| 摘要 |
<p>The system has an additional unit (23) comprising a connecting rod (32) that is integrated to a rigid structure (4) of an attachment strut (6) on one side and to a fan casing (26) of an aircraft engine on another side. The connecting rod is situated in a vertically imaginary plane and oriented according to a longitudinal direction, where the rod is not integrated during en-route phase of the engine. An independent claim is also included for an attachment strut of an aircraft engine including an assembly system.</p> |
