Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701)
12/2012
12/06/2012WO2012163538A1 Gas-turbine engine with a telescopic air inlet in the engine lining
12/06/2012DE102011103163A1 Gasturbinentriebwerk mit teleskopartigem Lufteinlass der Triebwerksverkleidung Gas turbine engine with telescopic air intake of the engine cowling
12/06/2012CA2837635A1 Nacelle for an aircraft bypass turbojet engine
12/06/2012CA2837439A1 Assembly for an aircraft nacelle
12/06/2012CA2778592A1 Clamping system and method for thrust reverser attachment
12/05/2012EP2530016A2 Aircraft engine cowl and process therefor
12/05/2012CN102806666A Polymer composite materials and processes therefor
11/2012
11/30/2012CA2778521A1 Aircraft engine cowl and process therefor
11/21/2012CN101772454B Nacelle comprising at least one surge trap
11/21/2012CN101506045B Locking system for a movable nacelle cowl
11/14/2012EP2522575A2 Device for attaching an aircraft engine, comprising clamping wedges for engine attachment with corner effect
11/14/2012CN102774502A Device for attaching an aircraft engine, comprising clamping wedges for engine attachment with corner effect
11/14/2012CN101784736B Locking device comprising a telescopic connecting rod equipped with return means
11/08/2012US20120280090 Connecting device particularly adapted for the connection between an air intake and an engine of an aircraft nacelle
11/07/2012CN202518455U Fireproof and heat-insulation structure of engine nacelle and wing connecting region
11/01/2012WO2012147802A1 Moulded article
11/01/2012US20120273610 Engine pylon comprising a vortex generator, and method for the production thereof
11/01/2012CA2832743A1 Molded part
10/2012
10/26/2012WO2012104561A3 Nacelle with articulated fan casing covers
10/24/2012EP2512928A1 Supporting structure for thrust reverser, in particular having cascades
10/17/2012EP2509870A1 Jet engine nacelle rear assembly
10/17/2012CN101801789B Lower rear aerodynamic fairing for an aircraft engine attachment device
10/09/2012CA2510673C Multi-engine aircraft with a vertical shaft
10/04/2012WO2012131230A1 Locking device with mechanical detection of closure and opening
10/04/2012WO2012131209A1 Anti-fire seal assembly and nacelle comprising such a seal
10/04/2012US20120248284 Supporting structure for thrust reverser, in particular having cascades
10/04/2012CA2829267A1 Anti-fire seal assembly and nacelle comprising such a seal
10/04/2012CA2828924A1 Locking device with mechanical detection of closure and opening
10/03/2012CN102713205A Turbojet engine nacelle component cooling assembly
09/2012
09/26/2012EP2501614A2 Attachment system for mounting an engine nacelle structure onto the body of an engine
09/26/2012CN202449214U Protective cover
09/26/2012CN101198785B Control system for the nacelle of a turboreactor
09/25/2012CA2638706C Linear acoustic liner
09/13/2012WO2011151577A3 Turbojet engine nacelle including a device for absorbing circumferential stresses
09/12/2012EP2496472A1 Engine pylon comprising a vortex generator, and method for the production thereof
09/05/2012EP2495402A2 Fan casing for a turbofan engine
09/05/2012EP2495401A2 A turbomachine casing assembly
09/05/2012EP2495400A2 A turbomachine casing assembly
09/05/2012CN102656087A Supporting structure for thrust reverser, in particular having cascades
08/2012
08/30/2012US20120217372 Assembly for holding the interface of stationary outer structure of a nacelle and housing of a jet engine
08/22/2012CN102648128A Jet engine nacelle rear assembly
08/22/2012CN102648125A Engine pylon comprising a vortex generator, and method for the production thereof
08/21/2012US8245966 Airship and vectored propeller drive therefor
08/09/2012WO2012104561A2 Nacelle with articulated fan casing covers
08/08/2012CN102627146A Tilt rotor aircraft with fixed engine arrangement
08/02/2012WO2012101364A1 Process of manufacturing a turbojet engine nacelle part
08/02/2012CA2825116A1 Process of manufacturing a turbojet engine nacelle part
08/01/2012EP2481669A2 Attenuation of open rotor noise
08/01/2012EP2344381B1 Air intake for an aeroplane engine with unducted propellers
08/01/2012CN102616382A Connecting device mainly suitable for connecting an engine of an aircraft nacelle and an air intake pipe
07/2012
07/31/2012CA2500957C Air intake structure for aircraft engine
07/24/2012US8226027 Engine assembly for aircraft with sliding nacelle
07/24/2012CA2669280C Turbofan gas turbine engine and nacelle arrangement
07/19/2012WO2012095602A1 Method for repairing at least a portion of an acoustic panel for a nacelle
07/19/2012WO2012095600A1 Device for linking a front frame to a fan casing
07/19/2012CA2824005A1 Device for linking a front frame to a fan casing
07/19/2012CA2823857A1 Method for repairing at least a portion of an acoustic panel for a nacelle
07/18/2012CN102596721A Assembly for holding the interface of stationary outer structure of a nacelle and housing of a jet engine
07/17/2012US8220739 Beam mounted rear propulsion system for an aircraft and aircraft with such system
07/17/2012US8220738 Nacelle and method of assembling the same
07/11/2012EP2242921B1 Control system for turbojet engine nacelle
07/11/2012CN202320774U 未来救援隐身航母所载短体飞机 Short-body aircraft coming out of stealth aircraft rescue
07/11/2012CN102563149A Spring loaded pressure relief door for a nacelle cowl
06/2012
06/27/2012EP2179119B1 Locking device comprising a telescopic connecting rod equipped with return means
06/27/2012CN101535122B Structural element of an aircraft
06/21/2012WO2012080617A1 Fibrous structure for a part made of composite material having one or more arch-shaped portions
06/21/2012WO2012080604A1 Nacelle for a bypass turbojet engine
06/21/2012CA2820774A1 Nacelle for a bypass turbojet engine
06/21/2012CA2820415A1 Fibrous structure for a part made of composite material having one or more arch-shaped portions
06/20/2012CN102501977A Engine fairing
06/20/2012CN101448701B Aircraft comprising a device for reducing the induced drag
06/14/2012CA2758211A1 Aircraft comprising a reversible rotary electrical machine
06/06/2012EP2459445A2 Engine assembly for an aircraft of which the attachment strut comprises a structural case forming an internal radial delimitation of the secondary flow
06/05/2012US8191822 Device for an aircraft power unit
06/05/2012CA2470926C Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls
05/2012
05/31/2012WO2012071339A1 Inlet nose cowl with uninterrupted airflow surface
05/31/2012US20120132749 Tail-cone of an aircraft with movable fairing
05/30/2012CN102481981A 其发动机附连支柱包括形成次级气流的内半径定界的结构壳体的用于飞行器的发动机组件 Its engine attachment strut includes an engine assembly for aircraft structures within a radius of the secondary airflow is formed a housing delimited
05/24/2012WO2012066211A1 Turbojet engine nacelle reinforcing structure
05/24/2012CA2816455A1 Turbojet engine nacelle reinforcing structure
05/23/2012EP2455281A2 Spring loaded pressure relief door for a nacelle cowl
05/23/2012EP2454154A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine
05/23/2012CN102470929A Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine
05/23/2012CN101384485B Turbojet engine nacelle with lateral opening of covers
05/22/2012US8181912 Engine pod for an aircraft with a vortex generator arrangement
05/16/2012CN102458991A Method for installing heat shielding on a fixed internal structure of a jet engine nacelle
05/15/2012CA2485435C Device for assembly of a shroud placed between an aircraft engine air intake and a pylon
05/10/2012US20120111995 Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow
05/09/2012EP2450861A1 Wireless engine monitoring system
05/09/2012CN202213711U Low-emission silenced civil aircraft for short and medium voyages
05/09/2012CN102448822A Aircraft engine nacelle comprising a mobile cowl moved by electric motors
05/03/2012WO2012056155A2 Leading edge structure, in particular for an air inlet of an aircraft engine nacelle
05/03/2012CA2813925A1 Leading edge structure, in particular for an air inlet of an aircraft engine nacelle
05/02/2012EP2447519A2 Gas turbine engine with variable area fan nozzle
05/02/2012EP2447159A2 Aircraft cowl including a means for limiting pneumatic scoop phenomena
05/02/2012EP2447158A2 Aircraft cowl including a means for limiting magnetic scoop phenomena
05/02/2012EP2179118B1 Locking device
05/02/2012CN101541635B Nacelle for turbofan
05/02/2012CN101528543B Side-opening jet engine nacelle
04/2012
04/26/2012WO2012052643A1 Locking device with mechanical detection of closing and opening
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