Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
04/2014
04/10/2014WO2014055113A1 Geared turbofan with high fan rotor power intensity
04/10/2014WO2014055110A1 Static guide vane with internal hollow channels
04/10/2014WO2014055109A1 Guide vane seal
04/10/2014WO2014055105A1 Reduced fan containment threat through liner and blade design
04/10/2014WO2014055103A1 Pylon shape with geared turbofan for structural stiffness
04/10/2014WO2014055101A1 Sensor adapter
04/10/2014WO2014011304A3 Turbine engine variable area vane
04/10/2014US20140099198 Duct assembly
04/10/2014US20140096509 Geared Turbofan Engine With Increased Bypass Ratio and Compressor Ratio ...
04/10/2014US20140096508 Systems and methods involving multiple torque paths for gas turbine engines
04/10/2014US20140096507 Bi-Directional Compression Fan Rotor for a Gas Turbine Engine
04/09/2014EP2715091A1 Gas turbine engine comprising three rotary bodies
04/09/2014EP2715072A1 Turbomachine fan case
04/09/2014CN103717867A Aircraft propulsion unit including at least one turbojet engine and a nacelle
04/09/2014CN103711608A Engine airflow passage structure and fanjet
04/08/2014US8689558 Propfan engine
04/08/2014US8689539 Methods and apparatuses for model based control for counter-rotating open-rotor gas turbine engine
04/08/2014US8689538 Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
04/03/2014WO2014052967A1 Case assembly for a gas turbine engine
04/03/2014WO2014052800A1 Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
04/03/2014WO2014052797A1 Flexible connection between a wall and a case of a turbine engine
04/03/2014WO2014052765A1 Wrenching mechanism
04/03/2014WO2014052744A1 Modulated turbine vane cooling
04/03/2014WO2014052597A1 Structural guide vane internal topology
04/03/2014WO2014052538A1 Gas turbine engine airfoil with vane platform cooling passage
04/03/2014WO2014052384A1 Thermally constrained high temperature optical fiber holder
04/03/2014WO2014052323A1 Uber-cooled turbine section component made by additive manufacturing
04/03/2014WO2014052297A1 Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
04/03/2014WO2014052281A1 Gas turbine engine assembly including a thrust reverser
04/03/2014WO2014052279A1 Gas turbine engine components and method of assembly
04/03/2014WO2014052277A1 Gas turbine engine airfoil cooling circuit
04/03/2014WO2014052269A1 Off-take power ratio
04/03/2014WO2014052221A1 Fuel distribution within a gas turbine engine combustor
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
04/03/2014WO2014052039A1 Turbomachine rotor groove
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
04/03/2014WO2014051667A1 Divot for blocker doors of thrust reverser system
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
04/01/2014US8683811 Jet engine with compressor air circulation and method for operating the jet engine
04/01/2014CA2598983C A bleed structure for a bleed passage in a gas turbine engine
03/2014
03/27/2014WO2014047038A1 Multi-stage high pressure compressor case
03/27/2014WO2014046960A1 Gear carrier flex mount lubrication
03/27/2014WO2014046891A1 Fire seal
03/27/2014WO2014046842A1 System for decoupling drive shaft of variable area fan nozzle
03/27/2014WO2014044970A1 System for holding blades and assembly method
03/27/2014WO2014018141A3 Geared turbofan with three turbines all counter-rotating
03/27/2014US20140086739 Transition duct for use in a turbine engine and method of assembly
03/27/2014US20140083079 Geared turbofan primary and secondary nozzle integration geometry
03/26/2014CN103670795A Magnetic bearing aircraft engine of outer rotating vane structure
03/26/2014CN103670794A Magnetic levitation type turbofan aircraft engine
03/26/2014CN103670793A Magnetic suspension aircraft engine main shaft suitable for turbofan engine
03/26/2014CN103670792A Special magnetically conductive ring for magnetic levitation type turbofan jet engine
03/25/2014US8677733 Ducted fan gas turbine assembly
03/25/2014US8677732 Thrust reverser with grids for jet engine
03/20/2014WO2014043493A1 Improved fan case drainage system
03/20/2014WO2014042996A1 Hard lead egress adapter for an instrumentation component
03/20/2014WO2014042975A1 Hollow fan blade with honeycomb filler
03/20/2014WO2014042956A1 Turbine airfoil platform rail with gusset
03/20/2014WO2014042955A1 Gas turbine engine serpentine cooling passage
03/20/2014WO2014007902A3 Tie shaft arrangement for turbomachine
03/20/2014WO2014007880A3 Reverse core gear turbofan
03/20/2014WO2013154649A3 Gas turbine engine with high speed low pressure turbine section
03/20/2014WO2011146096A3 Combustor system
03/20/2014US20140075919 Tec mixer with variable thicknesses
03/20/2014US20140075918 Nacelle leading edge electrical latching system
03/19/2014EP2708698A2 Rotor Assembly
03/19/2014EP2707589A1 Tail cone for a microjet rotary turbine engine
03/19/2014CN102619642B Efficient turbojet engine
03/13/2014WO2014039934A1 Sensor and tooth arrangement for shaft speed detection
03/13/2014WO2014039274A1 Threaded seal for a gas turbine engine
03/13/2014WO2014039256A1 Combustion turbine flashback sensing system employing fiber bragg grating sensors
03/13/2014WO2014039187A1 Turbine engine transmission gutter
03/13/2014WO2014037673A1 Turbine engine comprising a means for measuring the speed and torque of a shaft of the turbine engine and method for monitoring said shaft
03/13/2014WO2014007875A3 Gas turbine engine thrust reverser system
03/13/2014WO2013176709A3 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case
03/12/2014DE202013011243U1 Mantelstromtriebwerk das eine Schubvektorsteuerung mit mindestens einer schwenkbaren Antriebsdüse an der Seite hat Turbofan engine having a thrust vector control with at least one propulsion nozzle at the side of the pivotable
03/12/2014CN203476533U Turbo-charging rotor engine
03/12/2014CN102378855B Rotating inlet cowl for turbine engine, including eccentric front end
03/11/2014US8667777 Bypass engine with contrarotating turbine wheels including a reversing module
03/11/2014US8667775 Reverse flow engine core having a ducted fan with integrated secondary flow blades
03/11/2014US8667774 Coannular ducted fan
03/06/2014WO2014036554A1 Assembly for mounting a turbine engine to a pylon
03/06/2014WO2014035848A1 Gas turbine engine airfoil cooling circuit arrangement
03/06/2014WO2013184495A3 Combustor liner with decreased liner cooling
03/05/2014EP2703148A1 Moulded article
03/05/2014CN203463193U Miniature turbojet engine
03/05/2014CN103620165A Turbomachine fan case
02/2014
02/27/2014WO2014031199A2 Protecting operating margin of a gas turbine engine
02/27/2014WO2014031197A2 Gas turbine engine with a counter rotating fan
02/27/2014WO2014031160A1 Compliant cantilevered airfoil
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