| 摘要 |
<p>An aircraft propulsion assembly includes a support providing a transfer of a force torque to an aircraft from a suspension assembly which is interposed between the support and a turbojet engine. The suspension assembly is mounted on an intermediate housing, a main housing or a fan housing, and on the support. In particular, the suspension assembly includes following suspension fasteners:—a first suspension fastener having a device for absorbing thrust forces and forces“Fz”along an axis“Z”,—a second suspension fastener to absorb, with the first suspension fastener, a moment“Mx”around an axis“X”and forces“Fy”along an axis“Y”,—a third suspension fastener to absorb, with the first suspension fastener, a moment“My”along the axis“Y”and forces“Fx”along an axis“X”. A moment“Mz”along the axis“Z”is absorbed by one of the suspension fasteners.</p> |
