| 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 (1, 2) that are located next to one another in the direction of the span of the aerofoil (T) and that are adjusted by means of a drive device (50), each of said adjusting mechanisms (10) having: a first adjusting lever (11, 21), hinged to the main wing by means of a first pivot joint (13, 23), forming a first rotational axis (A11, A21); a second adjusting lever (12, 22), hinged to the high lift flap (K) by means of a second pivot joint (23), forming a second rotational axis (A21, A22), a central joint (15, 25) which hinges the first adjusting lever (11, 21) to the second adjusting lever (12, 22), forming a third rotational axis (A31, A32). An intermediate joint part (Z) for coupling the first adjusting lever (11, 21) to the main wing (H), or for coupling the second adjusting lever (12, 22) to the high lift flap (K) is located on at least one of the adjusting mechanisms (1, 2).</p> |
