| 发明名称 |
Stiffening Element, Method For Coupling The Same, And Shell Component For An Aircraft Or Spacecraft |
| 摘要 |
A method for coupling a first and a second stiffening element for a skin of an aircraft or spacecraft, wherein the first stiffening element has a cross-sectional profile with first and second web portions extending from a flange portion of a predefined width toward the skin includes forming a coupling zone of the first stiffening element wherein the second web portion is at least partially removed to expose an inner surface of the first web portion, and a step of fastening a coupling element, for coupling the stiffening elements, to the coupling zone of the first stiffening element. |
| 申请公布号 |
US2015225065(A1) |
申请公布日期 |
2015.08.13 |
| 申请号 |
US201514618022 |
申请日期 |
2015.02.10 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Brunner Stefan;Schulze Wolfgang;Tiryaki Memis;Eilken Wolfgang |
| 分类号 |
B64C1/12;B64G1/22 |
主分类号 |
B64C1/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for coupling a first and a second stiffening element for a skin of an aircraft or spacecraft, wherein the first stiffening element has a cross-sectional profile with first and second web portions extending from a flange portion of a predefined width toward the skin, the method comprising:
forming a coupling zone of the first stiffening element wherein the second web portion is at least partially removed to expose an inner surface of the first web portion; and fastening a coupling element, for coupling the stiffening elements, to the coupling zone of the first stiffening element. |
| 地址 |
Hamburg DE |
