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EP0088511A1 Expired / Lapsed EP ⏱️ 0.0 years remaining

Improvements in or relating to aluminium alloys

Assignee: Qinetiq Ltd
•
Filing: 1983-02-01
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Granted: —
•
Expires: 2003-02-01
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Abstract

Abstract Aluminium alloys having compositions within the ranges (in wt%) 2 to 2.8 lithium - 0.4 to 1 magnesium - 1 to 1.5 copper - 0 to 0.2 zirconium - 0 to 0.5 manganese - 0 to 0.5 nickel - 0 to 0.5 chromium - balance aluminium. The alloys are precipitation hardenable and exhibit a range of properties, according to heat treatment, which make them suitable for engineering applications where light weight and high strength are required.

Inventors

  • 👤 Brian Evans
  • 👤 Christopher John Peel

Bibliographic Details

Application Number —
Jurisdiction EP
Data Source google_patents
Last Synchronized 2026-10-31 21:07
CPC Classifications
C; C22; C22C; C22C21/00

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 52 words
An aluminium alloy characterised in that the composition lies within the ranges expressed below in weight per cent; Lithium 2.0 to 2.8 Magnesium 0.4 to 1.0 Copper 1.0 to 1.5 Zirconium 0 to 0.2 Manganese 0 to 0.5 Nickel 0 to 0.5 Chromium 0 to 0.5 Aluminium Balance (except for incidental impurities)
Claim 2
Dependent Claim 52 words
An aluminium alloy characterised in that the composition lies within the ranges expressed below in weight per cent; Lithium 2.0 to 2.8 Magnesium 0.4 to 1.0 Copper 1.0 to 1.5 Zirconium 0 to 0.2 Manganese 0 to 0.5 Nickel 0 to 0.5 Chromium 0 to 0.5 Aluminium Balance (except for incidental impurities)
Claim 3
Dependent Claim 18 words
An aluminium alloy according to claim 1 characterised in that it is produced by an ingot metallurgy route.
Claim 4
Dependent Claim 24 words
An aluminium alloy according to claim 1 characterised in that it has a magnesium content in the range 0.7 to 1.0 weight per cent.
Claim 5
Dependent Claim 18 words
An aerospace airframe structure characterised in that it is produced from an aluminium alloy according to claim 1.

References Cited (Backward Citations)

FR518023A Cited
CH216204A Cited
FR1148719A Cited
FR1161306A Cited
US2915390A Cited
US2915391A Cited
GB1172736A Cited
DE1927500A1 Cited
DE2127909A1 Cited
FR2190930A1 Cited

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