Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701)
06/2010
06/02/2010EP2190741A1 Jet engine nacelle with dampers for half-shells
06/02/2010EP2190740A1 Nacelle equipped with a device for detecting the locking state of a locking device
06/02/2010EP2190739A1 Lower rear aerodynamic fairing for an aircraft engine attachment device
06/01/2010CA2369206C Device for attachment of an engine onto an aircraft nacelle stub
06/01/2010CA2364951C Procedure for manufacturing a protected laminated soundproofing panel and the acoustic panel produced by the procedure
05/2010
05/27/2010WO2010057627A1 Method for optimising the shape of an aerofoil and corresponding aerofoil
05/26/2010EP2188178A1 Jet engine nacelle intended to equip an aircraft
05/26/2010EP2188177A1 Attachment of a jet engine nacelle structure by means of a reinforced knife-edge/groove coupling
05/20/2010WO2010055224A1 Air intake for an aeroplane engine with unducted propellers
05/20/2010WO2010055220A1 Nacelle air intake structure
05/20/2010WO2010055217A1 Turbojet engine nacelle
05/20/2010WO2010055216A1 Turbojet engine nacelle with translatable upstream cowl
05/20/2010WO2010055213A1 System for controlling the cowl of a turbojet engine nacelle thrust reverser
05/20/2010CA2743009A1 Air intake for an aeroplane engine with unducted propellers
05/20/2010CA2740824A1 Turbojet engine nacelle with translatable upstream cowl
05/20/2010CA2740490A1 Turbojet engine nacelle
05/20/2010CA2736594A1 Nacelle air intake structure
05/20/2010CA2711945A1 System for controlling the cowl of a turbojet engine nacelle thrust reverser
05/14/2010WO2009138681A3 Turbojet engine nacelle downstream assembly
05/06/2010WO2010049610A1 Airplane having engines partially encased in the fuselage
05/06/2010CA2732664A1 Airplane having engines partially encased in the fuselage
05/05/2010EP2181269A2 Actuator for opening an aircraft engine nacelle cowl
05/05/2010EP2181040A2 Device for controlling maintenance actuators of the cowlings of a turbojet engine nacelle
05/05/2010EP2181039A1 Device and method for controlling the power supply of at least one aircraft maintenance actuator
05/05/2010EP2181038A1 Coupling device intended to connect first and second elements which are articulated with respect to one another
04/2010
04/28/2010EP2179119A1 Locking device comprising a telescopic connecting rod equipped with return means
04/28/2010EP2179118A1 Locking device
04/28/2010EP2179117A1 Locking device
04/28/2010EP2178761A1 Locking device
04/28/2010EP2178760A1 Jet engine nacelle intended to equip an aircraft
04/28/2010EP2178759A1 Locking device designed to be arranged in a junction region of a nacelle
04/28/2010EP2178758A1 Coupling device intended to connect first and second elements which can move relative to one another
04/28/2010EP2178757A1 A jet engine nacelle having dampers for half-shells
04/28/2010EP2178756A2 Coupling device for connecting the two half-shells of an aircraft engine nacelle, and nacelle equipped with such a device
04/28/2010EP2178755A2 Coupling system connecting an internal structure and an external structure of a jet engine nacelle
04/28/2010EP2178754A1 Nacelle comprising at least one surge trap
04/28/2010EP2178753A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
04/28/2010EP2178752A1 Rear section of aircraft nacelle and nacelle equipped with such rear section
04/28/2010EP2178751A1 Nacelle equipped with at least one excess pressure flap
04/27/2010US7703716 Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device
04/15/2010WO2010040907A1 Air intake structure for a turbine engine nacelle
04/15/2010CA2733602A1 Air intake structure for a turbine engine nacelle
04/08/2010WO2010037923A1 Turbojet engine nacelle
04/08/2010WO2010037917A1 Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut
04/08/2010CA2735951A1 Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut
04/08/2010CA2735530A1 Turbojet engine nacelle
03/2010
03/31/2010EP2167380A1 Engine nacelle of an aircraft comprising a vortex generator arrangement
03/31/2010CN101687542A Engine nacelle of an aircraft comprising a vortex generator arrangement
03/30/2010CA2293076C Fan and compressor noise attenuation
03/25/2010WO2010031958A2 Rear part of an aircraft comprising two semi-structures for supporting engines mounted one on the other in an inside space of an aircraft
03/25/2010WO2010031910A1 Method for monitoring the seals in a turbojet engine nacelle
03/25/2010US20100072324 Nacelle for double flow engine
03/25/2010CA2736911A1 Rear part of an aircraft comprising two semi-structures for supporting engines mounted one on the other in an inside space of an aircraft
03/24/2010CN101680252A Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device
03/24/2010CN101678898A Nacelle rear assembly for turbojet engine
03/24/2010CN101678897A Propulsion assembly for aircraft with sliding nacelle
03/23/2010US7681833 Turboprop unit for aircraft with improved aerodynamic installation
03/17/2010EP2162359A2 Nacelle rear assembly for turbojet engine
03/11/2010WO2010026302A1 Device for centering an air inlet structure on a central structure of a nacelle
03/11/2010US20100059634 Locking system for a movable nacelle cowl
03/11/2010US20100059624 Aircraft comprising a device for reducing the induced drag
03/11/2010CA2734416A1 Device for centering an air inlet structure on a central structure of a nacelle
03/03/2010EP2158370A2 Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device
02/2010
02/25/2010US20100044503 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle
02/25/2010US20100044502 Beam mounted rear propulsion system for an aircraft and aircraft with such system
02/24/2010EP1999022B1 Air inlet shroud structure
02/18/2010WO2010019131A1 Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
02/17/2010EP2152582A1 Propulsion assembly for aircraft with sliding nacelle
02/16/2010CA2503068C Transition block between the means used to attach a wing to an aircraft fuselage and the said wing, and the aircraft equipped with such a block
02/04/2010WO2010012900A2 Acoustic attenuation panel for aircraft engine nacelle
02/04/2010WO2010012899A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
02/04/2010WO2009140042A4 Combination spar and trunnion structure for a tilt rotor aircraft
02/04/2010US20100024435 Nacelle for turbofan
02/04/2010CA2732351A1 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
02/04/2010CA2731974A1 Acoustic attenuation panel for aircraft engine nacelle
01/2010
01/28/2010US20100019102 Gas turbine engine nacelle
01/28/2010US20100019081 Airplane with pitch and yaw command by propulsion system
01/27/2010EP2146898A1 Rear lower aerodynamic fairing for the attachment device of an aircraft engine
01/27/2010EP2146897A1 Articles made from composite materials having toughened and untoughened regions
01/21/2010WO2010007313A1 Device for shrouding an aircraft nacelle
01/21/2010WO2010007311A1 Device for shrouding an aircraft nacelle
01/21/2010WO2010007258A1 Aircraft engine nacelle air intake assembly
01/21/2010WO2010007226A2 Aircraft propulsion system
01/21/2010WO2010007218A1 Fairing device for nacelle of an aircraft propulsion power unit
01/21/2010CA2731132A1 Device for shrouding an aircraft nacelle
01/21/2010CA2731131A1 Device for shrouding an aircraft nacelle
01/21/2010CA2728743A1 Aircraft propulsion system
01/21/2010CA2728700A1 Fairing device for nacelle of an aircraft propulsion power unit
01/21/2010CA2727864A1 Aircraft engine nacelle air intake assembly
01/14/2010WO2010004076A2 Device for an aircraft propulsion unit
01/14/2010WO2009138833A3 Coupling for inducing high temperature drops between connected parts on an aircraft
01/07/2010WO2010001009A2 Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
01/07/2010WO2010000953A1 Nacelle for turbojet engine
01/07/2010US20100001123 Translatable thrust inverter for jet engine
01/07/2010DE102008027275A1 Air-breathing nacelle for aircraft engine, has circular front contour and sucking unit that is provided for sucking air into nacelle, where sucking unit comprises turbocharger with fan and turbine
01/07/2010CA2711604A1 Nacelle for turbojet engine
01/06/2010EP2139770A2 Rear nacelle structure for a jet engine, such as a thrust reverser
12/2009
12/30/2009WO2009115674A3 Air intake for aircraft engine nacelle, and nacelle equipped with such air intake
12/30/2009WO2009115662A8 System for actuating and controlling the mobile cowling of a turbojet engine nacelle
12/30/2009EP1984248B1 Turbojet engine nacelle with cowls opening laterally
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