Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
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04/26/2012 | CA2813553A1 Locking device with mechanical detection of closing and opening |
04/25/2012 | EP2443034A2 Method for installing heat shielding on a fixed internal structure of a jet engine nacelle |
04/25/2012 | EP2178761B1 Locking device |
04/24/2012 | CA2489717C Drain specifically for jet engine support strut |
04/24/2012 | CA2457289C Load-bearing structure for a turboprop and assembly comprising such a load-bearing structure |
04/19/2012 | US20120091270 Aircraft configuration |
04/18/2012 | EP2442285A1 Wireless engine monitoring system |
04/18/2012 | EP2441674A1 Aircraft nacelle including a rear frame tilted towards the rear |
04/04/2012 | EP2435307A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors |
03/29/2012 | WO2012037988A1 Nacelle with hinged cowl doors enabling access to the engine |
03/29/2012 | CA2812580A1 Nacelle with hinged cowl doors enabling access to the engine |
03/28/2012 | CN102395509A Actuator system for a mobile panel of a nacelle of a turbojet |
03/21/2012 | EP2331404B1 Device for centering an air inlet structure on a central structure of a nacelle |
03/14/2012 | EP2117932B1 Nacelle for the jet engine of an aircraft |
03/14/2012 | CN202163619U 闩锁装置 Latch means |
03/06/2012 | CA2657254C Nacelle inlet lip |
02/29/2012 | EP2152582B1 Propulsion assembly for aircraft with sliding nacelle |
02/22/2012 | EP2420447A2 Capacitive sensors for monitoring load bearing on pins |
02/22/2012 | EP2419330A1 Actuator system for a mobile panel of a nacelle of a turbojet |
02/08/2012 | EP2414228A2 Rear section of an aircraft including an engine mounting structure swingably mounted on the fuselage |
02/08/2012 | CN102348600A Aircraft nacelle comprising a reinforced outer wall |
02/01/2012 | EP2411281A2 Aircraft nacelle comprising a reinforced outer wall |
02/01/2012 | EP2310269B1 Device for shrouding an aircraft nacelle |
01/26/2012 | WO2012010774A2 Turbojet engine nacelle |
01/25/2012 | EP2409921A2 Nacelle for Aircraft |
01/25/2012 | CN102333697A Turbojet engine nacelle with a removable air intake structure |
01/18/2012 | CN102320377A Anti-collision aircraft engine |
01/11/2012 | CN102317161A Method for closing a mobile cradle element |
01/11/2012 | CN102310947A Manufacturing method for a rib of an aerodynamic engine strut fairing involving superplastic forming and splicing |
01/05/2012 | WO2012001259A1 Turbojet engine nacelle |
01/05/2012 | US20120001019 Pylon for attaching a gas turbine engine |
01/05/2012 | CA2803307A1 Turbojet engine nacelle |
01/04/2012 | EP2402251A2 A jet engine installation |
01/04/2012 | EP2402250A2 Pylon for attaching a gas turbine engine |
01/04/2012 | EP2401202A1 Turbojet engine nacelle with a removable air intake structure |
01/04/2012 | EP2313317B1 Device for shrouding an aircraft nacelle |
01/04/2012 | CN102307784A Turbojet engine nacelle |
01/03/2012 | CA2472876C Turbojet nacelle hood locking mechanism |
12/28/2011 | EP2399827A2 Guide system for nacelle assembly |
12/28/2011 | EP2398707A1 Method for closing a mobile cradle element |
12/28/2011 | CN102301122A 用于飞行器发动机机舱的声衰减板 Sound attenuation for aircraft engine nacelle board |
12/22/2011 | WO2011157953A1 Air inlet duct for a turbojet nacelle |
12/21/2011 | EP2397410A1 Fusible link device between a mobile part and a stationary part of an aircraft nacelle |
12/21/2011 | EP2162359B1 Nacelle rear assembly for turbojet engine |
12/14/2011 | EP2393713A2 Turbojet engine nacelle |
12/14/2011 | EP2393712A1 Suspension assembly for an aircraft turbojet engine |
12/13/2011 | CA2507168C Engine nacelle for a supersonic aircraft |
12/08/2011 | WO2011151577A2 Turbojet engine nacelle including a device for absorbing circumferential stresses |
12/08/2011 | US20110297787 Dual function door for an aircraft engine nacelle |
12/08/2011 | CA2801400A1 Turbojet engine nacelle including a device for absorbing circumferential stresses |
12/07/2011 | EP2392509A1 Dual function door for aircraft engine nacelle |
11/30/2011 | EP2390187A2 Manufacturing method for a rib of an aerodynamic engine strut fairing involving superplastic forming and splicing |
11/30/2011 | EP2390186A2 Manufacturing method for a rib of an aerodynamic engine strut fairing involving superplastic forming and splicing |
11/30/2011 | EP2222560B1 Aircraft nacelle guidance system installation |
11/30/2011 | EP2178760B1 Jet engine nacelle intended to equip an aircraft |
11/24/2011 | US20110284686 Suspension assembly for an aircraft turbojet engine |
11/23/2011 | EP2388193A2 Guide system for nacelle assembly |
11/16/2011 | EP2181040B1 Device for controlling maintenance actuators of the cowlings of a turbojet engine nacelle |
11/16/2011 | CN102245473A Overpressure hatch intended to be mounted on a wall of a turbojet engine nacelle |
11/10/2011 | WO2011138571A1 Unit for an aircraft thruster |
11/10/2011 | WO2011107682A3 Turbojet engine nacelle provided with a cooling assembly for cooling a component |
11/03/2011 | WO2011135217A1 Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle |
11/03/2011 | WO2011135214A1 Nacelle for an aircraft engine |
11/03/2011 | WO2011135213A1 Nacelle for an aircraft engine |
11/02/2011 | EP2383442A2 Gas turbine engine |
11/02/2011 | EP2057071B1 Locking system for a movable nacelle cowl |
10/27/2011 | WO2011131874A1 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
10/27/2011 | WO2011131873A1 Nacelle for an aircraft engine with variable cross-section nozzle |
10/27/2011 | CA2795691A1 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
10/27/2011 | CA2792968A1 Nacelle for an aircraft engine with variable cross-section nozzle |
10/13/2011 | US20110250054 Device for controlling maintenance actuators for the cowlings of a turbojet engine nacelle |
10/12/2011 | CN202006875U Ducted fan |
10/12/2011 | CN102216158A Air intake for an aeroplane engine with unducted propellers |
10/06/2011 | WO2011123392A2 Unitized engine nacelle structure |
10/06/2011 | US20110240137 Overpressure hatch intended to be mounted on a wall of a turbojet engine nacelle |
10/06/2011 | CA2794770A1 Unitized engine nacelle structure |
10/05/2011 | EP2371714A2 Non-circular aft nacelle cowling geometry |
10/05/2011 | EP2370674A1 Nacelle and method of assembling the same |
10/05/2011 | CN102209667A Turbojet engine nacelle with translatable upstream cowl |
09/29/2011 | WO2011117521A1 Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly |
09/28/2011 | CN102202974A Turbojet engine nacelle |
09/28/2011 | CN102202973A Airplane having engines partially encased in the fuselage |
09/22/2011 | WO2011115792A1 Latch with adjustable handle |
09/14/2011 | CN102186724A Nacelle air intake structure |
09/13/2011 | US8016227 Non-handed engine cowl doors for fuselage mounted turbine engines |
09/09/2011 | WO2011107682A2 Turbojet engine nacelle component cooling assembly |
09/09/2011 | WO2011070260A3 Assembly for holding the interface of stationary outer structure of a nacelle and housing of a jet engine |
09/09/2011 | CA2786542A1 Turbojet engine nacelle provided with a cooling assembly for cooling a component |
09/06/2011 | CA2485322C Soundproofing panels with beads and process for producing the said panels |
08/31/2011 | EP2288543B1 Aircraft engine nacelle air intake assembly |
08/31/2011 | EP2190741B1 Jet engine nacelle with dampers for half-shells |
08/31/2011 | CN201951712U Saucer-shaped aircraft |
08/31/2011 | CN102171101A Air intake structure for a turbine engine nacelle |
08/31/2011 | CN102171100A Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut |
08/30/2011 | CA2485242C Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
08/24/2011 | CN102164820A Turbojet engine nacelle |
08/17/2011 | EP2356028A1 Overpressure hatch intended to be mounted on a wall of a turbojet engine nacelle |
08/17/2011 | EP2247912B1 Air intake, in particular for an aircraft chaff dispenser |
08/17/2011 | CN102159460A Rear part of an aircraft comprising two semi-structures for supporting engines mounted one on the other in an inside space of an aircraft |
08/03/2011 | EP2350439A1 Method for optimising the shape of an aerofoil and corresponding aerofoil |