Aircraft fuselage
US8336823B2 · kind B2 · utility
1Cited by
6References
12Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Dec 21, 2007 |
| Grant date | Dec 25, 2012 |
| Priority date | — |
| Expiry date | Nov 13, 2028 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2001/0045
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft fuselage including a front part including a cockpit, a central part, and a rear part. The central part of the fuselage includes a first zone located at the front part and that increases in width to a maximum width towards the rear of the aircraft, a second zone that decreases in width, and a third zone that has an essentially constant width and is located behind the second zone, width begin measured along the pitch axis.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.