Method for shaping panels by a bending operation, in particular panels for aircraft fuselage skin, and apparatus for implementing such method
US4498325A · kind A · utility
4Cited by
4References
10Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Sep 29, 1982 |
| Grant date | Feb 12, 1985 |
| Priority date | — |
| Expiry date | Sep 29, 2002 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB21D11/20
- WIPO fieldMachine tools
- WIPO sectorMechanical engineering
Abstract
A method is disclosed for bending panels which are provided with reinforcing stiffening ribs. The bending is caused by upsetting or elongating the ribs. Apparatus for carrying out the method also is disclosed and includes means which engage the ribs at points spaced a predetermined distance from the panel skin. The invention is particularly applicable to the shaping of aircraft fuselage skin sections.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.