| 摘要 |
A thrust reverser (36) includes forward and aft louvers (54, 56) pivotally mounted in a compartment (50) defining a flow tunnel (52) through the outer and inner skins (38, 40) of a fan nacelle (16). An aft flap (60) is integrally joined to the aft louver (56) for rotation therewith. A unison link (64) joins together the forward and aft louvers (54, 56). And, an actuator (66) is joined to the louvers for rotation thereof between a stowed position in which the louvers and flap are closed in the nacelle skins and a deployed position in which the louvers and flap are pivoted open from the skins. |
