| 摘要 |
<p>A thrust reverser for use with a jet engine comprising a pair of symmetrical thrust reverser doors (10, 12), each of which doors are pivotally attached to an attachment element (50) on the jet engine pipe (18) so as to be pivotally movable between reversing and non-reversing positions, each of the doors (10, 12) having a scarfed trailing edge portions (34, 36) so that in the reversing position, the trailing edge portions (34, 36) of the doors (10, 12) are in abutting contact; a pair of half-shells (22, 24), one being associated with and surrounding the trailing edge portion of each of the doors (10, 12), the half shells (22, 24) being pivotally attached to the attachment element (50) and cooperatively forming a planar exhaust outlet (38) for the jet engine (18).</p> |
