| 发明名称 |
STRUCTURAL MEMBER AND ASSOCIATED METHOD |
| 摘要 |
The present disclosure relates to a structural member for an aircraft or spacecraft, including a first part having a first material having a first coefficient of thermal expansion and a second part including a second material having a second coefficient of thermal expansion, wherein the first part and the second part are rigidly connected with each other, and wherein the second part is configured to induce forces in the first part upon a drop in temperature to counteract loading stresses. A corresponding method of forming a structural member is also provided. |
| 申请公布号 |
US2014370256(A1) |
申请公布日期 |
2014.12.18 |
| 申请号 |
US201414303216 |
申请日期 |
2014.06.12 |
| 申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
BENTHIEN Hermann;HEGENBART Matthias;MICHAILIDIS Ioannis;RENNER Mathias |
| 分类号 |
B64C1/00;B32B7/02;B32B15/08;B32B37/14 |
主分类号 |
B64C1/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A structural member for an aircraft or spacecraft, comprising:
a first part comprising a first material having a first coefficient of thermal expansion; and a second part comprising a second material having a second coefficient of thermal expansion; wherein the first part and the second part are rigidly connected with each other, and wherein the second part is configured to induce forces in the first part upon a drop in temperature to counteract loading stresses. |
| 地址 |
Hamburg DE |
