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Porosity
Defects in Gray and Ductile Iron Castings |
by
Dr. R. L. (Rod) Naro, ASI
International, Inc.
October
21, 2000
Introduction:
Surface and subsurface gas defects have always been common and
troublesome defects in gray and ductile iron castings poured in green
sand molds. During the
past 30 years, innovations in synthetic binder technology have
resulted in movement away from green sand molding and toward total
no-bake molding and core making processes and accompanying new types
of casting defects. In the year 2000, it is estimated that phenolic
urethane binders, in both the cold box and no bake versions, will
account for over 60% of all chemical binders used by the U.S. foundry
industry. Although
millions of tons of gray and ductile iron castings are cast using
these resins for both core and mold binders, casting defects stemming
from mold-metal reactions continue to pose problems for foundry men.
Generally speaking, there are three major
sources that may contribute to porosity formation in gray iron
castings. These are:
1) high initial gas content of the melt originating from either
the charge ingredients, melting practice or atmospheric humidity, 2)
reaction of carbon and dissolved oxygen under certain melt conditions,
and 3) mold-metal reactions between evolved mold and core gases at the
solidifying casting surface.1-16
In addition, any combination of these three sources may have a
cumulative effect on promoting porosity formation.
However, the gases normally held responsible for subsurface
porosity defects are nitrogen and hydrogen.
The
appearance of the subsurface porosity defects resulting from the
preceding sources may take numerous shapes but usually form as either
small, spherical holes (sometimes elongated or pear- shaped) and
called pinholes, or larger, irregularly rounded holes or irregularly
shaped fissure type defects.1,8,13,15,16 The
internal surfaces of the resultant holes may be 1) oxidized, 2) lined
with a shiny graphite film, or 3) contain slag or manganese sulfide
inclusions.1, 5, 8
The phenolic urethane resin
system consists of no-bake and gas cured resins; both systems
consisting of two resin components.
Part I is a phenolic resin (poly-benzylic-ether-phenolic resin)
diluted approximately 50% by solvents.
Part II is a polymeric di-isocyanate resin diluted with
approximately 25% solvents.
The solvent can be either aliphatic and aromatic in
composition. The
primary purpose of the solvents is to reduce binder viscosity.
Typically, the viscosity of the Part I and Part II resins are
adjusted to 200 cps or lower to provide good pump ability, rapid and
efficient sand coating qualities and good flow ability of mixed sand.
A second purpose of the solvents is to enhance resin
reactivity. An
amine-based catalyst is used as the curing agent for the no-bake
binder while a gaseous amine (triethylamine or dimethylethyl amine) is
used for the gas-cured binder.
The general chemistry of phenolic
urethane binders remains essentially the same as when the binders were
developed in the late 1960 to early 1970's.
There have been some changes in basic resin formulations
involving the solvent systems as well as base phenolic resin system.
The Part I phenolic resin has been modified to reduce odor by
reduction in the level of free formaldehyde, and this becomes
especially apparent when hot foundry sands are used. In addition, because of efforts to reduce solvent
evaporation into the atmosphere, the solvent system has been modified
extensively to incorporate higher boiling point solvents or new
solvents systems having improved environmental properties.
Being
organic based systems, the phenolic-urethane family of binders are
composed of only four basic elements:
72% carbon (C), 8.5% hydrogen (H), 3.9% nitrogen (N) and 15.5%
oxygen (O).
With phenolic urethane systems, the nitrogen
component is associated solely with the polyphenyl polyisocyanate
(Part II) binder component. Part
I, or the hydroxyl containing phenolic binder component, contains no
nitrogen. The gases
typically responsible for subsurface porosity in iron castings are
nitrogen and hydrogen; carbon and oxygen from binder decomposition
usually present no problem because the high silicon content of gray
iron acts to suppress the formation of carbon monoxide porosity.
Binder -----------
> H (nascent) -> H2
(g)
Binder -----------
> N (nascent) ---> N2
(g)
Fe + H2O
vapor (binder) -------->
FeO + 2H (nascent)
3 H2
(binder ) + N2
(binder) > 2NH3(g)
--------> 6H(nascent) + 2N(nascent)
FeO + C (binder) ---------> CO (g) + Fe
While the first four reactions are likely to provide both
surface and subsurface porosity defects, the last reaction usually
results only in surface defects, such as pock marking or more
frequently, lustrous carbon laps and surface wrinkles17.
When an organic binder thermally degrades, hydrogen and
nitrogen are liberated in the nascent or atomic form.
In this mono-atomic state, they are readily soluble in molten
iron, and if present, dissolve quite easily in both molten gray and
ductile irons. If
ammonia forms, it also may dissociate into both nascent hydrogen and
nitrogen. Since the
solubility of hydrogen and nitrogen in liquid iron is far greater than
in solid iron, these gases will precipitate out of solution as gas
bubbles during solidification if they are present in amounts greater
than the solid solubility limits.
The shapes of the resulting gas holes may vary from small,
widely dispersed spherical shaped holes lying just under the surface
to numerous fissure type holes, often resembling shrinkage defects and
are usually perpendicular to the casting surface.
In either case, absorption of nitrogen and\or hydrogen by the
molten iron, either individually or jointly, may result in subsurface
porosity defects.
Clearly,
many factors are involved in the development of binder-associated
defects; neither they nor the various core making parameters and
foundry melting variables that have a direct influence on the
occurrence of such defects were well understood in the early 1970's.
Recognizing this situation, the object of this investigation
was aimed at determining how such variables influence the occurrence
of porosity defects. Also,
the development of remedial techniques to alleviate these problems was
also extensively studied.
Experimental
Procedure
The experimental program used in this investigation was divided into
two phases. The first
phase was devoted to 1.) the development of a suitable test having the
capability to produce porosity defects and 2.) the delineation of core
making and metal processing variables having an effect on porosity
generation. The
cylindrical test casting shown in Figure 1 was developed for
these tests to observe the extent of porosity formation under various
test conditions. This
"stepped cone" configuration was selected because its design
was such that core decomposition gases would be generated rapidly
while the casting was still in the molten state.
Also, this design easily lent itself to the study of section
size, re-entrant angle (hot spot) and other geometric effects (see
Figure 2).
The
majority of molds used for the production of test castings were made
with a zero nitrogen no-bake furan binder.
The base core sand mix used for most of the experimental work
consisted of the phenolic urethane no-bake binder (PUN) mixed with a
high purity, washed and dried, round grained, silica (W/D) sand.
The core making procedure used throughout most of this work
consisted of adding the phenolic polyol resin component (Part I) and
the catalyst to the sand and mixing for two minutes, followed by the
addition of the polyisocyanate component (Part II) and mixing for an
additional two minutes. The
mix was immediately hand rammed into the core box and the stepped cone
cores were stripped within five minutes.
Gray and
ductile irons of the compositions shown in Table I were
utilized in the investigation, although the bulk of the experimental
work was conducted with a high carbon equivalent iron (4.3 C.E)
inoculated with standard foundry grade (0.75% minimum calcium)
ferrosilicon in the ladle.
Inoculant addition levels were 0.25% silicon, based on the
pouring weight.
All heats
were prepared with virgin charge materials to insure low initial gas
content and were poured at selected temperatures as measured with a
Pt-Pt 10% Rd immersion pyrometer and a high speed, strip chart
recorder. Variables
studied during this phase of the investigation included binder ratio,
binder level, pouring temperature, sand type and permeability, mixing
effects, metal composition and core age.
Within each series of tests, the conditions were controlled as
carefully as possible and individual variables altered to determine
their effect on porosity.
The second
phase of the experimental work was devoted to developing remedial
techniques to prevent porosity. To
a great extent, this effort was very dependent upon the first phase of
the work in that conditions that were found to promote porosity were
used exclusively. Therefore,
it was a prerequisite to develop the capability to produce
binder-associated gas defects at will.
The same melting and core making procedures previously
described were likewise used at this time. Techniques studied in attempt to eliminate defects included
1.) Investigation of various grades of iron oxide, 2.) Ladle additions
of ferrotitanium, as well as titanium and zirconium based ferroalloy
inoculants, 3.) Use of core sand additives, 4.) Core baking, and
lastly, 5.) A study of experimental core coatings.
During this phase of the work, variables found responsible for
porosity formation were held constant during the preparation of test
castings.
The extent
of porosity formation in all castings was determined by careful
sectioning at several locations.
To determine whether any metallurgical changes resulting from
porosity formation had occurred, metallographic investigations of the
cast structure in the mold-metal interface area were also carried out.
To observe the nature of the internal surfaces of gas porosity
defects, a scanning electron microscope was utilized.
Results
Parameters
Affecting Formation of Binder Related Porosity Defects
Effect of
Binder Part I to Part II ratio
-- The effect of the ratio of Part I to Part II resin
components for PUN binders on porosity propensity is shown in Table
2.
Binder ratios of 60 : 40 (Part I : Part II) provided sound test
castings in every case under the test conditions used.
As this ratio became balanced (50 : 50), trace amounts of
porosity were found in a few test castings but the majority of test
castings made with balanced ratios were sound.
In those cases where porosity was found, a substantial portion
was as surface porosity or semi-rounded holes (pock marking).
As the binder ratio was unbalanced again in favor of excess
Part II (40 : 60 and 35 : 65), greater amounts of subsurface porosity
formed in the test casting.
The types of defects observed and described as varying in
intensity from nil to very severe are shown in Figure 3.
Although the recommended ratio for running PUN binders varies
between a 55:45 to 60:40 ratio, in actual practice, extreme ratios
favoring excess Part II or polyisocyanate are often encountered.
Such problems often arise from worn or defective binder pumps,
air in binder lines, changes in binder viscosity from temperature,
inefficient mixing, and numerous other less incidental, but often
overlooked sources. For
example, in the early 1970's, it was not unusual to foundries to run
binder ratios favoring excess polyisocyanates to facilitate the
stripping of difficult cores or to increase fully cured core
strengths.
New resin
formulations (1998 versions) showed very little difference in casting
performance compared to early 1970 versions.
Binder ratios in which unbalanced ratios of 60 : 40 were
employed produced sound castings.
Unbalanced binder ratios favoring excess Part II or the
isocyanate component once again were very susceptible to severe
subsurface porosity.
Effect of
Binder Level -- To
determine the effect of binder level on porosity susceptibility, test
castings were poured with test cores made with binder levels ranging
from 1.25% to an extreme of 3.0%.
At some of these levels, the ratio of Pt I: Pt II was again
varied to determine effect on porosity formation. (It should also be
noted that although these higher levels may never be encountered in
actual practice, they were intentionally selected to magnify the
effect of binder level or the effect of reclaimed sands having high
"LOI" values.) The
results obtained from these tests showed that as the binder level
increased at the same Pt I : Pt II ratio, the severity of the porosity
defects likewise increased.
At the highest binder level tested, porosity tended to form at
even balanced ratios as shown in Table 3.
These
results show that if sufficient amounts of evolved hydrogen and / or
nitrogen decomposition gases are made available to the solidifying
irons, porosity will generally occur even with favorable binder ratios
and using relatively high pouring temperatures.
These same phenomena can be extrapolated to include what the
consequences will be when using reclaimed core or molding sands having
high loss on ignition values.
Excessive amounts of dissolved gases stemming from
inappropriate charge materials or liquid metal processing will
likewise be more susceptible to core gas defects from absorption of
hydrogen and / or nitrogen.
Effect of
Casting Temperature --
Although the previously reported results have shown significant
effects of both binder ratio and level on porosity formation, their
effect was very temperature dependent.
Results obtained from test castings poured at several casting
temperatures and incorporating unbalanced binder component ratios
favoring excess Part II are shown in Table 4.
These
results demonstrate the temperature dependency of porosity formation
with PUN binders. Pouring
temperatures of 2700oF
and higher (as measured in the pouring ladle) produce severe
subsurface defects when unbalanced ratios are used.
Such pronounced behavior is not observed when these ratios are
balanced or when excess Part I is used.
Reducing the pouring temperature at both binder levels resulted
in lesser amounts of porosity until at the lowest temperature sound
castings were achieved.
Pouring
temperature effects were further demonstrated by pouring experimental
test step cores that were coated with the polyisocyanate binder
component (Part II). For
these tests, pouring temperatures of 2500oF
were employed and test cores were bonded with an unbalanced (35:65
ratio) binder system containing 3.0% total resin.
Sectioned test castings obtained under these conditions were
entirely sound.
The
porosity-temperature dependency can best be illustrated in Figure 4. In this figure, pouring temperature is plotted against binder
ratio. It is interesting
to note that there appears to be a definite region in which porosity
seems to form and also another definite region where sound castings
are obtained. In between these two areas, porosity may or may not occur
depending on other liquid metal processing factors. Similar findings on the effect of pouring temperature with
other binder systems have been reported by other investigators.4,
16
Effect of
Section Size -- In
those castings containing porosity, it occurred in preferential
locations. Deep seated,
subsurface porosity was usually located adjacent to the 90o
re-entrant angle or "step" and most often occurred in
section thickness' ranging between 7/8 in. and 1-3/8 in.
These locations act as localized hot spots since a small volume
of the core is heated from both sides by the solidifying iron.
In thinner sections, varying degrees of surface porosity or pock marking
were often found. From
the appearance of these defects, it appears probable that they were
formed late in the solidification process by gaseous decomposition
products pushing away the semi-skinned over casting surface.17 Since these bubbles are formed late in the solidification
process at the mold-metal interface, not enough time was available for
their dissolution. Consequently,
a depression is left in the surface when final solidification
commences. The extent of
this surface porosity varied between somewhat large, semi-rounded
holes extending at most only 1/8 in. into the surface to very small
surface pores having no appreciable depth.
Sand
Effects -- The type of
sand used in experimental test cores had a significant effect on
porosity formation. Some results obtained with typical lake sand and washed and
dried silica sand are listed in Table 5.
Although
several castings were poured under identical conditions and also from
the same ladle, severe subsurface porosity was very prevalent with
washed and dried silica sand while castings made with the Michigan
lake sand were entirely sound. The
behavior of lake sand in eliminating gas defects may possibly be
attributed to either its significantly larger quantity of surface
impurities, bulk impurities or greater permeability.
To
determine the effect of surface purity on influencing gas porosity, an
acid treatment was administered to the lake sand to remove trace
surface impurities. The acid treatment consisted of soaking the sand in a
10% solution of sulfuric acid for 24 hours followed by a 24-hour water
wash and drying. Such
treatments have been shown to be very effective in removing these
impurities.18
Comparisons
of casting results obtained with acid-treated versus untreated Lake
Sands are shown in Table 6.
The results in Table 6 showed that removal of surface
impurities by acid leaching was not effective in promoting porosity
and no porosity was observed in the test castings.
Because of the known effect of permeability
on porosity defects and the potential chemical effect of sand type,
several other sands having a wide range of compositions,
permeabilities and AFS grain fineness distributions were selected for
testing. These tests were
run to determine relative porosity susceptibilities of common core and
molding sands. The
results of casting tests all run under identical conditions along with
the physical properties and resultant porosity sensitivities are
summarized in Tables 7 and 8.
Based on
the preceding, even though the sands tested had a wide range of AFS
grain fineness and permeabilities, there doesn't appear to be any
correlation between these parameters and porosity sensitivity.
The trend in Tables 7 and
8
is such that the lower the
impurity level, and particularly the iron oxide content of the sand,
the greater the sensitivity of the system for promotion of porosity
defects. Hence,
although very pure, round grained sands offer outstanding core and
mold making properties, they may not produce the best castings, as
less impure sands seem to do.
The
intentional addition of impurities such as iron oxide to sand mixes is
widely recognized as an effective means of controlling porosity,
veining, improving hot strength and other less incidental properties.
However, the presence of such a small amount of iron oxide as a
bulk impurity associated with the sand mineralogy appears to have a
significant effect on retarding or inhibiting porosity formation.
In addition, the type and purity of iron oxide will be shown to
have an overriding effect on porosity formation.
Binder
Dispersion or Mixing Effects
-- Proper dispersion of the liquid binder components on sand surfaces
is a necessary prerequisite in the production of high quality cores
and molds. Mixers which were prevalent in the early to mid 1970's often
provided relatively poor blending of binders and subsequent coating of
sand grain surfaces. This
was especially true of slow speed screw or auger types, which left
something to be desired where high mixing efficiency is desired.
Also, if the screw blades or paddles and trough are not cleaned
regularly to remove resin buildup, are poorly designed or wide
clearances exist due to wear, then poor mixing action will result. If proper dispersion of the binder components is not
realized, many areas of the core surface will essentially contain
varying ratios of binder components even though the bulk core may
contain the proper total amount of each component.
Although high speed, high efficiency sand mixers along with
advanced resin metering systems, often with computerized controls,
have been developed in the 1990's and have resulted in dramatically
improved mixing, consideration must still be given to properly
maintaining the equipment.
To determine the effect of proper
binder dispersion on mixing efficiency, several core mixes were made
in a laboratory high intensity batch mixer and mixed for various times
to simulate mixing conditions ranging from very poor to excellent.
Experimental test cores were made using mixing times of 5, 10,
20, 30 and 60 seconds for each component (double for actual total mix
cycle). All of
these cores were prepared with balanced ratios of Pt. I : Pt. II (50 :
50) on the standard washed and dried silica sand.
Cores prepared with total mixing times of 10, 20 and 30 seconds exhibited pronounced non-uniform binder
dispersion and were spotty in appearance.
This was found to be most pronounced with the 10 and 20 second
mix cycles. Longer mixing
times of 80, 120, and 240 seconds provided very uniform results.
Physical properties such as scratch and tensile strengths of
mixes mixed for total times of 40 seconds and longer were not impaired
even though traces of inadequate mixing were apparent on the 40-second
mix.
The
results obtained from casting tests using test cores prepared in the
described manner are listed in Table 9.
To briefly summarize these results, short mix cycles of 10 to
40 seconds total time tended to promote the formation of both surface
and subsurface porosity. Only trace amounts of subsurface porosity, probably better
described as microporosity, were found in the remaining castings made
with cores mixed for intermediate times of 60 to 80 seconds total.
In castings containing pronounced defects, these defects were
obviously formed where the solidifying casting was in contact with
binder-rich areas and particularly those containing excess
polyisocyanate. Sound
castings were obtained when total mixing times ranged from 2 to 4
minutes.
Effect of
Metal Composition -- The
type and composition of the castings poured had a significant effect
on porosity formation. Results
of these tests are shown in Table 10.
The porosity forming tendencies seemed to be greatest for the
low carbon equivalent iron and least for ductile iron.
Porosity defects in all gray iron castings formed readily when
unbalanced binder ratios favoring excess polyisocyanate were employed.
Porosity defects that formed in low carbon equivalent irons
were predominantly fissure type defects, although some rounded and
irregularly shaped holes also formed.
Ductile iron castings seemed to be far less susceptible to
defect formation than either composition of gray iron.
Results obtained with a high carbon equivalent iron as used
throughout this investigation have been previously reported and remain
unchanged.
Although it
is commonly accepted 1,19
that ductile iron is more susceptible to porosity defects, the present
investigation tends to show just the opposite.
However, most of these previous findings or observations have
been with ductile irons containing appreciable amounts of aluminum and
poured in green sand molds. 8,15
It is also generally held that ductile irons are more prone to
hydrogen defects arising from interactions with water vapor and
magnesium. This is
probably related to the fact that the residual magnesium is
influencing hydrogen solubility 15,20,21
or is assisting the reduction of water vapor.
However, Dawson and Smith also showed that although high
residual magnesium contents increased hydrogen solubility in ductile
iron castings poured in green sand molds, pinholes still did not form.20
Since the
chemistry and gaseous thermal decomposition products for PUN binders
are obviously more complex than those interactions with green sand
molds, the performance of ductile iron with these binders may in
actuality differ considerably.
However, one would expect porosity formation in ductile irons
to be much more difficult due to the higher melt interfacial surface
energy. Other
investigators have also reported a relationship between porosity and
surface tension in ductile irons. 9,22,23
Lastly, the bubbling of magnesium vapor through the metal
during the nodularizing process effectively purges most dissolved
gases from the metal, allowing for possible absorption of core gases
without super saturation. 23,
24
Effect of
Core Age -- The effect
of test core age within the first 24 hours after strip had no effect
on porosity formation. Test castings poured with cores used immediately after strip
or after overnight aging performed in a similar manner. Results obtained from aging tests poured at three pouring
temperatures are listed in Table
11.
If test cores made with unbalanced systems
were aged over several days under ambient conditions, the severity of
the defects increased slightly. This
phenomenon appears to be related to moisture from atmospheric humidity
combining with unreacted NCO groups in the polyisocyanate and forming
urea structures. 25,26
The porosity forming tendencies of this latter group of
substances is well known.1,2,8
They are reported to readily break down into ammonia
derivatives at high temperatures that later dissociate into nascent
hydrogen and nitrogen,1,27
both of which are highly soluble and dissolve very readily in molten
irons.
Elimination
of Porosity Defects
Numerous methods, both
metallurgical and chemical, were investigated as potential remedial
techniques to eliminate defects in castings poured under somewhat
adverse conditions. Most
of these techniques were straightforward in approach; however, those
techniques that may have resulted in reduced melt quality, such as
trace element additions of tellurium, selenium or bismuth, were not
examined in the original research work since it was felt that these
methods would not be very feasible.
Any potential gains in porosity elimination may have been
overshadowed by chilling and/or poor metal quality.
New techniques incorporating the use of proprietary inoculants
containing carefully controlled additions of surface active elements
as well as elements that neutralize nitrogen (by forming stable
nitride compounds) were examined and are reported herein.
Effect of
Titanium and Zirconium Additions
-- Additions of titanium have long been recognized as helpful
additives in reducing subsurface porosity defects related to nitrogen.1,3
To determine if such additions were effective in controlling
porosity in test castings poured with PUN test cores, varying levels
of 70% ferrotitanium (20 mesh x down) were added in the ladle prior to
pouring. Besides using
70% FeTi, two commercial gray iron inoculants containing titanium were
also examined. The
effect of zirconium on porosity reduction was evaluated by adding
0.05% zirconium as ferrosilicon zirconium as well as incorporating
zirconium into a high potency proprietary inoculant.
The casting results obtained from these tests are listed in Table
12.
In almost
all cases, the addition of small amounts of titanium as a ladle
addition was effective in eliminating subsurface porosity in castings
made with cores bonded with excessive Part II polyisocyanate levels.
In the case of 70% ferrotitanium additions, titanium additions
of 0.05% were effective in removing subsurface porosity defects, a
considerable amount of surface porosity or small pores remained.
Since it is well known that 70% ferrotitanium
may be difficult to dissolve at temperatures below 2,700oF,
resulting in erratic recoveries and results, two proprietary titanium
containing gray iron inoculants were also investigated.
Proprietary Inoculant A was effective in eliminating porosity
when the titanium addition level was 0.03%.
Inoculant B is based on 75% ferrosilicon, and since inoculants
based on 75% FeSi dissolve more rapidly than those based on 50% FeSi 28
, Inoculant B appeared to be more effective at somewhat lower titanium
addition rates.29 No porosity was found when titanium addition levels of
0.025% were employed with Inoculant B.
Ferrosilicon zirconium was almost as effective in eliminating
porosity but somewhat higher levels of 0.05% zirconium had to be
added. This was not
unexpected because of the higher atomic weight of zirconium.
Inoculant C is a potent proprietary gray and ductile iron
inoculant30 containing 30 to 33% oxy-sulfide forming elements
that was modified by the addition of 9.0% zirconium ( in the form of
ferrosilicon zirconium). With
zirconium additions of 0.025%, trace to no subsurface porosity was
found. Since zirconium
forms much more stable nitrides than titanium, more zirconium must be
added because of its higher atomic weight.
Hence, it is likely that higher levels of zirconium need to be
added to Inoculant C for complete porosity elimination.
Although Inoculant C did not entirely eliminate porosity, it
was the most effective of the three inoculants tested in reducing
chill and produced the most uniform microstructure, consisting of
100% Type A graphite flakes.
Metallographic
inspection of the castings made with 70% ferrotitanium showed that
higher addition rates of titanium (0.05% and greater) were effective
in tying up nitrogen as titanium compounds (TICN or TiN) and
preventing re-precipitation as gas holes during solidification.
Similar results were observed with the proprietary inoculants.
The ferrotitanium additions were not, however, effective in
preventing surface reactions associated with lustrous carbon pock marking
reactions from the high pouring temperatures employed
during this phase of the investigation.
The proprietary inoculants also showed some signs of lustrous
carbon related surface porosity.
Effect of
Zirconium and Selenium Inmold Additions
-- Addition of selenium to stainless steel castings poured in green
sand molds is very effective in eliminating porosity.31
Selenium is
a surface-active element and can result in degenerate graphite forms.
To evaluate the effect of controlled amounts of zirconium and
selenium on porosity elimination in gray iron, very small amounts were
added (8.0% zirconium as FeSiZr) to a proprietary 9-gram inmold
inoculating tablet. A
second experiment was also run with a supplemental addition of 3.3%
selenium to a 8.0% zirconium modified proprietary inmold inoculating
tablet. The casting
results obtained from these tests are listed in Table 13.
Effect of Iron
Oxide Additions -- The
addition of even small amounts of red iron oxide had an overwhelming
effect on porosity elimination. The
results of additions of varying amounts of 200 mesh red iron oxide (Fe2O3
or hematite) to PUN core sand mixes are shown in Table 14.
Additions
of as little as 0. 25% red (hematite) iron oxide were sufficient to
inhibit the formation of all traces of porosity in test castings
poured under adverse testing conditions.
It must be noted that since commercial foundry grades of red
iron oxide occur naturally, not all grades may work like the grades
used in the experiments. Further,
it has been shown that additions of Fe3O4 (magnetite) are
not nearly as effective as hematite in controlled casting tests.32,33
Casting tests run comparing hematite to magnetite are shown in Table
15.
These
results clearly show the effects of iron oxide mineralogy and
chemistry. Although two of the iron oxides had similar mesh sizes
(325 mesh x down), the 325 mesh red iron oxide (hematite) clearly
outperformed the black iron oxide (magnetite) as well as a coarser
(100 mesh) European hematite ore of relatively high purity.
It can be concluded that iron oxide purity doesn't appear to be
a determining factor in the performance of an iron oxide and its
subsequent effect on porosity elimination.
Although black iron oxide additions are commonly in use today,
much of the acceptance of black oxides is more likely related to
reduced surface area considerations.
Sand additives with reduced surface area allow for reduced
resin consumption and improved core making economics.
However, careful consideration must be given to the superior
effectiveness of red oxide in preventing porosity when choosing an
oxide addition.
It should
be noted that although some iron oxides may contain various
percentages of TiO2
(titanium dioxide) in their mineralogy, it is doubtful whether
sufficient time or quantities of the element titanium could be reduced
and be available to react with nitrogen during the casting process.
Hence, the presence of titanium dioxide in iron oxide would not
impart any beneficial effect on minimizing porosity susceptibility of
nitrogen bearing resins. All
of these findings illustrate that red iron oxide almost always
outperforms black iron oxide in producing sound, porosity free
castings as well as minimizing other resin related defects such as
lustrous carbon. 34
To determine the effect of iron oxide granularity, other grades
of hematite (Fe2O3)
were tested using the conditions outlined in Table
15.
At 1.5% and 4.00% levels, a much coarser grained hematite
addition was also was effective in eliminating defects even though it
was relatively randomly distributed in the core due to its large
particle size. This
behavior, coupled with how effective 0.25% red iron oxide was in
eliminating porosity, appears to preclude the long accepted role of
iron oxide in preventing defects. The role of iron oxide in preventing porosity has long
been linked with its ability to react with silica to form fayalite
which in turn forms a "physical" barrier preventing gas
solution. At the low
levels investigated and because of the behavior of the coarse grained
hematite, it appears probable that iron oxide is somehow affecting the
kinetics of gas absorption by the solidifying metal.
Regardless, such small additions could certainly not be
effective barrier formers at the levels employed.
To further establish if the formation of a
slag-type barrier at the mold-metal interface is a viable mechanism
responsible for porosity elimination, additions of sodium
fluoroaluminate (or cyrolite) were employed as sand additives.
Cryolite has a melting point of 1,825oF
and does not rely on reacting with silica as does iron oxide to form a
slag; cryolite will liquefy in-situ to form such a barrier.
Additions of 0.5%, 1.0% and 2.0% were evaluated in exactly the
same manner as the previously reported iron oxide additions.
The results obtained from these tests are shown in Table 16.
In these castings, veining defects were minimized but
considerable burn-on was present which appeared to be the result of
severe sand fluxing. However,
in all cases, severe subsurface porosity was found in the test
castings.
Core Washes
-- A considerable number of experimental core washes were applied
to test cores to determine effectiveness as porosity inhibitors.
Most of the washes were proprietary formulations but contained
varying amounts of red iron oxide.
Others were made by incorporating additives to a base gel.
Casting tests were run using those conditions previously
described that promoted porosity.
Results of these tests indicated that proprietary red iron
oxide (Fe2O3)
bearing washes provided very slight or no reduction in porosity
defects. Experimental
washes composed of aluminum powder and titanium powder provided
similar performance. However,
a 100% red iron oxide (Fe2O3)
wash, and another prepared with sodium silicate and iron oxide (Fe2O3)
completely prevented the formation of porosity.
This achievement was accomplished but at the expense of severe
surface finish degradation. The
sodium silicate red iron oxide wash deteriorated the casting surface
only slightly but the 100% red iron oxide wash had a very deleterious
effect on the surface. Overall
results tended to indicate that adequate amounts of iron oxide were
not employed in proprietary washes; however, in experimental washes
with red iron oxide, too much was added with a resultant loss in
surface smoothness. Apparently,
a delicate balance exists between the amount of iron oxide needed for
porosity elimination compared to the amount that results in
deteriorated surface finish.
Core
Post-Baking -- To determine
the effect of core baking on porosity elimination, several test cores
were subjected to post-baking or curing for three different times.
The results of these tests are summarized in Table 17.
Castings made with test cores baked at 450oF
but for only one hour contained severe porosity defects.
Intermediate times of 2 hours significantly reduced the extent
of porosity. Baking
for 4 hours at 450oF
produced a distinctive core color change to chocolate brown and had a
significant effect on porosity elimination.
For thorough baking to occur, it has been found that a color
change usually accompanies such a treatment and up to 55% of the
binder is volatilized. Although
such lengthy times may be impractical, higher baking temperatures or
short times at high temperatures might be effective in reducing
overall binder level in the core surface layers.
Baking also demonstrates that some free hydrocarbons are
undoubtedly volatilized and nitrogen components from the Part II resin
may undergo further reactions to form more stable compounds.
DISCUSSION
Although several variables have been
identified that either exaggerate or promote the formation of porosity
defects in PUN binders, these variables are in one way or another
related to the gaseous decomposition products generated by the resin
during casting. Decomposition
gases consisting of both hydrogen and nitrogen are readily liberated
during casting pouring and during subsequent solidification.
High pouring temperatures further enhance both the breakdown
rate and amount as well as favor increased gas solubility in the
liquid metal. High
pouring temperatures also have a significant effect on liquid metal
surface tension, which has been shown to have a significant effect on
porosity formation. 9,11
Because both hydrogen and nitrogen are readily available and
extremely soluble at the casting temperatures employed, their effect
on potential porosity defects is often additive.
Numerous
chemical analyses taken during this investigation showed that
considerable pickup of both hydrogen and nitrogen occurred in the
immediate subsurface layers when conditions favoring porosity were
employed. At depths of
0.25 in. and more below the cored surface, hydrogen and nitrogen
levels tended to be quite low and representative of the base metal.
It is probable that just before solidification, momentary super saturation
of both hydrogen and nitrogen exist just under the casting surface.
This complex nitrogen/hydrogen effect has long been recognized
by other investigators. 6,27,35
Further, if a considerable amount of nascent nitrogen is
dissolved in a casting from unbalanced binder ratios favoring
excessive polyisocyanate components, the presence of even a small
amount of hydrogen will serve to lower the overall solubility of
nitrogen. Stated another
way, hydrogen may be exerting a catalytic effect on nitrogen to
enhance porosity formation.
The same
effect of alloying elements on gas solubility is well known and acts
in a similar manner. To
further aggravate conditions, if the melt initially has a high gas
content resulting from the use of poor charge metallics or carbon
additives, 36 then the
tolerance for additional solution of nascent mold or core gases is
reduced considerably and porosity formation becomes extremely
favorable.
Microstructures
of sound and porosity containing castings taken in the immediate
vicinity of the mold-metal interface were identical.
In all cases, no differences in either matrix structure or
graphite morphology were found. Both
microstructures contained the same ferritic type matrix with Type A
graphite. The solidification rate and composition of all base gray iron
heats favored this type of structure.
Although it is widely recognized that hydrogen and nitrogen are
carbide stabilizers and favor formation of pearlite as well as alter
graphite structure,37-41 it
appears that insufficient time was available during solidification and
subsequent cooling through the transformation temperatures, for such
phases to form.
Although
most gas holes exhibited a bright or shiny interior of a graphitic
nature, no such films were observed during optical metallography.
Further examination of these areas with a scanning electron
microscope showed distinct layers of what appeared to be a crystalline
graphitic coating lining the interior of the gas holes.
The presence of this crystalline film has been reported by
numerous other investigators. 1,8
The morphology of gas holes that formed took many shapes, even
in the same casting. Both
fissure type gas holes as well as small spherical and pear shaped
holes were very often observed in the same casting.
Although for the most part, gas holes that formed were located
just underneath the surface, and most extended no more than 0.25 in.
into the casting, a few castings contained gas fissures almost 0.50
in. long (see Figure 5). Because
of the sub-surface nature of the defects, the incorporation of large
amounts of alloying elements that form stable nitrogen compounds may
not be needed since only these sub-surface layers are affected.
Incorporation of proprietary nitrogen stabilizing elements or
"scavengers," which include both titanium and zirconium
based ferroalloys, may offer additional possibilities for treating
binder induced porosity defects.
Likewise, inmold inoculating tablets incorporating zirconium
for nitrogen control and small amounts of selenium for hydrogen
control also offer promise for defect elimination.
Although the porosity studies focused on
using ladle additions of nitrogen stabilizing ferroalloys, the use of
beneficiated ilminite ore has also been shown to be a very effective
method of introducing the element titanium.
Mikelonis42 reported
that ilmenite ore was the most cost effective method of introducing
0.04 to 0.07 percent titanium levels to cupola melted irons.
The ilmenite was added as 3 in. x 2 in. ilmenite ore to the
cupola charge. In this research, it was reported that titanium
recovery levels were 30 to 40 percent of the total amount of titanium
in the ore. Other
developments aimed at improving titanium recoveries are based on using
beneficiated ilmenite ore that incorporate a proprietary blend of
halide containing fluxes.43
Such products are available in the form of a briquette
or tablet and can be used either as a furnace addition or ladle
addition. These products may also provide improved melt quality
by coalescing liquid and / or solid slags with the mild fluxing agents
incorporated in the tablet or briquette.
It
is not well understood how small amounts of red iron oxide (0.25%
addition rates) were so effective in eliminating subsurface porosity
in the test castings. It has been suggested that the red iron oxide is
exerting some type of "catalytic effect" on binder
decomposition products that minimize or alter the generation of
nitrogen and hydrogen gases.
One such theory is that when exposed to the sudden high
temperatures of iron casting, red iron oxide (Fe2O3)
readily releases oxygen. This
released oxygen immediately reacts with nitrogen decomposition
products from the binder to form stable NOX
compounds 44.
Since hematite (red iron oxide) has a much higher concentration
of oxygen compared to magnetite (black iron oxide), and based on the
improved performance of red iron oxide compared to black, this
mechanism certainly appears to be very feasible.
CONCLUSIONS
Unbalanced PUN systems favoring excess Part II or polyisocyanates promote the occurrence of gaseous mold-metal reactions resulting in both surface and subsurface gas defects. High binder levels also tended to slightly increase defect propensity even when balanced ratios were employed. Balanced or slightly unbalanced isocyanate / polyol hydroxyl ratios favoring excess Part I were relatively unsusceptible to such defects although a few cases of slight porosity were found.
Inadequate mixing that results in poor distribution of the binder components in the mix was also found to accentuate porosity formation.
The temperature of the molten iron as it contacted the core surface was found to have a significant effect on porosity formation when castings were poured under conditions favoring their formation. Severe porosity defects were formed at 2700o F and higher. As the temperature was reduced, these defects became fewer in number and intensity until none formed at 2550o F.
Porosity formation was found to be very sensitive to core sand type. Lake sands were relatively insensitive to defect formation while high purity, round grained white silica sands were found to be very sensitive.
Cast iron composition had an effect on porosity formation. Ductile iron was least susceptible to defect formation while low carbon equivalent irons were most susceptible.
Addition of titanium compounds, either in the form of 70% ferrotitanium or proprietary gray iron inoculants containing titanium were effective in eliminating porosity defects. Zirconium additions were also somewhat effective in eliminating defects at the addition levels employed. Incorporation of ferrosilicon zirconium into a proprietary inoculant was also found to reduce the incidence of defects.
The addition of small amounts of red iron (Fe2O3) oxide (82% minimum purity) to silica sand mixes was extremely effective in eliminating porosity. Sound castings were obtained with additions as small as 0.25% red iron oxide. Black iron oxides were not anywhere as effective as red iron oxide.
No metallurgical changes in either graphite morphology or matrix structure occurred in the gas affected mold-metal interface region. A layer or film, probably graphitic in nature, was found lining the internal surfaces of most gas holes.
Porosity defects tended to form in geometric hot spots or re-entrant angles on the test casting. The location seems to indicate that localized heating of the core re-entrant angles creates a condition that results in a momentary super saturation of the surface layers. Gas analysis taken well beneath the affected surface layers showed normal gas contents.
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List of Figures:
Figure 2:
Dimensions of cylindrical test casting.
Figure 3.
Types of porosity defects encountered in test castings
Figure 4:
Effect of pouring temperature on porosity formation.
Figure 5:
Morphology of subsurface gas porosity (1.5 x magnification)
List
Table 1:
Compositions of Test Castings Poured
Table 2:
Effect of Binder Ratio on Porosity Formation
Table 3:
Effect of Binder Level on Porosity Formation
Table 4:
Effect of Pouring Temperature on Porosity Formation
Table 5:
Effect of Sand on the Formation of Porosity
Table 6:
Effect of Acid Surface Treatments on Porosity
Susceptibility
Table 7:
Effect of Sand Type on Porosity Formation
Table 8:
Physical and Chemical Properties of Sands
Table 9:
Effect of Mixing Time and Mixing Efficiency on Porosity
Formation
Table 10:
Effect of
Type and Composition of Castings on Porosity Formation
Table 11:
Effect of Core
Aging on Porosity Formation
Table 12:
Effect of Titanium
and Zirconium Additions on Porosity Formation
Table 13:
Effect of Selenium
and Zirconium Additions on Porosity Formation
Table 14:
Effect of red iron oxide (hematite) on Porosity Formation
Table 15:
Effect of Iron Oxide Type on Porosity Elimination
Table 16:
Results of Casting Tests with Cryolite Additions
Table 17:
Results of Casting Tests with Test Cores baked for 1, 2,
and 4 hours
Tables
Table 1:
Compositions of Test Castings Poured
| High C.E. | Low C.E. | Ductile | ||||
|
%C |
3.50 | 2.90 | 3.5-3.6 | |||
| %Si | 2.40 | 1.70 | 2.5-2.6 | |||
| %Mn | 0.50 | 0.50 | 0.35 | |||
| %S | 0.02 | 0.02 | 0.01 max | |||
| %P | 0.02 | 0.02 | 0.01 | |||
| %Mg | -- | -- | 0.04 | |||
| %Ni | -- | -- | 0.80 | |||
Table 2:
Effect of Binder Ratio on Porosity Formation
Back to
Article
| Binder Level | Ratio Pt I: Pt. II | Porosity Extent |
| 1.50% (1998 version) | 60 : 40 | nil |
| 1.50% | 60 : 40 | nil |
| 1.50% | 50 : 50 | nil to trace |
| 1.50% | 40 : 60 | traces to moderately severe |
| 1.50% (1998 version) | 35 : 65 | severe |
| 1.50% | 35 : 65 | severe |
|
Test conditions: PUN binder with washed and dried silica sand (W/D) Iron Chemistry - 4.3 C.E. iron, Pouring temperature - 2700oF |
||
Table 3:
Effect of Binder Level on Porosity Formation
| Binder Level | Ratio: Pt I : Pt. II | Porosity Extent |
| 3.0% | 60:40 | nil to trace |
| 3.0% | 50:50 | moderate |
| 3.0% | 40:60 | severe |
| 3.0% | 35:65 | very severe |
| 1.8% | 60:40 | none |
| 1.8% | 50:50 | trace |
| 1.8% | 35:65 | severe |
| 1.5% | 60:40 |