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2016
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Invention
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Thrust reverser of a turbofan pod comprising a single control for movable cowlings and a variable... |
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Invention
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Door-type thrust reverser device for aircraft turbojet engine nacelle. A door-type thrust reverse... |
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Invention
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System for locking a thrust reverser with flaps, comprising locks for an intermediate opening pos... |
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Invention
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Thrust reverser of a turbojet engine nacelle, comprising control cylinders of movable cowls and a... |
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Invention
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Device for de-icing an aircraft turbojet engine nacelle air intake lip. The invention relates to ... |
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Invention
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Woven preform for producing a circumferential or toroidal reinforcement having an omega-shaped cr... |
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Invention
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Use of a code for marking a nacelle.
An automatic identification device is provided on a surface... |
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Invention
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Hydraulic control for a thrust reverser of a turbojet engine, including a variable-displacement m... |
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Invention
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Device and assembly for non-destructive testing of a composite part and method for non-destructiv... |
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Invention
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Method for repairing sandwich panels made of composite materials involving the creation of a core... |
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Invention
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Device for de-icing the inlet of a nacelle of an aircraft engine, method for producing such a de-... |
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Invention
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Method for assessing the damage to a paint-covered composite material, measuring two separate cri... |
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Invention
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Nacelle for an aircraft engine with variable section nozzle. The present disclosure concerns a na... |
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Invention
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Seal for a thrust reverser of a turbojet engine nacelle. The present disclosure relates to a seal... |
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Invention
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Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary gui... |
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Invention
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Nacelle with a thrust reverser device with maintained moveable cascades.
A thrust reverser devic... |
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Invention
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Unducted fan for an aircraft turbine engine. An unducted fan for an aircraft turbine engine, incl... |
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Invention
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Key tool and composite panel in particular for an aircraft engine nacelle manufactured by means o... |
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Invention
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Integrated thrust reverser device and aircraft engine nacelle equipped therewith. The present dis... |
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Invention
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Electric thrust reverser system for an aircraft engine nacelle and aircraft engine nacelle equipp... |
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Invention
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Nacelle for a turbojet engine with a variable nozzle. The present disclosure provides a turbojet ... |
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2015
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Invention
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Thrust reverser for a turbojet engine nacelle, comprising cascades partially integrated in the co... |
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Invention
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Assistance device for operating a cowl and a nacelle for turbojet engine equipped therewith.
An ... |
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Invention
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De-icing and conditioning device for an aircraft. The present disclosure provides a device for de... |
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Invention
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Control device for a turbojet engine thrust reverser, blocking the reverser. A control device for... |
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Invention
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Method for the repair of an acoustic panel made from composite material. The invention relates to... |
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Invention
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Method for characterising the thermal ageing of composite materials, especially composite materia... |
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Invention
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Turbojet engine nacelle including a thrust reversing device with doors, including inner flanks on... |
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Invention
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Turbojet engine nacelle thrust reverser comprising cascades secured to the mobile cowls.
A thrus... |
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Invention
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Propulsion unit for an aircraft.
An aircraft propulsion assembly including a turbojet nacelle, a... |
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Invention
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Device for displaying a luminous message on the fairing of an aircraft.
A device for displaying ... |
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Invention
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Nacelle for an aircraft turbojet engine with an extended front lip. A nacelle for an aircraft tur... |
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Invention
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Brazing without tools. A method for assembling a set including an inner wall, a shrouded outer wa... |
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Invention
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Nozzle for an aircraft turboprop engine with an unducted fan. The present disclosure provides a n... |
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Invention
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Aircraft element requiring an anti-frost treatment. The present disclosure provides an aircraft e... |
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Invention
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Cooling device for a turbojet engine of an aircraft nacelle.
The present disclosure provides a c... |
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Invention
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Mechanical inhibiting device integrated into a defence line of a thrust reverser.
The present di... |
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Invention
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Nacelle equipped with an oil-cooling circuit comprising an intermediate heat exchanger. The prese... |
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Invention
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Thrust reverser device. A thrust reverser device for an aircraft turbojet engine includes: a mova... |
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Invention
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Method for producing a honeycomb core panel. The invention concerns a method for producing a hone... |
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Invention
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Nacelle jet pipe devices for regulating pressure.
A nacelle jet pipe is equipped with a device f... |
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Invention
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Propulsion unit for an aircraft. The present disclosure relates to a propulsion unit for an aircr... |
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Invention
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Active lock with mobilization assistance and thrust reverser incorporating such a lock.
The pres... |
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Invention
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Turbojet engine nacelle comprising a unit assembly capable of moving along a guide assembly.
The... |
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Invention
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Fixed structure of a thrust reverser device. The present disclosure relates to a thrust reverser ... |
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Invention
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Front frame for a cascade thrust reverser structure. The present disclosure relates to a front fr... |
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Invention
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Cascade thrust reverser for an aircraft turbojet engine. The present disclosure relates to a casc... |
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2014
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Invention
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Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that i... |
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Invention
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Turbojet engine nacelle having a variable nozzle. A turbojet engine nacelle has a thrust reverser... |
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2013
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Invention
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Actuating device for moving a thrust reverser. The invention concerns an actuating device (1) for... |
