Inventor

SOULIE ADELINE

FR26 patents

⚠️ This page may combine multiple inventors who share the name “SOULIE ADELINE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SOULIE ADELINE

AIRBUS OPERATIONS SAS

Propulsive assembly for aircraft

Assembly for an aircraft, the assembly including a pylon and a tank containing an extinguisher fluid

Assembly for an aircraft, said assembly having a pylon and a reservoir containing an extinguishing fluid

Assembly for an aircraft engine mounting comprising an articulation axis supported by a yoke joint and translationally immobile

Aircraft pylon equipped with a guidance system for mounting or dismounting a tank and method of mounting/dismounting said tank

Assembly for an aircraft, said assembly comprising a pylon and a reservoir containing an extinguishing fluid

Assembly of at least one extinguishing agent tank in the interior of an aircraft strut

Aircraft pylon comprising a coaxial heat exchanger

Compact heat exchange device incorporated into an aircraft pylon

Rear engine attachment for an aircraft engine

Assembly having a structure and a reservoir fastened to the structure and containing an extinguishing fluid

Double-wall hydrogen pipeline comprising at least one system for detecting a leak at at least one coupling system, and aircraft comprising at least one such pipeline

Enclosure containing an inerting gas and comprising a liquid discharging system, aircraft having such an enclosure

Aircraft propulsion assembly comprising a plate heat exchanger, of hexagonal longitudinal section, positioned in a bifurcation

Cold regulating valve for a heat exchanger system of an aircraft propulsion system

Aircraft engine attachment comprising inclined fixing elements, aircraft comprising said engine attachment and method for fixing an engine to an aircraft pylon using said engine attachment

Aircraft comprising at least one cowling equipped with an improved hinge system

Aircraft propulsion assembly comprising a cold bleed air intake device with variable aerodynamic profile

Aircraft bypass turbojet engine with opening fitted with a hinge with gooseneck fitting

Aircraft propulsion assembly

Engine attachment system for an aircraft engine

Dual-flow jet engine for an aircraft with an improved aperture

Aircraft propulsion assembly comprising a fire-fighting system with a line for distributing extinguishing agent

AIRBUS SAS

Aircraft propulsion system including a heat exchanger system

Aircraft propulsion system including a heat exchanger system

Aircraft propulsion system including a heat exchanger system