Aircraft fuselage reinforcement system
US9227717B2 · kind B2 · utility
0Cited by
8References
10Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 29, 2010 |
| Grant date | Jan 5, 2016 |
| Priority date | — |
| Expiry date | Dec 29, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2001/0072
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A fuselage of a fiber-reinforced composite material for an aircraft with a skin and with a multiplicity of circumferential stiffeners and only a small number of longitudinal stiffeners, the skin having a multiplicity of local reinforcements.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.