Patents
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
12/2013
12/05/2013WO2013181050A1 Turbine gear assembly support having symmetrical removal features
12/05/2013WO2013181002A1 Liner hanger cable
12/05/2013WO2013180797A2 Shark-bite tip shelf cooling configuration
12/05/2013US20130323013 Nacelle inner flow structure leading edge latching system
12/05/2013US20130318983 Aircraft energy management system including engine fan discharge air boosted environmental control system
12/05/2013US20130318980 Spraybar face seal retention arrangement
12/05/2013US20130318945 Aviation gas turbine thrust reversing device
12/04/2013EP2669501A2 Acoustic panel
12/04/2013CN103429909A Guide vane attachment structure and fan
12/04/2013CN103429880A Turbomachine with fan(s) for aircraft, with mobile jet nozzle
12/03/2013US8596072 Gas turbine engine with variable area fan nozzle positioned for starting
12/03/2013US8596040 Rocket multi-nozzle grid assembly and methods for maintaining pressure and thrust profiles with the same
12/03/2013US8596037 Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle
11/2013
11/28/2013WO2013177030A1 Method and device for modifying a secondary air system in a gas turbine engine
11/28/2013WO2013176920A1 Shield system for gas turbine engine
11/28/2013WO2013176863A1 Passive thermostatic valve
11/28/2013WO2013176717A2 Pressure balanced area control of high aspect ratio nozzle
11/28/2013WO2013176709A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case
11/28/2013US20130312387 Variable area fan nozzle actuation system
11/28/2013US20130312385 Gas turbine system having a plasma actuator flow control arrangement
11/27/2013EP2665909A2 Nacelle for an aircraft bypass turbojet engine
11/27/2013EP2665908A2 Nacelle for an aircraft bypass turbojet engine
11/26/2013US8590288 Fan control apparatus
11/26/2013US8590286 Gas turbine engine systems involving tip fans
11/21/2013WO2013173006A1 Method for making metal plated gas turbine engine components
11/21/2013WO2013172906A2 Counter rotating low pressure turbine with splitter gear system
11/21/2013WO2013172905A2 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame
11/21/2013WO2013172903A2 Tapered thermal coating for airfoil
11/21/2013WO2013172899A2 Gas turbine engine systems involving tip fans
11/21/2013WO2013172893A2 Composite airfoil with local tailoring of material properties
11/21/2013WO2013172892A2 Debris detection in turbomachinery and gas turbine engines
11/21/2013US20130305686 Combined turbojet and ramjet engine
11/20/2013EP2663777A1 Turbofan engine
11/20/2013EP2074309B1 Nacelle assembly for a high-bypass gas turbine engine and corresponding method of varying a fan nozzle exit area
11/20/2013EP2069630B1 Nacelle assembly and corresponding method
11/20/2013CN103403301A Cooling air inlet and method for operating cooling air inlet
11/20/2013CN103397933A Extreme heat machine and operating method thereof
11/14/2013WO2013169604A1 Blade tip having a recessed area
11/14/2013WO2013169316A2 Geared turbofan gas turbine engine architecture
11/14/2013WO2013122635A3 Gas turbine fan composite containment case and methods of manufacture
11/14/2013CA2854082A1 Geared turbofan gas turbine engine architecture
11/13/2013CN102588143B Minitype turbofan engine
11/12/2013US8578697 Fan section
11/12/2013CA2586433C Flameholder fuel shield
11/12/2013CA2586431C Purged flameholder fuel shield
11/12/2013CA2551711C Augmentor radial fuel spray bar with counterswirling heat shield
11/07/2013WO2013165868A1 Gas turbine engine combustor surge retention
11/07/2013WO2013165865A1 Hollow fan blade with braided fabric tubes
11/07/2013WO2013165862A1 Geared turbofan with three turbines all co-rotating
11/07/2013WO2013165790A1 Extraction tool assembly
11/07/2013WO2013165771A1 Geared turbofan with distributed accessory gearboxes
11/07/2013WO2013165769A1 Manifold for geared turbofan engine
11/07/2013WO2013165527A2 High order shaped curve region for an airfoil
11/07/2013WO2013165524A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case
11/07/2013WO2013165518A2 Gas turbine engine component with cusped, lobed cooling hole
11/07/2013WO2013165517A2 Gas turbine engine component with diffusive cooling hole
11/07/2013WO2013165513A2 Counter-rotating low pressure turbine without turbine exhaust case
11/07/2013WO2013165511A2 Edm method for multi-lobed cooling hole
11/07/2013WO2013165510A2 Multi-lobed cooling hole and method of manufacture
11/07/2013WO2013165509A2 Multi-lobed cooling hole
11/07/2013WO2013165508A2 Multi-lobed cooling hole array
11/07/2013WO2013165507A2 Cooling hole with asymmetric diffuser
11/07/2013WO2013165506A2 Cooling hole with crenellation features
11/07/2013WO2013165505A2 Composite fan containment case assembly
11/07/2013WO2013165504A2 Manufacturing methods for multi-lobed cooling holes
11/07/2013WO2013165503A2 Cooling hole with enhanced flow attachment
11/07/2013WO2013165502A2 Cooling hole with thermo-mechanical fatigue resistance
11/07/2013WO2013122687A3 Gas turbine engine bifurcation located fan variable area nozzle
11/06/2013EP2660454A2 Thrust reverser assembly and method of operation
11/06/2013EP2659119A1 Gas turbine engine with bypass mixer
11/06/2013CN203271949U Novel small-sized duct turbofan engine
11/06/2013CN102257260B System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
11/05/2013US8572947 Gas turbine engine with ejector
10/2013
10/31/2013WO2013163604A1 Fuel injector with purged insulating air cavity
10/31/2013WO2013163049A1 Airfoil including loose damper
10/31/2013WO2013163048A1 Airfoil with powder damper
10/31/2013WO2013163047A1 Airfoil including damper member
10/31/2013WO2013163046A1 Airfoil having tapered buttress
10/31/2013WO2013163029A1 Airfoil cooling enhancement and method of making the same
10/31/2013WO2013163020A1 Gas turbine engine core providing exterior airfoil portion
10/31/2013WO2013162946A1 Blade having porous, abradable element
10/31/2013WO2013162887A1 Airfoil with break-way, free-floating damper member
10/31/2013WO2013162866A1 Airfoil support method and apparatus
10/31/2013WO2013162752A1 Thermal management system for a gas turbine engine
10/31/2013WO2013162665A2 Engine hot section vane with tapered flame holder surface
10/31/2013WO2013160602A1 Turbine engine incorporating thermoelectric generators
10/30/2013EP2655842A1 Gas turbine engine heat exchanger
10/30/2013CN103380279A Driveshaft for the gearbox of auxiliary machines of a turbojet engine
10/30/2013CN103375304A Modular louver system
10/30/2013CN103375303A Thrust reverser assembly and method of operation
10/30/2013CN103375302A Turboprop engine and usage method thereof
10/30/2013CN101558224B Device for improving effectiveness of acoustic treatments in aircraft drive duct
10/29/2013US8567202 Support links with lockable adjustment feature
10/24/2013WO2013158187A1 Geared turbofan gas turbine engine architecture
10/24/2013CA2856912A1 Geared turbofan gas turbine engine architecture
10/23/2013EP2653701A1 Control apparatus for a variable section nozzle of an aircraft
10/23/2013CN103370522A Cowl assembly
10/22/2013US8566000 System and method for controlling a single-spool turboshaft engine
10/22/2013US8561383 Turbine engine with differential gear driven fan and compressor
10/22/2013CA2606525C Air compression type engine for aviation
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