Turbojet thrust reverser with downstream obstacles

Details Turbojet thrust reverser with downstream obstacles Turbojet thrust reverser with downstream obstacles

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/70 (2006.01)

Patent

CA 2286381

The invention concerns a turbojet thrust reverser comprising downstream obstacles (2) integrated in the turbojet ejector nozzle rear wall in direct thrust position and constituting in unfolded position flux deviating obstacles providing thrust reversal. Each downstream obstacle (2) is equipped with a mobile inner panel (13), obstacle (2) and panel (13) having different angular displacements when shifting to reversal position and the displacing means (6, 7) being common to the downstream obstacle (2) and the inner panel (13)

Un inverseur de poussée de turboréacteur comporte des obstacles aval (2) intégrés à la paroi extérieure du canal d'éjection du turboréacteur en position de poussée directe et constituant en position déployée des obstacles de déviation du flux en procurant une inversion de poussée. Chaque obstacle aval (2) est équipé d'un panneau interne mobile (13), obstacle (2) et panneau (13) ayant des débattements angulaires différents lors du passage en position d'inversion et le moyen de déplacement (6, 7) étant commun à l'obstacle aval (2) et au panneau interne (13).

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