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7065 aluminium alloy

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This is the current revision of this page, as edited by Ivtue (talk | contribs) at 04:08, 8 April 2024 (Adding local short description: "Aluminum zinc alloy", overriding Wikidata description "aluminum alloy"). The present address (URL) is a permanent link to this version.

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7065 is high zinc containing aluminum alloy. It is used for making plate.

Chemical Composition

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Element[1] Weight percentage
Aluminum 87.02 - 89.45 %
Chromium <= 0.04 %
Copper 1.9 - 2.3 %
Iron <= 0.08 %
Magnesium 1.5 - 1.8 %
Manganese <= 0.04 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon <= 0.06 %
Titanium <= 0.06 %
Zinc 7.1 - 8.3 %
Zirconium 0.05 - 0.15 %

Properties

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7065-T7451 alloy properties[2]
Property Value
Ultimate Tensile strength 77 ksi
Yield strength 71 ksi
Elongation percentage 11%

Application

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  1. Plate
  2. Aerospace
  3. The combination of high strength and fracture toughness properties and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475 and other alloys for critical intermediate thickness applications.[3]
  4. Spar, rib, and integrally machined structural parts for new, derivative, or retrofit aircraft.[3]

References

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  1. ^ "Aluminium 7065 composition".
  2. ^ "Aluminum alloy properties" (PDF). Archived (PDF) from the original on 2016-11-14.
  3. ^ a b "Aluminum 7065 alloy". Archived from the original on 2021-01-08.

Aluminum alloy table

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