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2025
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Invention
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Method for manufacturing a cellular core for an acoustic attenuation panel. The invention relates... |
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Invention
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Transport tool configured to be temporarily mounted on a thrust reverser of an aircraft turbojet ... |
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Invention
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Fan of an aircraft turbine engine and method for using same. The invention relates to a fan (1) o... |
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Invention
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Airflow ejector nozzle having a constant outlet cross-section provided with a stream adjustment d... |
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2024
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Invention
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Thrust-reversal system for an aircraft turbojet engine, nacelle and propulsion assembly including... |
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Invention
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Method for manufacturing a composite panel. The invention relates to a method for manufacturing a... |
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Invention
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Thrust-reversal system for an aircraft turbojet engine, nacelle and propulsion unit comprising su... |
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Invention
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Assembly comprising a stationary surface and a movable surface of an aircraft.
An assembly for a... |
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Invention
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Opening cowl for a turbine engine. The invention relates to an aircraft propulsion assembly (1) e... |
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Invention
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Method for manufacturing a multi-perforated composite acoustic skin without mechanical piercing. ... |
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Invention
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Propulsion unit for an aircraft. The invention relates to a propulsion assembly (1) comprising a ... |
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Invention
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Surface heat exchanger comprising a pressure loss reducer and aircraft nacelle provided with such... |
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Invention
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Hydraulic control device for a thrust reverser. The invention relates to a hydraulic control devi... |
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Invention
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Air intake for an aircraft turboprop and method for using same when the aircraft is on the ground... |
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Invention
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Thrust reverser with sealing membrane and retention system. The invention relates to a thrust rev... |
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Invention
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Acoustic panel for an aircraft turbine engine. The invention relates to an acoustic panel (17) co... |
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Invention
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Thrust reverser comprising at least one deployable membrane, and a membrane-deployment member arr... |
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G/S
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Constructions en acier; réservoirs métalliques [structures]; métaux communs et leurs alliages, y ... |
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G/S
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Steel buildings; metal tanks [structures]; common metals and their alloys, including stainless st... |
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G/S
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Steel buildings; metal tanks [structures]; common metals and
their alloys, including stainless s... |
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Invention
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Thrust reverser comprising an improved safety system for deploying a membrane for sealing off the... |
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Invention
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Air flow ejector nozzle with detachable internal structure and turbine engine provided with such ... |
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Invention
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Airflow ejection nozzle with constant outlet section and turbine engine equipped with such a nozz... |
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Invention
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Thrust reverser comprising at least one deployable membrane, having low-mass deployment means. Th... |
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Invention
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Device for handling an element of an aircraft and handling assembly provided with such a device. ... |
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Invention
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Thrust reverser comprising at least one deployable deflection membrane with improved attachment. ... |
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Invention
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Method for manufacturing an open part with reinforced ribs. The invention relates to a method for... |
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Invention
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Method for producing a part made of composite material and having raised elements, and correspond... |
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Invention
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Propulsion assembly with longitudinal locking of at least one nacelle cover. The invention relate... |
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Invention
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Thrust reverser comprising at least one deployable deflection membrane having a design that facil... |
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G/S
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Motors and engines, thrusters, and thrust reversers for aircraft, namely, nacelles; All of the af... |
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G/S
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Moteurs, propulseurs, inverseurs de poussées pour appareils de locomotion (à l'exception de ceux ... |
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G/S
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Motors/engines, thrusters, thrust reversers for locomotion
apparatus (except for land vehicles),... |
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G/S
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Steel fabrications; Reservoirs (metal -) [structures]; Common metals and their alloys including s... |
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G/S
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Motors and engines, thrusters, and thrust reversers for aeronautical vehicles, excluding land veh... |
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G/S
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Motors, Propellers, thrust reverser, For use with the following goods: Apparatus for locomotion (... |
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2023
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Invention
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Air flow ejector nozzle with a constant outlet cross-section and turbine engine provided with suc... |
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Invention
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Thrust reverser comprising means facilitating the mounting of a membrane for sealing off the seco... |
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Invention
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Assembly for a turbine engine.
An assembly for a turbine engine having a longitudinal axis, incl... |
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Invention
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Thrust reverser comprising a simplified-deployment obturator membrane.
A thrust reverser for an ... |
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Invention
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Method for detecting an anomaly in a system of an aircraft.
A method for detecting an anomaly in... |
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Invention
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Propulsion assembly for an aircraft, comprising an intermediate cowl of the stationary, removable... |
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Invention
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Gripper, in particular for applying a honeycomb-shaped element to a target surface, and machine p... |
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Invention
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Seal comprising a succession of zones with and without anti-friction coatings.
A seal is configu... |
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Invention
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Ejection cone for an aircraft turbine engine.
An exhaust cone for an aircraft turbomachine, exte... |
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Invention
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Method for joining two anodised elements by friction stir welding.
The present application descr... |
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Invention
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Method for producing a part made of composite material.
A method for producing a part made of co... |
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Invention
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Propulsion assembly for an aircraft comprising a thrust reverser with movable cascades and with a... |
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Invention
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Thrust reverser comprising movable cascades and a sealing membrane. A thrust reverser for an airc... |
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Invention
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Thrust reverser comprising fixed cascades and a sealing membrane. A thrust reverser for an aircra... |
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2022
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Invention
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System for cooling a liquid for lubricating an aircraft turbomachine.
A system for cooling a liq... |
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Invention
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Air intake lip for a nacelle of an aircraft propulsion assembly. An annular air intake lip for a ... |
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Invention
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Process for digital diagnosis of a system of actuators in an aircraft undergoing maintenance.
An... |
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Invention
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Acoustic panel having oblique cavities.
An acoustic panel comprising a first group of cavities o... |
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Invention
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De-icing of an aircraft part.
A de-icing system which includes actuators attached to the part; a... |
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Invention
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Suspension of a triple-flow aircraft turbine engine. A triple-flow turbine engine for an aircraft... |
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Invention
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Movable-cascade thrust reverser comprising a multi-functional fixed structure.
A movable-cascade... |
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2018
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G/S
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Industrialization machines in the field of aeronautics and space, namely, machines for production... |
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G/S
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Industrialization machines in the field of aeronautics and
space; production machines for compos... |
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G/S
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Machines for industrialisation in the aeronautical and space sector; Machines for the production ... |
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G/S
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Electric and electronic systems and equipment, including on-board, for data capture and processin... |
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G/S
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Electric and electronic systems and equipment, onboard or not, for data acquisition and processin... |
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G/S
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Electric and electronic systems and equipment, onboard or
not, for data acquisition and processi... |
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2009
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G/S
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Motors, propulsive units, thrust reversers for apparatus for
locomotion (excluding those for lan... |
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G/S
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Engines and motors, propellers, thrust reversers for apparatus for locomotion (except for land ve... |
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2008
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G/S
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Aircraft engine pods; parts of aircraft engine pods;
aircraft engines; thrust reversers for airc... |
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1998
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G/S
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Inverseurs de poussée. |
