Assembly comprising a translationally and rotationally immobile link axis, engine attachment or aircraft comprising such an assembly
GB202017533D0
Multifrequency absorption acoustic panel for an aircraft nacelle
GB202016608D0
Pylon
US2021024221A1
Leading edge member for an airfoil of an aircraft
US2020198804A1
System and method for determining the separation between two parts using eddy current sensors
GB201917559D0
A control system for controlling a landing gear drive system
US2020172221A1
Linking part designed to be linked to a support element of an aircraft
US2020175734A1
Method and system for generating a display comprising a curve representative of a circular limit on a terrestrial surface
US2020160736A1
Determination of a pavement state from on-board measurements of pavement contamination, associated system and aircraft
US2020160877A1
Method and system for processing audio signals for a microphone of an aircraft oxygen mask
US2020164997A1
Acoustic Absorption Structure Comprising At Least One Rotationally-Indexed Acoustic Element And Aircraft Propulsion Assembly Comprising Said Acoustic Absorption Structure
EP3660295A1
Process for producing an acoustic element of an acoustic absorption structure from at least one sheet of material
EP3660299A1
Structure for acoustic absorption including a system for draining liquid and propulsion assembly comprising such a structure for acoustic absorption
CN111204463A
Aircraft nacelle comprising a fairing with two hinged doors
EP3667438A1
System for flight control of an aircraft
EP3813038A1
Method and system for aiding the landing of an aircraft
FR3102617A1
Coupling of electric machine rotors
FR3102461A1
Aircraft structure comprising a fairing and at least one liquid evacuation drain having a connection system by interlocking, aircraft mast or aircraft comprising said structure