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)
12/2009
12/10/2009DE102008026941A1 Device for connecting honeycomb seal with seal carrier for gas turbine, has lifting plunger with contour that is adapted to honeycomb seal, where honeycomb seal and seal carrier are compressible with crimping force using plunger
12/10/2009DE10135566B4 Verfahren und System zur aktiven Minderung der Schallabstrahlung von Triebwerken Method and system for active reduction of sound radiation of engines
12/09/2009EP2131179A2 An apparatus and method for evaluating a hydrocarbon to determine the propensity for coke formation
12/09/2009EP2130933A1 Coating material, method for production thereof, coating method, rotor blade equipped with shroud
12/09/2009EP2129893A2 System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft
12/09/2009EP2129580A1 Lockable guiding system for a mobile part of a nacelle
12/09/2009CN101600854A Seal for a turbine engine
12/09/2009CN100567082C Method for designing intake oblique cut inlet
12/08/2009CA2445756C Turbine or compressor device and method for assembling the device
12/08/2009CA2423700C Device for producing a plasma, ionisation method, use of said method and production processes using said device
12/03/2009WO2009144975A1 Brazing repair material and brazing repair method using the brazing repair material
12/03/2009WO2009068807A3 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method
12/03/2009WO2009036970A3 Hydraulic drive, hydraulic supply device, airplane with a hydraulic supply device and method for configuring a hydraulic supply device
12/03/2009US20090297359 High Modulus Metallic Component For High Vibratory Operation
12/03/2009US20090297350 Hoop snap spacer
12/03/2009US20090293498 Pivoting liner hanger
12/03/2009US20090293497 Gas turbine engine assembly
12/03/2009US20090293496 Gas turbine engines generating electricity by cooling cooling air
12/03/2009US20090293495 Turbine airfoil with metered cooling cavity
12/03/2009US20090293494 Hybrid drive for an aircraft
12/03/2009US20090293493 Advanced humid air turbine power plant
12/03/2009US20090293492 Combustion apparatus
12/03/2009US20090293491 Gas Turbine For A Thermal Power Plant, And Method For Operating Such A Gas Turbine
12/03/2009US20090293490 Combustor wall with improved cooling
12/03/2009US20090293486 Combustors with igniters having protrusions
12/03/2009US20090293485 Diffusers, diffusion systems, and methods for controlling airflow through diffusion systems
12/03/2009US20090293484 Gas turbine combustor and method for supplying fuel to the same
12/03/2009US20090293483 Vibration damper
12/03/2009US20090293482 Fuse for flame holding abatement in premixer of combustion chamber of gas turbine and associated method
12/03/2009US20090293481 Method and Device for Damping Thermoacoustic Oscillations, in Particular in a Gas Turbine
12/03/2009US20090293446 Method for low NOx combustion with low pressure drop
12/03/2009DE102009025813A1 Geräuscharmer Ejektor für eine Turbomaschine Quiet ejector for a turbomachine
12/03/2009DE102009022613A1 Abgasturbolader Exhaust gas turbocharger
12/03/2009DE102009003856A1 Primärverteiler-Dualgas-Turbinenbrennstoffsystem Primary manifold dual gas turbine fuel system
12/03/2009DE102008025058A1 Axial bearing seal for exhaust-gas turbocharger, has sealing gap formed between seal ring and housing such that oil pressure existing in gap during operation of turbocharger is larger than air pressure in axial bearing
12/03/2009DE102008023052A1 Combustion chamber wall for combustion chamber, has inner wall, outer wall and cooling channel located between inner wall and outer wall, where bridges are arranged and formed between inner wall and outer wall
12/03/2009DE102008022188A1 Verfahren zum Betreiben einer Dampfturbine A method of operating a steam turbine
12/03/2009DE102008017962A1 Combustion air feeding device for aircraft i.e. helicopter, engine, has air inlet pipelines extended to engines from outer surface, where air feeding of engines is switched to inlet pipelines by control device when air inlets are blocked
12/02/2009EP2128404A2 Gas turbine drive system for auxiliaries with lock-up clutch
12/02/2009EP2128403A2 An electrical generator arrangement for a gas turbine
12/02/2009EP2128402A2 Gas turbine engine nacelle assembly
12/02/2009EP2128389A2 A gas turbine engine arrangement
12/02/2009EP2128284A1 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE VANE USING THE SAME
12/02/2009EP2128023A1 Bleed air cooler assembly for a gas turbine engine, corresponding kit and installation method
12/02/2009EP2126898A1 Acoustic septum cap honeycomb
12/02/2009EP2126316A2 Gas turbine engine with fuel booster
12/02/2009EP2126290A1 Cleaning device
12/02/2009EP2126004A1 Processing biomass
12/02/2009EP2125273A1 Boring machine for turbine casings
12/02/2009CN201354680Y Dual-fuel energy-saving turbojet engine
12/02/2009CN101592084A Low noise ejector for turbomachine
12/02/2009CN101592082A Distributed gas turbine power generation system of heavy oil combustion and application of heavy oil combustion thereof
12/02/2009CN101592081A Gas turbine generating engine
12/02/2009CN101592071A Axial bearing seal for exhaust-gas turbocharger
12/02/2009CN100565012C Liquid fuel injection with purge air and the method
12/02/2009CN100564834C Counterflow film cooled wall
12/02/2009CN100564833C Ventilating air intake arrangement
12/02/2009CN100564832C Gas and steam turbine installation and method for operating the same
12/02/2009CN100564831C Gas turbine engine assembly and methods of assembling same
12/02/2009CN100563908C Method for local application of diffusion aluminide coating
12/02/2009CA2667122A1 Vane for air inlet of a turbine
12/01/2009US7625126 Bifurcated oil scavenging bearing compartment within a gas turbine engine
12/01/2009CA2356305C Forming of an aluminide coating containing a reactive element, over a metallic substrate
11/2009
11/26/2009WO2009141368A1 Compressor cleaning
11/26/2009WO2009122066A3 Air intake lip for turbojet nacelle
11/26/2009US20090289456 Gas turbine engine apparatus
11/26/2009US20090289227 Production of Fuel Materials Utilizing Waste Carbon Dioxide and Hydrogen from Renewable Resources
11/26/2009US20090288422 Component arrangement, combustion chamber arrangement and gas turbine
11/26/2009US20090288421 Turbine drive system with lock-up clutch and method
11/26/2009US20090288420 Method for operating a gas turbine
11/26/2009US20090288384 System for reducing oil consumption in gas turbine engines
11/26/2009DE102009025803A1 System und Verfahren zur Kühlung erhitzter Komponenten in einer Turbine System and method for cooling heated components in a turbine
11/26/2009DE102008024146A1 Kombinierter Wirbelgleichrichter Combined vortex reducer
11/25/2009EP2124123A2 Pressurizing and pressure regulating valve and fuel supply system employing the same
11/25/2009EP2123884A2 Dual clutch arrangement
11/25/2009EP2123883A2 Gearbox assembly
11/25/2009EP2123864A1 Compressor cleaning
11/25/2009EP2122129A1 Power plant system and method for the operation thereof
11/25/2009CN101586879A Solar thermal utilization system combined with gas-steam combined cycle
11/25/2009CN101586496A Systems and methods for cooling heated components in a turbine
11/24/2009US7622411 Thermal barrier coating material
11/24/2009US7621717 Suction filter, turbo compressor, and method of packaging the compressor
11/24/2009US7621133 Methods and apparatus for starting up combined cycle power systems
11/24/2009US7621117 Apparatus and method for controlling engine windmilling
11/24/2009CA2484402C Deflector embedded impingement baffle
11/24/2009CA2444862C Turbine blade having a cooling air deflector
11/24/2009CA2387462C Centripetal flow air bleed device
11/19/2009WO2009140100A1 Method and apparatus for controlling fuel in a gas turbine engine
11/19/2009WO2009140019A1 Shape-changing structure with superelastic foam material
11/19/2009WO2009139801A2 Offset ambient level fuel feed system
11/19/2009WO2009139374A1 Gas turbine blade and gas turbine equipped with the same
11/19/2009WO2009138581A2 Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means
11/19/2009WO2009138580A1 Propulsion unit for an aircraft and air intake structure for such a unit
11/19/2009US20090284013 Dry 3-way catalytic reduction of gas turbine NOx
11/19/2009US20090282837 Gas turbine unit and its cooling method
11/19/2009US20090282836 Configurations And Methods For LNG Fueled Power Plants
11/19/2009US20090282834 Combined Vortex reducer
11/19/2009US20090282831 Method for reducing emissions from a combustor
11/19/2009US20090282830 Combustor with reduced carbon monoxide emissions
11/19/2009US20090282805 Systems involving fiber optic igniters