Thrust reverser nozzle for a turbofan gas turbine engine

Details Thrust reverser nozzle for a turbofan gas turbine engine Thrust reverser nozzle for a turbofan gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/56 (2006.01) F02K 1/58 (2006.01)

Patent

CA 2660001

The thrust reverser comprises a first reverser door (24) and a second reverser door (26) asymmetrically pivotable between a stowed position and a deployed position, one having a pivot axis closer to the central axis (32) than the other.

invention concerne un inverseur de poussée comprenenant une première porte d'inverseur (24) et une seconde porte d'inverseur (26) qui peut pivoter de façon asymétrique entre une position arrimée et une position déployée, l'une étant dotée d'un axe de pivot plus proche de l'axe central (32) que l'autre.

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