FOLDABLE WING FOR AN AIRCRAFT AND AIRCRAFT HAVING FOLDABLE WING

A foldable wing for an aircraft includes a base wing having a base wing end region, a wing tip having a connection region, a first engagement means integrated into the base wing, a second engagement means integrated into the wing tip, and a drive mechanism coupled with the wing tip for moving the wing tip relative to the base wing. The first and second engagement means are adapted for engaging each other along a sliding course from a first position, in which the connection region of the wing tip and the base wing end region are in a flush contact to form a continuous wing, up to a second position, in which the first engagement means and the second engagement means disengage. The drive mechanism includes a first movement element and a second movement element at least partially extending in a spanwise direction, and supported in a linear guide each. 种用于飞行器的可折叠机翼，包括基翼、翼梢、整合到基翼中的第接合装置、整合到翼梢中的第二接合装置、以及与翼梢联接以使翼梢相对于基翼移动的驱动机构。第和第二接合装置适于沿着从第位置直到第二位置的滑动路线彼此接合，在第位置翼梢的连接区域与基翼端部区域齐平地接触以形成连续翼，在第二位置第和第二接合装置断开接合。驱动机构包括至少部分地沿