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