In order to reduce the mass of a primary structure of a mounting pylon for an engine of an aircraft, the mounting pylon includes a box and a rear sub-structure fastened to the box which includes two lateral panels, each equipped at its rear end with a first linking portion through which passes a first connection orifice that is designed to receive a connection pin of a lateral front wing attachment. The rear sub-structure is made in one piece and includes two opposite lateral flanks that are respectively fastened to the two lateral panels of the box by fastening elements. Each lateral flank has a second linking portion through which passes a second connection orifice that is aligned with the first connection orifice, and is also designed to receive the connection pin of the lateral front wing attachment.
STRUCTURE PRIMAIRE ALLEGEE POUR MAT D'ACCROCHAGE DE MOTEUR D'AERONEF
LIGHT PRIMARY STRUCTURE FOR AIRCRAFT ENGINE MOUNTING STRUT
LEICHTE PRIMÄRSTRUKTUR FÜR AUFHÄNGEMAST EINES TRIEBWERKS EINES LUFTFAHRZEUGS
09.10.2019
Patent
Elektronische Ressource
Französisch
STRUCTURE PRIMAIRE ALLEGEE POUR MAT D'ACCROCHAGE DE MOTEUR D'AERONEF
Europäisches Patentamt | 2019
|STRUCTURE PRIMAIRE A CONCEPTION AMELIOREE POUR MAT D'ACCROCHAGE DE MOTEUR D'AERONEF
Europäisches Patentamt | 2019
|SYSTEME D’ATTACHE MOTEUR AVANT POUR UN MOTEUR D’AERONEF QUI COMPORTE UNE STRUCTURE ALLEGEE
Europäisches Patentamt | 2021
|STRUCTURE PRIMAIRE D’UN MÂT POUR LA FIXATION D’UN MOTEUR D’AÉRONEF.
Europäisches Patentamt | 2023
|ASSEMBLAGE D'UN MÂT D'ACCROCHAGE AVEC UN MOTEUR D'AÉRONEF
Europäisches Patentamt | 2025
|