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) |
---|
10/06/2011 | US20110239654 Angled seal cooling system |
10/06/2011 | US20110239653 Annular ring-manifold quaternary fuel distributor |
10/06/2011 | US20110239652 Segmented annular ring-manifold quaternary fuel distributor |
10/06/2011 | US20110239621 Fiber optic microphones for active combustion control |
10/06/2011 | US20110239619 Combustor and gas turbine |
10/06/2011 | DE102010015113A1 Turbocharger housing comprises two housing halves, in which assembled state sectionally form bearing housing, turbine housing, and compressor housing |
10/06/2011 | DE102010013706A1 Method for manufacturing turbocharger housing, involves providing measurement section at spiral housing, where turbocharger housing with its two housing halves is formed as cast parts |
10/06/2011 | DE102010013699A1 Turbo charger for internal combustion engine, has turbocharger housing divided into housing halves that are directed or aligned to each other by fitting groove in one of halves and mating hole in another housing halve |
10/06/2011 | DE102010013697A1 Turbocharger, has turbocharger housing divided into two housing halves, and bearing block device and housing half aligned to each other via fitting groove in housing half and assigned locating hole in other housing half |
10/06/2011 | CA2794770A1 Unitized engine nacelle structure |
10/05/2011 | EP2372697A1 Method of retrofitting an acoustic treatment into a fluid handling module |
10/05/2011 | EP2372129A2 Mounting arrangement for gas turbine engine accessories and gearbox therefor |
10/05/2011 | EP2372107A2 Flow discharge device |
10/05/2011 | EP2372106A1 Turbogenerator |
10/05/2011 | EP2371470A2 Method and apparatus for production of a cast component |
10/05/2011 | EP2370674A1 Nacelle and method of assembling the same |
10/05/2011 | CN202001114U Admission air silencer of auxiliary power unit utilizing locally reacting acoustic liner principles |
10/05/2011 | CN1991143B A cooling apparatus for a gas turbine engine igniter lead |
10/05/2011 | CN1971012B Combustion turbine fuel recirculation system and nitrogen purge system |
10/05/2011 | CN1782345B Spark igniter of gas turbine engine |
10/05/2011 | CN102207032A Fluid cooled reformer and method for cooling a reformer |
10/05/2011 | CN101709672B High-efficiency high-temperature internal and external mixed gas turbine |
10/05/2011 | CN101693163B Drying device of absorption gas turbine |
10/05/2011 | CN101438039B Modular fuel supply device for a gas turbine |
10/05/2011 | CN101105150B An engine core stand arrangement and method of removal and transportation of an engine core |
10/05/2011 | CN101042072B Temperature and/or pressure sensor assembly |
10/04/2011 | US8028530 Device for attaching a combustion chamber |
10/04/2011 | US8028513 Variable bypass turbine fan |
10/04/2011 | CA2564242C Turbofan engine |
09/29/2011 | WO2011118474A1 Seal structure for turbine rotor |
09/29/2011 | WO2011118372A1 Lean-fuel intake gas turbine |
09/29/2011 | WO2011118210A1 Fuel supply device of gas turbine engine |
09/29/2011 | WO2011118131A1 Double-jet film cooling structure |
09/29/2011 | WO2011080433A3 Guiding of a spark plug into a turbine engine combustion chamber |
09/29/2011 | WO2011056907A3 Variable performance valve |
09/29/2011 | WO2011026636A3 Method for the operation of a micro gas turbine arrangement, and micro gas turbine arrangement for converting biomass into energy |
09/29/2011 | US20110236217 Gas turbine engine nose cone |
09/29/2011 | US20110236206 Gas turbine bucket with serpentine cooled platform and related method |
09/29/2011 | US20110236190 Turbine rotor wheel |
09/29/2011 | US20110236188 Blade outer seal for a gas turbine engine |
09/29/2011 | US20110236183 Bimetallic spline seal |
09/29/2011 | US20110233876 Turbine sealing system |
09/29/2011 | US20110232299 Impingement structures for cooling systems |
09/29/2011 | US20110232298 System and method for cooling gas turbine components |
09/29/2011 | US20110232297 Method and system for testing an overspeed protection system of a powerplant machine |
09/29/2011 | US20110232296 Optical fuel nozzle flashback detector |
09/29/2011 | US20110232294 Methods and systems for mitigating distortion of gas turbine shaft |
09/29/2011 | US20110232293 Fuel heat management system |
09/29/2011 | US20110232290 Press-fitting corrosion resistant liners in nozzles and casings |
09/29/2011 | DE10116452B4 Gasturbine und Reparaturverfahren für diese Gas turbine and repair procedures for these |
09/29/2011 | CA2794201A1 Sealing device for jet engine oil chamber |
09/29/2011 | CA2793966A1 Seal mechanism for use with turbine rotor |
09/28/2011 | EP2369156A2 System and method for cooling gas turbine components |
09/28/2011 | EP2369155A2 A gas turbine engine nose cone |
09/28/2011 | EP2369145A1 Power generation system and method |
09/28/2011 | EP2369137A1 One-stage stator vane cooling structure and gas turbine |
09/28/2011 | EP2368031A1 Gas turbine with external combustion, applying a rotating regenerating heat exchanger |
09/28/2011 | EP2368030A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
09/28/2011 | CN201991616U 超燃双工质汽轮机 Supersonic combustion turbine duplex quality |
09/28/2011 | CN102203475A Fluid valve drive mechanism |
09/28/2011 | CN102203397A Gas turbine control device and gas turbine starting method |
09/28/2011 | CN102200057A System and method for cooling gas turbine component |
09/28/2011 | CN102200056A Impingement structures for cooling system |
09/28/2011 | CN102200055A A gas turbine engine nose cone |
09/28/2011 | CN102200054A System and method for exhaust diffuser |
09/28/2011 | CN102200053A Method and apparatus for radial exhaust gas turbine |
09/28/2011 | CN102200030A Turbine rotor wheel |
09/28/2011 | CN101037946B Fastening arrangement of a pipe on a circumferential surface |
09/27/2011 | US8024934 System and method for attenuating combustion oscillations in a gas turbine engine |
09/27/2011 | CA2456700C Device for cooling turbine disks |
09/26/2011 | CA2733072A1 Oil supply system with main pump deaeration |
09/22/2011 | WO2011115149A1 Engine generator device |
09/22/2011 | WO2011056928A3 Micro-turbine combustor |
09/22/2011 | US20110229337 Hybrid ceramic matrix composite turbine blades for improved processibility and performance and process for producing hybrid turbine blades |
09/22/2011 | US20110229307 Optical Monitoring System for a Turbine Engine |
09/22/2011 | US20110225979 Turbo engine |
09/22/2011 | US20110225978 Turbomachine drive arrangement |
09/22/2011 | US20110225977 Turbine system |
09/22/2011 | US20110225974 Multiple Zone Pilot For Low Emission Combustion System |
09/22/2011 | US20110225973 Combustor with Pre-Mixing Primary Fuel-Nozzle Assembly |
09/22/2011 | US20110225948 Apparatus for high-frequency electromagnetic initiation of a combustion process |
09/22/2011 | US20110225947 System and methods for altering air flow in a combustor |
09/21/2011 | EP2366060A1 Fan for a turbine engine including a balancing system with blind holes for housing bodies, and related turbine engine |
09/21/2011 | CN102192508A Axially staged premixed combustion chamber |
09/21/2011 | CN102192012A Load monitoring for electromechanical systems |
09/20/2011 | US8020384 Fuel injector nozzle with macrolaminate fuel swirler |
09/20/2011 | US8020366 Turbine engine combustor |
09/20/2011 | US8020269 Methods and apparatus for fabricating a turbine nozzle assembly |
09/20/2011 | CA2475148C Lateral deflection interblade platform for a turbojet blade support |
09/20/2011 | CA2470089C Guiding device for a blade with variable blade angle |
09/20/2011 | CA2457256C Production of turbines for turbine engines having blades with different adjusted resonance frequencies and process for adjusting the resonance frequency of a turbine blade |
09/20/2011 | CA2456696C Turbine blades cooled by reduced escapement of cooling air |
09/15/2011 | WO2011112108A2 Bullgear gas turbine with intercooler and reheat |
09/15/2011 | WO2011111433A1 Shaft seal device and rotary machine with shaft seal device |
09/15/2011 | WO2011110554A1 Power generation system and method |
09/15/2011 | US20110223005 Airfoil Having Built-Up Surface with Embedded Cooling Passage |
09/15/2011 | US20110223004 Apparatus for cooling a platform of a turbine component |
09/15/2011 | US20110220218 Turbojet engine nacelle |
09/15/2011 | US20110219783 Turbojet engine nacelle with translatable upstream cowl |
09/15/2011 | US20110219782 Aerodynamically shaped supporting and/or fairing element in the bypass duct of a gas-turbine engine |