Deployable grille with fins for aircraft turbine engine thrust-reversal system
AssigneeSafran Aircraft Engines
InventorJeremy Edmond Fert
Life of this patent
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Abstract
A deployable grille with fins for a thrust-reversal system for an aircraft turbine engine. The grille can adopt a rest position and a deployed, active position wherein the fins are axially spaced further apart than in the rest position. At least between two fins, the grille includes resilient return device forcing the two fins to move apart axially from one another.
Claims10
A deployable grille with fins for an aircraft turbine engine thrust-reversal system, wherein the grille is configured to adopt a rest position and a deployed active position in which the fins are more separated axially from one another than in the rest position, and wherein said grille comprises, at least between two of the fins, a resilient return configured to force said two of the fins to separate axially from each other.
Dependencies are inferred from the claim text.