|
BMT Brekelmans Techniek B.V. |
| Terug |
| |
| EN AW-6060 / ISO: Al MgSi
Applications |
Evenals de legering AlMgSi 1 is de kwaliteit AlMgSi 0,5 een
precipitatie hardbare legering. Door de gunstige combinatie van
goede warmvervormbaarheid (bijvoorbeeld extruderen) en redelijke
sterkte in uitgeharde toestand wordt deze kwaliteit veelvuldig
gebruikt voor de fabricage van uiteenlopende profielen. Toepassing
van gecompliceerde profielen kan in de produktie een aantal
bewerkingen (zetten, lassen) uitsparen en daardoor de
productieviteit verbeteren.
Onder "normale" atmosferische omstandigheden en ook in wat
agressievere omgevingen zoals maritieme milieus heeft de kwaliteit
AlMgSi 0,5 een uitstekende weerstand tegen corrosie, die nog
verbeterd kan worden door anodiseren.
Bij het lassen dient rekening gehouden te worden met een daling
van de sterkte in de warmtebeïnvloede zone en de gevoeligheid voor
warmscheuren. Door een geschikte warmtebehandeling (oplosgloeien
en uitharden) is de sterkte van de wamtebeïnvloede zone weer op
het oorspronkelijke niveau te brengen. De lasnaad daarentegen zal
in principe altijd een lagere sterkte hebben dan het
basismateriaal. Door de warmscheurgevoeligheid zal in het algemeen
met een geschikt toevoegmateriaal gelast moeten worden.
Toepassingen zijn o.a. te vinden in de apparatenbouw (opslagtanks,
drukvaten), de bouw (dragende constructies, roldeuren),
transportmiddelen en de jachtenbouw (masten).
Lasbaarheid: enigzins gevoelig voor warmscheuren;
daling sterkte
Lastoevoegmateriaal: 5356, 4034
Warmtebehandelingen: warmvervormen 520 -450șC
/ zachtgloeien 360 -400șC, tot 250șC langzaam afkoelen / oplosgloeien
525 -540șC, afschrikken in water / uitharden 155-190șC, 4
gedurende 4 tot 16 uur |
|
|
| |
|
EN AW-6060 / ISO Al MgSi
Corrosion and Anodizing
Properties |
|
Temper
|
Corrosion
|
Anodizing
|
|
|
COA
|
COIA
|
COMA
|
CORA
|
SCOA
|
EXCA
|
ICOA
|
PCA
|
ANBA
|
ANCA
|
ANHA
|
ANPA
|
|
|
6
|
5
|
5
|
6
|
-
|
6
|
6
|
5
|
5
|
6
|
6
|
6
|
|
|
6
|
5
|
5
|
6
|
6
|
6
|
6
|
5
|
5
|
6
|
6
|
6
|
|
|
6
|
5
|
5
|
6
|
6
|
6
|
6
|
5
|
5
|
6
|
6
|
6
|
|
|
6
|
5
|
5
|
6
|
6
|
6
|
6
|
5
|
5
|
6
|
6
|
6
|
|
|
6
|
5
|
5
|
6
|
6
|
6
|
6
|
5
|
5
|
6
|
6
|
6
|
|
|
| Key to Parameters: |
| COA: |
Corrosion index, general |
scale 2-7 |
| COIA: |
Industrial atm corr index |
scale 2-7 |
| COMA: |
Marine atm corr index |
scale 2-7 |
| CORA: |
Rural atm corr index |
scale 2-7 |
| SCOA: |
Stress corrosion index |
scale 2-7 |
| EXCA: |
Exfoliation corrosion index |
scale 2-7 |
| ICOA: |
Intercrystalline corrosion index |
scale 2-7 |
| PCA: |
Pitting corrosion index |
scale 2-7 |
| ANBA: |
Bright anodising index |
scale 2-7 |
| ANCA: |
Colour anodising index |
scale 2-7 |
| ANHA: |
Hard anodising index |
scale 2-7 |
| ANPA: |
Protective anodising index |
scale 2-7 |
|
 |
| Key to Values: |
| -: |
No information available |
|
| 1: |
Not applicable |
|
| 2: |
Unsuitable |
|
| 3: |
Not recommended |
|
| 4: |
Acceptable |
|
| 5: |
Good |
|
| 5-6: |
Good to Very Good |
|
| 6: |
Very Good |
|
| 7: |
Excellent |
|
|
| |
Full tempers: O
| O |
Annealed - products achieving the required annealed
properties after hot forming processes may be designated as O
temper. |
| O1 |
Thermally treated at approximately the same time and
temperature required for solution treatment and slow cooled to
room temperature. |
| O2 |
Thermomechanically processed to enhance formability, such
as required for super-plastic forming (SFP). |
| O3 |
Homogenized. |
|
|
|
| |
Full tempers:
T1
| T1 |
Cooled from elevated temperature shaping process and
naturally aged. |
| T1X |
Cooled from elevated temperature shaping process and
naturally aged. When a second digit is present it is material
dependent and has no general interpretation. |
|
|
|
| |
Full tempers:
T4
| T4 |
Solution heat treated and naturally aged. |
| T42 |
Solution heat treated from the O or the F temper to
demonstrate response to heat treatment, and naturally aged to
a substantially stable condition. |
| T4X |
Solution heat-treated and naturally aged. When a second
digit is present it is material dependent and has no general
interpretation except for T42. |
|
|
|
| |
Full tempers:
T5
| T5 |
Cooled from elevated temperature shaping process and
artificially aged. |
| T5X |
Cooled from elevated temperature shaping process and
artificially aged.When a second digit is present it is
material dependent and has no general interpretation. |
|
|
|
| |
Full tempers:
T6
| T6 |
Solution heat treated and artificially aged. |
| T62 |
Solution heat treated from the O or the F temper to
demonstrate response to heat treatment, and artificially aged. |
| T651 |
Solution heat treated, stress relieved by stretching a
controlled amount (permanent set 1.5 to 3% for sheet and plate,
1 to 3% for rolled or cold finished rod and bar, 1 to 5% for
hand or ring forging and rolled ring) and then artificially
aged. The products receive no further straightening after
stretching. |
| T6510 |
Solution heat treated, stress relieved by stretching a
controlled amount (permanent set 1 to 3% for extruded rod,
bar, shapes and tube, 0.5 to 3% for drawn tube) and then
artifically aged. The products receive no further
straightening after stretching. |
| T6511 |
Same as T6510 except that minor straightening is allowed
after stretching to comply with standard tolerances. |
| T652 |
Solution heat treated, stress relieved by compressing to
produce a permanent set of 1 to 5% and then artificially aged. |
| T654 |
Solution heat treated, stress relieved by restriking cold
in the finish die and then artificially aged. |
| T66 |
Solution heat treated and then artificially aged -
mechanical property level higher than T6 achieved through
special control of the process (6000 series alloys). |
|
|
|
| |
|
EN AW-6060 / ISO Al MgSi
Physical and Elastic Properties |
|
Temper
|
Elastic
|
Physical
|
|
|
E
|
G
|
n
|
Tsol
|
Tliq
|
Cp
|
a
|
r
|
rel
|
l
|
EC
|
|
|
MPa
|
MPa
|
|
°C
|
°C
|
J kg-1 K-1
|
”m m-1 K-1
|
kg m-3
|
nW m
|
W m-1 K-1
|
%IACS
|
|
|
69500
|
26100
|
0.33
|
610
|
655
|
898
|
23.4
|
2700
|
-
|
-
|
-
|
|
|
69500
|
26100
|
0.33
|
610
|
655
|
898
|
23.4
|
2700
|
35
|
195
|
49.5
|
|
|
69500
|
26100
|
0.33
|
610
|
655
|
898
|
23.4
|
2700
|
36
|
187
|
48
|
|
|
69500
|
26100
|
0.33
|
610
|
655
|
898
|
23.4
|
2700
|
32
|
209
|
54
|
|
|
69500
|
26100
|
0.33
|
610
|
655
|
898
|
23.4
|
2700
|
32
|
209
|
54
|
|
|
| |
|
| Key to Parameters: |
| E |
Modulus of elasticity |
MPa |
| G |
Modulus of rigidity |
MPa |
| n |
Poisson's ratio |
|
| Tsol |
Solidus temperature |
°C |
| Tliq |
Liquidus temperature |
°C |
| Cp |
Specific heat capacity |
J kg-1 K-1 |
| a |
Coefficient of thermal expansion |
”m m-1 K-1 |
| r |
Density |
kg m-3 |
| rel |
Resistivity |
nW m |
| l |
Thermal conductivity |
W m-1 K-1 |
| EC |
Electrical conductivity |
%IACS |
|
| |
|
EN AW-6060 / ISO Al MgSi
Cold Formability, Machinability
and Weldability |
|
Temper
|
Cold Formability
|
Mach.
|
Joinability
|
|
|
CFA
|
CFDA
|
CFPA
|
CFSPA
|
EXTR
|
MAA
|
WEEB
|
WEGA
|
WEAA
|
WESA
|
BRAZA
|
SOLDA
|
|
|
|
|
|
|
7
|
|
5
|
5
|
6
|
|
6
|
5
|
|
|
5
|
5
|
|
5
|
7
|
4
|
5
|
5
|
6
|
5
|
6
|
5
|
|
|
5
|
5
|
|
5
|
7
|
4
|
5
|
5
|
6
|
5
|
6
|
5
|
|
|
5
|
4
|
3
|
4
|
7
|
5
|
5
|
5
|
6
|
5
|
6
|
5
|
|
|
4
|
4
|
|
4
|
7
|
5
|
5
|
5
|
6
|
5
|
6
|
5
|
|
|
| |
|
| Key to Parameters: |
| CFA: |
Cold formability index |
scale 2-7 |
| CFDA: |
Deep drawability index |
scale 2-7 |
| CFPA: |
Stretch formability index |
scale 2-7 |
| CFSPA: |
Suitability for spinning |
scale 2-7 |
| EXTR: |
Extrudability index |
scale 2-7 |
| MAA: |
Machinability index |
scale 2-7 |
| WEEB: |
Electron beam weldability index |
scale 2-7 |
| WEGA: |
Oxy-gas weldability index |
scale 2-7 |
| WEAA: |
Shielded arc weldability index |
scale 2-7 |
| WESA: |
Spot & seam weldability index |
scale 2-7 |
| BRAZA: |
Brazability index |
scale 2-7 |
| SOLDA: |
Solderability index |
scale 2-7 |
|
 |
| Key to Values: |
| -: |
No information available |
|
| 1: |
Not applicable |
|
| 2: |
Unsuitable |
|
| 3: |
Not recommended |
|
| 4: |
Acceptable |
|
| 5: |
Good |
|
| 5-6: |
Good to Very Good |
|
| 6: |
Very Good |
|
| 7: |
Excellent |
|
|
| |
EN AW-6060
Alloy Composition Details
| Mg |
 |
0.35 - 0.6 |
| Si |
 |
0.30 - 0.6 |
| Fe |
 |
0.10 -0.30 |
| Total Other |
 |
<= 0.15 |
| Zn |
 |
<= 0.15 |
| Ti |
 |
<= 0.10 |
| Mn |
 |
<= 0.10 |
| Cu |
 |
<= 0.10 |
| Other Elem |
 |
<= 0.05 |
| Cr |
 |
<= 0.05 |
| Al |
 |
Remainder |
All compositions in wt%. |
| |
|
EN AW-6060 Mechanical Properties |
|
Temper
|
Form
|
RP02N
|
RP02
|
RMN
|
RM
|
RG
|
A5N
|
A5
|
A50N
|
A50
|
HBN
|
HB
|
HV
|
|
|
Unspecif.
|
-
|
50
|
-
|
100
|
70
|
-
|
27
|
-
|
26
|
-
|
25
|
25
|
|
|
Unspecif.
|
-
|
90
|
-
|
150
|
95
|
-
|
25
|
-
|
24
|
-
|
45
|
45
|
|
|
Extr. Tube
|
65
|
90
|
130
|
160
|
105
|
15
|
20
|
-
|
20
|
45
|
50
|
55
|
|
|
Unspecif.
|
-
|
185
|
-
|
220
|
140
|
-
|
13
|
-
|
13
|
-
|
75
|
80
|
|
|
Extr. Tube
|
195
|
215
|
245
|
245
|
150
|
10
|
13
|
-
|
12
|
75
|
85
|
90
|
|
|
| Key to Properties |
| RP02N: |
Min proof stress 0.2% |
MPa |
| RP02: |
Proof stress 0.2% |
MPa |
| RMN: |
Min ultimate tensile strength |
MPa |
| RM: |
Ultimate tensile strength |
MPa |
| RG: |
Shear stress |
MPa |
| A5N: |
Min elongation A5 |
% |
| A5: |
Elongation A5 |
% |
| A50N: |
Min elongation A50 |
% |
| A50: |
Elongation A50 |
% |
| HBN: |
Min hardness, Brinell |
HBN |
| HB: |
Hardness, Brinell |
HB |
| HV: |
Hardness, Vickers |
HV |
|
|
| |
|
BMT Brekelmans Techniek B.V. |
| Terug |