An aircraft propulsion assembly including a front engine mount including a transverse beam which is connected to the engine via first and second convergent connection rods. This transverse beam includes an upper extension which is at least partially positioned opposite a front transverse reinforcement of the primary structure and which is connected thereto via at least one first connection element and right and left lateral extensions which are positioned at one side and another of the upper extension, each of them being connected via a least one second fixing element to a first wing of a right or left bracket, a second wing of the right or left bracket being connected via at least one third connection element to the primary structure.
ENSEMBLE PROPULSEUR D'AÉRONEF COMPRENANT UNE ATTACHE MOTEUR AVANT COMPORTANT UNE POUTRE TRANSVERSALE PARTIELLEMENT POSITIONNÉE FACE À UN RENFORT TRANSVERSAL AVANT D'UNE STRUCTURE PRIMAIRE D'UN MÂT
AIRCRAFT PROPELLER ASSEMBLY COMPRISING A FRONT ENGINE ATTACHMENT COMPRISING A TRANSVERSE BEAM PARTIALLY POSITIONED FACED WITH A FRONT TRANSVERSE REINFORCEMENT OF A PRIMARY STRUCTURE OF A MAST
FLUGZEUG-PROPELLERBAUGRUPPE, DIE EINE VORDERE MOTORBEFESTIGUNG UMFASST, DIE EINEN QUERTRÄGER UMFASST, DER TEILWEISE MIT EINER VORDEREN QUERVERSTÄRKUNG EINER PRIMÄRSTRUKTUR EINES MASTS POSITIONIERT IST
01.05.2024
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2023
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