| 摘要 |
<p>An aircraft propulsion assembly includes a turbojet engine, a support providing a transfer of force torque to an aircraft from a suspension assembly, and the suspension assembly interposed between the support and the turbojet engine. The suspension assembly includes a device for absorbing thrust forces, an upstream suspension fasteners mounted on a fan housing and an intermediate housing of the turbojet engine. In particular, the suspension assemble further includes a main upstream suspension fastener to absorb a moment (Mx) along an axis (X) of the turbojet engine and forces (Fy and Fz) in a plane perpendicular to the axis (X), and a pair of additional upstream suspension fasteners separate from the main upstream suspension fastener to absorb a moment (Mz) along an axis (Z) and a moment (My) along an axis (Y) and forces (Fx) along the axis (X).</p> |
