| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
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| 07/27/2011 | EP2348171A1 Device for locking a structural element against an adjacent structure, aircraft equipped with said device and extraction method implemented by said device |
| 07/21/2011 | US20110174930 Fuse link device between a mobile part and a fixed part of an aircraft nacelle |
| 07/20/2011 | EP2344385A1 Turbojet engine nacelle with translatable upstream cowl |
| 07/20/2011 | EP2344384A1 Turbojet engine nacelle |
| 07/20/2011 | EP2344383A1 Air intake structure for a turbine engine nacelle |
| 07/20/2011 | EP2344382A1 Nacelle air intake structure |
| 07/20/2011 | EP2344381A1 Air intake for an aeroplane engine with unducted propellers |
| 07/20/2011 | CN102131704A Device for centering an air inlet structure on a central structure of a nacelle |
| 07/20/2011 | CN102131703A Device for shrouding an aircraft nacelle |
| 07/20/2011 | CN102131702A Device for shrouding an aircraft nacelle |
| 07/14/2011 | US20110168852 Method of depositing a coating for improving laminar flow |
| 07/13/2011 | EP2342128A1 Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut |
| 07/06/2011 | EP2340203A1 Airplane having engines partially encased in the fuselage |
| 07/06/2011 | EP2188177B1 Attachment of a jet engine nacelle structure by means of a reinforced knife-edge/groove coupling |
| 07/06/2011 | CN101472797B Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft |
| 06/30/2011 | US20110155847 Aft pylon fairing for an aircraft engine suspension system |
| 06/30/2011 | CA2725696A1 Turbomachine nacelle and anti-icing system and method therefor |
| 06/23/2011 | WO2011073551A1 Supporting structure for thrust reverser, in particular having cascades |
| 06/23/2011 | CA2780666A1 Supporting structure for thrust reverser, in particular having cascades |
| 06/22/2011 | EP2336500A2 Aircraft engine inlet having zone of deformation |
| 06/22/2011 | EP2336030A2 Hinge arm repair |
| 06/22/2011 | EP2334555A2 Rear part of an aircraft comprising two semi-structures for supporting engines mounted one on the other in an inside space of an aircraft |
| 06/21/2011 | CA2726503A1 Integrated nacelle assembly |
| 06/16/2011 | WO2011070266A1 Jet engine nacelle rear assembly |
| 06/16/2011 | WO2011070260A2 Assembly for holding the interface of stationary outer structure of a nacelle and housing of a jet engine |
| 06/16/2011 | US20110139940 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 06/16/2011 | US20110138578 Coupling for inducing high temperature drops between connected parts on an aircraft |
| 06/16/2011 | CA2780299A1 Jet engine nacelle rear assembly |
| 06/16/2011 | CA2777262A1 Assembly for holding the interface of stationary outer structure of a nacelle and housing of a jet engine |
| 06/15/2011 | EP2333288A2 Thermally actuated venting system for a compartment of an aircraft gas turbine engine |
| 06/15/2011 | EP2331404A1 Device for centering an air inlet structure on a central structure of a nacelle |
| 06/15/2011 | EP2146897B1 Fan casing made from composite materials having toughened and untoughened regions |
| 06/14/2011 | US7959106 Integrated propulsive system comprising a bypass turbojet engine |
| 06/08/2011 | EP2330037A2 Fan cowl support for a turbofan engine |
| 06/08/2011 | EP2330036A2 Fan cowl support for a turbofan engine |
| 06/08/2011 | EP2328808A1 Turbojet engine nacelle |
| 06/02/2011 | US20110127370 Fan cowl support for a turbo fan engine |
| 06/02/2011 | US20110127369 Fan cowl support cradle mounted on the attachment pylon and on the air inlet of the nacelle |
| 06/01/2011 | EP2327628A2 Methods and systems for minimizing flow disturbances in aircraft propeller blades caused by upstream pylons |
| 06/01/2011 | EP2327627A2 Aircraft de-icing device and engine nacelle of an aircraft turbine with a de-icing device |
| 06/01/2011 | CA2718684A1 Engine mount of aircraft and aircraft |
| 05/25/2011 | CN102076564A Fairing device for nacelle of an aircraft propulsion power unit |
| 05/19/2011 | US20110114796 Device for shrouding an aircraft nacelle |
| 05/19/2011 | DE102009053002A1 Exhaust outlet for lubricating oil system of aircraft engine, is arranged at exterior surface of engine- or engine mount lining, where region of exterior surface is limited to edge of outlet |
| 05/18/2011 | CN102066198A Aircraft engine nacelle air intake assembly |
| 05/12/2011 | WO2011055062A1 Engine pylon comprising a vortex generator, and method for the production thereof |
| 05/11/2011 | EP2319762A2 Linking device intended for mutually connecting first and second mobile elements |
| 05/11/2011 | EP2318683A2 Acoustic attenuation panel for aircraft engine nacelle |
| 05/11/2011 | EP2198143B1 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 05/11/2011 | EP2178751B1 Nacelle equipped with at least one excess pressure flap |
| 05/11/2011 | CN101484359B Aircraft engine assembly comprising a junction aerodynamic fairing mounted on two separate elements |
| 05/10/2011 | US7938359 Propulsion system with integrated pylon |
| 05/04/2011 | EP2317108A2 A boundary layer energiser |
| 04/27/2011 | EP2314509A2 Device for an aircraft propulsion unit |
| 04/27/2011 | EP2313317A1 Device for shrouding an aircraft nacelle |
| 04/20/2011 | EP2310269A1 Device for shrouding an aircraft nacelle |
| 04/20/2011 | EP2310267A1 Method for making deicing system on a nacelle panel |
| 04/20/2011 | CN201800919U Rainproof and dustproof protection structure of aircraft engine |
| 04/19/2011 | CA2389873C Procedure for producing a reinforced, acoustically resistive layer, the resistive layer so produced, and the panel that utilizes such a layer |
| 04/12/2011 | CA2412714C Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle |
| 04/06/2011 | EP2303693A1 Fairing device for nacelle of an aircraft propulsion power unit |
| 03/31/2011 | WO2011012822A3 Engine assembly for an aircraft of which the attachment strut comprises a structural case forming an internal radial delimitation of the secondary flow |
| 03/30/2011 | CN101992855A Airplane |
| 03/23/2011 | EP2178757B1 A jet engine nacelle having dampers for half-shells |
| 03/23/2011 | EP2178754B1 Nacelle comprising at least one overpressure valve |
| 03/16/2011 | EP2181039B1 Device and method for controlling the power supply of at least one aircraft maintenance actuator |
| 03/10/2011 | WO2010146287A3 Method for installing heat shielding on a fixed internal structure of a jet engine nacelle |
| 03/09/2011 | EP2291310A2 Coupling for inducing high temperature drops between connected parts on an aircraft |
| 03/02/2011 | EP2288797A1 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/02/2011 | EP2288543A1 Aircraft engine nacelle air intake assembly |
| 03/02/2011 | EP2288542A2 Aircraft propulsion system |
| 02/09/2011 | EP2282011A2 Cross-sectional profile of the supports or of the cover of the supports with supply lines of a Turbofan |
| 02/03/2011 | WO2011012822A2 Engine assembly for an aircraft of which the attachment strut comprises a structural case forming an internal radial delimitation of the secondary flow |
| 02/02/2011 | EP2279115A1 Impact resistant aircraft fuselage |
| 02/02/2011 | EP2190739B1 Lower rear aerodynamic fairing for an aircraft engine attachment device |
| 02/01/2011 | CA2420352C Fastener for attaching components to an aircraft structure |
| 01/27/2011 | US20110017866 Locking device |
| 01/26/2011 | EP2178752B1 Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 01/26/2011 | EP1633935B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 01/26/2011 | CN101959760A System for actuating and controlling the mobile cowling of a turbojet engine nacelle |
| 01/26/2011 | CN101087928B Static gas turbine component and method for repairing such a component |
| 01/25/2011 | CA2465324C Disengageable support for engine cowls |
| 01/20/2011 | WO2011007074A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
| 01/20/2011 | US20110014043 System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 01/20/2011 | CA2767870A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
| 01/12/2011 | CN101946081A System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 01/05/2011 | EP2179117B1 Locking device |
| 12/30/2010 | US20100327120 Air outlet system for aircraft leading edge |
| 12/23/2010 | WO2010146287A2 Method for installing heat shielding on a fixed internal structure of a jet engine nacelle |
| 12/23/2010 | WO2010109152A3 Aircraft nacelle comprising a reinforced outer wall |
| 12/23/2010 | CA2761666A1 Method for installing heat shielding on a fixed internal structure of a jet engine nacelle |
| 12/22/2010 | CN101925516A Guiding system for aircraft nacelle maintenance |
| 12/22/2010 | CN101925515A Locking system for air intake structure for turbojet engine nacelle |
| 12/15/2010 | CN101918276A Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 12/15/2010 | CN101913429A Aircraft engine nacelle with translating inlet cowl |
| 12/08/2010 | EP2146898B1 Rear lower aerodynamic fairing for the attachment device of an aircraft engine |
| 12/08/2010 | CN101910000A Nacelle for turbojet engine |
| 12/08/2010 | CN101909999A Locking system for air intake structure for turbojet engine nacelle |
| 12/08/2010 | CN101909998A Aircraft nacelle guidance system installation |
| 12/08/2010 | CN101909997A Twelve-hour structure for thrust reverser, in particular with grids |