U.S. patent number 3,853,635 [Application Number 05/299,048] was granted by the patent office on 1974-12-10 for process for making carbon-aluminum composites.
This patent grant is currently assigned to Pure Carbon Company, Inc.. Invention is credited to Joseph F. Demendi.
United States Patent |
3,853,635 |
Demendi |
December 10, 1974 |
PROCESS FOR MAKING CARBON-ALUMINUM COMPOSITES
Abstract
A process for impregnating a mass of carbon particles with
metal, preferably an aluminum alloy, to form a solid billet
suitable for machining therefrom articles having advantageous
durability and lubricity characteristics, particularly as apex
seals for Wankel engines. A mass of carbon particles is heated to a
temperature at or above the melting point of the metal in a closed
crucible of permeable refractory material such as porous carbon,
and the molten metal is poured over the porous crucible into a
second crucible wherein the porous crucible becomes enveloped by
the molten metal but the molten metal does not penetrate the porous
crucible. The atmosphere surrounding the molten metal and porous
crucible is then pressurized to force the molten metal through the
porous crucible and thus cause controlled impregnation of the mass
of particles.
Inventors: |
Demendi; Joseph F. (St. Marys,
PA) |
Assignee: |
Pure Carbon Company, Inc. (St.
Mary, PA)
|
Family
ID: |
23153087 |
Appl.
No.: |
05/299,048 |
Filed: |
October 19, 1972 |
Current U.S.
Class: |
148/549; 148/437;
164/120; 420/548; 164/97; 264/128; 428/614 |
Current CPC
Class: |
F01C
19/02 (20130101); C04B 41/51 (20130101); C04B
41/009 (20130101); C04B 35/52 (20130101); C04B
41/009 (20130101); C04B 41/88 (20130101); C04B
41/51 (20130101); C04B 41/4505 (20130101); C04B
35/52 (20130101); Y10T 428/12486 (20150115) |
Current International
Class: |
C04B
35/52 (20060101); F01C 19/02 (20060101); C04B
41/45 (20060101); C04B 41/51 (20060101); C04B
41/88 (20060101); F01C 19/00 (20060101); C22f
001/04 () |
Field of
Search: |
;148/3,13,127,131,4,32,34 ;75/2R,2F,143,138,148,68R ;164/97,86,120
;264/128,29 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Dean; R.
Attorney, Agent or Firm: Bosworth, Sessions & McCoy
Claims
I claim:
1. A process for impregnating a mass of carbon particles with an
alloy of aluminum, silicon and at least one other metal comprising
the steps of:
melting a quantity of said alloy,
placing a mass of carbon particles in a porous crucible formed from
a refractory material, said particles being smaller than 40 microns
and having a porosity range of 30 to 60 percent by volume, the
porosity of the porous crucible being at least 20 percent by
volume,
placing the porous crucible in an impermeable crucible,
pouring the molten alloy over said porous crucible and into said
impermeable crucible,
equalizing the temperature between said molten alloy and said
crucibles,
subjecting said crucibles, carbon particles and molten alloy to a
gas pressure of between 2,000 psi and 4,500 psi for from one to
five minutes to force said molten alloy to penetrate the porous
crucible and impregnate the carbon particles,
rapidly cooling the porous crucible to room temperature, and
then
removing the thus formed billet of alloy-impregnated carbon
particles.
2. A process as defined in claim 1 wherein said metal comprises a
hyper-eutectic aluminum-silicon alloy, said particles comprise
calcined coconut shell char, and said alloy is at a temperature of
about 1,100.degree.F. when the pressure is applied.
3. A process as defined in claim 1 wherein the billet is annealed
for from 6 to 10 hours at 900.degree. to 1,000.degree.F. and then
further held for from 3 to 5 hours at 400.degree. to 500.degree.F.
and then rapidly cooled to room temperature.
4. A process as defined in claim 1 wherein the porous crucible is
made of a non-graphitized carbon and the billet is removed from the
crucible by breaking away the crucible.
Description
BACKGROUND OF THE INVENTION
This invention relates to the manufacture of a seal material for
use in sealing moving parts of expansion chambers such as the
combustion chambers of rotary piston internal combustion engines.
More particularly, the invention relates to a method for making a
billet or blank of a composite carbon-aluminum alloy material
having advantageous properties, from which seals such as apex seals
may be machined.
The apex seals for rotary piston engines (e.g., Wankel engines) are
fitted at each apex of the rotary piston or trochoid and are
adapted to make a planetary motion with the piston while being
urged against the inner surface of the stator by the combined
action of the elastic force of springs disposed behind the apex
seal, gas pressure in the operating chamber and centrifugal force
produced by the rotation and orbiting of the piston. The seal moves
in sliding contact with the inner surface of the stator and
maintains an airtight seal between adjacent expansion chambers on
opposite sides of the apex. Therefore, the apex seal used for this
purpose must have excellent mechanical strength at all temperatures
encountered and sufficient lubricity that it does not produce an
excessive wear on the inner surface of the stator. In view of these
considerations and others, the quality of the apex seal has a
significant bearing on the performance and durability of the
engine.
Many and various materials have been proposed for the apex seal
such as those shown in U.S. Pat. No. 3,619,430 and in British Pat.
No. 1,234,634. The most successful material presently available
comprises carbon particles impregnated with an aluminum silicon
alloy.
Carbon is an excellent bearing material due to its heat resistance,
wear resistance and corrosion resistance as well as other
advantages such as high thermal conductivity and low thermal
expansion. Accordingly, carbon in various forms and combinations is
used for many types of mechanical elements, particularly sliding
members in view of its wear resistance and lubricity. The use of
carbon products as sliding members and the like, however, is
limited because of their inherently low durability, particularly
where they are subjected to considerable vibration and impact.
Methods have been devised for manufacturing apex seals of a mass of
carbon particles impregnated with a continuous phase of aluminum or
an aluminum alloy and while aluminum is somewhat inferior in wear
resistance to many other metals and has a relatively low melting
point, the resulting composite material has increased strength and
better resistance against vibration and impact. One reason that the
aluminum-impregnated carbon type apex seal has superior
characteristics is that a high ratio of impregnation can be
achieved with aluminum and the aluminum in the resulting product is
intimately and tightly bonded to the carbon due to the formation of
aluminum carbide at the carbon-aluminum interface.
One impregnating process is accomplished in an autoclave by
immersing a porous press-molded blank made from carbon particles
and a binder in a molten aluminum or aluminum alloy bath. The
autoclave is evacuated and the pre-pressed blank is impregnated
with the molten metal in a nitrogen or argon atmosphere in order to
prevent the carbon from oxidizing. Following immersion of the
carbon blank a high pressure is applied to force the molten metal
into the voids in the carbon blank. For suitable properties, it is
necessary that the impregnation of the carbon blank with the alloy
be as complete as possible. It has been found that a sufficient
impregnation of metal is difficult to achieve without using high
temperatures and pressures over relatively long times.
An autoclave and related equipment for achieving the impregnation
is disclosed in U.S. Pat. No. 3,599,601. Using the apparatus shown
in that patent, a sintered or otherwise preformed molded part is
loaded in a dip cage formed of refractory material having a
plurality of slits formed therein to permit entry of molten metal.
The product is heated in the dip cage to the desired temperature
and then with the autoclave partially evacuated, lowered into a
bath of molten metal. A pressure is applied and the molten meal is
thus forced through the porous article to be impregnated.
The method of the present invention affords an improved process
which can be accomplished more quickly, more efficiently, is
accurately controlled, eliminates the need for preforming the part
or parts to be impregnated, permits a higher alloy to carbon ratio,
and affords other features and advantages heretofore not
obtainable.
SUMMARY OF THE INVENTION
It is among the objects of the invention to provide an improved
method for impregnating a carbonaceous product with a molten
metal.
Another object is to provide an improved method for making
combustion chamber seals for rotary piston-type internal combustion
engines.
These and other objects are achieved through a method for
impregnating carbon particles with a molten metal, preferably an
aluminum or aluminum alloy, which includes the following steps:
1. placing a quantity of carbon particles in a porous crucible
formed of refractory material such as porous carbon and densifying
the particles by vibration or jarring,
2. heating the carbon powder in the porous crucible to a
temperature within or above the melting point range of the metal in
an inert atmosphere,
3. placing the heated porous crucible and carbon particles in an
impermeable crucible formed, for example, of ceramic material,
4. heating the metal within or above its melting point range,
5. pouring the metal in molten form over the porous crucible and
into the impermeable crucible,
6. holding the porous crucible in the molten metal for at least
half an hour in order to establish thermal equilibrium at a
temperature within the melting point range of the metal,
7. placing the two crucibles in a pressure chamber such as an
autoclave, and pressurizing the atmosphere to a pressure between
2,000 and 4,500 psi for a very short time, 1 to 10 minutes, to
force the molten metal to penetrate the porous carbon crucible and
impregnate the mass of carbon particles, and
8. removing the porous crucible, quenching and cooling to room
temperature and then breaking away the porous crucible to obtain a
billet of impregnated material.
When the metal is an aluminum-silicon alloy, the billet is rough
machined into blank parts and further heat treated. It should be
heated to approximately 935.degree.F. for about 8 hours, then
heated at about 450.degree.F. for about 4 hours, and then final
machined into apex seals. This treatment imparts dimensional
stability and the desired grain structure. When other alloys and
metals are used, further annealing and heat treatment should be
employed as is appropriate to the particular alloy or metal.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a sectional view showing an initial portion of the method
of the invention using apparatus that is illustrated in
diagrammatic form merely for the purpose of illustrating the
method;
FIG. 2 is a sectional view showing the apparatus in a manner
similar to FIG. 1 and illustrating a subsequent step in the
practice of the invention;
FIG. 3 is still another sectional view illustrating apparatus in a
manner similar to FIGS. 1 and 2 and showing a still further step in
the practice of the method of the invention; and
FIG. 4 is a sectional view in diagrammatic form illustrating the
breaking away of the material forming the impregnated porous
crucible from the carbon-alluminum composite product made in
accordance with the method of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
As indicated above, the invention resides in a method for making
carbon-aluminum impregnates suitable for use in fabricating seals
for various types of mechanical equipment such as seals used in the
trochoid of rotary piston-type internal combustion engines. The
method first requires the selection of appropriate materials. It
has been found that a particularly advantageous form of particulate
carbon material is calcined coconut char which is a particularly
hard and abrasion-resistant type of char. This material preferably
has a particle size of no more than 100 microns, and preferably no
more than about 40 microns. Other hard, abrasion-resistant chars
such as those made from walnut shells or other nut shells may also
be used.
The molten aluminum alloy used as the impregnate is, in accordance
with the preferred aspect of this invention, an aluminum-silicon
alloy having a silicon content ranging from 5 to 35 percent by
weight. The silicon in the alloy forms small grains which give the
alloy strength at high temperatures. Preferably this is a
hyper-eutectic alloy having 14 to 19 percent silicon. Silicon is
soluble in aluminum to about 11 percent by weight, after which the
silicon crystallizes out as tiny grains or crystals. A particularly
advantageous alloy is an aluminum-silicon material sold the
Aluminum Association trade designation "A-390." This is a
hyper-eutectic alloy in the sense that it has more silicon than the
eutectic point, in the case of A-390, about 17 percent silicon.
Simple binary alloys of aluminum and silicon are not believed to be
desirable. I prefer 2 to 5 percent copper or nickel and other
elements found in A-390 and similar alloys.
An aluminum alloy is preferred because it readily "wets" and
penetrates the carbon char particle powder. Other metals and alloys
may be adapted to this process such as copper or other metals
listed in column 2 of U.S. Pat. No. 3,599,601. Aluminum-magnesium
alloys may be used. However, for the immediate purposes of this
invention, I prefer a metal which is principally aluminum, by which
I mean at least 50 percent aluminum by weight.
The porous baked carbon crucible preferably has a porosity of at
least about 20 percent of the total volume thereof. Crucibles of
lower porosities, as low as 5 percent by volume, may be employed
but they are not as suitable because they require a longer
impregnation time and because they are more expensive to
manufacture. The porous crucible is preferably made of a
nongraphitized carbon.
The porosity of the mass of carbon particles is of a higher order,
as at least 20 percent and preferably around 50 percent by volume.
After being placed in the porous crucible, the carbon particles are
densified by vibration or jarring and the above porosities are to
be taken after such densification. The preferred porosity range is
30 to 60 percent by volume.
Referring more particularly to the drawings which show apparatus
for practicing the invention, in diagrammatic form only, a
preferred embodiment of the method will be illustrated and
described using materials found to be particularly advantageous.
Initially the mass of carbon particles, or more specifically, the
calcined coconut char 10, is placed in a porous ceramic crucible 11
preferably formed of fairly thin-walled baked carbon material and a
lid 12 formed of the same material is placed thereon (FIG. 1). The
powder is densified by vibration or jarring. The porous crucible 11
preferably has a porosity of about 20 percent by volume and the
carbon powder preferably has a porosity of about 50 percent by
volume.
The crucible 11 is heated in an induction furnace to a temperature
in excess of the melting point of the metal or within the melting
point range, in the case of the aluminum-silicon alloy, around
1,100.degree.F. The heating is done in a nitrogen or argon or other
inert gas atmosphere ot reduce or eliminate the oxygen. The
crucible 11 may be heated by itself or it may be placed inside the
ceramic crucible and the assembly heated in the induction furnace
in an inert atmosphere.
The metal 13 is also heated to a molten condition, again in this
instance around 1,100.degree.F. in an induction furnace. The
heating may advantageously be accomplished in the same furnace and
the temperature should be very carefully monitored. Preheating of
the porous crucible and carbon powder to that high a temperature,
however, is only preferable. Preheating to lower temperatures,
about 350.degree.F, may be employed and is beneficial in that it
drives out some gas and moisture from the carbon powder.
When the metal is heated, it may also be purified as is well known
in the art. In the case of an aluminum-silicon alloy, chlorine gas
may be bubbled through the molten alloy to eliminate entrapped
oxygen and hydrogen. Alternatively, degassing tablets may be added
to the melt. Also, to control grain size, a nucleating agent such
as aluminum phosphide may be added.
The volume of metal to be melted should be weighed and selected in
accordance with a predetermined amount of material needed depending
upon the volume of the mass of carbon particles 10. After the
necessary heating of the carbon particles 10 and the metal 13 has
been accomplished, the porous crucible 11 is carefully fitted into
an impermeable ceramic crucible 15 preferably formed of
graphite-clay material and having spacers 16 located on the bottom
thereof as indicated in FIG. 1. A lid 21 provided with holes 22 is
placed on the ceramic crucible 15 and over the porous crucible to
keep it in place.
Referring next to FIG. 2, it will be seen that the molten alloy 13
is poured from the ceramic crucible 14 over the lid 21 so that it
overflows down and around the walls of the porous crucible 11 to
fill the spaces within the impermeable ceramic crucible 15. The
spacers 16 serve to support the porous crucible 11 above the floor
of the impermeable ceramic crucible 15 so that the molten metal
essentially surrounds all surfaces of the porous crucible 11.
The assembly of the impermeable ceramic crucible 15, porous carbon
crucible 11, carbon particles 10 and molten aluminum 13 is then
maintained at a temperature approximately above or within the
melting point range of the metal for a time sufficient to equalize
the temperature between the crucibles and the molten metal. There
is no pressure on the system and the molten metal does not
penetrate the porous crucible 11. Finally, the assembly is placed
in a quick-opening autoclave 17 (see FIG. 2) and a lid 18 is
tightly attached to provide a hermetic seal.
After this thermal equilibration, the space within the autoclave 17
is then pressurized using a pump 19 to provide a pressure between
about 2,000 to 4,500 psi for from 1 to 10 minutes and preferably 2
to 5 minutes. This is a pneumatic pressure, air or an inert gas
such as nitrogen or argon. A pressure of 4,200 psi is believed to
be particularly advantageous. The high pressure in the autoclave
atmosphere forces the molten metal 13 to penetrate the porous
carbon crucible 11 and lid 12 and then to impregnate the mass of
carbon particles 10. Any scum that may form on the surface of the
molten metal will be filtered out by the porous crucible 11 and
thus not penetrate into the mass of carbon particles. The extent of
impregnation of the voids or spaces within the mass of carbon
particles 10 is essentially complete and any gas originally
contained within the mass of particles is either dissolved into the
molten metal or expelled through the porous crucible 11.
The application of pressure is continued for a short period of
time, preferably 2 to 5 minutes, just barely sufficient to cause
complete impregnation of the mass of particles 10. As soon as the
impregnation is believed to be complete, the pressure is reduced to
normal, the lid 18 removed and the assembly within the autoclave
removed and quenched to room temperature.
The duration of the application of pressure is minimized so as to
carefully control the reaction of aluminum and carbon which forms
aluminum carbide. While the presence of aluminum carbide in the
product of amounts of around 3 to 6 percent is desirable,
quantities in excess of such percentages are to be avoided for the
reason that excess aluminum carbide reacts with water vapor thus
causing erosion of the seal material. The reaction between the
molten aluminum and carbon to form an aluminum carbide interface
facilitates impregnation by the molten metal.
After quenching, the billet of impregnated material is broken away
from the porous crucible (FIG. 4). In the case of the
aluminum-silicon alloy, the billet is then cut up into blanks and
further heat treated and annealed. The billet may be annealed for
from 6 to 10 hours at 900.degree. to 1,000.degree.F. and then from
3 to 5 hours at 400.degree. to 500.degree.F., preferably at the
times and temperatures previously noted, and then quenched in air
to room temperature. After heat treatment, the blanks are finally
machined into apex seals.
As should be apparent, the process of the present invention has
particular utility in the manufacture of aluminum silicon alloy
impregnated seals. The A-390 alloy solidifies within a range of
1,050.degree. to 1,200.degree.F.
In dealing with such alloys, the temperature of impregnation, by
which I means the temperature at which the air pressure is
introduced into the autoclave, should be within the melting point
range, about 1,100.degree.F. When the temperature is much over
1,100.degree.F. and towards the top end of the melting point range,
there is too much of a reaction between the aluminum and carbon
resulting in the formation of too much aluminum carbide and a part
of poor physical properties.
While pressures in the order of 3,500 to 4,500 psi are preferred, I
am able to impregnate a powder with pressures down as low as 100
psi. When there is no problem of chemical reactions between the
metal and carbon powder, I believe that such lower pressures may be
satisfactory for production operations. I prefer the higher
pressures in the case of aluminum-silicon alloys because I can
obtain impregnation in shorter times, more surely in
production.
The following example illustrates the invention:
Calcined coconut shell charcoal was placed in a porous carbon
crucible. The material had the following particle size range:
6% above 32 micron 50% above 20 micron 95% above 8 micron
It was vibrated to a density of 0.8 grams per cubic centimeter.
Aluminum Association A-390 aluminum-silicon alloy was melted and
chlorine gas bubbled through it. Aluminum Association A-390 alloy
has the following composition:
16 to 18% silicon 4-5% copper 0.5 max iron 0.45-0.65 magnesium .2%
max titanium .1% max manganese .1% max zinc trace phosphorus
balance aluminum
The porous carbon crucible was placed in a ceramic crucible and
heated to 1,100.degree.F. in a nitrogen atmosphere. The molten
A-390 was poured over it and the assembly soaked at 1,100.degree.F.
for 30 minutes to equalize the temperature. Then it was placed in a
quick-opening autoclave. Then air at 4,200 psi was admitted to the
autoclave for 2 minutes. Thereafter, the pressure was released and
the autoclave opened up, and the porous crucible removed from the
molten metal and quenched to room temperature.
Thereafter, the billet was broken out and cut into rough blocks
which were heated at 935.degree.F. for 8 hours and then at
450.degree.F. for 4 hours. The heat-treated blocks were final
machined into apex seals.
The material had the following physical characteristics:
apparent density 2.06 gm/cc hardness RG 90 transverse strength
27,000 psi resistance .000033 ohm-inches
Seals made from this material were tested in a Wankel engine. The
engine was a 32 cubic inch engine with an 81/2 to 1 compression
ratio. The seals lasted for 159 hours with a wear of 0.0042 inches.
The seals broke due to a malfunction of another component.
The above-described seal material contained approximately 38
percent carbon by weight. A suitable carbon weight percentage range
is 35 to 45 percent. The aluminum-silicon alloy and carbon reaction
products comprise the balance. I could not measure the amount of
carbide reaction products. The aluminum-silicon alloy contained
about 17 percent silicon, the desired range being between 14 and 20
percent silicon, from 0 to 5 percent copper or nickel and less than
1 percent other elements selected from magnesium, titanium and
iron.
The carbon powder density was 0.8 grams/cc and the alloy density
was 2.7 grams/cc. The density of the seal material was 2.1
grams/cc. A suitable density range is 1.9 to 2.3 grams/cc.
The electrical resistance ranges from 20 to 60 micro-ohm inches.
The transverse strength should be at least 25,000 psi. The Rockwell
G hardness should be in the range of 80-100.
The foregoing seal material functions as described as a Wankel
engine apex seal, a most difficult application.
While the invention has been shown and described in connection with
a specific embodiment thereof, this is intended for the purpose of
illustration rather than limitation and other variations and
modifications of the specific method herein shown and described
will be apparent to those skilled in the art all within the
intended spirit and scope of the invention. Accordingly, the patent
is not to be limited to the specific embodiment of the method of
the invention herein shown and described nor in any other way that
is inconsistent with the extent to which the progress in the art
has been advanced by the invention.
* * * * *