BACKGRDUND OF THE INVENTION
[0001] The present invention deals with the provision of cast structures having good hot
rollability.
[0002] The commercial production of wrought copper base alloys is naturally seriously affected
by edge cracking of the alloys during hot rolling or hot working. Silicon-tin bronzes
in particular have been found to be susceptible to this edge cracking phenomenon.
This is naturally a serious problem commercially. Ternary copper base alloys which
contain silicon and tin are even more susceptible to the edge cracking phenomenon,
but these ternary alloys are nonetheless desirable for commercial production because
they provide a good combination of stress corrosion resistance, high strength and
formability.
[0003] Various means have been suggested in the art in order to counteract the edge cracking
problem, especially in silicon and tin containing copper base alloys. Such means have
included both different combinations of elemental additions and ways to vary the hot
working process. For example, copper base alloys containing silicon and tin together
with mischmetal are taught in U.S. Patent 4,148,633. While this patent does provide
improvement in the edge cracking phenomenon, it is naturally desirable to provide
even greater improvement and to provide such improvement without the necessity for
adding alloying additions..Of further interest is "A Preliminary Assessment of the
Value of Minor Alloy Additions in Counteracting the Harmful Effect of Impurities on
the Hot Workability of Some Copper Alloys" by R.J. Jackson et al. in the Journal of
the Institute of Metals, Volume 98 (1970), Pages 193-198. This article discusses copper
alloys which contain impurities such as lead and bismuth. These metals may have their
tendencies to crack during hot working reduced by the addition of such materials as
thorium, uranium and mischmetal. Other patents of interest include U.S. 1,881,257,
U.S. 1,956,251, German 756,035, U.S. 2,257,437, U.S. 2,062,448 and U.S. 3,923,555.
[0004] It is, therefore, a principal object of the present invention to provide a method
of processing silicon-tin bronzes to provide cast structures having good hot rollability.
[0005] It is a still further object of the present invention to provide such a method which
yields a copper base alloy which is resistant to edge cracking during hot working.
[0006] It is a further object of the present invention to provide a method as aforesaid
which does not rely on expensive processing variations or alloying additions.
[0007] It is a still further object of the present invention to provide improved cast copper
alloys which are resistant to edge. cracking during hot rolling.
[0008] Further objects and advantages of the present invention will appear from a consideration
of the following specification.
SUMMARY OF THE INVENTION
[0009] The foregoing objects and advantages are readily accomplished in accordance with
the method of the present invention. The method of the present invention.is a method
for processing copper base alloys especially those containing silicon and tin to provide
cast structures having good hot workability. Hot rolling is the preferred processing
practice, however, any hot working step is contemplated in accordance with the process
of the present invention, such as drawing or extrusion. Throughout the present specification,
however, I hot rolling will be discussed as the preferred hot working step.
[0010] In accordance with the method of the present invention ingots are direct chill cast,
preferably of silicon-tin bronzes, in a mold from liquid metal wherein the melt temperature
entering the mold is 100 to 350°C in excess of the liquidus temperature. This simple,
convenient and expeditious practice provides a copper base alloy which is resistant
to edge cracking during hot rolling.
[0011] The present invention also provides improved_cast structures which exhibit surprisingly
good hot rollability. The cast copper base alloys comprise a first external inversely
segregated surface zone, a second bulk ingot zone and a subsurface denuded zone bridging
said first and second zones exhibiting a uniform coarse grain structure which is devoid
of second phases. Although the improved cast structures are preferably present in
silicon-tin bronzes as aforesaid, it is a finding of the present invention that the
present process preferentially provides said structures with resultant improved hot
rollability in copper alloys generally, as, for example, in aluminum bronzes, tin
bronzes and tin brasses. In view of the remarkable improvement effected by the present
invention with regard to the particularly troublesome silicon-tin bronzes, the present
invention will be discussed hereinbelow with regard to this'alloy system.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012]
Figure 1 is a photograph of a DC cast silicon-tin bronze showing the subsurface region
thereof produced using conventional processing with the photograph taken at a magnification
of 12X;
Figure 2 'is a photograph of a heavily cracked plate produced from the casting of
Figure 1 by hot rolling said casting, with the photograph at a magnification of 0.6X;
Figure 3'is a photograph of a DC cast silicon-tin bronze of substantially the same
composition as in Figure 1 produced in accordance with the present invention showing
the subsurface region thereof with the photograph at a magnification of 12X; and
Figure 4 is a photograph of a crack-free plate produced by hot rolling the casting
of Figure 3, with the photograph taken at a magnification of 0.6X.
DETAILED DESCRIPTION
[0013] In preparing castings for molten metal, it is necessary to superheat the liquid metal
in order to provide sufficient fluidity to fill the mold. In accordance with conventional
practice, an excess superheat is avoided in order to maximize utilization of energy,
minimize pickup of harmful gases, minimize the loss of volatile elements and minimize
wear on refractory parts.
[0014] Hence, normal pouring practices for silicon-tin bronzes provide for a 30 to 70°C
superheat at the point where the liquid metal enters the casting mold.
[0015] In accordance with the process of the present invention, surprisingly improved cast
structures are obtained utilizing higher than normal superheats in direct chill casting.
The process of the present invention superheats the liquid metal to a temperature
of from 100 to 350°C in excess of the liquidus temperature, and preferably 150 to
250°C in excess of the liquidus temperature. Ingots are then cast in a mold from the
liquid metal wherein the melt temperature entering the mold is in said higher superheated
range.. It is surprising and unexpected to find that this simple and expeditious practice
yields the improvements of the present invention.
[0016] Ingots cast by the DC or direct chill casting method exhibit characteristic structural
features that are inherent in the modes of heat extraction effected by this technique.
Thus, a typical DC casting arrangement provides for the transfer of molten metal into
a water cooled copper mold via a downspout distributor or similar distribution means.
Solidification of the liquid metal is effected by heat transfer through the water
cooled mold and by the direct impingement of water onto the ingot as it emerges from
the mold. The ingot shell with associated fine grained structure is formed rapidly
under high rates of heat extraction when the molten metal and mold are in contact.
After reaching some critical thickness the ingot shell shrinks away from the mold
wall. Solidification continues but under lower heat transfer conditions. Accordingly,
the subsurface region so formed exhibits a coarser structure. Solidification of the
major part of the ingot section is achieved by the direct impingement of the sub-mold-coolant
onto the ingot surface. The resultant structure is fine adjacent to the above subsurface
region, and coarsens gradually on approaching the ingot center. Typically, the high
growth rate conditions operative during this solidification of the bulk realizes formation
of columnar grains.
[0017] . The formation of the subsurface region is of particular relevance to the present
invention. In solidifying alloys, solute rich phases are formed in the dendrite arms
and at grain boundaries. These phases possess lower melting temperatures than the
primary dendrites. Accordingly, during formation of the above discussed subsurface
region, when the heat extraction process is diminished the temperature of the ingot
shell increases and these solute rich phases tend to remelt. As a result, inverse
segregation and seams or spikes of these phases form along grain boundaries in these
reheated regions. These features can and frequently are detrimental to the hot rolling
performance of the resultant cast silicon-tin bronze.
[0018] In accordance with the present invention, it has now been found that in preparing
direct chill castings, particularly of silicon-tin bronzes, that the structural features
in the subsurface region can be controlled by manipulating the superheat as discussed
hereinabove. When using conventional practice with superheats of 30 to 70°C, the subsurface
regions contain spikes or grain boundary films of low melting point silicon-tin rich
phases as clearly shown in Figure 1. The hot rollability of such structures is very
poor. Cracking initiated at these grain boundary features propagates extensively into
the bulk of the ingot as clearly shown in the heavily cracked plate produced by hot-rolling
the material of Figure 1, shown clearly in Figure 2.
[0019] However, the use of higher superheats in accordance with the practice of the present
invention surprisingly and unexpectedly avoids formation of these seams of low melting
point phases as clearly shown in Figure 3. In addition, the subsurface region exhibits
a uniform coarse grain structure which is devoid of second phase. The associated hot
rollability is exceptionally good as shown in Figure 4.
[0020] Cracks which may be initiated in the exterior inversely segregated surface zone are
blunted in this subsurface region so that the hot rollability of the resultant ingot
is excellent.
[0021] Thus, as clearly shown in Figure 3, the cast copper alloys of the present invention
are characterized by a first external inversely segregated surface zone, a second
internal bulk ingot zone, a subsurface denuded zone bridging said first and second
zone exhibiting a uniform coarse grain structure which is devoid of second phases.
Thus, in accordance with the present invention there are no distinctive phases that
bridge the zone between the outside (inversely segregated region) and the bulk of
the casting, i.e., the casting is characterized by the presence of a denuded zone
as clearly shown in Figure. 3. This should be contrasted to the continuum of second
phases which characterize conventional processing as clearly shown, in Figure 1. Hence,
cracks initiated in the ingot of Figure 3 would be blunted by the denuded zone, but
would propagate through the continuum of the ingot of Figure 1. Naturally, the thickness
of the zones will depend upon the particular alloy composition and exact processing
conditions.
[0022] As indicated hereinabove, the process of the present invention preferably deals with
silicon and tin containing copper base alloys. The preferred silicon content is from
1 to 6% and the preferred tin content is from 0.2 to 5%. Naturally, if desired for
particular properties, alloying additions may readily be added to the silicon-tin
bronze, such as mischmetal, chromium, manganese, iron, nickel and the like. Chromium
is a particularly preferred addition in an amount of at least 0.03% and preferably
in an amount from 0.03 to 1.0%. Also, conventional impurities may be readily tolerated.
[0023] The process of the present invention and improvements obtained thereby may be readily
seen from a consideration of the following illustrative example.
EXAMPLE I
[0024] DC castings 6" x 30" in cross section were prepared from alloys having the following
compositions:

These alloys exhibit a liquidus temperature of about 1050°C. An ingot was direct chill
cast from Alloy A such that the melt temperature entering the casting mold was 1130°C,
that is, superheat conditions of 80°C in excess of liquidus were utilized. The resultant
cast structure is shown in Figure 1. As clearly shown in Figure 1, the subsurface
regions contain spikes or grain boundary films of lower melting point tin rich phases.
The hot rollability of this casting was poor as clearly shown in Figure 2 wherein
the ingot was hot rolled .from 840°C at two passes with a 15% reduction in each pass.
When hot rolling was attempted, cracking was initiated at the aforesaid grain boundaries
and propagated extensively into the bulk of the ingot.
[0025] When the aforesaid casting practice was modified to Alloy B in accordance with the
process of the present invention with all conditions remaining comparable except that
the melt temperature entering the casting mold was increased to 1225°C in accordance
with the practice of the present invention, i.e., superheat conditions of 175°C in
excess of liquidus, a preferred coarse subsurface region was obtained free from grain
boundary films as clearly shown in Figure 3: The subsurface region was a denuded zone
which exhibited a uniform coarse grain structure devoid of second phases. As a result,
when the ingot was hot rolled in the same manner as indicated above for Alloy A, the
hot rollability of Alloy B was excellent . as clearly shown in Figure 4.
[0026] The patents set forth in this application are intended to be incorporated by reference
herein.
[0027] This invention may be embodied in other forms or carried out in other ways without
departing from the spirit or essential characteristics thereof. The present embodiment
is therefore to be considered as in all respects illustrative and not restrictive,
the scope of the invention being indicated by the appended claims, and all changes
which come within the meaning and range of equivalency are intended to be embraced
therein.
1. A method of processing copper base alloys to provide cast structures having good
hot workability which is characterized in that it comprises direct chill casting ingots
of said alloys in a mold from liquid metal wherein the melt temperature entering the
mold is 100 to 350°C in excess of the liquidus temperature, to provide a copper base
alloy which is resistant to edge cracking during hot working.
2. A method according to claim 1 characterized in that said alloy is a copper base
alloy containing silicon and tin.
3. A method according to claim 1 or 2 characterized in that the liquid metal is superheated
to said temperature prior to entering the mold.
4. A method according to any one of claims 1 to 3 characterized in that said resistant
cast structure has good hot rollability and including the step of hot rolling said
ingot to provide a hot rolled material free from edge cracking.
5. A method according to claim 2 characterized in that said copper base alloy contains
from 1 to 6% silicon and from 0.2 to 5% tin.
6. A method according to any one of claims 1 to 5 characterized in that the melt temperature
entering the mold is 150 to 250°C in excess of the liquidus temperature.
7. A method according to any one of claims 1 to 6 characterized in that the resulting
cast ingot exhibits a subsurface region having a uniform coarse grain structure which
is devoid of second phase.
8. A cast copper base alloy characterized in that it is produced in accordance with
the method of any one of claims 1 to 7.
9. Cast copper base alloys having good hot workability characterized by comprising
a first external inversely segregated surface zone, a second internal bulk ingot zone,
and a subsurface denuded zone bridging said first and second zones exhibiting a uniform
coarse grain structure which is devoid of second phases.
10. Cast alloys according to claim 9 characterized in that said alloy is a copper
base alloy containing silicon and tin.
11. Cast alloys according to claim 10 characterized in that said silicon content is
1 to 6% and said tin content is 0.2 to 5%.