Inventor

GELIOT JEAN

FR31 patents

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

GELIOT JEAN

AIRBUS OPERATIONS SAS

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

Forward secondary structure for a mounting pylon of an aircraft

Aircraft nacelle comprising a cowl with two articulated doors

Aircraft turbomachine assembly comprising an articulated cowl

Device for attaching an electrical harness in an aircraft

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

Aircraft turbomachine assembly comprising an articulated cowl

Compact heat exchange device incorporated into an aircraft pylon

Rear engine attachment for an aircraft engine

Aircraft turbine engine assembly comprising a hinged cover

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

Aircraft nacelle comprising a seal system with a spring for a cap of said nacelle

Aircraft propulsion assembly comprising a front engine mount which comprises a transverse beam which is partially positioned opposite a front transverse reinforcement of a primary structure of a strut

Rear engine attachment of an aircraft having two-part rods and aircraft comprising at least one such rear engine attachment

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

Propulsion assembly for an aircraft, comprising a nacelle load support fastened to a pylon

Propulsive assembly of an aircraft comprising a junction fairing between a nacelle and a pylon of the aircraft equipped with a removable cowl and aircraft equipped with said propulsive assembly

Engine attachment system for an aircraft engine

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

Propulsion assembly for an aircraft, comprising a load support

Aircraft pylon comprising at least one seal interposed between a fixed structure and a removable panel of a fairing

Metal fire seals system for aircraft engine mount

AIRBUS SAS

Method for assembling an aircraft pylon and aircraft pylon obtained by this method