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ZINC BASE
ALLOYS
There are two alloys which are mainly
used Zamak-3 (ASTM AG40A, SAE 903, ZL3) and Zamak-5
( ASTM AC41A, SAE 925, ZL5). Both containing about 4%
aluminium and 0.04% magnesium, but one contains copper
whilst the other is copper-free.
Structure
The major use of zinc as a structural
material is in the form of alloys for die castings.
The zinc die-castingalloys are low in cost and easy
to cast and have greater strength than all die castingmetals
except the copper alloys. They can be cast to close
dimensional limits and are machined at minimum cost.
The Al-Zn phase diagram shows that a
lamellar eutectic forms at 382 C and 5% aluminium, containing
alpha and Beta solid solution. The alpha constituent
of the eutectic is stable only at temperatures above
275 C. At that temperature it transforms by a eutectoid
reaction into alpha and beta phases and both of the
alloys are structurally unstable at room temperature.
However, all commercial diecasting alloys are cooled
fast enough to prevent the eutectoid transformation
and retain the eutectic mixture of alpha and Beta.
The primary zinc solid solution phase
continues to reject aluminium from solid solution (a
precipitation or aging process). In a chill-cast copper-free
alloy, the structure consists of primary dendrites of
alphaZn/Beta-Al eutectic (Fig. 1). At a higher magnification
(Fig. 2), the precipitate in alpha-Zn can be seen, but
the precipitate in the Beta-Al of the eutectic is not
resolved. The same alloy, when sand cast (Fig. 3), shows
a coarser eutectic than when it is chill cast. In the
sand cast alloy, at higher magnification (Fig. 4), the
precipitate as well as being resolved in the Alpha-Zn
phase is also resolved in the Beta-Al of the eutectic
phase.
Typical Chemical Composition
(%)
Alloy |
Al |
Cu |
Mg |
Zn |
ZL3 |
3.8-4.3 |
- |
0.03-0.06 |
Bal. |
| ZL5 |
3.8-4.3 |
0.75-1.25 |
0.03-0.06 |
Bal. |
Impurities in both alloys are restricted
to Fe <01, Ni <0.06, Pb <0.005, Cd <0.005,
Sn 0.002, Th <0.001, In <0.0005, and for alloy
A, Cu <0.1.
Typical Mechanical Properties
The aging process causes a continuous
change in properties, as typified by the following data:
| Alloy |
Tensile
Strengths (Rm) N/mm2 |
Elongation
(A) |
Impact
Value (J) |
Hardness
(HB) |
| |
5 weeks after casting |
12 months after
casting |
weeks after casting |
12 months after
casting |
weeks after casting |
12 months after
casting |
weeks after casting |
12 months after
casting |
| ZL3 |
286 |
264 |
15 |
25 |
57 |
58 |
83 |
67 |
| ZL5 |
335 |
320 |
9 |
12 |
58 |
57 |
92 |
74 |
The aging process is also accompanied
by dimensional contraction and castings may be given
a stabilising beat treatment (6h at 1000 C followed
by air cooling) which reduces the extent of mechanical
and dimensional changes due to aging.
Specification
Zinc alloys are made to BS 1004 : 1972
and the copper-free alloy illustrated in Figs. 1, 2,
3 and 4 is likely to meet the following specifications.
Specification |
Grade |
BS1004:1972 |
A |
DIN
1743 |
GD-Zn
A14 (Z400 |
ASTM
B86 |
AG40
(XXIII) |
SAE
J468b |
903 |
Typical Applications
The 4%Al alloy is more widely used in
the UK, but the 4%Al-1%Cu alloy is equally widely used
in other countries. The main applications of both alloys
are in the motor trade, followed by toys, hardware and
hand tools industries and domestic applications. Both
alloys are essentially pressure die cast but, on a smaller
scale, they are also used for gravity die casting, as
well as an alloy containing 11 - 13%Al.
ZINC BASE ALLOYS
Fig 1 - Zinc alloy, A,
chill cast............x200.............Fig 2 - Zinc
alloy, A, chill cast (same as Fig. 1) ..x1000
Etchant : 1% nital.......................................................
Etchant : 1% nital
Fig 3- Zinc alloy,
A sand cast ...........x200....Fig 4-Zinc alloy,
A, sand cast (same as Fig.3)..x1000
Etchant : 1% nital
.......... ....................................Etchant
: 1% nital
ALUMINIUM BASE
ALLOYS - AlSi
Structure
Al-Si alloys form the largest family
of the aluminium base casting alloys, ranging from simple
binary to more complex alloy systems. Structurally,
however, all of the alloys belong to three distinct
groups, hypoeutectic, eutectic, and hypereutectic, although
a few alloys are borderline between the hypo- and eutectic
groups. The constituents in all alloys are the same;
however, only their relative volumes, size and distribution
differ; these are alpha-Al, which is present in all
alloys, and can occur even in hypereutectic alloys under
strong nonequilibrium freezing and silicon, as divorced
in hypoeutectic alloys and equally divorced in eutectic
or hypereutectic alloys. Primary silicon occurs in hypereutectic
alloys but can also be found occasionally in eutectic
alloys. Other intermetallic constituents which can occur
in some alloys are CuAl2 or alpha-Al/CuAl2,
eutectic, Mg2Si or a-AI/Mg2 Si
eutectic, (AlFeNi), and various alpha-(FeMnSiAl) compounds.
The matrix of hypoeutectic alloys, alpha-Al,
is usually grain refined as in the case of the Al-Cu
alloys. The eutectic and hypereutectic alloys are, however,
seldom grain refined, but the structural condition of
the silicon phase in the microstructure is controlled
by melt treatments as well as by the cooling rate. The
macrostructure of a chill-east untreated eutectic Al-Si
alloy, consisting of eutectic grains or cells, is shown
in Fig. 5, and that of the sand cast-alloy is shown
in Fig. 6
Dendrite arm spacing in hypoeutectic
alloys is controlled by both grain refinement and the
cooling rate during freezing. This in turn will affect
the size and the distribution of all dispersed constituents
including silicon. The case of silicon is different,
however, and requires special considerations. In the
plane of the micro-section, silicon particles appear
as elongated plates of lamellae apparently disconnected
from one another. In fact, deep etching and scanning
photomicrography reveals that silicon particles are
interconnected into a single, coral-like silicon mesh,
the sections of which appear in the plane of the photomicrograph.
Clearly, therefore, the state of silicon in the microstructure
is dependent upon the number of silicon "corals"
and the degree of branching of such corals. Fine branching
is achieved either by fast cooling during freezing or
by melt treatments with small amounts of sodium (0.01%)
or strontium (0.05%). This is often described as a "modification"
treatment. Some hypoeutectic alloys may be modified,
but eutectic and hypereutectic alloys are generally
modified, particularly for sand castings. In hypereutectic
alloys, primary silicon is grain refined by small additions
of phosporus (0.01%) to form AIP compounds which nucleate
a large number of cuboidal silicon crystals. The eutectic
silicon can be also "modified" in these alloys
as well as primary silicon refined, by introducing together
with phosphorus small concentrations of strontium and
sodium into the alloy (double refinement). Impurity
intermetallics can occur as needles but with correct
proportions of iron and manganese the morphology of
alpha-(FeMnSiAl) may be rendered more equiaxial.
The microstructure of a chill cast AI-Si
alloy in Fig. 7 shows primary alpha-Al, alpha-Al/Si
eutectic (dark) and intermetallic a-(FeSiMn) (light).
When sand cast, the microconstituents are the same but
coarser (Fig. 8). When modified with 0.05%Sr, the structure
(Fig. 9) consists of primary alpha-Al and a finer eutectic
of a-Al and Si which is more eutectic-like than in Fig.
7. The sand cast alloy, similarly modified (Fig. 10)
is similar to the chill cast alloy, but exhibits a coarser
eutectic and acicular alpha-(FeSiMn). Scanning electron
micrographs of the structures shown in Figs. 9 and 10,
taken after deep etching, reveal the branching of silicon
crystals (Figs. 11 and 12).
The microstructure of a chill cast AI-Si-Mg
alloy shows silicon (dark) and script a-(FeSiMnAl) in
an alpha-Al matrix. The sand cast alloy reveals dark
grey silicon, light grey script and dark Mg, Si in an
alpha-Al matrix.
The chill-east Al-Si-Cu alloy has dark
grey silicon, light angular or globular alpha-Al/CuAl2
in an a-AI matrix. When sand cast, the microstructure
is similar but coarser showing dark grey silicon, globular
a-AI/CuAI2 eutectic and needles of alpha-(FeSiAl)
in an alpha-Al matrix.
The chill-cast Al-Si-Cu-Mg-Ni alloy
has dark grey alpha-Al/Si eutectic, light grey CuAl,
and needles of alpha-(FeSiAl) in an alpha-Al matrix.
A sand cast alloy shows dark grey silicon; light faceted
or globular CuAl, needles of alpha-(FeSiAl) and black
Mg2Si in an alpha-Al matrix. A similar alloy
but with approximately twice the silicon content when
chill-cast, the structure consists of dark grey cuboids
or primary silicon, dark grey eutectic silicon, black
Mg2Si and light NiAl3 in an alpha-Al
matrix. When sand cast, the structure is coarser but
has similar microconstituents, namely, dark grey cuboids
of primary silicon, dark grey eutectic silicon, black
Mg2 Si and light NiAl3 in an alpha-Al
matrix.
AI-Si alloys are amenable to hardening
heat treatment by utilising either CuAl2
or Mg2 Si precipitation mechanisms.
Alloys LM4, LM6 and LM25 are widely
used for gravity die and sand castings.
Typical Chemical Composition
| ALLOY |
Cu |
Mg |
Si |
Fe |
Mn |
Ni |
Zn |
Pb |
| LM4 EN 45200 |
2-4 |
0.15 |
4-6 |
0.8 |
0.2-0.6 |
0.3 |
0.5 |
0.1 |
| LM6 EN 44100 |
0.1 |
0.1 |
10-13 |
0.6 |
0.5 |
0.1 |
0.1 |
0.1 |
| LM24 EN 46500 |
3-4 |
0.30 |
7.5-9.5 |
1.3 |
0.5 |
0.5 |
3.0 |
0.3 |
| LM25 EN 42000 |
0.1 |
0.2-0.45 |
6.5-7.5 |
0.5 |
0.3 |
0.1 |
0.1 |
0.1 |
| LM26 |
2-4 |
0.5-1.5 |
8.5-10.5 |
1.2 |
0.5 |
1.0 |
1.0 |
0.2 |
| LM28 |
1.3-1.8 |
0.8-1.5 |
17-20 |
0.7 |
0.6 |
0.8-1.5 |
0.2 |
0.1 |
| ALLOY |
Sn |
Ti |
Cr |
Co |
Al |
| LM4 |
0.1 |
0.2 |
- |
- |
Bal. |
| LM6 |
0.05 |
0.2 |
- |
- |
Bal. |
| LM24 |
0.2 |
0.2 |
- |
- |
Bal |
| LM25 |
0.05 |
0.2 |
- |
- |
Bal. |
| LM26 |
0.1 |
0.2 |
- |
- |
Bal. |
| LM28 |
0.1 |
0.2 |
0.6 |
0.5 |
Bal. |
Typical Mechanical Properties
Sand
Cast |
| |
LM4
(M) |
LM6
(M) |
LM24 |
LM25
(M) |
LM26
(M) |
LM26
(TB) |
LM26
(TF) |
LM28
(TF) |
| Tensile Strength, (Rm)
N/mm2 |
140-150 |
160 |
|
130-150 |
130-140 |
160-170 |
230 |
120 |
| 0.2% Proof Strength (Rp0.2)
N/mm2 |
70-80 |
60 |
|
80-100 |
70-80 |
80-140 |
200-220 |
120 |
| Elongation (A) % |
1-2 |
5 |
|
2-3 |
2-3 |
2-4 |
0 |
0.3 |
| Hardness HB |
65-70 |
50 |
|
55-65 |
55-65 |
65-80 |
90-100 |
100 |
Chill
Cast |
| |
LM4
(M) |
LM6
(M) |
LM24 |
LM25
(M) |
LM26
(M) |
LM26
(TB) |
LM26
(TF) |
LM28
(M) |
LM28
(TF)
|
| Tensile Strength, (Rm)
N/mm2 |
150-180 |
190 |
180 |
160-200 |
130-170 |
230-245 |
280 |
150-160 |
190 |
| 0.2% Proof Strength (Rp0.2)
N/mm2 |
80-100 |
70 |
100-120 |
80-100 |
80-100 |
90-140 |
200-250 |
150-160 |
170 |
| Elongation (A) % |
1-2 |
7 |
1.5 |
3-6 |
2-6 |
3-10 |
0.2 |
0.5 |
0.3 |
| Hardness HB |
65-70 |
50 |
85 |
55-65 |
55-70 |
65-80 |
90-100 |
110 |
100 |
(M = as-east; TB = solution
treated only; TF = solution treated and precipitation
treated).

Fig. 5 - Alloy LM6 macrostructure,
chill cast untreated..x 5 ..Fig. 6 - Alloy LM6 macrostructure,
sand cast untreated...x 5
Etchant : CuCI.2 soln.
......................................................Etchant
: CUC12 soln.
Fig. 7 - Alloy LM6, chill
cast...................x 400 ..Fig. 8- Alloy LM6, sand
cast ................x 400
Etchant : 0.5%HF .....................................Etchant
: 0. 5% HF
Fig. 9 - Alloy LM6, chill
cast, modified with 0.05%Sr Alloy..x 400...Fig.10 -
LM6, sand cast, modified with 0. 0 5%Sr...x 400
Etchant : 0.5% HF ............................................Etchant
: 0.5% HF
Fig. 11- Alloy LM6, chill
cast, modified with 0.05%Sr .x 2000 ....Fig. 12 - Alloy
LM6, sand cast, un- modified with 0.05%Sr..x 2000
Scanning electron micrograph. Deep etched.............
Scanning elec.tron micrograph. Deep etched
25% HCl, Aq. 15 mins
.........................................25% HCl, Aq.
15 mins
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