| 摘要 |
<p>The invention relates to a system for attaching an element (3) capable of vibrating onto an aircraft structure (2), comprising at least one pair of scoops (10) attached onto the element capable of vibrating, as well as onto the structure, each scoop (10a, 10b) of the pair of scoops comprising: an outer rigid element (12) attached onto the structure; an inner rigid element (13) mounted inside the outer rigid element and rigidly connected to the element capable of vibrating; and a flexible element (14) placed along each outer rigid element flank, between the outer rigid element and the inner rigid element.</p> |
