AIRCRAFT STABILISER TRAILING EDGE

摘要

The invention relates to the trailing edge (3) of an aircraft stabiliser (1) which is made from a composite material and includes an outer skin (40) and an inner skin (41) which are joined to the trailing edge (3) by means of clip-type coupling element (20). The invention is characterised in that the ends of the clip-type coupling element (20) include recesses (23) intended to be coupled to the inner area of the upper and lower skins (40, 41) of the stabiliser (1), said clip-type coupling element being sufficiently flexible for it to be clipped in such a way that the ends are housed by means of the aforementioned recesses (23) between the outer and inner skins (40, 41) of the aircraft stabiliser (1), so that the outer area on the trailing edge (3) of the stabiliser (1) is formed by a continuous aerodynamic surface without any changes in slope.