Patent · US Expired

Aluminum alloy products suited for commercial jet aircraft wing members

US5863359A · kind A · utility

23Cited by
16References
34Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 9, 1995
Grant dateJan 26, 1999
Priority date
Expiry dateJun 9, 2015

Classification

  • Technology area (CPC C)Chemistry; Metallurgy
  • CPC primaryC22C21/16
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

There is claimed a lower wing structure for a commercial jet aircraft which includes a substantially unrecrystallized rolled plate member made from an aluminum alloy consisting essentially of about 3.6 to 4.0 wt. % copper, about 1.0 to 1.6 wt. % magnesium, about 0.3 to 0.7 wt. % manganese, about 0.05 to 0.25 wt. % zirconium, the balance aluminum and incidental elements and impurities. On a preferred basis, the alloy products of this invention include very low levels of both iron and silicon, typically on the order of less than 0.1 wt. % each, and more preferably about 0.05 wt. % or less iron and about 0.03 wt. % or less silicon. This alloy composition may be rolled to form lower wing skin plates and extruded or rolled to form wing box stringers therefrom.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.