An engine assembly for an aircraft, comprising an engine mounting pylon comprising a primary structure forming a box closed by a front closing rib, a front engine mount comprising at least two connecting link rods that are disposed laterally on either side of the box and each comprise a first end mounted on a first fitting of the casing. The rib forms a part of the front mount, comprising at least one transverse fitting made in one piece so as to close a front end of the box and to have lugs protruding laterally on each side of the box, each lug being provided with a first orifice for mounting a second end of one of the link rods.
ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON
25.10.2018
Patent
Elektronische Ressource
Englisch
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