| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
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| 04/15/2009 | EP2046638A1 Structural element of an aircraft |
| 04/15/2009 | CN101410300A Air inlet shroud structure |
| 04/15/2009 | CN101410294A Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel |
| 04/14/2009 | US7516918 Morphable ceramic composite skins and structures for hypersonic flight |
| 04/09/2009 | WO2009043635A1 Locking device comprising a telescopic connecting rod equipped with return means |
| 04/09/2009 | CA2696831A1 Locking device comprising a telescopic connecting rod equipped with return means |
| 04/02/2009 | WO2009042549A2 Method for manufacturing and attachment of wing fairings |
| 04/02/2009 | US20090084889 Aircraft having a reduced acoustic signature |
| 04/01/2009 | EP2042429A2 Force sensing clevis insert |
| 04/01/2009 | EP2041399A2 Aircraft engine inlet having zone of deformation |
| 03/26/2009 | WO2009037267A1 Lower rear aerodynamic fairing for an aircraft engine attachment device |
| 03/26/2009 | CA2699840A1 Lower rear aerodynamic fairing for an aircraft engine attachment device |
| 03/25/2009 | EP2038176A1 Engine assembly for aircraft comprising an aerodynamic coupling fairing mounted on two separate elements |
| 03/24/2009 | CA2639762A1 Member for locking ring sectors onto a turbomachine casing, comprising means allowing it to be grasped |
| 03/19/2009 | US20090072079 Aircraft having a pivotable powerplant |
| 03/18/2009 | EP2035279A1 Structural nacelle |
| 03/12/2009 | WO2009030836A2 Device for controlling maintenance actuators for the cowlings of a turbojet engine nacelle |
| 03/12/2009 | CA2693359A1 Device for controlling maintenance actuators for the cowlings of a turbojet engine nacelle |
| 03/11/2009 | EP2033893A2 Aircraft engine system with gearbox unit |
| 03/11/2009 | CN101384485A Turbojet engine nacelle with lateral opening of covers |
| 03/05/2009 | WO2009027591A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 03/05/2009 | WO2009027590A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | WO2009027589A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | WO2009027588A1 Locking device |
| 03/05/2009 | WO2009027587A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | WO2009027586A1 Locking device |
| 03/05/2009 | CA2696765A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | CA2696763A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | CA2696728A1 Locking device |
| 03/05/2009 | CA2696722A1 Jet engine nacelle intended to equip an aircraft |
| 03/05/2009 | CA2696718A1 Locking device |
| 03/05/2009 | CA2696393A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 03/04/2009 | EP2029429A2 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft |
| 02/26/2009 | WO2009024666A2 Actuator for opening an aircraft engine nacelle cowl |
| 02/26/2009 | WO2009024662A2 Coupling system connecting an internal structure and an external structure of a jet engine nacelle |
| 02/26/2009 | WO2009024661A2 Coupling device for connecting the two half-shells of an aircraft engine nacelle, and nacelle equipped with such a device |
| 02/26/2009 | WO2009024657A1 Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 02/26/2009 | WO2009024656A1 Device and method for controlling the power supply of at least one aircraft maintenance actuator |
| 02/26/2009 | WO2009024655A1 Attachment of a jet engine nacelle structure by means of a reinforced knife-edge/groove coupling |
| 02/26/2009 | WO2009024654A1 Jet engine nacelle with dampers for half-shells |
| 02/26/2009 | WO2009024487A1 Locking device designed to be arranged in a junction region of a nacelle |
| 02/26/2009 | WO2009024477A1 Locking device |
| 02/26/2009 | WO2009024470A1 Coupling device intended to connect first and second elements which are articulated with respect to one another |
| 02/26/2009 | WO2009024469A1 Nacelle equipped with a device for detecting the locking state of a locking device |
| 02/26/2009 | WO2009024461A1 Nacelle equipped with at least one excess pressure flap |
| 02/26/2009 | WO2009024431A1 Coupling device intended to connect first and second elements which can move relative to one another |
| 02/26/2009 | WO2009024428A1 A jet engine nacelle having dampers for half-shells |
| 02/26/2009 | WO2008151843A4 Engine nacelle of an aircraft comprising a vortex generator arrangement |
| 02/26/2009 | CA2696720A1 Locking device designed to be arranged in a junction region of a nacelle |
| 02/26/2009 | CA2696719A1 Locking device |
| 02/26/2009 | CA2696716A1 Coupling device intended to connect first and second elements which artsarticulated with respect to one another |
| 02/26/2009 | CA2696714A1 Nacelle equipped with a device for detecting the locking state of a locking device |
| 02/26/2009 | CA2696712A1 Nacelle equipped with at least one excess pressure flap |
| 02/26/2009 | CA2696710A1 Coupling device intended to connect first and second elements which cansmove relative to one another |
| 02/26/2009 | CA2696709A1 A jet engine nacelle having dampers for half-shells |
| 02/26/2009 | CA2696465A1 Actuator for opening an aircraft engine nacelle cowl |
| 02/26/2009 | CA2696461A1 Coupling device for connecting the two half-shells of an aircraft engine nacelle, and nacelle equipped with such a device |
| 02/26/2009 | CA2696359A1 Coupling system connecting an internal structure and an external structure of a jet engine nacelle |
| 02/26/2009 | CA2696358A1 Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 02/26/2009 | CA2696346A1 Jet engine nacelle with dampers for half-shells |
| 02/26/2009 | CA2696204A1 Attachment of a jet engine nacelle structure by means of a reinforced knife-edge/groove coupling |
| 02/26/2009 | CA2693352A1 Device and method for controlling the power supply of at least onr aircraft maintenance actuator |
| 02/26/2009 | CA2691283A1 Viscous shear damping strut assembly |
| 02/05/2009 | WO2008145832A3 Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device |
| 02/04/2009 | EP2019776A1 Aircraft comprising a device for reducing the induced drag |
| 02/04/2009 | EP2019775A1 Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel |
| 02/04/2009 | CN101360649A Fixing system for a component of a turbojet pod |
| 02/04/2009 | CN100457548C Non-axial-symmetry combination processing machine box |
| 01/27/2009 | CA2277783C Composite board with edge protection |
| 01/22/2009 | WO2008142242A3 Nacelle rear assembly for turbojet engine |
| 01/15/2009 | WO2009009732A1 Mechanical latch locking detection sensors |
| 01/14/2009 | EP2014550A2 Apparatus having inlet-mounted engine controls |
| 01/09/2009 | CA2637134A1 Device and method for protecting an aircraft component from collision with flying objects |
| 12/31/2008 | WO2008132297A3 Rear nacelle structure for a jet engine, such as a thrust reverser |
| 12/30/2008 | US7469528 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/18/2008 | WO2008151843A1 Engine nacelle of an aircraft comprising a vortex generator arrangement |
| 12/18/2008 | DE102007027697A1 Eddy generator arrangement for use at engine nacelle of aircraft, has eddy generators provided at side of engine nacelle at mutual distance from each other with respect to circumferential or longitudinal direction of engine nacelle |
| 12/10/2008 | EP1999022A1 Air inlet shroud structure |
| 12/09/2008 | US7461813 Air input device for a turboprop engine |
| 12/09/2008 | CA2538806C Annular acoustic panel |
| 12/04/2008 | WO2008145832A2 Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device |
| 12/04/2008 | WO2008145725A1 Propulsion assembly for aircraft with sliding nacelle |
| 12/04/2008 | CA2689111A1 Propulsion assembly for aircraft with sliding nacelle |
| 12/04/2008 | CA2688143A1 Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device |
| 12/03/2008 | EP1998012A2 Access door for gas turbine engine components |
| 11/27/2008 | WO2008142242A2 Nacelle rear assembly for turbojet engine |
| 11/27/2008 | CA2687454A1 Nacelle rear assembly for turbojet engine |
| 11/20/2008 | WO2008139048A2 Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 11/20/2008 | US20080283676 Variable contraction ratio nacelle assembly for a gas turbine engine |
| 11/18/2008 | CA2379192C Thrust reverser door emergency locking system |
| 11/13/2008 | US20080277529 Nacelle Cowling for Turbojet and Nacelle Comprising at Least One Such Cowling |
| 11/11/2008 | US7448573 Engine suspension pylon for aircraft |
| 11/06/2008 | WO2008132321A1 Lockable guiding system for a mobile part of a nacelle |
| 11/06/2008 | WO2008132297A2 Rear nacelle structure for a jet engine, such as a thrust reverser |
| 11/06/2008 | CA2677567A1 Lockable guiding system for a mobile part of a nacelle |
| 11/04/2008 | US7445179 Engine assembly for aircraft |
| 10/30/2008 | WO2008130739A1 Articles made from composite materials having toughened and untoughened regions |
| 10/30/2008 | CA2683851A1 Articles made from composite materials having toughened and untoughened regions |
| 10/29/2008 | EP1985870A2 A joint for a shape memory material |
| 10/29/2008 | EP1985537A2 Nacelle door arrangement |