| 发明名称 |
Method of assembling panelized aircraft fuselages |
| 摘要 |
A method of assembling a panelized aircraft fuselage comprises loading a keel structure on a cradle; attaching stanchions to a floor grid; positioning the floor grid and stanchions over the keel structure and attaching the stanchions to the keel structure; obtaining a full fuselage contour including locating lower panels on the floor grid while using the cradle, the floor grid, and the keel structure to support the lower panels, and locating upper panels on the lower panels; and fastening the lower panels to the keel structure and the upper panels. The fuselage is assembled upright from the keel structure without changing orientation of the fuselage. |
| 申请公布号 |
US9090357(B2) |
申请公布日期 |
2015.07.28 |
| 申请号 |
US201113327669 |
申请日期 |
2011.12.15 |
| 申请人 |
The Boeing Company |
发明人 |
Oberoi Harinder S.;Nelson Blair P.;Draper Alan S.;Hu Charles Y.;Matthewson Randall;Sarh Branko |
| 分类号 |
B64F5/00 |
主分类号 |
B64F5/00 |
| 代理机构 |
|
代理人 |
Gortler Hugh P. |
| 主权项 |
1. A method of assembling a panelized aircraft fuselage, the method comprising:
loading a keel structure on a cradle; attaching stanchions to a floor grid; positioning the floor grid and stanchions over the keel structure and attaching the stanchions to the keel structure; obtaining a full fuselage contour including locating lower panels on the floor grid while using the cradle, the floor grid, and the keel structure to support the lower panels, and locating upper panels on the lower panels; and fastening the lower panels to the keel structure and the upper panels, wherein the fuselage is assembled upright from the keel structure without changing orientation of the fuselage. |
| 地址 |
Chicago IL US |
