摘要 |
The present invention relates to a suspension for suspending a jet engine on an aircraft strut, comprising a beam having a platform provided with means for fastening it to the said strut and arranged transversely with respect to the axis of the engine, first and second lateral links each connected by a first pin to the beam and by a second pin to the engine casing, the second lateral link being prolonged in the region of the first pin by a finger housed with clearance in a cavity provided in the beam so as to form a standby safety connection, and a central link arranged between the two lateral links and connected by a first pin to the beam and by a second pin to the said casing. In the case the beam comprises a clevis for housing the first connecting pin of the central link, and the said first pin is distant from the platform so that a space is provided between the platform and the central link, this space forming the said cavity in which the finger of the second lateral link is housed with clearance in normal operation. The solution of the invention makes it possible to reduce the weight of the suspension and to simplify the machining thereof. |