|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-10 2005 023 117 (2005-05-19); DE-10 2005 028 688 (2005-06-21)|
|§371/§102 date||20071114 (20071114)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 10|
A device for adapting aerodynamic characteristics of a wing element, includes a winglet, movably attachable to a wing element. The winglet or parts of the winglet may be rotatable in relation to the wing element such that an associated rotary axis with a main direction of extension of the wing element encompasses an angle that differs from an angle of 90°. In addition, a method is disclosed.
1. An adaption device for adapting aerodynamic characteristics of a wing element, comprising: a winglet movably attachable to the wing element, wherein the winglet is attachable on an attachment axis to the wing element, such that the winglet is rotatable around the attachment axis as a rotary axis having a rotary axis direction, and an angle between the rotary axis direction and a direction of a main axis of extension of the wing element differs from 90°, wherein the direction of the main axis of extension is perpendicular to an axial direction along th...