| 发明名称 | Method and apparatus for attaching an aircraft fuselage frame to a wing box | ||
| 摘要 | The present disclosure is generally directed to an aircraft body including a fuselage skin on an outboard member of the aircraft body and a wing box extending through a member of the aircraft body. The wing box being enclosed and capable of being pressurized is fixedly attached at an outer surface to at least one pair of an attachment member and an attachment link member that is fixedly attached to the aircraft body. | ||
| 申请公布号 | US8857765(B2) | 申请公布日期 | 2014.10.14 |
| 申请号 | US201213652975 | 申请日期 | 2012.10.16 |
| 申请人 | The Boeing Company | 发明人 | Thomas Grant Brian;Lin Chun-Liang;Andrews Francis E.;Choy Wendell C. K. |
| 分类号 | B64C1/00 | 主分类号 | B64C1/00 |
| 代理机构 | Hope Baldauff LLC | 代理人 | Hope Baldauff LLC |
| 主权项 | 1. An aircraft comprising: an aircraft body including a fuselage skin on an outboard member of the aircraft body; a wing box extending through a member of the aircraft body, the wing box being enclosed and capable of being pressurized; andat least one pair of an attachment member and an attachment link member fixedly attached to an outer surface of the wing box and the fuselage skin, the attachment member including an upwardly extending projection that receives the outboard member of the aircraft body, a downwardly extending member that receives the outboard member of the aircraft body and the outer surface of the wing box, and an inboard extending projection that receives the attachment link member being connected to an inboard outer surface of the wing box. | ||
| 地址 | Chicago IL US | ||