Wing of an aircraft or spacecraft, comprising a mobile flow body

摘要

A wing of an aircraft or spacecraft, the wing including at least a movable flow body, the wing including a movable support member, which is connected to the flow body, for rotating the flow body on the wing, the wing including a flow body control element, the flow body control element being fixed to the wing in a first point and the support member in a second point, the two points of the flow body control element and of the support member forming an axis, the flow body control element being formed at a predetermined angle to the axis and the flow body control element guiding the flow body in a predetermined plane about this axis.

主权项

1. A wing of an aircraft or spacecraft, the wing comprising:
at least a movable flow body, wherein: the wing comprises a movable support member, which is connected to the flow body, for rotating the flow body on the wing, wherein the support member is connected to the flow body and the wing, the wing comprising a flow body control element, wherein the flow body control element is connected to the flow body and the wing, the flow body control element being connected to the wing in a first point and the support member being connected to the wing in a second point, which is a bearing point defined on both the support member and the wing, the two points of the flow body control element and of the support member forming an axis, the flow body control element being formed at a predetermined angle to the axis and wherein the flow body control element guides the flow body in a predetermined plane about the axis, wherein at least one point of the flow body control element at which said flow body control element is connected to the flow body and a point of the support member at which said support member is connected to the flow body each form a separate connected point or a common connection on the flow body.