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)
12/2013
12/12/2013DE19925773B4 Abgasturbolader mit einem Notöltank Turbocharger with an emergency oil tank
12/12/2013DE102012209566A1 Fuel supply system for gas turbine, has supply line connected to inlet of first fuel reservoir and outlet of second fuel reservoir, where outlet of first fuel reservoir is connected to return line and branch
12/12/2013DE102012209549A1 Kühlmittelüberbrückungsleitung für eine Gasturbine Coolant bypass line for a gas turbine
12/12/2013DE102012012085A1 Slide ring seal, particularly running gear seal, has slide ring and counter ring, which have receptacle area for elastomer ring, and upper outer region of sliding surfaces is clearly cut, so that dirt catching groove arises
12/12/2013CA2874948A1 Modular gas turbine plant with a heavy duty gas turbine
12/12/2013CA2874935A1 High pressure ratio compressors with multiple intercooling and related methods
12/12/2013CA2874933A1 Combination of two gas turbines to drive a load
12/11/2013EP2672090A2 Fuel metering valve fail-fixed and back-up control system
12/11/2013EP2672076A2 Method for Shutting Down a Generator to Prepare the Generator for Restart
12/11/2013EP2670954A1 Axial brush seal
12/11/2013CN203335246U Box-type filter for ship gas turbine
12/11/2013CN203335245U Aircraft pipeline wheel gas engine
12/11/2013CN103443542A Gas turbine assembly and corresponding operating method
12/11/2013CN103443421A Combustor and gas turbine provided with same
12/11/2013CN103443420A Injection aperture for a steam power plant
12/11/2013CN103437889A Branch gas film hole structure for cooling gas turbine engine
12/11/2013CN103437888A Transition section structure of high-pressure and low-pressure turbines
12/11/2013CN101737803B Fuel nozzle assembly of a gas turbine engine and gas turbine engine
12/10/2013US8601822 Pressure-based fuel metering unit
12/10/2013US8601820 Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
12/10/2013US8601785 Oil supply system with main pump deaeration
12/10/2013CA2663247C Power recovery machine
12/10/2013CA2612687C Variable arc gap plasma igniter element
12/10/2013CA2506092C Aircraft engine with means of hanging from an aircraft structure
12/08/2013CA2816504A1 Oil scavenge arrangement
12/05/2013WO2013181399A1 Retention assembly including sleeve
12/05/2013WO2013181396A1 Stress-relieved wire seal assembly for gas turbine engines
12/05/2013WO2013181389A2 Ladder seal system for gas turbine engines
12/05/2013WO2013181312A1 Turbine damper
12/05/2013WO2013181311A1 Turbine damper
12/05/2013WO2013181254A1 Actuator mounted to torque box
12/05/2013WO2013181051A1 Lubrication arrangement for a gas turbine engine gear assembly
12/05/2013WO2013181050A1 Turbine gear assembly support having symmetrical removal features
12/05/2013WO2013181006A1 Turbine cooling apparatus
12/05/2013WO2013181002A1 Liner hanger cable
12/05/2013WO2013180982A1 Auxiliary fire resistant mount system for an auxiliary power unit
12/05/2013WO2013180980A1 Auxiliary power unit mount with fire resistant shielding
12/05/2013WO2013180959A1 Exhaust-gas turbocharger
12/05/2013WO2013180954A1 High pressure turbine coolant supply system
12/05/2013WO2013180953A1 Mate face cooling holes for gas turbine engine component
12/05/2013WO2013180939A1 Auxiliary oil system for negative gravity event
12/05/2013WO2013180917A1 Adaptive fan with cold turbine
12/05/2013WO2013180916A1 Assembly fixture for a stator vane assembly
12/05/2013WO2013180899A1 Segmented seal with ship lap ends
12/05/2013WO2013180897A2 Gas turbine engine compressor stator seal
12/05/2013WO2013180895A1 Turbomachine containment structure
12/05/2013WO2013180894A1 Spraybar face seal retention arrangement
12/05/2013WO2013180797A2 Shark-bite tip shelf cooling configuration
12/05/2013WO2013180792A2 Gas turbine engine airfoil trailing edge passage and core for making same
12/05/2013WO2013180789A2 Pump system for hpc ecs parasitic loss elimination
12/05/2013WO2013180788A2 Constant speed pump system for engine ecs loss elimination
12/05/2013WO2013180778A2 Seal assembly
12/05/2013WO2013180761A1 Buffer system that communicates buffer supply air to a portion of a gas turbine engine
12/05/2013WO2013180049A1 Variable nozzle unit and variable capacity supercharger
12/05/2013WO2013179987A1 Power generation unit of integrated gearbox design for aircraft engine
12/05/2013WO2013178956A1 Fluid circuit in a turbine engine
12/05/2013US20130324343 Reduction gear with epicyclic gear train having roller-bearing-mounted planet spindles
12/05/2013US20130323063 System for attaching a turbojet engine spinner
12/05/2013US20130319008 Turbine blade support
12/05/2013US20130319005 Floating segmented seal
12/05/2013US20130319002 Nacelle bifurcation for gas turbine engine
12/05/2013US20130319001 Turbine gear assembly support having symmetrical removal features
12/05/2013US20130319000 Turbine gear assembly support having symmetrical removal features
12/05/2013US20130318996 Cooling assembly for a bucket of a turbine system and method of cooling
12/05/2013US20130318995 Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
12/05/2013US20130318994 Ultra-violet flame detector with high temperature remote sensing element
12/05/2013US20130318993 Utilization of fuel gas for purging a dormant fuel gas circuit
12/05/2013US20130318992 Combustor with a Brief Severe Quench Zone
12/05/2013US20130318986 Impingement cooled combustor
12/05/2013US20130318982 Turbine cooling apparatus
12/05/2013US20130318977 Fuel injection assembly for use in turbine engines and method of assembling same
12/05/2013US20130318942 Flame detection in no-flame region of gas turbine
12/05/2013US20130318940 Lubrication arrangement for a gas turbine engine gear assembly
12/05/2013US20130318939 Lubrication arrangement for a gas turbine engine gear assembly
12/05/2013DE102012010935A1 Heat exchanger for aircraft gas turbine, has substantially tubular twisting element that is arranged at fuel inlet, and is formed for applying twist on flowing fuel by twisting of twisting element
12/05/2013DE102004061173B4 Gasturbinentriebwerk mit einem Partikelseparator A gas turbine engine with a particle separator
12/05/2013DE102004018585B4 Triebwerkeinlaufkonus für ein Gasturbinentriebwerk Engine inlet cone for a gas turbine engine
12/05/2013CA2809985A1 Deoiler seal
12/04/2013EP2669501A2 Acoustic panel
12/04/2013EP2669493A2 Utilization of fuel gas for purging a dormant fuel gas circuit
12/04/2013EP2669490A2 Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
12/04/2013EP2669489A2 Axial compressor and gas turbine having axial compressor
12/04/2013EP2669488A2 Method and exergy power plant for decentralised power generation
12/04/2013EP2668387A1 Mixing element for gas turbine units with flue gas recirculation
12/04/2013CN103429909A Guide vane attachment structure and fan
12/04/2013CN103422993A System and method for producing hydrogen rich fuel
12/04/2013CN103422992A Method for manufacturing a hot gas path component
12/04/2013CN103422991A Systems and methods for minimizing coking in gas turbine engines
12/04/2013CN103422990A Cooling system and method for turbine system
12/04/2013CN103422989A Gas turbine system having a plasma actuator flow control arrangement
12/04/2013CN103422988A Apparatus and system for changing temperature of vane separators in a power generating system
12/04/2013CN103422987A Pressure gradient controllable S-shaped inlet channel design method
12/04/2013CN102691576B Power transmission mechanism of gas compressor and turbine
12/04/2013CN102588080B Dynamic fluid gas working medium compression system
12/04/2013CN101581252B Method for controlling set point for extracting air to provide cooling air
12/04/2013CN101554924B Device for feeding combustion air to an air craft engines
12/03/2013US8596075 System and method for high efficiency power generation using a carbon dioxide circulating working fluid
12/03/2013US8596035 Apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbines
12/03/2013CA2746909C High pressure drop muffling system
12/03/2013CA2620415C Hydrostatic flow barrier for flexible fuel manifold
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