Aircraft structural element located at the interface between a wing and the fuselage
US8720823B2 · kind B2 · utility
3Cited by
15References
13Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 13, 2008 |
| Grant date | May 13, 2014 |
| Priority date | — |
| Expiry date | Nov 16, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C1/06
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft structural element situated at an interface between a wing and the fuselage, and including a web and profiled elements flanking the web. At least one the profiled element includes a flat part positioned without overlap in the continuation of a flat part of the web and connected thereto by a welded butt joint using friction stir welding.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.