Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › 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)
04/2014
04/03/2014WO2014052210A1 Axial sealing gravity based siphon system
04/03/2014WO2014052209A1 Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
04/03/2014WO2014052207A1 Multiple reservoir lubrication system
04/03/2014WO2014052100A1 Thermodynamic cycle with compressor recuperation, and associated systems and methods
04/03/2014WO2014052039A1 Turbomachine rotor groove
04/03/2014WO2014052007A1 Mid-turbine frame with fairing attachment
04/03/2014WO2014051988A1 Liner and method of assembly
04/03/2014WO2014051845A1 Piston ring coated carbon seal
04/03/2014WO2014051831A2 Combustor bulkhead assembly
04/03/2014WO2014051700A1 Radially coacting ring seal
04/03/2014WO2014051691A1 Buffer airflow to bearing compartment
04/03/2014WO2014051690A1 Fastened joint for a tangential on board injector
04/03/2014WO2014051688A1 Seal damper with improved retention
04/03/2014WO2014051686A1 Combined high pressure turbine case and turbine intermediate case
04/03/2014WO2014051678A1 Gas turbine engine thermal management system for heat exchanger using bypass flow
04/03/2014WO2014051673A1 Bleed duct for laminar fan duct flow
04/03/2014WO2014051672A1 Split-zone flow metering t-tube
04/03/2014WO2014051670A1 Airfoil array with airfoils that differ in geometry according to geometry classes
04/03/2014WO2014051669A1 Reduction in jet flap interaction noise with geared turbine engine
04/03/2014WO2014051668A1 Gas turbine engine including vane structure and seal to control fluid leakage
04/03/2014WO2014051666A1 Liner lock segment
04/03/2014WO2014051663A1 Alignment tool for use in a gas turbine engine
04/03/2014WO2014051662A1 Gas turbine engine having support structure with swept leading edge
04/03/2014WO2014051661A1 Turbomachine control system
04/03/2014WO2014051658A1 Seal assembly for a static structure of a gas turbine engine
04/03/2014WO2014051656A2 Turbine engine vane arrangement having a plurality of interconnected vane arrangement segments
04/03/2014WO2014050163A1 Method for controlling gas turbine cooling system, control device for executing this method, and gas turbine facility equipped with same
04/03/2014WO2014011290A3 Airfoil having internal lattice network
04/03/2014WO2011139314A3 Gas turbine engine component construction
04/03/2014US20140093371 Mid-turbine frame heat shield
04/03/2014US20140093370 Gas turbine engine combustor liner
04/03/2014US20140093368 Outer case with gusseted boss
04/03/2014US20140093362 Gas turbine engine components and method of assembly
04/03/2014US20140093356 Axial sealing gravity based siphon system
04/03/2014US20140093351 Apparatus and method of operating a turbine assembly
04/03/2014US20140091531 Spline seal with cooling pathways
04/03/2014US20140091529 Clamshell seal
04/03/2014US20140090923 Acoustic panel
04/03/2014US20140090402 Combustor Bulkhead Assembly
04/03/2014US20140090399 Panel support hanger for a turbine engine
04/03/2014US20140090398 Flexible connection between a wall and a case of a turbine engine
04/03/2014US20140090395 Gas turbine engine
04/03/2014US20140090393 Minimum Pressure and Shutoff Valve
04/03/2014US20140090388 Off-take power ratio
04/03/2014US20140090387 Fuel heating system for a power plant and method of heating fuel
04/03/2014US20140090385 System and method for swirl flow generation
04/03/2014US20140090355 Reduced trim flow gas turbine engine oil system
04/03/2014DE19945581B4 Turbomaschine Turbomachine
04/03/2014DE10348447B4 Montage- und Wartungshilfsmittel für eine Gasturbine Installation and maintenance tool for a gas turbine
04/03/2014DE102013201714A1 Gas turbine engine has actuator device having pistons that are respectively coupled to piezoelectric actuator and throttle valve main portion
04/03/2014DE102013112506A1 Turbofan engine for combustion chamber of turbine, has fuel-air-mixture that is introduced in flow direction towards compressor in core flow, where combustion chamber is supplied with core flow and is combusted in explosive manner
04/03/2014DE102013109117A1 Gleichmäßige Umfangsverteilung eines Fluids in einem Verteiler Uniform circumferential distribution of a fluid into a manifold
04/03/2014DE102012017918A1 Lufteinlasssystem für eine stationäre Brennkraftmaschine, insbesondere eine stationäre Gasturbine Air intake system for a stationary internal combustion engine, in particular a stationary gas turbine
04/02/2014EP2713051A1 A turbine-driven reciprocating compressor and method of operating said compressor
04/02/2014EP2713028A2 Adaptive fuel manifold filling function for improved engine start
04/02/2014EP2713027A2 A gas turbine engine
04/02/2014EP2713013A1 Gas turbine engine
04/02/2014EP2712395A1 Compressor blade with nozzle
04/02/2014EP2712392A1 Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
04/02/2014CN203515812U Gas exhausting device with multilayered heat preservation and insulation layer of gas turbine
04/02/2014CN203515811U Split supporting device of power turbine of gas turbine
04/02/2014CN203515810U Transition section structure of high-low-pressure turbine
04/02/2014CN1952366B Turbofan engine assembly and method of assembling same
04/02/2014CN103703230A Gas turbine auxiliaries relay gearbox incorporating uncoupling means
04/02/2014CN103703229A Combustion systems and combustion system components for rotary ramjet engines
04/02/2014CN103703228A Method for operating a static gas turbine, and intake duct for intake air of a gas turbine
04/02/2014CN103696855A Integrated system for heating and cooling inflow air of gas turbine
04/02/2014CN102498274B Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
04/02/2014CN102383939B Multi-working-medium turbine engine
04/02/2014CN102076939B Cooling air supply structure of gas turbine and gas turbine
04/02/2014CN101981292B Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same
04/02/2014CN101946072B Gas turbine, and interior opening method for the gas turbine
04/02/2014CN101749286B Deep chilled air washer
04/02/2014CN101644192B System und anordnungen zur heisswasserentnahme zum vorheizen von brennstoff in einem kombizykluskraftwerk
04/01/2014US8685126 Device for filtering the intake air of an internal combustion engine having ventilation means
04/01/2014US8683814 Gas turbine engine component with impingement and lobed cooling hole
04/01/2014US8683813 Multi-lobed cooling hole and method of manufacture
04/01/2014US8683810 Injection device for combustion chambers of liquid-fueled rocket engines
04/01/2014US8683808 Late lean injection control strategy
04/01/2014US8683805 Injector seal for a gas turbomachine
04/01/2014CA2791563A1 Adaptive fuel manifold filling function for improved engine start
04/01/2014CA2719626C Aircraft starter generator
04/01/2014CA2577898C Process for installing a thermal barrier using a plasma gun
03/2014
03/27/2014WO2014047038A1 Multi-stage high pressure compressor case
03/27/2014WO2014047022A1 Gas turbine engine component cooling circuit
03/27/2014WO2014046960A1 Gear carrier flex mount lubrication
03/27/2014WO2014046931A1 Turbomachine hybrid lift-off face seal
03/27/2014WO2014046926A1 Turbomachine fluid delivery manifold and system
03/27/2014WO2014046891A1 Fire seal
03/27/2014WO2014046735A1 Fan blade tall dovetail for individually bladed rotors
03/27/2014WO2014046713A1 Geared gas turbine engine accessory gearbox
03/27/2014WO2014045896A1 Gap measurement device for combustor, and gap measurement method
03/27/2014WO2014018138A3 Airfoil cooling circuits
03/27/2014WO2014014539A3 Blade dovetail bottom
03/27/2014WO2014014538A3 Manifold for gas turbine engine
03/27/2014WO2014011289A3 Airfoil having minimum distance ribs
03/27/2014WO2014011242A3 Hybrid airfoil for a gas turbine engine
03/27/2014WO2014007884A3 Turbomachine thermal management
03/27/2014US20140086741 Turbomachine hybrid lift-off face seal
03/27/2014US20140083115 Article with dielectric mirror coating system
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