AL-P16 (Italy / UNI) Material Properties
Material group:
Nonferrous Alloys / Aluminium
Country/Standard:
Italy / UNI
Data updates
Latest Update: 2020-12
Total number of updates: 2
Update History:
2019-11
Mechanical Properties
Temperature
Physical Properties
Temperature
Composition
CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
Remainder
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
Cr
VALUE
≤ 0.10
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
3.9 – 5.0
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
EN 2125: 2019 / Aerospace series - Aluminium alloy Al-P16-T6151 - Plates - 6 mm < a ≤ 120 mm
Heat Treatments
- <b> Delivery heat treatment: </b><br> <b> Solution treated T451 </b> <br> Solution treated 503°C ± 5°C, quenched in water θ ≤ 40°C; <br> 1.5% ≤ controlled stretched ≤ 3% <br> <b> Solution treated and Artificially aged T6151 </b> <br> Solution treated 503°C ± 5°C, quenched in water θ ≤ 40°C; <br> 1.5% ≤ controlled stretched ≤ 3%. <br> Artificially aged 180°C ± 5°C, 3h ≤ t ≤ 7h <br> <br> <b> Heat treatment - Use: </b> <br> <b> Solution treated and Artificially aged T6151 </b> <br> Delivery condition then Artificially aged 180°C ± 5°C, 3h ≤ t ≤ 7h
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151 Cross References
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12 Composition
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51 Mechanical Properties
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5 Physical Properties
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1 Heat Treatment
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- Metallography
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- Machinability
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- Stress-Strain
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- Formability
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- Fatigue
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- Fracture
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- Creep
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- Joints
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- Coatings
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- Dimensions
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- Tribology
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- Corrosion
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- Ageing
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- Weatherability
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- Irradiation
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- Total Suppliers