A mount mechanism used to mount an accessory gear box on an engine case in an aircraft engine, includes a pair of first brackets fastened to one of the engine case and the accessory gear box, the pair of first brackets being apart from each other in a circumferential direction of the engine case; a link extending in such a manner that the pair of first brackets are connected to each other via the link, both end portions of the link being coupled to the pair of first brackets by a pair of first pins, respectively; an annular anti-vibration element penetrated by each of the pair of first pins, the annular anti-vibration element being retained by at least one of each of the pair of first brackets and the end portion of the link; and a second bracket fastened to the other of the engine case and the accessory gear box, the second bracket box being coupled to the link by a second pin at a location between the pair of first brackets.
MOUNT MECHANISM FOR ACCESSORY GEARBOX
MONTAGEMECHANISMUS FÜR HILFSGETRIEBE
MÉCANISME DE MONTAGE POUR BOÎTIER D'ENTRAÎNEMENT DES ACCESSOIRES
2020-02-26
Patent
Elektronische Ressource
Englisch
Engineering Index Backfile | 1955
MOUNT ASSEMBLY FOR ACCESSORY GEARBOX OF AIRCRAFT ENGINE AND ASSOCIATED METHOD OF ASSEMBLY
Europäisches Patentamt | 2022
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