Metals & alloys · Aluminium alloys

7050-T7451 aluminium alloy

A high-strength, thick-section Al–Zn–Mg–Cu aerospace plate alloy developed for improved stress-corrosion resistance and through-thickness toughness relative to many 7075 products.

Family
7xxx Aluminium Alloy
Record
Standard
Conditions
2
Sources
3
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01

Overview

Material class
Metals & alloys
Category
Aluminium alloys
Family
7xxx Aluminium Alloy
Product forms
Sheet/plate, Bar/rod, Casting

Composition

ConstituentMinMaxTypicalNote
Zn5.76.76.2
Mg1.92.62.3
Cu22.62.3
Zr0.080.150.12
Fe0.150.08
AlBalance

02

Properties and conditions

Engineering properties

PropertyValueUnitCondition
Density2.83g/cm³Representative; verify product form and condition
Elastic modulus71.7GPaRepresentative; verify product form and condition
Yield strength~455–505MPaT7451 plate
Tensile strength~510–570MPaRepresentative; verify product form and condition
Elongation7–12%Representative; verify product form and condition
Fracture toughnesshighproduct/thickness dependent

Conditions

temper

T7451

Overaged and stress-relieved plate condition.

temper

T7651

Intermediate overage and stress-relieved condition.

03

Processing and use

Processing

  • Product form, thermal history and manufacturing route materially affect performance.

Applications

  • Wing spars
  • Bulkheads
  • Fuselage frames
  • Thick machined structures

Selection considerations

  • Use the current governing standard and supplier certification for design or procurement.

04

Standards and related materials

Standards and designations

SystemDesignationNote
AA7050-T7451
UNSA97050
AMS4050plate

05

Sources and context

Sources

Confirm the applicable specification, product form and condition before using values for design or procurement.

Supply and sustainability

Availability and lead time depend on grade, product form, certification and regional supply chain.

Segregated recovery and closed-loop recycling improve material efficiency where practical.