AL-P7175 (Italy / UNI) Material Properties
Material group:
Nonferrous Alloys / Aluminium
Country/Standard:
Italy / UNI
Data updates
Latest Update: 2025-01
Total number of updates: 2
Update History:
2019-06
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
0.1800 – 0.2800
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
1.2000 – 2.0000
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 4215: 2005 / Aerospace series - Aluminium alloy AL-P7175-T651 - Plate - 6 mm < a ≤ 80 mm
Heat Treatments
- 460 °C <= θ <= 480°C / WQ θ <= 40°C+ 1,5 % <= controlled stretched <= 3 % + 100°C <= θ <= 135°C / 3 h <= t <= 24 h + 155°C <= θ <= 175°C / 8 h <= t <= 30 h.
- 460°C <= T <= 500°C / WQ T <= 40°C; +1.5% <= controlled stretched <= 3%; +115°C <= T <= 125°C / 20h <= t <= 30h or +125°C <= T <= 138°C / 12h <= t <= 18h. Artificial ageing may be carried out using the following alternative single stage method: heating to a temperature of 155°C = θ = 175°C at a rate not exceeding 20°C/h and soaking at this temperature for 8 h = t = 30 h.
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72 Cross References
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44 Composition
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108 Mechanical Properties
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7 Physical Properties
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4 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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42 Total Suppliers