Wing unit`s aerodynamic characteristics adapting device for e.g. aircraft, has winglet rotatable in relation to wing unit, such that angle between rotary axis and main direction of extension of unit differs from specified degree

摘要

The device has a winglet movably attachable to a wing unit (1), and rotatable in relation to the wing unit, such that an angle between an associated rotary axis (7) and a main direction of extension (6) of the wing unit differs from 90 degree. An aerodynamic fairing unit is arranged between the wing unit and the winglet and/or winglet parts. A suspension unit is provided for attaching the winglet to the wing unit and movable by using a driven spindle. Independent claims are also included for the following: (1) a method for adapting aerodynamic characteristics of a wing unit (2) a locomotion device comprising an adaption device.