A primary support strut structure and a method of manufacturing thereof for an aircraft power plant is disclosed having a first half-shell including a first free edge, and a second half-shell having a second free edge. The first half-shell and the second half-shell are assembled together by joining the first free edge and the second free edge so as to form a box-shaped structure. The two half-shell construction results in very rigid box structure, and a reduced number of ribs in the primary structure.
STRUCTURE PRIMAIRE DE MÂT DE SUPPORT D'UN GROUPE PROPULSEUR D'AÉRONEF EN CAISSON FORMÉE PAR ASSEMBLAGE DE DEUX DEMI-COQUILLES
PRIMARY STRUCTURE OF MAST FOR SUPPORTING AN AIRCRAFT DRIVE UNIT IN A BOX, FORMED BY JOINING TWO HALF-SHELLS
PRIMÄRSTRUKTUR EINES HALTEMASTS EINER LUFTFAHRZEUG-ANTRIEBSGRUPPE MIT GEHÄUSE, DIE AUS ZWEI ZUSAMMENGEBAUTEN HALBSCHALEN GEBILDET WIRD
2020-03-18
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2019
|European Patent Office | 2020
|European Patent Office | 2023
|GROUPE PROPULSEUR D'AERONEF COMPORTANT UNE SOUFFLANTE CONJOINTEMENT ENTRAINEE PAR DEUX MOTEURS
European Patent Office | 2018
|European Patent Office | 2015
|