| 摘要 |
<p>1. A driving and guiding mechanism of a flap system arranged on an airfoil (1), in particular of a trailing edge flap system of a trans-sonic aeroplane wing for commercial and transport aircraft, whereby in the span direction the flap system is divided into separate segments which over their extent have a limited torsion-soft configuration and are individually actuated, comprizing spindle mechanisms (25, 28, 29) which are frictionally connected to the segments and acted on by a drive unit, and guide rails (16, 116) which determine the path curve of the segments during extension/retraction, characterized in that the drive system for the spindle mechanisms (25, 28, 29) is designed so that the rates of feed of the individual spindle mechanisms can be controlled independently of each other.</p> |
