| 摘要 |
A high- lift system on a wing of an aircraft, which wing comprises a right-hand (46) and a left-hand (44) wing half with movably held high-lift flaps (16, 18) and is attached to an aircraft fuselage, thus forming a wing root (30), in each wing half in a region in close proximity to the wing root, comprises a drive unit (32). In each case this drive unit is joined to a transmission shaft (34) mechanically connected to the respective drive unit, which transmission shaft extends from the drive unit in the direction of the end of the respective wing half and is designed to mechanically move the high- lift flaps arranged in the respective wing half. By means of such an arrangement it is possible to do without deflection gear arrangements from a central drive unit to the individual wing halves. |
