| 摘要 |
A thrust reverser nozzle (22) for an engine nacelle (20) includes opposite and asymmetrically pivoting first and second doors (24,26) defining a nacelle aft section (20a), first and second trailing edges (24a, 26a) of the first and second doors (24,26) adjacent to an outlet (28) of the nacelle, the doors being pivotable simultaneously between a stowed position and a deployed position such that the first trailing edge (24a) is positioned behind the second trailing edge (26a) when the doors are in the deployed position, and the first and second fairings (34,36) attached to the first and second doors in relative fixed positions to the first and second doors respectively Male contour middle portions (38) of the first fairings (34) may complementarily match female contour middle portions (40) of the second fairings (36) and are received within the female contour middle portion when the doors are in the stowed position.
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