| 发明名称 | Aircraft wing box joint | ||
| 摘要 | An aircraft wing box spanwise joint, comprising a rib having a web, and a pair of rib fittings joined together, each rib fitting forming a closed loop around the periphery of the rib, wherein the rib is integrally formed with one of the rib fittings. Also, an aircraft wing including two or more of the joints. Also, a method of forming an aircraft wing box spanwise joint, the method comprising forming a pair of rib fittings, wherein one of the rib fittings is integrally formed with a rib having a web, each rib fitting forming a closed loop around the periphery of the rib, bringing the rib fittings together, and joining the rib fittings together. | ||
| 申请公布号 | US9004406(B2) | 申请公布日期 | 2015.04.14 |
| 申请号 | US201113697847 | 申请日期 | 2011.06.03 |
| 申请人 | Airbus Operations Limited | 发明人 | Soenarjo Mochamad Agoes |
| 分类号 | B64C1/26;C08L23/02;C08K5/14;C08K5/3492;B64C3/18;C08K3/04 | 主分类号 | B64C1/26 |
| 代理机构 | Lowe Hauptman & Ham, LLP | 代理人 | Lowe Hauptman & Ham, LLP |
| 主权项 | 1. An aircraft wing box spanwise joint comprising a rib having a web, and a pair of rib fittings, wherein the rib is integrally formed with one of the rib fittings, each rib fitting including a planar abutment surface and a spanwise projecting flange forming a closed loop around the periphery of the rib, and wherein the rib fittings are joined back-to-back by their planar abutment surfaces. | ||
| 地址 | Bristol GB | ||