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)
02/2013
02/28/2013US20130048098 Supersonic aircraft jet engine installation
02/28/2013US20130047629 Integrated turbomachine plant
02/28/2013US20130047626 Gas turbine engine generator switchable drive
02/28/2013US20130047624 Distributed lubrication system
02/28/2013US20130047620 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same
02/28/2013US20130047577 Ignition exciter system and ignition exciter circuit
02/28/2013US20130047576 Method for operating a gas turbine power plant with flue gas recirculation
02/28/2013CA2851226A1 Air inlet arrangement and method of making the same
02/27/2013EP2562396A2 Gas turbine engine generator switchable drive
02/27/2013EP2562395A2 Power plant start-up method
02/27/2013EP2562394A1 Fuel supply device of gas turbine engine
02/27/2013EP2562393A2 Variable temperature chiller coils
02/27/2013EP2562391A2 Power Plant and Control Method
02/27/2013EP2562384A2 Method of operating a power plant
02/27/2013EP2562383A2 Method of operating a power plant
02/27/2013EP2562358A1 Split-ring cooling structure and gas turbine
02/27/2013CN102947550A Gearbox in turbomachine
02/27/2013CN102943712A Variable-flow fuel adjusting valve
02/27/2013CN102943711A Device for cooling guiding device group of turbine
02/26/2013US8381543 System for enhanced fuel gas composition control in an LNG facility
02/26/2013US8381533 Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plate
02/26/2013US8381530 System and method for controlling combustion dynamics
02/26/2013CA2695048C Sensor head for a dry powder agent
02/26/2013CA2541127C Turbojet rear suspension
02/21/2013WO2013025818A1 Fuel system using dual pressure hi-speed centrifugal pump arrangement
02/21/2013WO2009108079A3 Method and plant for generating mechanical or electrical power from waste heat and apparatus for a power plant
02/21/2013US20130042631 Seal end attachment
02/21/2013US20130042630 Gas turbine engine accessory mount
02/21/2013US20130042629 Turbomachine load management assembly
02/21/2013US20130042628 Gas turbine engine internal compartment structure having egress feature
02/21/2013US20130042627 Combustion chamber head of a gas turbine with cooling and damping functions
02/21/2013US20130042625 Micromixer heat shield
02/21/2013US20130042622 Flow balancing valve
02/21/2013US20130042621 Method for increasing the efficiency of a power plant which is equipped with a gas turbine, and power plant for carrying out the method
02/21/2013DE102012107320A1 Bürstendichtung mit Stützplattenzahn Brush seal with backing plate tooth
02/21/2013DE102011081200A1 Wälzlageranordnung eines Abgasturboladers Roller bearing assembly of a turbocharger
02/21/2013DE102011081112A1 Verfahren zur Herstellung eines Bauteils für hohe thermische Belastungen, ein Bauteil herstellbar mit dem Verfahren und ein Flugzeugtriebwerk mit dem Bauteil A method for producing a component for high thermal loads, a component produced by the method and an aircraft engine with the component
02/20/2013EP2559883A2 Gas turbine engine accessory mount
02/20/2013EP2559882A1 Ignition system for a gas turbine combustor
02/20/2013EP2559881A2 Adiabatic compressed air energy storage system and corresponding method
02/20/2013EP2559867A1 Method for generating electrical energy with a combination power plant and combination power plant and device for carrying out the method
02/20/2013EP2559857A1 Gas turbine and turbine stationary blade for same
02/20/2013EP2559848A2 Method for Regenerating Oxide Coatings on Gas Turbine Components by Addition of Oxygen into SEGR System
02/20/2013EP2559618A2 Ice protection system for a multi-segment aircraft component
02/20/2013EP2558699A1 Device and method for preserving fluid systems and an engine
02/20/2013EP2558688A1 A strut, a gas turbine engine frame comprising the strut and a gas turbine engine comprising the frame
02/20/2013CN202746017U Energy-saving-type air intake anti-icing device of gas turbine
02/20/2013CN102939438A Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing
02/20/2013CN102937051A Swirling type plasma ignition nozzle
02/20/2013CN102937050A High pressure air path system for stable combustion of vehicle gas turbine fuel oil
02/20/2013CN102937049A Cross arranged centrifugal micro-type gas turbine
02/19/2013US8376697 Gas turbine sealing apparatus
02/19/2013US8375900 External combustion engine and method of converting internal combustion engine thereto
02/19/2013US8375726 Combustor assembly in a gas turbine engine
02/19/2013US8375724 Method of operating a multi-fuel combustion system
02/19/2013US8375697 Electrolytic igniter for rocket engines using liquid propellants
02/19/2013CA2605220C Gas turbine internal manifold mounting arrangement
02/19/2013CA2594321C Fuel conveying member for a gas turbine engine
02/19/2013CA2573206C Aircraft propulsion system
02/19/2013CA2510670C Venting tube for low-pressure shaft of a turbine engine
02/19/2013CA2503039C Device for balancing a rotating part, particularly of a turbojet engine rotor
02/19/2013CA2492418C Methods and apparatus for operating gas turbine engines
02/19/2013CA2487839C Structure for mounting a turboprop under an aircraft wing
02/17/2013CA2779318A1 Flow balancing valve
02/14/2013WO2013021118A1 Method for estimating the temperature of the fuel leaving a turbomachine exchanger
02/14/2013US20130038057 Gas turbine engine apparatus
02/14/2013US20130038022 Seal assembly and method for flowing hot gas in a turbine
02/14/2013US20130036748 System and method for producing carbon dioxide for use in hydrocarbon recovery
02/14/2013US20130036747 Method for cooling a gas turbine plant and gas turbine plant for implementing the method
02/14/2013US20130036742 Combustor liner cooling system
02/14/2013US20130036741 Multipoint injectors with auxiliary stage
02/14/2013US20130036740 Multi-fuel injection nozzle
02/14/2013US20130036738 Turbomachine fueling system with jet pump
02/14/2013US20130036723 Oxy-combustion gas turbine hybrid
02/14/2013US20130036722 Fuel system having fuel control unit and heat exchanger
02/14/2013DE102011109948A1 Gasturbine Gas turbine
02/14/2013DE102011080596A1 Anordnung für ein Leiten eines Abgases in einer axial angeströmten Abgasturbine Arrangement for passing a gas in an axial flow gas turbine
02/13/2013EP2557304A1 Jet flow nozzle and jet engine
02/13/2013EP2557296A2 System and method for hot ambient and grid frequency compensation for a gas turbine
02/13/2013CN202732118U System for reducing inlet air temperature of gas turbine
02/13/2013CN202732117U Lubricating oil device for gas turbine
02/13/2013CN102933904A Damping device for damping pressure oscillations within a combustion chamber of a turbine
02/13/2013CN102933820A Preheat spark plug
02/13/2013CN102933819A Lean-fuel intake gas turbine
02/13/2013CN102933798A Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine
02/13/2013CN102927141A Coupler assembly
02/13/2013CN102926972A Seal assembly and method for flowing hot gas in a turbine
02/13/2013CN102926874A Combustion gas turbine fuel supply device capable of flexibly blending and switching fuels and control method
02/13/2013CN102926873A Gas turbine support system
02/12/2013US8371127 Cooling air system for mid turbine frame
02/12/2013US8371126 Gas turbine combustor
02/12/2013US8371101 Radial inlet guide vanes for a combustor
02/12/2013CA2683382C Bearing support structure for turbine
02/12/2013CA2524141C Counter-rotating turbine engine and method of assembling same
02/12/2013CA2517182C Gas turbine engine having improved core system
02/12/2013CA2502374C Methods and apparatus for exhausting gases from gas turbine engines
02/12/2013CA2453634C Turbo recuperator device
02/10/2013CA2784660A1 Acoustic dampening device for use in gas turbine engine
02/07/2013US20130034432 Corrugated core cowl for a gas turbine engine
02/07/2013US20130033036 Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle
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