|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-10 2004 045 651(2004-09-21)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 10 인용 특허 : 7|
A wing, particularly an airfoil of an aircraft, having a changeable profile, which extends in the wing depth direction (5) running essentially in the flow direction and transversely thereto in the wing span direction and has a first planking (55a) and a second planking (55b), and having a flexible area (11), through which the profile of the wing (1) is adjustable, is described. The flexible area (11) may comprise one or more than one vortex elements (154") extending in a longitudinal direction, which are connected to one another in an articulated way on ...
What is claimed is: 1. A wing having a changeable profile and extending in an airflow direction and in a direction substantially transverse to the airflow direction, the wing comprising: a first planking; a second planking; and an adjustment mechanism; comprising: a drive element, a lever element, and a vortex element having a drive or adjustment area, wherein the lever element is coupled, rotatably or pivotably, between the second planking on a first side of the lever element and the drive or adjustment area of the vortex element at an axis of rotatio...