| 发明名称 |
ADJUSTABLE LIFT MODIFICATION WINGTIP |
| 摘要 |
An adjustable lift modification wingtip may be attached to a baseline wing of an aircraft. The adjustable lift modification wingtip may comprise a horizontal portion including a control surface and a vertical portion coupled to the horizontal portion. The vertical portion may move about an axis that may be substantially perpendicular to the horizontal portion. The control surface and the vertical portion may be adjusted in conjunction to increase wing efficiency at a flight condition. |
| 申请公布号 |
US2016009378(A1) |
申请公布日期 |
2016.01.14 |
| 申请号 |
US201314097122 |
申请日期 |
2013.12.04 |
| 申请人 |
Tamarack Aerospace Group, Inc. |
发明人 |
Guida Nicholas R. |
| 分类号 |
B64C23/06;B64C13/16;B64C5/10 |
主分类号 |
B64C23/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A winglet fixedly attachable to a baseline wing of an aircraft comprising:
a horizontal portion comprising a control surface; and a vertical portion coupled to the horizontal portion, the vertical portion being configured to move about an axis that is substantially perpendicular to the horizontal portion, the control surface and the vertical portion which, when attached to the baseline wing of the aircraft increase wing efficiency at a flight condition. |
| 地址 |
Sandpoint ID US |
