Fuselage element comprising a fuselage segment and junction means, fuselage portion, fuselage and aircraft
US8876053B2 · kind B2 · utility
4Cited by
6References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jul 2, 2010 |
| Grant date | Nov 4, 2014 |
| Priority date | — |
| Expiry date | Jul 22, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2001/0081
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A fuselage element including a first fuselage segment including a skin, and a junction device for connecting the first segment to a second adjacent fuselage segment is disclosed. The first segment extending along the longitudinal axis of the fuselage element includes stiffening elements extending along the axis. The end of at least one stiffening element extends beyond a free edge of the skin by a predetermined length.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.