SAE 7249 Aluminium Alloys

Material group: Nonferrous Alloys / Aluminium Alloys
Country / Standard: United States / SAE
Indicative price:

Data updates

Latest Update: 2024-10
Total number of updates: 10
Update History

This material has 217 properties — only a subset is shown here.

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SAE 7249 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
Remainder
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
Cr
VALUE
0.12 – 0.18
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
1.3 – 1.9
UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mg
VALUE
val1
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UNIT
%
CAS NUMBER
7439-95-4
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Other each
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Other total
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
Zn
VALUE
val1
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UNIT
%
CAS NUMBER
7440-66-6

SAE AMS 4334B: 1995 / Aluminum Alloy, Forgings 7.8Zn - 2.2Mg - 1.6Cu - 0.15Cr (7249-T74 and -T7452)

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SAE 7249 Physical Properties


Temperature

PROPERTY / VALUE
Compression Modulus
72 — 74 GPa
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Modulus of Elasticity
69 — 79 GPa
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Density
val1
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kg/dm³
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Electrical Conductivity
val1
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S/m
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Thermal Conductivity
val1
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W/(m∙°C)
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Electrical Resistivity
≤ 0.0466 Ω∙mm²/m
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Poisson Coefficient
val1
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Shear Modulus
val1
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GPa
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This material has 217 properties — only a subset is shown here.

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SAE 7249 Heat Treatments


  • Solution Heat Treatment: Heat to 466 to 477°C (870 to 890°F), hold at heat for a time commensurate with product thickness and rapidly cool in a suitable quenching medium.
  • Solution heat treating at 468°C for all forms (the aging treatment for 7049 alloy shall not be initiated until at least 48h at room temperature have elapsed after quenching), (to avoid stress corrosion cracking of thick 7049 parts, delay between quenching and start of aging should not exceed 72h).
    Solution heat treating soaking times and maximum quench delay times is on specifications.
    Aging treatment is mandatory. For forgings: Starting temper is W, final temper is T73 (sometimes used to designate final tempers), 1st step: aging at 121°C for 10-12h, 2nd step: aging at 162°C for 6.5-7.5h. For extrusions: Starting temper is W, final temper is T76 (sometimes used to designate final tempers), 1st step: aging at 121°C for 4-28h, 2nd step: aging at 162°C for 4-10.
    Full anneal: At 399-427°C, soaking time is minimum 2h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in furnace (furnace cool at 28°C degrees per hour maximum, to 232°C, hold at 232°C for 6 hours, furnace or air cool to room temperature). Stress relief: At 333-349°C, soaking time is minimum 2h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in air.

SAE 7249 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 455 MPa
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Brinell Hardness (HB)
≥ 135
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Compression Yield Strength
val1
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MPa
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Elongation, A
≥ 5 %
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Yield Strength, Rp0.2
val1
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MPa
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SAE 7249 International Equivalent Materials


Showing 3 of 3 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
AA
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
ISO
COUNTRY / PRODUCER
International
EQUIVALENCE CATEGORY
Composition 100%

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  • 3Cross References

  • 22Composition
  • 131Mechanical Properties
  • 15Physical Properties
  • 4Heat Treatment
  • 2Metallography
  • -Machinability

  • 40Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • -Creep

  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation

  • -Total Suppliers