EN
AW-2017A alloy belongs to the group of Al-Cu-Mg alloys, susceptible
to heat treatment. In the precipitation hardening process, they gain
high strength properties. The EN AW-2017A alloy in hardened condition
T4 / T451 is characterized by high tensile strength, fatigue
strength, and hardness. I also have good machinability. It is used
for the production of aircraft structural components, parts for
machine construction, and components for the automotive and military
industries. Alloy
markings according to different standards:
Alloy
AA
PN
CSN
ASTM USA
BS GB
DIN GER
EN
ISO
JIS Japan
2017A
2017
PA6
424201
2017
2017A
AlCuMg1
2017A
AlCu4MgSiA
A2017
NF France
SFS Finland
SN Switz
SS Sweden
UNI Italy
UNS
WNR Germany
NS
2017A
–
–
–
9002/2
A92017
3.1325
–
UNE
ASV
ALUSUISSE
CSA Old
GOST old
L-3120
–
2100
CM41
D1/V65
Alloy composition according to EN 573-1:
Alloy
Mg [%]
Mn [%]
Fe [%]
Si [%]
Si+Fe [%]
Cu [%]
Zn [%]
Cr [%]
Mn+Cr [%]
2017A
0,40-1,00
0,40-1,00
≤0,70
0,20 – 0,80
–
3,50 – 4,50
≤0,25
≤0,10
–
Ti [%]
Bi [%]
Ni [%]
Pb [%]
Sn [%]
Zr [%]
Zr+Ti [%]
Inne [%]
Inne razem [%]
Al [%]
–
–
–
–
–
–
≤0,25
≤0,05
≤0,15
rest
Strength properties according to EN 485-2:
Alloy
Tensile strength Rm min.
The
yield point Rp02 min.
Elongation min. A
Hardness Scalle Brinella
2017A T4
350-390 [MPa]
240-260 [MPa]
12 [%]
110 [HB]
EN AW-6082 alloy belongs to the group of Al-Mg-Si alloys, also susceptible to heat treatment. When hardened T6 / T651, the material is characterized by high mechanical strength, impact strength, corrosion resistance, and polishability. It is used, among others, in the automotive, shipbuilding and railway industries.
