CROSS REFERENCE TO RELATED APPLICATIONS
BACKGROUND OF THE INVENTION
1. Field of the Invention
[0002] The invention relates generally to a secondary aluminum alloy for casting, a method
of forming the aluminum alloy, a cast component formed of the cast aluminum alloy,
and a method of manufacturing the cast component.
2. Related Art
[0003] Casting of aluminum alloys is oftentimes used in the automotive industry to form
lightweight components, including complex structural, body-in-white, suspension, and
chassis components. There are many types of known casting processes, for example,
high pressure die casting, low pressure casting, and squeeze casting. The die is typically
formed of a hardened tool steel. Although the casting equipment is expensive, the
cost per component formed is relatively low, which makes the process suitable for
high volume production.
[0004] However, improvements to the casting process and materials used in the casting process
are desired. For example, an aluminum alloy capable of forming a component having
high ductility, without loss of fluidity or castability, is desired. The aluminum
alloy should also be resistant to damage associated with hot cracking, soldering,
shrinkage, and corrosion. In addition, although lightweight components are desired,
the components should still provide a high strength and toughness.
SUMMARY
[0005] One aspect of the disclosure provides a secondary structural aluminum alloy, comprising
at least 80 weight percent (wt. %) aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt.
% to 8.0 wt. % silicon, 0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt.
% zinc, 0.12 wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater
than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each
in an amount of not greater than 0.05 wt. %, and other elements in a total amount
of not greater than 0.15 wt. %, based on the total weight of the aluminum alloy.
[0006] Another aspect of the invention provides a method of manufacturing a component. The
method comprises casting a recycled aluminum alloy, the recycled aluminum alloy including
at least 80 weight percent (wt. %) aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt.
% to 8.0 wt. % silicon, 0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt.
% zinc, 0.12 wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater
than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each
in an amount of not greater than 0.05 wt. %, and other elements in a total amount
of not greater than 0.15 wt. %, based on the total weight of the aluminum alloy.
[0007] A method of manufacturing an aluminum alloy, comprising the steps of: melting a 300
series or 6xxx series recycled aluminum alloy; and adding at least one additional
element to the melted aluminum alloy to form an improved aluminum alloy. The at least
one additional element is added so that the improved aluminum alloy includes at least
80 weight percent (wt. %) aluminum, 6.0 wt. % to 8.0 wt. % silicon, 0.1 wt. % to 0.6
wt. % copper, 0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.15
wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15
wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount
of not greater than 0.05 wt. %, and other elements in a total amount of not greater
than 0.15 wt. %, based on the total weight of the improved aluminum alloy.
[0008] The cast aluminum alloy is able to achieve a yield strength of at least 110 MPa,
ultimate tensile strength (UTS) of at least 220 MPa, and an elongation of 7 to 20
% (depending on flow length) at F temper. The cast aluminum alloy also has an unexpectedly
high level of corrosion resistance.
BRIEF DESCRIPTION OF THE DRAWING
[0009] Other advantages of the present invention will be readily appreciated, as the same
becomes better understood by reference to the following detailed description when
considered in connection with the accompanying drawing wherein:
Figure 1 is a portion of an example component formed of an aluminum alloy according
to an embodiment.
DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS
[0010] One aspect of the invention provides an improved aluminum alloy for casting components
10, such as a lightweight automotive vehicle component, is provided. The aluminum
alloy can be referred to as a secondary structural aluminum alloy. As a structural
aluminum alloy, the aluminum alloy can be used to form body structural components
10 with good crashworthiness due to high ductility. Examples of components 10 which
can be formed of the aluminum alloy include structural, body-in-white, suspension,
or chassis components. The aluminum alloy is capable of providing acceptable corrosion
resistance, as well as acceptable ductility and elongation, acceptable self-piercing
rivet behavior, without hot tearing or loss of fluidity or castability. Unlike a primary
aluminum alloy, which is made from an aluminum extraction operation (bauxite) and
alloying elements, the secondary aluminum alloy is made using recycled materials,
for example recycled 3xx castings and 6xxx wrought alloys.
[0011] The improved aluminum alloy is aluminum-based, and thus typically includes aluminum
in an amount of at least 80 weight percent (wt. %), based on the total weight of the
aluminum alloy. In one embodiment, the aluminum alloy is formed by modifying a recycled
300 series or recycled 6xxx series aluminum alloy. A specific example of the recycled
300 series aluminum alloy is a 356.2 aluminum alloy obtained from recycled road wheels.
The 356.2 aluminum alloy includes 91.3 to 93.2 wt. % aluminum, not greater than 0.10
wt. % copper, 0.13-0.25 wt. % iron, 0.30 to 0.45 wt. % magnesium, not greater than
0.05 wt. % manganese, 6.5 to 7.5 wt. % silicon, not greater than 0.20 wt. % titanium,
not greater than 0.05 wt. % zinc, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the improved aluminum alloy. However, other types
of recycled aluminum alloys, such as 6xxx series scraps, could be modified to form
the improved aluminum alloy.
[0012] Alloying elements are present in the improved aluminum alloy to achieve acceptable
elongation and ductility, and/or to achieve the desired strength and toughness. For
example, silicon (Si), magnesium (Mg), manganese (Mn), and/or iron (Fe) can be added
to control ductility, castability, strength, ductility, and/or toughness. In particular,
the manganese can be used to prevent die sticking, and the magnesium can be used to
form Mg
2Si for strengthening. The aluminum alloy can also include copper (Cu) and zinc (Zn)
to increase strength, preferably without negatively impacting corrosion resistance.
The zinc is also used as a solid solution strengthener and to improve machinability.
The additional alloying elements can provide other metallurgical effects as well,
such as improved resistance to hot cracking, soldering, shrinkage, and corrosion.
For example, special properties or other metallurgical effects can be achieved by
titanium (Ti). Strontium (Sr) can also be added to modify properties that occur due
to the silicon.
[0013] According to one example embodiment, in addition to at least 80 wt. % aluminum, the
aluminum alloy includes 0.1 wt. % to 0.3 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon,
0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30
wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium,
0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the aluminum alloy. The other elements can include
any element besides those listed above, for example impurities which are not intentionally
added to the composition.
[0014] The manganese and iron can form an intermetallic phase that prevents the alloy from
attacking tool steel of a die, which is typically caused by low iron content. When
the aluminum alloy is cast, the cast aluminum alloy has a yield strength of at least
110 MPa, ultimate tensile strength (UTS) of at least 220 MPa, and an elongation 7
to 20 % (depending on flow length) at F temper.
[0015] According to other example embodiments, the aluminum alloy consists of, or consists
essentially of, at least 80 wt. % aluminum, 0.1 wt. % to 0.3 wt. % copper, 6.0 wt.
% to 8.0 wt. % silicon, 0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt.
% zinc, 0.12 wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater
than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each
in an amount of not greater than 0.05 wt. %, and other elements in a total amount
of not greater than 0.15 wt. %, based on the total weight of the aluminum alloy.
[0016] According to preferred example embodiments, the aluminum alloy includes at least
80 wt. % aluminum, not greater than 0.30 wt. % copper, 7.1 wt. % to 7.5 wt. % silicon,
0.10 wt. % to 0.18 wt. % magnesium, not greater than 0.5 wt. % zinc, 0.15 wt. % to
0.30 wt. % iron, 0.4 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium,
0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the aluminum alloy. The combined content of iron and
manganese is around 0.8 wt. %, for example 0.7 wt. % to 0.9 wt. %, based on the total
weight of the aluminum alloy.
[0017] According to another preferred embodiment, the aluminum alloy consists of, or consists
essentially of, at least 80 wt. % aluminum, not greater than 0.30 wt. % copper, 7.1
wt. % to 7.5 wt. % silicon, 0.10 wt. % to 0.18 wt. % magnesium, not greater than 0.5
wt. % zinc, 0.15 wt. % to 0.30 wt. % iron, 0.4 wt. % to 0.6 wt. % manganese, not greater
than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each
in an amount of not greater than 0.05 wt. %, and other elements in a total amount
of not greater than 0.15 wt. %, based on the total weight of the aluminum alloy. The
combined content of iron and manganese is around 0.8 wt. %, for example 0.7 wt. %
to 0.9 wt. %, based on the total weight of the aluminum alloy.
[0018] According to another example embodiment, the aluminum alloy includes not greater
than 0.28 wt. % copper and not greater than 0.25 wt. % iron, based on the total weight
of the aluminum alloy.
[0019] Another aspect of the invention provides a method of manufacturing the aluminum alloy.
In one embodiment, the aluminum alloy is formed by modifying a 300 series and/or 6xxx
series recycled aluminum alloy. The aluminum alloy is preferable obtained from recycled
castings and wrought aluminum. A specific example of the 300 series aluminum alloy
is a 356.2 aluminum alloy obtained from recycled road wheels. The 356.2 aluminum alloy
includes 91.3 to 93.2 wt. % aluminum, not greater than 0.10 wt. % copper, 0.13 to
0.30 wt. % iron, 0.30 to 0.45 wt. % magnesium, not greater than 0.05 wt. % manganese,
6.5 to 7.5 wt. % silicon, not greater than 0.20 wt. % titanium, not greater than 0.05
wt. % zinc, other elements each in an amount of not greater than 0.05 wt. %, and other
elements in a total amount of not greater than 0.15 wt. %, based on the total weight
of the improved aluminum alloy. Manufacturing the improved aluminum alloy from one
or more of the recycled materials lowers the raw material cost, as it takes 95% less
energy to recycle an aluminum alloy than to create it from primary elements.
[0020] The method of forming the cast component 10 typically begins by melting the recycled
cast aluminum, or other base aluminum alloys. The melting step can be conducted by
a reverb or induction melter, or another source of heat. Once the base aluminum alloy
is melted, the method includes adjusting the content of silicon and/or at least one
other element in the melt and mixing the silicon and/or other element(s) with the
base aluminum alloy to achieve the final improved alloy composition. The additional
alloying elements, discussed above, can be added to the melted mixture to form the
improved aluminum alloy. Alternatively, the additional alloying elements could be
present in the wrought aluminum or other base aluminum alloy. Once all of the elements
are mixed together, the aluminum alloy is ready for casting.
[0021] The method then includes casting the aluminum alloy which includes at least 80 weight
percent (wt. %) aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon,
0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30
wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium,
0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the aluminum alloy. After the casting step, the cast
aluminum alloy has a yield strength of at least 110 MPa, ultimate tensile strength
(UTS) of at least 220 MPa, and an elongation of 7 to 20 % (depending on flow length)
at F temper.
[0022] The cast component
10 formed from the casting step can be, for example, a component for use in a vehicle.
Any casting process used to form components from an aluminum-based material can be
used with the improved aluminum alloy, for example high pressure die casting, low
pressure casting, or squeeze casting. In one example embodiment, the casting process
is a high pressure die casting process, which typically includes forcing the molten
aluminum alloy into an unheated die or mold cavity under pressure. The die is typically
formed from hardened tool steel. The molten aluminum is formed to a solid component
10 having the shape of the mold, which can be a complex shape. Many different types
of components
10 can be formed by the casting process, for example, a structural, body-in-white, suspension,
or chassis component. After the casting process, the method can include an optional
heat treating process, paint cure oven exposure or other finishing processes. However,
it has been found that a heat treatment process may not be necessary when the component
10 is formed from the improved aluminum alloy, which would provide the advantage of
reduced process time and costs.
[0023] As stated above, the component
10 formed from the improved aluminum alloy has a high level of corrosion resistance
which was unexpected in view of the prior art. The component
10 formed from the improved aluminum alloy also has acceptable ductility, elongation,
resistance to hot cracking, soldering, shrinkage, self-piercing riveting (SPR) behavior,
fatigue, bending, strength, and toughness. As discussed above, the cast component
10 formed of the aluminum alloy typically has a yield strength of at least 110 MPa,
ultimate tensile strength (UTS) of at least 220 MPa, and an elongation of 7 to 20
% (depending on flow length) at F temper.
[0024] Table 1 includes examples of the improved aluminum alloy according to the invention.
It was discovered that the example aluminum alloys according to the invention provide
the unexpected improvement in corrosion resistance relative to comparative example
alloys.
Table 1
| Alloy |
Cu |
Si |
Mg |
Zn |
Fe |
Mn |
Ti |
Sr |
Others |
Total Others |
| Aural 5R-preferred embodiment |
0.30 max |
7.1-7.5 |
0.1-0.18 |
0.5 max |
0.12-0.25 |
0.4-0.6 |
0.15 max |
0.015-0.03 |
0.05 max |
0.15 max |
| Ex. 1 new Aural 5R |
0.1 - 0.6 |
6.0 - 8.0 |
0.10 - 0.60 |
0.10 to 0.50 |
0.15 - 0.30 |
0.2 - 0.6 |
0.15 max |
0.015-0.03 |
0.05 max |
0.15 max |
[0025] Obviously, many modifications and variations of the present invention are possible
in light of the above teachings and may be practiced otherwise than as specifically
described while within the scope of the following claims.
1. An aluminum alloy, comprising:
at least 80 weight percent (wt. %) aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt.
% to 8.0 wt. % silicon, 0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt.
% zinc, 0.12 wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater
than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium, other elements each
in an amount of not greater than 0.05 wt. %, and other elements in a total amount
of not greater than 0.15 wt. %, based on the total weight of the aluminum alloy.
2. The aluminum alloy of claim 1 consisting of at least 80 wt. % aluminum, 0.1 wt. %
to 0.6 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon, 0.10 wt. % to 0.60 wt. % magnesium,
0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30 wt. % iron, 0.2 wt. % to 0.6 wt.
% manganese, not greater than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium,
other elements each in an amount of not greater than 0.05 wt. %, and other elements
in a total amount of not greater than 0.15 wt. %, based on the total weight of the
aluminum alloy.
3. The aluminum alloy of claim 1 or 2, wherein the aluminum alloy includes not greater
than 0.30 wt. % copper, 7.1 wt. % to 7.5 wt. % silicon, 0.10 wt. % to 0.18 wt. % magnesium,
not greater than 0.5 wt. % zinc, 0.15 wt. % to 0.30 wt. % iron, 0.4 wt. % to 0.6 wt.
% manganese, not greater than 0.15 wt. % titanium, 0.015 wt. % to 0.03 wt. % strontium,
other elements each in an amount of not greater than 0.05 wt. %, and other elements
in a total amount of not greater than 0.15 wt. %, based on the total weight of the
aluminum alloy.
4. The aluminum alloy of one of the preceding claims consisting of at least 80 wt. %
aluminum, not greater than 0.30 wt. % copper, 7.1 wt. % to 7.5 wt. % silicon, 0.10
wt. % to 0.18 wt. % magnesium, not greater than 0.5 wt. % zinc, 0.15 wt. % to 0.30
wt. % iron, 0.4 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium,
0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the aluminum alloy.
5. The aluminum alloy of one of the preceding claims, wherein the aluminum alloy is cast
and has a yield strength of at least 110 MPa, ultimate tensile strength (UTS) of at
least 220 MPa, and an elongation of 7 to 20 % (depending on flow length) in an F temper
condition.
6. A method of manufacturing a component, comprising: casting the aluminum alloy according
to one of the preceding claims.
7. The method of claim 6, wherein the component formed during the casting step is a component
for a vehicle.
8. The method of claim 6 or 7, wherein the casting step includes high pressure die casting,
low pressure casting, or squeeze casting.
9. A method of manufacturing a secondary aluminum alloy, comprising the steps of:
melting a recycled 300 series or 6xxx series aluminum alloy; and
adding at least one additional element to the melted aluminum alloy to form the secondary
aluminum alloy, the secondary aluminum alloy including: at least 80 weight percent
(wt. %) aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon, 0.10
wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30 wt.
% iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium, 0.015
wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater than
0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt. %, based
on the total weight of the secondary aluminum alloy.
10. The method of claim 9 including melting the recycled 300 series aluminum alloy.
11. The method of claim 9 or 10, wherein the recycled 300 series aluminum alloy is obtained
from recycled castings, wrought aluminum, or recycled road wheels.
12. The method of one of the preceding claims 9 to 11, wherein the recycled 300 series
aluminum alloy includes 91.3 to 93.2 wt. % aluminum, not greater than 0.10 wt. % copper,
0.13 to 0.30 wt. % iron, 0.30 to 0.45 wt. % magnesium, not greater than 0.05 wt. %
manganese, 6.5 to 7.5 wt. % silicon, not greater than 0.20 wt. % titanium, not greater
than 0.05 wt. % zinc, other elements each in an amount of not greater than 0.05 wt.
%, and other elements in a total amount of not greater than 0.15 wt. %, based on the
total weight of the recycled 300 series aluminum alloy.
13. A cast component, comprising:
an aluminum alloy, the aluminum alloy including at least 80 weight percent (wt. %)
aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon, 0.10 wt.
% to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30 wt. %
iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium, 0.015
wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater than
0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt. %, based
on the total weight of the aluminum alloy.
14. The cast component of claim 13, wherein the aluminum alloy includes an intermetallic
phase formed of the manganese and the iron.
15. The cast component of claim 13 or 14, wherein the aluminum alloy consists of at least
80 wt. % aluminum, 0.1 wt. % to 0.6 wt. % copper, 6.0 wt. % to 8.0 wt. % silicon,
0.10 wt. % to 0.60 wt. % magnesium, 0.10 wt. % to 0.50 wt. % zinc, 0.12 wt. % to 0.30
wt. % iron, 0.2 wt. % to 0.6 wt. % manganese, not greater than 0.15 wt. % titanium,
0.015 wt. % to 0.03 wt. % strontium, other elements each in an amount of not greater
than 0.05 wt. %, and other elements in a total amount of not greater than 0.15 wt.
%, based on the total weight of the aluminum alloy.