F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants

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)
11/2009
11/19/2009	US20090282804 Recuperators for gas turbine engines
11/19/2009	US20090282803 Emission reduction system for use with a heat recovery steam generation system
11/19/2009	DE102009003610A1 Trockene dreiwege-katalytische Reduktion von Gasturbinen-NOx Dry three-way catalytic reduction of gas turbine NOx
11/19/2009	DE102008024022A1 Gasturbinentriebwerk, insbesondere Flugtriebwerk Gas turbine engine, in particular aircraft engine
11/19/2009	DE102008023990A1 Zwei-Wellen-Triebwerk für eine Fluggasturbine Two-shaft engine for an aircraft gas turbine
11/19/2009	CA2724272A1 Method and apparatus for controlling fuel in a gas turbine engine
11/19/2009	CA2722162A1 Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means
11/19/2009	CA2719460A1 Propulsion unit for an aircraft and air intake structure for such a unit
11/18/2009	EP2119893A2 Recuperators for gas turbine engines
11/18/2009	EP2119892A2 Method for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine
11/18/2009	EP2119877A2 Arrangement of bearings in a dual-shaft engine for an aero gas turbine to compensate the bearingloads
11/18/2009	EP2119874A1 Continuous-flow machine, in particular a turbine or compressor
11/18/2009	EP2118471A2 Coating for acoustic treatment having a hot air icing processing function
11/18/2009	CN201347802Y Waste heat recycling utilization device for gas engine
11/18/2009	CN101581252A Method for controlling set point for extracting air from compressor to provide turbine cooling air in gas turbine
11/18/2009	CN101581237A System and method for modifying modal vibrations associated with turbine
11/18/2009	CN101581236A Cooling circuit for turbine bucket cooling
11/18/2009	CN100560958C Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm
11/17/2009	US7618825 Method for influencing and monitoring the oxide layer on metallic components of hot CO2/H20 cycle systems
11/17/2009	US7617689 Combustor dome assembly including retaining ring
11/17/2009	US7617684 Impingement cooled can combustor
11/17/2009	CA2430739C System to feed cooling air into a gas turbine rotor
11/17/2009	CA2419367C Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor
11/17/2009	CA2414992C Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
11/17/2009	CA2414034C Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
11/17/2009	CA2413422C Draining and cooling system for gas turbine bearings
11/13/2009	CA2665303A1 Starting and generating apparatus for engine
11/12/2009	WO2009136550A1 Blade structure for turbine
11/12/2009	WO2009136062A2 Acoustic treatment panel with integral connecting reinforcement
11/12/2009	WO2009135721A1 Fluid intake assembly
11/12/2009	WO2009112697A3 Method for drilling an acoustic part of an aircraft nacelle
11/12/2009	US20090280443 Burner with lance
11/12/2009	US20090280003 Method and system for monitoring particulate
11/12/2009	US20090277184 Turbomachine and a method for enhancing power efficiency in a turbomachine
11/12/2009	US20090277182 Fuel lance
11/12/2009	US20090277180 Combustor dynamic attenuation and cooling arrangement
11/12/2009	US20090277179 Swirler passage and burner for a gas turbine engine
11/12/2009	US20090277178 Burner
11/12/2009	US20090277177 Fuel nozzle for a gas turbine engine and method for fabricating the same
11/12/2009	US20090277176 Pure air blast fuel injector
11/12/2009	US20090277154 Recuperator for aircraft turbine engines
11/12/2009	US20090277153 Composite component
11/12/2009	DE19903770B4 Vergasungsbrenner für einen Gasturbinenmotor Combustor for a gas turbine engine
11/12/2009	DE102009020353A1 Proportionale Brennstoffdruckamplitudensteuerung/regelung in Gasturbinenmotoren Proportional fuel pressure amplitude control / regulation in gas turbine engines
11/12/2009	DE102009003858A1 Betrieb eines Dualgas-Turbinenbrennstoffsystems Operation of a dual gas-turbine fuel system
11/12/2009	DE102009003855A1 Dualgas-Turbinentreibstoffsystem mit Einzelverteiler Dual gas turbine fuel system with individual distributor
11/12/2009	DE102008022627A1 Abgasturbolader für eine Brennkraftmaschine und Verfahren zum Betreiben eines Abgasturboladers einer Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine and method for operating an exhaust gas turbocharger of an internal combustion engine
11/12/2009	CA2719898A1 Acoustic treatment panel with integral connecting reinforcement
11/11/2009	EP2116728A1 Fluid intake assembly
11/11/2009	EP2116714A1 Low noise aircraft
11/11/2009	EP2115274A1 Method for operating a power plant
11/11/2009	CN201344067Y Turbine battery
11/11/2009	CN101578440A Method of preparing through holes in tube body wall surfaces, and tube body structure
11/11/2009	CN101576010A Independent manifold dual gas turbine fuel system
11/11/2009	CN101576009A Operation of dual gas turbine fuel system
11/11/2009	CN101576008A Single manifold dual gas turbine fuel system
11/11/2009	CN101576007A Primary manifold dual gas turbine fuel system
11/11/2009	CN101576006A Apparatus for filtering gas turbine inlet air
11/11/2009	CN101575988A Turbomachine and a method for enhancing power efficiency in a turbomachine
11/11/2009	CN100559081C Gas turbine combustor
11/11/2009	CN100559021C Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings
11/10/2009	US7615087 Single/multiple guards(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational systems(s)—centrifuge chamber/manifold particle collector
11/10/2009	US7614846 Ceramic-based bushing for a variable-pitch vane system in a turbomachine
11/10/2009	US7614239 Turbine installation having a connectable auxiliary group
11/10/2009	US7614236 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop
11/10/2009	CA2356529C Apparatus and method to increase turbine power
11/10/2009	CA2246769C Turbogenerator/motor controller
11/05/2009	WO2009112782A3 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing
11/05/2009	WO2009112781A3 Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine
11/05/2009	WO2009102907A3 System, method and apparatus for lean combustion with plasma from an electrical arc
11/05/2009	US20090272124 Cooling channel for cooling a hot gas guiding component
11/05/2009	US20090272123 Gas Turbine Engine Systems and Related Methods Involving Thermally Isolated Retention
11/05/2009	US20090272122 Turbine shroud thermal distortion control
11/05/2009	US20090272117 Burner
11/05/2009	US20090272116 Axially staged combustion system for a gas turbine engine
11/05/2009	US20090272095 Ice shed reduction for leading edge structures
11/05/2009	DE102007052102B4 Verfahren zur Herstellung einer Schmiermittelzuführung eines Axiallagers A method for producing a lubricant feed of an axial bearing
11/03/2009	US7611093 Dual flow APU inlet and associated systems and methods
11/03/2009	US7610763 Tailorable design configuration topologies for aircraft engine mid-turbine frames
11/03/2009	US7610761 Method and device for the combustion of hydrogen in a premix burner
10/2009
10/29/2009	WO2009131793A1 Exhaust washed structure and associated composite structure and method of fabrication
10/29/2009	WO2009129787A1 Sealing arrangement
10/29/2009	WO2009112777A3 Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing
10/29/2009	WO2009085843A3 Ice protection system for a multi-segment aircraft component
10/29/2009	WO2008111098A8 Air intake for a gas turbine compressor
10/29/2009	US20090271086 Hybrid Engine Accessory Power System
10/29/2009	US20090269184 Gas Turbine Engine Systems Involving Turbine Blade Platforms with Cooling Holes
10/29/2009	US20090266545 Method and Device for Producing a Gaseous Medium Comprising Steam
10/29/2009	US20090266229 Vacuum system for membrane fuel stabilization unit
10/29/2009	US20090266080 Optimizing the angular positioning of a turbine nozzle at the outlet from a turbomachine combustion chamber
10/29/2009	US20090266079 Premix Nozzles and Gas Turbine Engine Systems Involving Such Nozzles
10/29/2009	US20090266078 Fuel flow anti-interruption
10/29/2009	US20090266048 Turbine Air-Intake Filter
10/29/2009	DE102008020932A1 Turbocharger, particularly for motor vehicle, has variable turbine geometry unit and one or multiple fastening elements for fastening variable turbine geometry unit in housing of turbocharger
10/29/2009	DE102008019892A1 Verfahren zum Reinigen eines Flugtriebwerks A method for cleaning an aircraft engine
10/29/2009	CA2713168A1 Exhaust washed structure and associated composite structure and method of fabrication
10/28/2009	EP2112353A1 Aircraft engine nacelle inlet
10/28/2009	EP2112352A2 Accessory gearbox system with compressor driven seal air supply and method of providing a seal air supply to an accessory gearbox
10/28/2009	EP2112331A2 Variable stator vane and gas turbine engine comprising such a vane
10/28/2009	EP1343956B1 Bypass duct fan noise reduction assembly

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