| 发明名称 |
Fuselage Manufacturing System |
| 摘要 |
A method and apparatus for processing fuselage sections. A first fuselage section is held in a cradle system. A current shape of the first fuselage section in the cradle system is measured. Forces to change the current shape of the first fuselage section to a desired shape for connecting the first fuselage section to a second fuselage section are identified. The forces identified are applied using a system to change the current shape of the first fuselage section towards the desired shape. |
| 申请公布号 |
US2016075451(A1) |
申请公布日期 |
2016.03.17 |
| 申请号 |
US201514717272 |
申请日期 |
2015.05.20 |
| 申请人 |
The Boeing Company |
发明人 |
Hunt Jeffrey H.;Hussain Naveed Moayyed |
| 分类号 |
B64F5/00;G01S17/89;B21D31/00;G01B11/25 |
主分类号 |
B64F5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus comprising:
a cradle system that holds a first fuselage section; a system that applies forces to the first fuselage section to change a current shape of the first fuselage section; a metrology system that makes measurements of the current shape of the first fuselage section; and a controller that receives the measurements from the metrology system, identifies the forces to change the current shape of the first fuselage section towards a desired shape for connecting the first fuselage section to a second fuselage section, and sends commands to the system to apply the forces to change the current shape of the first fuselage section towards the desired shape. |
| 地址 |
Chicago IL US |
