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