STRUCTURAL ASSEMBLY DISPOSED BETWEEN THE ATTACHMENT PYLON AND THE FAN CASING OF AN AIRCRAFT ENGINE

摘要

The invention relates to an aircraft propulsion system (1) comprising a bypass turbojet engine (2), a pylon (3) for attaching the engine (2) under a wing of the aircraft and means for fixing the pylon to the engine, these means essentially consisting of a rigid connection of the pylon (3) to a fan casing (4) of the engine (2). The rear part (11) of the engine (2) projects cantilever-fashion beyond the fan casing (4) under the pylon (3).