas turbine |
| 09/08/2011 | US20110214430 Accelerated cooling of a gas turbine |
| 09/08/2011 | DE102011003171A1 Lagergehäuse einer Ladeeinrichtung Bearing housing of a charging device |
| 09/08/2011 | DE102010025575A1 Cover for bearing housing of exhaust gas turbocharger of motor vehicle, has cylindrical fixing region for radial fixing of piston ring and disk-like covering region to cover inner region of bearing housing |
| 09/08/2011 | DE102010010712A1 Holder for mounting attaching parts at housing of motor, particularly jet engine, by fastening elements, has plastic deformable intermediate area between end areas, where plastic deformable intermediate area is formed from outward bendings |
| 09/08/2011 | DE102010010595A1 Verfahren zur Reparatur von Dichtsegmenten in der Rotor-/Statordichtung einer Gasturbine A process for the repair of sealing segments in the rotor / stator seal of a gas turbine |
| 09/08/2011 | DE102010010130A1 Aircraft gas turbine drive has core plant and two counter-rotating pusher propellers, where bleed air is removed from low-pressure compressor and is introduced in inner chamber of propeller hubs |
| 09/08/2011 | DE102010009879A1 Gas turbine intermediate shaft bearing arrangement, has roller bearing with inner and outer rings that are arranged at respective inner and outer shafts, where running surface of bearing is arranged in plane perpendicular to rotational axis |
| 09/08/2011 | DE102010009878A1 Fluid flow interruption device for fuel supply system for gas turbine, particularly aircraft gas turbine, comprises fluid passage which is formed in housing, where moving interruption element is locked in fluid passage in housing |
| 09/08/2011 | CA2728958A1 Cooled turbine rim seal |
| 09/07/2011 | EP2363221A2 Method and apparatus for production of a cast component |
| 09/07/2011 | EP2363220A2 Method and apparatus for production of a cast component |
| 09/07/2011 | EP1872002B1 Energy recovery system |
| 09/07/2011 | CN102177326A Methods and systems for controlling the products of combustion |
| 09/07/2011 | CN102177311A Sealing between a combustion chamber and a turbine distributor in a turbine engine |
| 09/07/2011 | CN102175043A Gas turbine engine combustor can with trapped vortex cavity |
| 09/07/2011 | CN101725410B Water washing device for gas turbine |
| 09/07/2011 | CN101344037B Method and apparatus for actuating fuel trim valves in a gas turbine |
| 09/07/2011 | CN101025117B Shrouded turbofan bleed duct |
| 09/06/2011 | US8012273 Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 09/06/2011 | US8011187 Fuel injection method and apparatus for a combustor |
| 09/06/2011 | CA2485322C Soundproofing panels with beads and process for producing the said panels |
| 09/04/2011 | CA2732899A1 Pulse detonation system |
| 09/01/2011 | WO2011105132A1 Aircraft gas turbine |
| 09/01/2011 | WO2011104477A1 Turbomachine comprising a vertical shaft |
| 09/01/2011 | US20110211940 System and method for inspection of stator vanes |
| 09/01/2011 | US20110209481 Turbine Combustor End Cover |
| 09/01/2011 | DE102011004856A1 Gleitlager zur Verwendung in Turboladern von Verbrennungsmotoren Plain bearings for use in turbochargers of internal combustion engines |
| 09/01/2011 | DE102011000772A1 Turbinenbrennkammerendabdeckung Turbinenbrennkammerendabdeckung |
| 09/01/2011 | DE102011000227A1 System und Verfahren zur Erfassung und Kontrolle eines Flammrückschlags und Flammenhaltens in einer Brennkammer System and method for detection and control of a flashback and flame holding in a combustion chamber |
| 09/01/2011 | DE102010009477A1 Fluggasturbinenantrieb Aircraft gas turbine engine |
| 09/01/2011 | CA2790002A1 Turbomachine comprising a vertical shaft |
| 09/01/2011 | CA2784315A1 Aircraft gas turbine |
| 08/31/2011 | EP2362081A1 Bearing compartment pressurization and shaft ventilation system |
| 08/31/2011 | EP2362072A2 Turbine starter lubricant cooling |
| 08/31/2011 | EP2361350A1 Magnetic advanced generation jet electric turbine |
| 08/31/2011 | EP2361346A1 Power plant comprising a turbine unit and a generator |
| 08/31/2011 | EP2142779B1 Acoustic panel having a variable acoustic characteristic |
| 08/31/2011 | CN201953484U 一种避免篦齿封严结构滑油泄漏的装置 A labyrinth seal structure to avoid oil leakage device |
| 08/31/2011 | CN201953483U 一种断流活门 One kind of shut-off valves |
| 08/31/2011 | CN201953482U 燃气轮机入口空气处理系统 Gas turbine inlet air handling systems |
| 08/31/2011 | CN201953481U 涡旋空气内能利用装置 The air inside the vortex energy utilization device |
| 08/31/2011 | CN1993535B Wheel chamber casing and gas turbine |
| 08/31/2011 | CN1925902B A fluid separation device |
| 08/31/2011 | CN102171101A Air intake structure for a turbine engine nacelle |
| 08/31/2011 | CN102168614A Methods and systems relating to fuel delivery in combustion turbine engines |
| 08/31/2011 | CN101389841B Integration of a starter/generator module in a gas turbine transmission housing |
| 08/31/2011 | CN101178040B Method for manufacturing full-functional high-energy induction and catalyst combined type complete combustion device |
| 08/30/2011 | US8006380 Method of replacing damaged aerofoil |
| 08/30/2011 | CA2485329C Connection device between a distributor and a power enclosure for cooling fluid injectors in a turbine engine |
| 08/30/2011 | CA2485242C Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 08/30/2011 | CA2444982C Crankcase, compressor, turbine and combustion turbine engine comprising said crankcase |
| 08/30/2011 | CA2442952C Case forming in particular a turbine engine rotor, compressor and turbine engine comprising a like case |
| 08/25/2011 | WO2011102014A1 Structure for gas turbine casing |
| 08/25/2011 | US20110206502 Turbine shroud support thermal shield |
| 08/25/2011 | US20110206501 Combined featherseal slot and lightening pocket |
| 08/25/2011 | US20110203294 Fuel injection system for a combustion chamber of a turbomachine |
| 08/25/2011 | US20110203291 Methods and systems relating to fuel delivery in combustion turbine engines |
| 08/25/2011 | US20110203284 Circumferential biasing and profiling of fuel injection in distribution ring |
| 08/25/2011 | US20110203251 Fireseal |