Deployable grille with fins for aircraft turbine engine thrust-reversal system
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.
Information query
Patent Agency Ranking
0/0