Inventor

DEFORET THOMAS

FR28 patents

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

DEFORET THOMAS

AIRBUS OPERATIONS SAS

Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system

Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system

Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system

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

Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system

Front engine attachment system for an aircraft engine, having rod systems with two rods

Front engine attachment system for an aircraft engine, having a beam made in three parts

Engine fastener for an aircraft

Aircraft engine fastener

Compact heat exchange device incorporated into an aircraft pylon

Rear engine attachment for an aircraft engine

Aircraft propulsion assembly having a jet engine, a pylon and means for attaching the jet engine to the pylon

Rear attachment of an aircraft engine comprising break detectors

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 propulsion assembly comprising links of a front engine mount that are directly connected to a front transverse reinforcement of a primary structure of an aircraft pylon

Front engine attachment system for an aircraft engine, having a beam made in two parts

Aircraft engine attachment comprising at least one system for immobilizing a shear pin in translation comprising a stop plate, method for mounting said engine attachment and aircraft comprising said engine attachment

Front engine attachment system for an aircraft engine, having a beam made in three parts

Aircraft engine attachment comprising at least one fork-type system for immobilizing a shear pin in translation, method for mounting said engine attachment and aircraft comprising said engine attachment

Forward engine attachment system for an aircraft engine comprising a direct coupling between the jet engine pylon and the engine

Engine attachment system for an aircraft engine

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

Mounting pylon for a jet engine of an aircraft comprising a particular structure

Linking device connecting an aircraft engine and a primary structure of an aircraft pylon comprising a spreader and a system for limiting the out-of-plane deflection of the spreader, aircraft comprising such a linking device

Aircraft propulsion assembly comprising at least one aerodynamic panel which is supported by at least one intermediate radial support, aircraft comprising at least one such propulsion assembly

Method for assembling a primary structure of an aircraft pylon

Assembly for an aircraft, the assembly comprising a pylon and a front engine mount

AIRBUS SAS

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