| 摘要 |
The invention relates to a system (58) for mounting a propulsion assembly (10) onto a pylon (11) of an aircraft and dismounting same therefrom, said propulsion assembly (10) being of the type comprising a nacelle (12) and a turbojet, the turbojet being joined to the pylon (11) by means of at least one front suspension (24) and a rear suspension (26), characterised in that it comprises a carrier structure (34) which is designed to carry a thrust-reversal device, a front suspension (24) of the turbojet, which carries a front part of the carrier structure (34) and is detachably fixed to a front part of the pylon (11), and a rear suspension (26) of the turbojet, which carries a rear part of the carrier structure (34) and is detachably fixed to a rear part of the pylon (11). Said suspensions (24, 26) can be detached from the pylon (11) in order to dismount the propulsion assembly (10) mounted on the pylon (11). |
