| 摘要 |
<p>The invention relates to an aerofoil (T) comprising a main wing and a high lift flap (K) which is movably mounted on the aerofoil (T) by means of at least two adjusting mechanisms (10a, 10b) that are located next to one another in the direction of the span of the aerofoil (T), each of said adjusting mechanisms (10) having three rotational axes (A11, A12, A13; A21, A22, A23) running through a common pole (P), said pole being fixed in relation to the position of the main wing during the adjustment of the high lift flap (K). According to the invention: the aerofoil (T) has a drive device (50) comprising a drive module (51) that is mounted on the main wing (H) and a lever (52) that can be moved in relation to said module and that is coupled to the high lift flap (K); and the aerofoil (T) has a stop device (60, 70) for limiting the maximum deployment position of the high lift flap (K).</p> |
