| 摘要 |
In order to assist deployment, the invention relates to a deployable grille (32) with fins (44) for a thrust-reversal system (6) for an aircraft turbine engine. The grille can adopt a rest position and a deployed, active position in which the fins (44) are axially spaced further apart than in the rest position. At least between two fins (44), the grille comprises resilient return means (56) forcing the two fins (44) to move apart axially from one another. |
