A structure for linking and supporting a turbine engine on an aircraft pylon, the structure having a first longitudinal axis intended to extend parallel to a second longitudinal axis of the pylon, the structure including a first axial portion for fastening to the pylon, the first portion having an upper end that defines a substantially horizontal plane of interface with the pylon, and a lower end bearing suspension rods for suspending the turbine engine, which extend in a rear vertical plane; and a second axial portion that is intended to extend forward of the pylon and includes at least one suspension member of the turbine engine in a front vertical plane.
STRUCTURE DE LIAISON ET DE SUPPORT D'UNE TURBOMACHINE A UN PYLONE D'AERONEF
STRUCTURE FOR LINKING AND SUPPORTING A TURBINE ENGINE ON AN AIRCRAFT PYLON
STRUKTUR ZUR VERBINDUNG UND STÜTZE EINES TURBINENMOTORS AUF EINEM FLUGZEUGPYLON
2024-04-10
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
STRUCTURE DE LIAISON ET DE SUPPORT D’UNE TURBOMACHINE A UN PYLONE D’AERONEF
European Patent Office | 2024
|STRUCTURE DE LIAISON ET DE SUPPORT D'UNE TURBOMACHINE A UN PYLONE D'AERONEF
European Patent Office | 2022
|ASSEMBLAGE ENTRE UN PYLONE D'AERONEF ET UNE TURBOMACHINE
European Patent Office | 2022
|ASSEMBLAGE ENTRE UN PYLÔNE D'AÉRONEF ET UNE TURBOMACHINE
European Patent Office | 2024
|