| 发明名称 |
Automated assembly of panelized aircraft fuselages |
| 摘要 |
A facility for assembling aircraft fuselages comprises a plurality of movable cradles. Each cradle is configured to support a fuselage keel structure and assemble a panelized fuselage from the keel structure to obtain a full fuselage contour in a single upright build position. |
| 申请公布号 |
US9205933(B2) |
申请公布日期 |
2015.12.08 |
| 申请号 |
US201514794925 |
申请日期 |
2015.07.09 |
| 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 facility for assembling aircraft fuselages, the facility comprising:
a plurality of movable cradles, each of the movable cradles configured to support a fuselage keel structure; and a movable gantry for loading fuselage keel structures on the cradles, and loading fuselage panels for each of the keel structures to build up from each of the keel structures and assemble obtain a full fuselage contour in a single upright build position without changing fuselage angular orientation. |
| 地址 |
Chicago IL US |
