Inventor

BROCHARD WOLFGANG

FR21 patents

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

BROCHARD WOLFGANG

AIRBUS OPERATIONS SAS

Sound attenuation panel for an aircraft

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

Flexible linking device for an aircraft propulsion system

Primary structure for an attachment pylon with firewall and thermal layers

Engine assembly for an aircraft comprising a front engine attachment which facilitates its assembly

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

Lateral propulsion unit for aircraft comprising a turbine engine support arch

Boomerang link with vibration filtering ability and aircraft engine mount provided with such link

Cellular sandwich panel containing boron nitride powder and manufacturing method for said panel

Method for manufacturing a door of a thrust reversal system

Nacelle of an aircraft propulsion assembly comprising a plurality of damper elements between a front section and a main section, and associated aircraft propulsion assembly

Method for manufacturing an acoustic element of a sound absorption structure from at least one sheet of material

Acoustic absorption structure comprising at least one rotationally-indexed acoustic element and aircraft propulsion assembly comprising said acoustic absorption structure

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

Output cone of an aircraft propulsive assembly forming an acoustic treatment system with at least two degrees of freedom

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

Aircraft air inlet comprising at least two walls connected end to end by welding, method for the assembly of such an air inlet, and aircraft comprising at least one such air inlet

Locking mechanism for at least one movable element situated in a first zone and comprising a component that can be adjusted from a second zone, and aircraft comprising at least one such locking mechanism

Aircraft propelling assembly including a duct forming a thermal barrier integrated in the caisson of the rigid structure of the engine mounting system

AIRBUS OPERATIONS SL

Aircraft with a protective shield against an engine blade release