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)
12/2010
12/29/2010EP2267289A1 Compressor starting torque converter
12/29/2010EP2267288A2 Lightweight start system for a gas turbine engine
12/29/2010EP2265801A1 A gas turbine housing component
12/29/2010EP1918549B1 Seal structure of gas turbine combustor
12/29/2010EP1394711B1 Filter maintenance and monitoring method
12/29/2010CN201687579U Docking device for gas turbine rotor and compressor rotor
12/29/2010CN201687529U Brush type sealing device
12/29/2010CN101932811A System and method for the reduction of harmful substances in engine exhaust gases
12/29/2010CN101932794A Method of regenerating gas turbine blade and gas turbine blade regenerating apparatus
12/29/2010CN101929406A Vortex cold vacuum aircraft engine
12/29/2010CN101929390A System and method for heating turbine fuel in simple recycle unit
12/29/2010CN101929389A Apparatus and method for cooling a turbine using heat pipes
12/29/2010CN101929388A System for cooling gas turbine inlet air
12/29/2010CN101929387A Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith
12/29/2010CN101025115B Aircraft auxiliary gas turbine engine and method for operating
12/29/2010CA2708459A1 Gas turbine with wired shaft forming part of a generator/motor assembly
12/29/2010CA2708458A1 Gas turbine with magnetic shaft forming part of a generator/motor assembly
12/28/2010US7857585 Gas turbine engine comprising a casing surrounding a rotary assembly and a manifold secured to the casing via a securing arrangement
12/28/2010US7857094 Combustion chamber for a gas turbine engine
12/28/2010US7857026 Method for repairing loose molded-in bushings
12/26/2010CA2707267A1 Spray system, power augmentation system for engine containing spray system and method of humidifying air
12/25/2010CA2707966A1 Turbine rotor blade
12/23/2010WO2010147003A1 Solar thermal gas turbine power plant
12/23/2010WO2010146999A1 FERRITIC Cr-STEEL FOR HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME, AND HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME
12/23/2010WO2010146805A1 Shaft seal and rotary machine with same
12/23/2010WO2010146797A1 Shaft seal device
12/23/2010WO2010109152A3 Aircraft nacelle comprising a reinforced outer wall
12/23/2010US20100320701 Compliant element
12/23/2010US20100319359 System and method for heating turbine fuel in a simple cycle plant
12/23/2010US20100319358 Nosecone ice protection system for a gas turbine engine
12/23/2010US20100319357 Device and a method for starting a turbine engine fitted to a helicopter, making use of an electrical energy source that includes discharge booster members
12/23/2010US20100319355 Heating a reaction chamber
12/23/2010US20100319353 Multiple Fuel Circuits for Syngas/NG DLN in a Premixed Nozzle
12/23/2010US20100319351 Gas turbine combustor
12/23/2010US20100319350 Flashback Resistant Fuel Injection System
12/23/2010US20100319349 Attenuation of Combustion Dynamics Using a Herschel-Quincke Filter
12/23/2010DE19882242B4 Gas- und Dampfturbinen-Kraftwerk Gas and steam turbine power plant
12/23/2010DE102010017317A1 System zur Kühlung von Gasturbineneinlassluft A system for cooling of gas turbine inlet air
12/23/2010DE102009024679A1 Compressor wheel for radial compressor of e.g. exhaust gas-turbocharger for internal combustion engine, has centrifugal flow-blocking units arranged to stop radially outward flow of liquid cooling fluid applied on side of wheel hub
12/22/2010EP2264340A2 Tamdem seal arrangement with reverse flow secondary seal
12/22/2010EP2264297A1 Device and method for starting of a helicopter turbine, using an electrical energy source comprising supplementary discharging means
12/22/2010EP2264280A1 Turbine balancing
12/22/2010EP2264208A1 Coating structure and surface treating method
12/22/2010EP2263809A2 System for washing an aero gas turbine engine
12/22/2010EP2262994A2 Method and system for enhancing start of a turbine engine, and ignition module
12/22/2010EP2262993A2 Adsorption-enhanced compressed air energy storage
12/22/2010CN1952368B Gas turbine engine assembly and methods of assembling same
12/22/2010CN1924320B Methods and apparatus for operating gas turbine engines
12/22/2010CN101925515A Locking system for air intake structure for turbojet engine nacelle
12/22/2010CN101922591A Shape memory polymer pipeline and use of shape memory polymer pipeline as aircraft engine intake
12/22/2010CN101922356A System relating to turbine engine control and operation
12/22/2010CN101922355A System and method for thermal control in cap of gas turbine combustor
12/22/2010CN101922354A Turbine combustor having a liner
12/22/2010CN101922353A Feeding film cooling hole from seal slot
12/22/2010CN101922352A Thermal circulation system cooled by liquefied natural gas and flow
12/21/2010CA2486841C Method for repairing coated components using nial bond coats
12/21/2010CA2385821C Method for isothermal brazing of single crystal components
12/17/2010CA2705980A1 Prechorded turbine nozzle
12/16/2010WO2010142820A1 Cooling system for thermal power stations
12/16/2010WO2010142584A1 Turbomachine
12/16/2010WO2010142573A2 Method and device for the recirculation of exhaust gases in a gas turbine
12/16/2010US20100318274 Combustor Flashback/Flame Holding Detection Via Temperature Sensing
12/16/2010US20100314877 Gas turbine bleed energy recovery via counter rotating generator
12/16/2010US20100314501 Locking system for air intake structure for turbojet engine nacelle
12/16/2010US20100313571 Gas turbine
12/16/2010US20100313570 Gas turbine combustor
12/16/2010US20100313568 Resonator assembly for mitigating dynamics in gas turbines
12/16/2010US20100313420 Through-hole manufacturing method for cylindrical body wall and cylindrical body structure
12/16/2010DE212009000051U1 Verdichterreinigung Compressor cleaning
12/16/2010DE10353039B4 Dual-Brennstoff-Kombi-Turbinenkraftwerk und Betriebsverfahren dafür Dual-fuel-fired combined cycle turbine power plant and operating method therefor
12/16/2010DE10342777B4 Betriebssteuer- bzw. -regelvorrichtung und Betriebssteuer- bzw. -regelverfahren für ein kombiniertes Einwellen-Kraftwerk Operation control regulating system and operation control -regelverfahren for a combined single-shaft power plant
12/16/2010DE102010017362A1 Mechanische Verbindung für eine Gasturbinenmaschine Mechanical seal for a gas turbine engine
12/16/2010DE102009026881A1 Antrieb für eine Turbine nebst Antriebsverfahren Drive a turbine together with driving method
12/16/2010DE102009024677A1 Charger, particularly exhaust gas turbocharger, has rotor, which is supported by bearing device, where bearing device has stator side receptacle with edge facing rotor, in which complementary rotor engages forming bearing gap
12/15/2010EP2261567A1 Gas turbine and method of forming insertion hole for combustor of gas turbine
12/15/2010EP2261485A2 Method of controlling gas turbine operation
12/15/2010EP2261484A2 Fuel delivery system for a turbine engine
12/15/2010EP2261468A1 Gas turbine
12/15/2010EP2261464A1 Turbomachine
12/15/2010EP2261461A1 Cover for cooling passage, method of manufacturing the cover, and gas turbine
12/15/2010EP2260197A1 Contra-rotating propeller system with device for feathering propeller blades
12/15/2010EP2260184A1 Centrifugal oil separator having variable channel section
12/15/2010EP2260182A1 A gas turbine component and a method for producing a gas turbine component
12/15/2010EP2066890B1 Modulating flow through gas turbine engine cooling system
12/15/2010EP1682758B1 Hybrid engine accessory power system
12/15/2010EP1432888B1 Spring mounted recuperator for a microturbine system
12/15/2010CN201672538U Whirlcone, pneumatic nebulization spray nozzle and gas turbine
12/15/2010CN101915165A A method and apparatus for gas turbine engine temperature management
12/15/2010CN101915164A Air inlet particle separating device for gas turbine
12/15/2010CN101915128A System comprising multiple spool generators
12/15/2010CA2706206A1 Mechanical joint for a gas turbine engine
12/14/2010US7849668 Rotor brake and windmilling lubrication system for geared turbofan engine
12/14/2010CA2506113C Method and apparatus for cleaning a turbofan gas turbine engine
12/14/2010CA2441514C Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine
12/09/2010WO2010140565A1 Solar gas turbine and solar gas turbine power generating device
12/09/2010WO2010140479A1 Method for manufacturing combustor constituent member, combustor constituent member, gas turbine combustor, and gas turbine
12/09/2010WO2010139798A1 Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device
12/09/2010WO2010139065A1 Hydrodynamic bore finger seal with sealing pads
12/09/2010US20100308135 Staging fuel nozzle
12/09/2010US20100307166 Combustor-turbine seal interface for gas turbine engine