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
03.11.2017
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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