基本信息:
- 专利标题： WING FOR AN AIRCRAFT
- 申请号：EP23181114.2 申请日：2023-06-23
- 公开(公告)号：EP4303123A1 公开(公告)日：2024-01-10
- 发明人： BENSMANN, Stefan
- 申请人： Airbus Operations GmbH
- 申请人地址： DE 21129 Hamburg Kreetslag 10
- 代理机构： LKGLOBAL Lorenz & Kopf Patentanwalt Attorney at Law PartG mbB
- 优先权： DE102022116950 20220707
- 主分类号： B64C9/02
- IPC分类号： B64C9/02 ; B64C3/50 ; B64C9/22 ; B64C9/16 ; B64C9/08 ; B64C13/28 ; B64C9/18 ; B64C9/24 ; B64C3/18 ; B64C3/28 ; F16H19/04 ; B64C9/14
摘要：
A wing for an aircraft is proposed, comprising a leading edge as a first chordwise edge, a trailing edge as a second chordwise edge, an upper skin extending between the leading edge and the trailing edge, a lower skin extending between the leading edge and the trailing edge, at least one spar extending between the upper skin and the lower skin in a spanwise direction to create wing box with the upper skin and the lower skin, and at least one high lift control surface movably supported at at least one of the chordwise edges by a support device, wherein the support device is attached inside or reaches into the wing box at least partially.
IPC结构图谱:
| B | 作业；运输 |
| --B64 | 飞行器；航空；宇宙航行 |
| ----B64C | 飞机；直升飞机 |
| ------B64C9/00 | 可调节的操纵面或操纵部件，例如舵 |
| --------B64C9/02 | .安装或其支承 |