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发明公开
CN102365203A 具有高升力襟翼的翼型 有权

具有高升力襟翼的翼型
摘要：
一种机翼(T)，该机翼(T)具有主翼面(H)、高升力襟翼(K)，高升力襟翼(K)设置在机翼(T)上使高升力襟翼(K)能够借助于至少两个调整机构(1、2)运动，至少两个调整机构(1、2)沿着机翼(T)的翼展方向并排设置并且能够借助于驱动装置(50)调整，每个调整机构(10)均具有：第一调整杆(11、21)，该第一调整杆(11、21)通过第一枢转铰接部(13、23)铰接在主翼面上，形成第一旋转轴线(A11、A21)；第二调整杆(12、22)，该第二调整杆(12、22)通过第二枢转铰接部(13、23)铰接在高升力襟翼(K)上，形成第二旋转轴线(A21、A22)；中心铰接部(15、25)，该中心铰接部(15、25)将第一调整杆(11、21)和第二调整杆(12、22)连结在一起，形成第三旋转轴线(A31、A32)。其中中间铰接部件(Z)设置在至少一个调整机构(1、2)上，以联接第一调整杆(11、21)和主翼面(H)，或联接第二调整杆(12、22)和高升力襟翼(K)。
摘要（英）：

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).

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