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
04/10/2014WO2014055499A1 Sheath with extended wings
04/10/2014WO2014055301A1 Reduced height ligaments to minimize non-integral vibrations in rotor blades
04/10/2014WO2014055299A1 Aluminum based abradable material with reduced metal transfer to blades
04/10/2014WO2014055152A2 Bifurcated inlet scoop for gas turbine engine
04/10/2014WO2014055124A1 Method of defining gas turbine engine control ratings
04/10/2014WO2014055122A1 Geared turbofan high gearbox power density
04/10/2014WO2014055116A1 Combustor with grommet having projecting lip
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
04/10/2014WO2014055106A1 Gas turbine engine including bleed system coupled to upstream and downstream locations of compressor
04/10/2014WO2014055105A1 Reduced fan containment threat through liner and blade design
04/10/2014WO2014055103A1 Pylon shape with geared turbofan for structural stiffness
04/10/2014WO2014055102A1 Low weight large fan gas turbine engine
04/10/2014WO2014055101A1 Sensor adapter
04/10/2014WO2014054825A1 Film shape structure of cooling hole for cooling gas turbine blades
04/10/2014WO2014053721A1 Supply and drain device for an injector
04/10/2014WO2014053421A1 A turboexpander and driven turbomachine system
04/10/2014WO2014028078A3 A gas turbine engine and nacelle noise attenuation structure
04/10/2014WO2014023726A3 Electrical apparatus
04/10/2014WO2014021973A3 Liner assembly
04/10/2014WO2014021966A3 Adjustable engine mount
04/10/2014US20140099591 Duct burner of hrsg with liner film cooling
04/10/2014US20140099194 Bimetallic turbine shroud and method of fabricating
04/10/2014US20140099187 Oil baffle for gas turbine engine fan drive gear system
04/10/2014US20140096827 Gas turbine engine with a multiple fuel delivery system
04/10/2014US20140096537 Thin Metal Duct Damper
04/10/2014US20140096535 Gas turbine system with reheat spray control
04/10/2014US20140096534 Low Profile Compressor Bleed Air-Oil Coolers
04/10/2014US20140096533 Bearing chamber venting system for an aircraft engine and method for providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber
04/10/2014US20140096528 Cooling for Combustor Liners with Accelerating Channels
04/10/2014US20140096527 Gas turbine engine combustor liner
04/10/2014US20140096508 Systems and methods involving multiple torque paths for gas turbine engines
04/10/2014US20140096503 Magnetic De-Icing
04/10/2014US20140096502 Burner for a gas turbine
04/10/2014US20140096500 Exhaust diffuser
04/10/2014DE102012218135A1 Lagerkammerentlüftungssystem für ein Flugzeugtriebwerk und Verfahren zum Bereitstellen eines gewünschten Druckverhältnisses an Lagerkammerdichtungen einer luftgedichteten Lagerkammer Storage chamber venting system for an aircraft engine and method for providing a desired pressure ratio of bearing chamber seals an air-sealed storage chamber
04/10/2014DE102010013697B4 Turbolader Turbocharger
04/09/2014EP2716890A2 Gas turbine engine with a multiple fuel delivery system
04/09/2014EP2716889A2 Redundant cooling for fluid cooled systems
04/09/2014EP2716396A1 Hollow curved plate, method for manufacturing same, and burner for gas turbine
04/09/2014EP2715094A1 A structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section
04/09/2014EP2715072A1 Turbomachine fan case
04/09/2014EP2714518A1 Gas-turbine engine with a telescopic air inlet in the engine lining
04/09/2014CN203532055U Gas-steam combined circulation type air inlet dehumidifying and cooling system
04/09/2014CN103717856A Turbo-compressor train with rolling bearings and related assembly method
04/09/2014CN103717844A Turbine engine drive shaft device
04/09/2014CN103717843A Method for running up a stationary gas turbine
04/09/2014CN103711590A Fuel heating system for a power plant and method of heating fuel
04/09/2014CN103711589A Flow balancing ventilation system and method of balancing a flow
04/09/2014CN103711588A Turbine components with adaptive cooling pathways
04/09/2014CN103711530A Solid seal with cooling pathways
04/09/2014CN103710614A Cast iron containing niobium and component
04/09/2014CN101892911B Gas turbine having seal assembly with side plate and seal
04/09/2014CN101718228B Method and system for operating turbomachine having unchoked valve
04/08/2014US8689933 Helmholtz resonator for a gas turbine combustion chamber
04/08/2014US8689568 Cooling hole with thermo-mechanical fatigue resistance
04/08/2014US8689567 Clutch locking plate with oil slinger
04/08/2014US8689566 Compressed air energy system integrated with gas turbine
04/08/2014US8689562 Combustion cavity layouts for fuel staging in trapped vortex combustors
04/08/2014US8689561 Vortex premixer for combustion apparatus
04/08/2014US8689558 Propfan engine
04/08/2014US8689536 Advanced laser ignition systems for gas turbines including aircraft engines
04/08/2014CA2594005C Turbomachine including a cooling system for the downstream face of an impeller compressor
04/08/2014CA2592626C Arrangement for turbine engine combustion chamber with a deflector flange
04/03/2014WO2014052967A1 Case assembly for a gas turbine engine
04/03/2014WO2014052966A1 Combustor section of a gas turbine engine
04/03/2014WO2014052965A1 Interface heat shield for a combustor of a gas turbine engine
04/03/2014WO2014052949A1 Combustor seal system for a gas turbine engine
04/03/2014WO2014052866A1 Flow modifier for combustor fuel nozzle tip
04/03/2014WO2014052857A1 Assembly for mounting a turbine engine case to a pylon
04/03/2014WO2014052842A1 Synchronization ring runner with cradle
04/03/2014WO2014052832A1 Cooled turbine blade with leading edge flow redirection and diffusion
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
04/03/2014WO2014052737A1 Inner diffuser case struts for a combustor of a gas turbine engine
04/03/2014WO2014052632A1 Gas turbine engine combustor
04/03/2014WO2014052629A1 Support hanger for flexibly connecting a plurality of panels
04/03/2014WO2014052626A1 Panel support hanger for a turbine engine
04/03/2014WO2014052603A1 Gas turbine engine preswirler with angled holes
04/03/2014WO2014052601A1 Turbomachine thrust balancing system
04/03/2014WO2014052597A1 Structural guide vane internal topology
04/03/2014WO2014052569A1 Airfoil with galvanic corrosion preventive shim
04/03/2014WO2014052558A1 Geared turbofan with fan and core mounted accessory gearboxes
04/03/2014WO2014052538A1 Gas turbine engine airfoil with vane platform cooling passage
04/03/2014WO2014052384A1 Thermally constrained high temperature optical fiber holder
04/03/2014WO2014052345A1 Full ring inner air-seal with locking nut
04/03/2014WO2014052323A1 Uber-cooled turbine section component made by additive manufacturing
04/03/2014WO2014052320A1 Uber-cooled multi-alloy integrally bladed rotor
04/03/2014WO2014052297A1 Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
04/03/2014WO2014052288A1 Seal hook mount structure with overlapped coating
04/03/2014WO2014052279A1 Gas turbine engine components and method of assembly
04/03/2014WO2014052277A1 Gas turbine engine airfoil cooling circuit
04/03/2014WO2014052272A1 Reduced trim flow gas turbine engine oil system
04/03/2014WO2014052269A1 Off-take power ratio
04/03/2014WO2014052221A1 Fuel distribution within a gas turbine engine combustor
04/03/2014WO2014052220A1 Turbine vane with mistake reduction feature
04/03/2014WO2014052211A1 Diode electrical ground for fan blades
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