AIRCRAFT ENGINE ASSEMBLY COMPRISING A TURBOJET ENGINE WITH REINFORCING STRUCTURES CONNECTING THE FAN CASING TO THE CENTRAL CASING

摘要

The invention relates to an aircraft engine assembly comprising an annular structure (60) surrounding a central casing (16) and mechanically connected to the latter by means of mounting means (62). To each of said first and second engine attachments (6a, 6b) is associated a reinforcing structure (64a, 64b) forming a shear plane, fixedly connected: at the level of the annular structure at a first anchoring point (68a, 68b) ; at the fan casing at a second anchor point (70a, 70b); and at a structural arm or intermediate housing at a third anchor point (72a, 72b), said structure extending in a radial notional plane passing through an anchor point of said fastener (6a, 6b) on the fan case.