Inventor

PAUTIS OLIVIER

FR49 patents

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

PAUTIS OLIVIER

AIRBUS OPERATIONS SAS

Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes

Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other

Propulsion assembly incorporating a turbofan and a mounting pylon enabling a new distribution of the forces between the turbofan and the wing

Thrust reverser system having limited aerodynamic disturbance

Assembly for an aircraft including a fitting secured to the upper surface of a wing box, for mounting an engine strut to said wing box

Foldable guiding ventilator cover for an aircraft engine assembly

Aircraft engine pylon having a mobile cowl

Assembly for an aircraft comprising a primary structure for an attachment pylon secured to a wing box by means of fittings that are more compact in the leading edge region

Aircraft engine assembly, comprising flexible force transmitting devices radially arranged between the thrust reversal cowls and the engine

Aircraft assembly comprising a mounting pylon primary structure integrated to the structure of the wing element

Assembly for an aircraft comprising an attachment pylon primary structure formed with three independent elements

Assembly for aircraft, comprising a primary attachment-pylon structure fixed to a wing box by fasteners partially embedded in the primary structure

Thrust reverser system limiting aerodynamic perturbation in an inactive configuration

Aircraft nacelle comprising at least one fan cowl door which is mounted so as to be able to rotate about the longitudinal axis of the nacelle

Propulsive assembly with enhanced engine cowl articulated in rotation on an axis of rotation positioned above top face of engine pylon, and aircraft comprising such an assembly

Braced-pylon architecture for mounting an engine to an aircraft

Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods

Nacelle for an aircraft engine assembly comprising at least one jointed nacelle cowling at its front end

Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box

Assembly for aircraft comprising a primary structure of an attachment pylon attached to a wing box using a bolted connection

Nacelle of a turbojet comprising a reverser flap and a deployment system with delay

Engine pylon for coupling a jet engine to a wing of an aircraft

Aircraft comprising an engine pylon with a movable cover assembly and a specific locking system

Aircraft engine pylon having a movable assembly of cowls

Assembly for an aircraft, the assembly comprising a mast and a wing

Assembly for an aircraft, the assembly having a pylon and a wing

Engine pylon for coupling a jet engine to a wing of an aircraft

Assembly for an aircraft comprising a primary structure for an attachment pylon secured to a wing box by means of fittings that are more compact in the leading edge region

Assembly of parts assembled by a through-shaft that can be fitted if the parts are in approximate alignment

Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch

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

Assembly including two links and an interleaved stiffener, aircraft engine attachment including at least one such assembly

Assembly for an aircraft having a wing and an engine pylon for coupling a jet engine to said wing

Aircraft propulsion assembly

Assembly for an aircraft comprising a wing and an engine pylon for coupling a propulsion system to said wing

Aircraft having an engine pylon with a mobile cowl

Assembly for an aircraft comprising a wing and an engine pylon for coupling a propulsion system to said wing

Shackle for fastening an aircraft engine comprising a pair of encapsulated anti-friction coatings, and aircraft comprising such a shackle

Method for mounting an aircraft pylon

Propulsion system for an aircraft comprising a turbojet, a pylon and engine attachment

Forward engine mount for a half or full wraparound pylon

Assembly for a nacelle of an aircraft engine, said assembly comprising a fixed cowl and a cowl mounted so as to be able to move on the fixed cowl

Junction of a pylon with an aircraft wing

Thrust reverser system exhibiting limited aerodynamic perturbation

Turbojet engine comprising a nacelle equipped with reverser flaps

Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box

AIRBUS FRANCE

Aircraft cockpit window

AIRBUS OPERATIONS LTD

Joint for connecting aircraft structures

PAUTIS OLIVIER

Fan comprising anti-deflagration housing