A device for suspending a casing of a turbine engine to the structure of an aircraft is provided. The device includes a suspension ring including a plurality of attachment surfaces positioned so as to protrude on the circumference of the suspension ring and having attachment holes for attachment to the structure; a circumferential flange including a plurality of holes for attaching the suspension ring to the casing; and one or several hanging surfaces for hanging at least one piece of equipment, positioned so as to protrude on the circumference of the suspension ring, and having holes for hanging the piece of equipment to the ring.
DISPOSITIF DE SUSPENSION D'UN CARTER, TURBOMACHINE ET ENSEMBLE PROPULSIF
2017-11-03
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
|European Patent Office | 2023
|European Patent Office | 2024
|ENSEMBLE PROPULSIF MUNI DE PARTIES DE CARTER DECOUPLABLES
European Patent Office | 2019
|