UNI 7010A Aluminium Alloys
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UNI 7010A Chemical Composition
UNI 9007-4: 1988 / Wrought primary aluminium and aluminium alloys, Aluminium-zinc alloys, Al Zn 6,2 Mg 2,3 Cu 1,8 Zr 0,12 Mn 0, Ti 0,04 (7010 A)
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UNI 7010A Physical Properties
Temperature
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UNI 7010A Heat Treatments
- Full Annealing (O) from 400 to 430°C for 1 to 3h to scheme with subsequent slow cooling in the oven (max. 25°C/h up to 200°C).
T6 - Hardening in water (up to 40°C) from 465 to 485°C, after preheating for 0.5 to 3h in scheme followed by artificial aging from 120 to 130°C for 24h to scheme.
T651 - Heat treatment equal to T6, planned for the laminates that receive after quenching and before aging. Artificial a relaxing ironing involving a permanent deformation of 1.5 to 3%
T6510 - Heat treatment equal to T6, planned for the extrudes that receive after quenching and before aging artificial a relaxing ironing comprising a 1 to 3% permanent deformation.
T6511 - Heat treatment equal to T6510, provided for receiving the extruded modest operations of straightening after ironing, for reasons of dimensional tolerances.
T652 - Heat treatment equal to T6, planned for forgings that receive after quenching and before aging artificial operation of cold compression for stretching the material comprising a permanent deformation from 1 to 4%
T76 Quenching in water (<40°C) from 465 to 485°C after preheating for 0.5 to 3 hours to scheme, followed by artificial aging in two stages the first of which from 100 to 110° C for 8 to 12h in scheme and the second from 155 to 160°C for 16 to 20h to scheme.
T73 - Quenching in water (<40°C) from 465 to 485°C after preheating for 0.5 to 3h to scheme, followed by artificial aging in two stages the first of which from 100 to 110°C for 8 to 12 has scheme and the second from 163 to 168°C for 22 to 26 has scheme.
T7352 - Heat treatment equal to T73, foreseen for the forgings and the printed receiving after hardening and before the first artificial aging stage a cold compression.
UNI 7010A Mechanical Properties
Temperature
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UNI 7010A International Equivalent Materials
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Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.
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- 1Cross References
- 12Composition
- 173Mechanical Properties
- 14Physical Properties
- 1Heat Treatment
- -Metallography
- -Machinability
- 44Stress-Strain
- -Formability
- -Fatigue
- -Fracture
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- -Coatings
- -Dimensions
- -Tribology
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