Patent · US Active

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 dateMay 13, 2008
Grant dateMay 13, 2014
Priority date
Expiry dateNov 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.