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
12/25/2013CN203362321U Film hole used for cooling of gas turbine engine
12/25/2013CN103477054A Anti-fire seal assembly and nacelle comprising such a seal
12/25/2013CN103477053A Solar collector including a solar turbine or a turbocompressor
12/25/2013CN103477032A 燃气轮机 Gas turbine
12/25/2013CN103471286A Multiple renewable energy complementary distributed energy system
12/25/2013CN103470379A Combined type energy-saving gas turbine inlet air cooling system
12/25/2013CN103470378A Method and device for improving oil-supplying reliability of lubricating-oil system of power generating set
12/25/2013CN103470377A Transition piece for a gas turbomachine
12/25/2013CN103470375A Cast superalloy pressure containment vessel
12/25/2013CN102748135B Method for designing fixed-geometry two-dimensional mixed-compression type supersonic velocity air inlet channel
12/25/2013CN102269059B Accessory case transmission device and aircraft engine comprising same
12/25/2013CN102143889B Method for making acoustic panel for air intake lip of nacelle
12/25/2013CN102143888B Method for making nacelle de-icing element
12/25/2013CA2813972A1 Contamination resistant butterfly valve
12/24/2013US8613199 Cooling fluid metering structure in a gas turbine engine
12/24/2013DE102013210994A1 Turboladerverdichtergeräuschminderungssystem und -Verfahren Turbocharger compressor noise reduction system and method
12/19/2013WO2013188723A1 Fluid conduit
12/19/2013WO2013188722A1 High durability turbine exhaust case
12/19/2013WO2013188325A1 Shaft alignment tools and methods
12/19/2013WO2013188324A1 Shaft alignment tools and methods
12/19/2013WO2013188115A1 Rotor assembly with interlocking tabs
12/19/2013WO2013188074A1 Turbomachine flow control device
12/19/2013WO2013188033A1 Gas turbine control systems and methods
12/19/2013WO2013187961A1 Manifold for flow distribution
12/19/2013WO2013187103A1 Blade root spring insertion tool and blade root spring insertion method
12/19/2013WO2013165518A3 Gas turbine engine component with cusped, lobed cooling hole
12/19/2013WO2013165517A3 Gas turbine engine component with diffusive cooling hole
12/19/2013WO2013165512A3 Variable area turbine
12/19/2013WO2013103469A3 Process of producing ceramic matrix composites and ceramic matrix composites formed thereby
12/19/2013US20130336758 Variable blade outer air seal
12/19/2013US20130336757 Active control of bucket cooling supply for turbine
12/19/2013US20130333393 Gas turbine control systems and methods
12/19/2013US20130333390 Cooling air inlet, engine bleed air system and method for operating a cooling air inlet
12/19/2013US20130333389 Cross fire tube retention system for a gas turbine engine
12/19/2013US20130333388 Combustor liner cooling assembly for a gas turbine system
12/19/2013CA2875800A1 Fluid conduit
12/18/2013EP2674593A2 Active control of bucket cooling supply for a turbine by means of an adjustable gas flow valve comprising a shape memory material
12/18/2013EP2674590A1 Power plant with solar energy system and method for operating the power plant
12/18/2013EP2673490A1 Radiation shield for a gas turbine combustor
12/18/2013EP1384856B1 Endface gap sealing of steam turbine packing seal segments and retrofitting thereof
12/18/2013EP1108857B2 Abradable seal
12/18/2013CN203347963U Split fuel pump
12/18/2013CN103459807A Generator apparatus for aircraft
12/18/2013CN103459806A Aircraft engine
12/18/2013CN103459805A Fuel circuit comprising means for controlling a pump
12/18/2013CN103459804A Process for cooling the turbine stage and gas turbine having a cooled turbine stage
12/18/2013CN103459781A 涡轮排气结构及燃气轮机 Structure and the turbine exhaust gas turbine
12/18/2013CN103459778A Gas turbine comprising a heat shield and method of operation
12/18/2013CN103459776A Vane member and rotary machine
12/18/2013CN103459080A Hollow curved plate, method for manufacturing same, and burner for gas turbine
12/18/2013CN103452838A Gear pump, pumping apparatus including the same, and aircraft fuel system including gear pump
12/18/2013CN103452704A Miniature turbojet midair windmill ignition device
12/18/2013CN103452672A Electrical unit for gas turbine and electrical equipment wiring method of electrical unit
12/18/2013CN103452671A Gas turbine compressor inlet pressurization and flow control system
12/18/2013CN103452595A Novel air film hole with improved cooling efficiency
12/18/2013CN102562314B Plasma catalysis based chemical heat extraction cycle gas turbine device
12/18/2013CN102072022B Heat exchange matrix of double-wave primary surface recuperator for micro gas turbine
12/18/2013CN102007282B Propulsion unit for aircraft and air intake structure for such unit
12/18/2013CN101858254B Filter retention systems and devices
12/18/2013CN101629518B Turbomachine filter system having drain with one-way valve
12/18/2013CN101576009B Operation of dual gas turbine fuel system
12/17/2013US8607577 Attaching ceramic matrix composite to high temperature gas turbine structure
12/17/2013CA2576698C Radially compact bearing assembly between a turbine shaft and a turbine engine compressor shaft
12/12/2013WO2013185044A1 Fan blade platform
12/12/2013WO2013184619A1 Single turbine driving dual compressors
12/12/2013WO2013184608A1 Vibration data collection and processing for a gas turbine engine
12/12/2013WO2013184568A1 Compressor power and torque transmitting hub
12/12/2013WO2013184504A1 Combustor liner with reduced cooling dilution openings
12/12/2013WO2013184502A1 Combustor liner with improved film cooling
12/12/2013WO2013184454A1 Seal land for static structure of a gas turbine engine
12/12/2013WO2013184436A1 Insulated tubing
12/12/2013WO2013184431A1 Manufacturing a family of airfoils
12/12/2013WO2013184430A1 Turbine rotor cover plate lock
12/12/2013WO2013184429A1 Front bearing support for a fan drive gear system
12/12/2013WO2013184426A1 Nacelle bifurcation for gas turbine engine
12/12/2013WO2013184400A1 Thermally insulative attachment
12/12/2013WO2013184336A1 Active clearance control for gas turbine engine
12/12/2013WO2013184330A1 Nacelle inner flow structure leading edge latching system
12/12/2013WO2013184329A1 Compressor tip clearance management for a gas turbine engine
12/12/2013WO2013184264A1 Integrated fuel pump and control
12/12/2013WO2013184015A1 Installation for treating a fuel to increase its caloric power
12/12/2013WO2013183618A1 Fuel injection device
12/12/2013WO2013182797A1 Turbine engine comprising an upstream attachment means for a deoiling pipe
12/12/2013WO2013182697A1 Modular gas turbine plant with a heavy duty gas turbine
12/12/2013WO2013182655A1 Combination of two gas turbines to drive a load
12/12/2013WO2013182492A1 High pressure ratio compressors with multiple intercooling and related methods
12/12/2013WO2013130157A3 Adaptive eductor system
12/12/2013US20130327061 Turbomachine bucket assembly and method of cooling a turbomachine bucket assembly
12/12/2013US20130327059 Draining device
12/12/2013US20130327058 Device for suspending a turbojet engine
12/12/2013US20130327057 Combustor liner with improved film cooling
12/12/2013US20130327056 Combustor liner with decreased liner cooling
12/12/2013US20130327055 Transition piece for a gas turbomachine
12/12/2013US20130327054 Hybrid slinger combustion system
12/12/2013US20130327052 Exhaust system for gas turbines
12/12/2013US20130327046 Combustor assembly having a fuel pre-mixer
12/12/2013US20130327045 Gas turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzle
12/12/2013US20130327044 Fuel metering valve fail-fixed and back-up control system
12/12/2013US20130327012 Gas turbine anti-icing system
12/12/2013US20130327011 Method And Apparatus For A Fuel Nozzle Assembly For Use With A Combustor
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