| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 01/23/2013 | EP2547893A2 Determining fan parameters through pressure monitoring |
| 01/22/2013 | US8356469 Gas turbine engine with dual compression rotor |
| 01/17/2013 | US20130014490 Gas turbine engine with low stage count low pressure turbine |
| 01/17/2013 | US20130014489 Gas turbine engine with low stage count low pressure turbine |
| 01/17/2013 | US20130014488 Efficient, low pressure ratio propulsor for gas turbine engines |
| 01/16/2013 | EP2546658A1 Method for determining the air speed of an aircraft and aircraft provided with a means for implementing same |
| 01/16/2013 | CN1779225B Methods and systems for operating oxidizer systems |
| 01/16/2013 | CN101326138B Metal part and brazed joint of metal part produced from ceramic material |
| 01/10/2013 | US20130008147 Aircraft gas turbine with variable bypass nozzle |
| 01/10/2013 | US20130008146 Efficient, low pressure ratio propulsor for gas turbine engines |
| 01/10/2013 | US20130008144 Efficient, low pressure ratio propulsor for gas turbine engines |
| 01/10/2013 | DE102011106964A1 Gas turbine engine, particularly turbomachine for aircraft, has fan, core engine surrounded by adjacent flow channel and cladding element comprising exhaust area, where cladding element is supported elastically on turbine housing |
| 01/10/2013 | DE102011106961A1 Flight gas turbine engine i.e. turbomachine, has flow guide element designed as radiator element, and core thruster surrounded by by-pass channel, where partial flow is conducted from channel through engine casing for cooling core thruster |
| 01/10/2013 | DE102011106959A1 Fluggasturbine mit variabler Nebenstromdüse Aircraft gas turbine with variable Nebenstromdüse |
| 01/09/2013 | EP2543868A2 Turbofan engine |
| 01/09/2013 | EP2543867A2 Efficient, low pressure ratio propeller for gas turbine engines |
| 01/09/2013 | EP2543866A2 Propulsion fan for gas turbine engines |
| 01/09/2013 | EP2543865A2 Turbofan engine with heat exchanger on the core engine housing |
| 01/09/2013 | EP2543829A2 Fan Stagger Angle for Dirt Rejection |
| 01/09/2013 | EP2543820A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 01/09/2013 | EP2543819A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 01/09/2013 | EP2542772A1 Flow mixer and corresponding gas turbine engine |
| 01/09/2013 | EP2542470A1 Counterweight-based device for controlling the orientation of fan blades of a turboprop engine |
| 01/09/2013 | CN102869570A Counterweight-based device for controlling the orientation of fan blades of a turboprop engine |
| 01/08/2013 | US8347601 Device for pivoting at least one pivotable element in a gas turbine engine |
| 01/03/2013 | US20130000273 Gas-driven propulsor with tip turbine fan |
| 01/02/2013 | EP2540991A2 Mechanism for turbine engine start from low spool |
| 01/02/2013 | EP2540974A2 Fan blade with sheath |
| 01/02/2013 | CN102852567A Energy-saving method by adopting jetting exhausting in thermal process |
| 01/01/2013 | US8341935 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 12/27/2012 | WO2012175864A1 Dual-flow turbine engine having a decoupling device |
| 12/27/2012 | WO2012175863A2 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine |
| 12/27/2012 | CA2839459A1 Dual-flow turbine engine having a decoupling device |
| 12/27/2012 | CA2837829A1 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine |
| 12/25/2012 | US8336290 Pitch change apparatus for counter-rotating propellers |
| 12/25/2012 | US8336289 Gas turbine engine systems and related methods involving multiple gas turbine cores |
| 12/25/2012 | US8336288 Gas-turbine engine in particular aircraft engine |
| 12/20/2012 | WO2012174247A1 Aircraft powerplant |
| 12/20/2012 | US20120317957 Aircraft powerplant |
| 12/20/2012 | DE102011077502A1 Device for connecting inner wall and outer wall of bypass filter channel of turbojet engine unit, has two wall-like supporting elements, which are partially arranged in assembled state in direction of fluid flow in bypass filter channel |
| 12/20/2012 | CA2839412A1 Aircraft powerplant |
| 12/19/2012 | EP2535548A2 Turbine section of high bypass turbofan |
| 12/19/2012 | EP2535519A2 A retention device for a rotating blade |
| 12/19/2012 | EP2535518A2 Blade mounting system |
| 12/19/2012 | CN202611925U Engine of high-thrust aircraft |
| 12/18/2012 | CA2460598C Confluent variable exhaust nozzle |
| 12/14/2012 | CA2778584A1 Mounting system |
| 12/13/2012 | US20120315141 Flow mixer |
| 12/12/2012 | CN101230789B Turbo-propeller comprising a propeller formed by blades with adjustable orientation |
| 12/11/2012 | CA2506208C Device for fastening a fluid conduit onto the casing of a turbojet engine |
| 12/06/2012 | WO2012164228A1 Gas turbine engine comprising three rotary bodies |
| 12/06/2012 | WO2012164224A1 Turbomachine with blow‑off valves located at the intermediate case |
| 12/06/2012 | WO2012164204A1 Turbomachine fan case |
| 12/06/2012 | WO2012163667A1 Adiabatic compressed air storage power plant |
| 12/06/2012 | US20120304621 Clamping system and method for thrust reverser attachment |
| 12/06/2012 | US20120304619 Engine for thrust or shaft output and corresponding operating method |
| 12/06/2012 | CA2837476A1 Gas turbine engine comprising three rotary bodies |
| 12/06/2012 | CA2837258A1 Turbomachine fan case |
| 12/05/2012 | EP2530283A1 Adiabatic pressurised air storage power plant |
| 11/28/2012 | CN102797515A Method for saving energy through injection air suction in thermodynamic process |
| 11/28/2012 | CN101469647B Turbojet engine suspended from a support strut of an aircraft |
| 11/27/2012 | CA2512375C Turbojet with means of protection for a fuel injection unit, the injection unit and the turbojet undershield |
| 11/22/2012 | US20120291416 Crack and Delamination Stoppers For Aircraft Propulsion System Components |
| 11/21/2012 | EP2525046A2 Propulsion engine |
| 11/21/2012 | CN102787945A Secondary booster jet engine |
| 11/15/2012 | WO2012153074A1 Tail cone for a microjet rotary turbine engine |
| 11/15/2012 | WO2012097797A3 Heat exchanger and jet engine comprising same |
| 11/15/2012 | CA2835353A1 Tail cone for a microjet rotary turbine engine |
| 11/14/2012 | EP2521851A1 Contra-rotating propeller system for an aircraft turbine engine |
| 11/14/2012 | CN101297107B Turbofan engine for stol aircraft |
| 11/13/2012 | US8307658 Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct |
| 11/13/2012 | US8307628 Rear fan case for a gas turbine engine |
| 11/13/2012 | CA2440529C Counter rotating fan aircraft gas turbine engine with aft booster |
| 11/08/2012 | US20120279198 Gas turbine engine with bypass mixer |
| 11/07/2012 | EP2520763A2 Impeller |
| 11/07/2012 | EP2519723A2 Gas turbine engine and heat exchange system |
| 11/01/2012 | WO2012147802A1 Moulded article |
| 11/01/2012 | CA2832743A1 Molded part |
| 10/31/2012 | EP2518296A2 Fan drive gear system integrated carrier and torque frame |
| 10/31/2012 | EP2518293A2 Multiple core variable cycle gas turbine engine and method of operation |
| 10/31/2012 | EP2518279A2 Fan drive planetary gear system integrated carrier and torque frame |
| 10/30/2012 | US8297039 Propulsion engine |
| 10/26/2012 | WO2012118994A3 Fault tolerant control system for distributed micro-thrusters |
| 10/26/2012 | WO2012087952A3 Method and tooling for partial disassembly of a bypass turbofan engine |
| 10/23/2012 | US8291690 Gas turbine engine with variable area fan nozzle positioned for starting |
| 10/23/2012 | US8291689 Corrugated core cowl for a gas turbine engine |
| 10/18/2012 | US20120260623 Coupling shaft for gas turbine fan drive gear system |
| 10/16/2012 | US8290683 Apparatus and method for reducing aircraft fuel consumption |
| 10/16/2012 | US8286654 Gas turbine engine inlet with noise reduction features |
| 10/16/2012 | US8286415 Turbofan engine having inner fixed structure including ducted passages |
| 10/16/2012 | CA2650511C Fan rotating blade for turbofan engine |
| 10/11/2012 | US20120259483 Actuation control system |
| 10/11/2012 | US20120255276 Load limited actuator |
| 10/10/2012 | CN101457771B Abradable support panel in a turbine engine |
| 10/09/2012 | US8285467 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine |
| 10/09/2012 | CA2637277C Fan blade retaining structure |
| 10/09/2012 | CA2512377C Turbojet with a guard plate to protect burner ring fuel rail, the burner ring and the guard plate |
| 10/04/2012 | US20120247083 Porous core cowling for a turbojet engine |
| 10/04/2012 | DE102011015703A1 Method for integrating intercooler in compression process of thermal turbomachine e.g. turbofan engine, involves redirecting and rerouting compressor air in fan housing into engine after air is flowed through fan stator |
| 10/04/2012 | DE102011006241A1 Vorrichtung zum Mischen von Treibstoff und Luft eines Strahltriebwerks Apparatus for mixing fuel and air in a jet engine |