| 发明名称 |
FUSELAGE SECTION AND TRANSVERSE BUTT JOINT CONNECTING TWO FUSELAGE SECTIONS OF AN AIRCRAFT OR SPACECRAFT |
| 摘要 |
A fuselage section of an aircraft or spacecraft includes a stringer, an outer skin on the inside of which the stringer is arranged, and a stringer coupling. The stringer coupling includes a first coupling portion, by means of which the stringer coupling is connected to the stringer at a head end of the stringer, and a second coupling portion which is planar and by means of which the stringer coupling is connected to the outer skin so as to overlap the head end of the stringer in the longitudinal direction of the stringer. The second coupling portion has a wider surface area than the first coupling portion and the stringer, such that the stringer is widened beyond the head end in the longitudinal direction by means of the stringer coupling. |
| 申请公布号 |
US2016318594(A1) |
申请公布日期 |
2016.11.03 |
| 申请号 |
US201615141078 |
申请日期 |
2016.04.28 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Paul Carsten |
| 分类号 |
B64C1/06;B64F5/00 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuselage section of an aircraft or spacecraft, comprising:
a stringer; an outer skin on the inside of which the stringer is arranged; and a stringer coupling that comprises a first coupling portion, by means of which the stringer coupling is connected to the stringer at a head end of the stringer, and comprises a second coupling portion which is planar and by means of which the stringer coupling is connected to the outer skin so as to overlap the head end of the stringer in the longitudinal direction of the stringer, wherein the second coupling portion has a wider surface area than the first coupling portion and the stringer, such that the stringer is widened beyond the head end in the longitudinal direction by means of the stringer coupling. |
| 地址 |
Hamburg DE |
