| 发明名称 | Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces | ||
| 摘要 | A composite structure including a panel and a stringer bonded to the surface of the panel, the stringer having an end surface and a pair of sides extending lengthwise along the stringer away from the end surface. The surface of the panel is formed with a first wall which engages the end surface of the stringer and a second wall which engages another part of the stringer. Compressive forces are transmitted from the panel to the stringer by a normal reaction between the first wall formed in the surface of the panel and the end surface of the stringer. Tensile forces are transmitted from the panel to the stringer by a normal reaction between the second wall formed in the surface of the panel and the other surface of the stringer. | ||
| 申请公布号 | US9371127(B2) | 申请公布日期 | 2016.06.21 |
| 申请号 | US200812451178 | 申请日期 | 2008.04.15 |
| 申请人 | Airbus Operations Limited | 发明人 | Cosentino Enzo |
| 分类号 | B64C1/00;B64C1/12;B29D99/00;B29L31/30 | 主分类号 | B64C1/00 |
| 代理机构 | Nixon & Vanderhye P.C. | 代理人 | Nixon & Vanderhye P.C. |
| 主权项 | 1. A composite structure comprising: a panel; and a stringer bonded to a surface of the panel, the stringer having an end surface and a pair of sides extending lengthwise along the stringer away from the end surface, wherein the surface of the panel is formed with a first wall which abuts the end surface of the stringer and a second wall opposite to said first wall, said second wall abuts another part of the stringer. | ||
| 地址 | Bristol GB | ||