U.S. patent number 3,894,863 [Application Number 05/511,794] was granted by the patent office on 1975-07-15 for graphite composite.
This patent grant is currently assigned to Fiber Materials, Inc.. Invention is credited to Apul F. Jahn, Walter L. Lachman, Robert A. Penty.
United States Patent |
3,894,863 |
Lachman , et al. |
July 15, 1975 |
**Please see images for:
( Certificate of Correction ) ** |
Graphite composite
Abstract
A novel graphite fiber/metal composite material, the graphite
fibers having a coat of titanium boride which may be mixed with
titanium carbide. The coat, which promotes wetting by metals such
as aluminum, copper and lead, is formed by an intermediate
temperature vapor deposition technique involving the reduction with
zinc vapor of a mixture of gaseous titanium and boron halides.
Inventors: |
Lachman; Walter L. (Concord,
MA), Penty; Robert A. (Kennebunk, ME), Jahn; Apul F.
(Chelmsford, MA) |
Assignee: |
Fiber Materials, Inc.
(Biddeford, ME)
|
Family
ID: |
26993559 |
Appl.
No.: |
05/511,794 |
Filed: |
October 3, 1974 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
|
343650 |
Mar 22, 1973 |
3860443 |
|
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|
Current U.S.
Class: |
148/400; 148/432;
148/437; 428/367; 428/611; 428/902; 428/366; 428/389; 428/614;
428/938 |
Current CPC
Class: |
C04B
41/507 (20130101); C23C 16/56 (20130101); C22C
49/14 (20130101); C04B 41/87 (20130101); C23C
16/38 (20130101); C04B 41/009 (20130101); C04B
41/507 (20130101); C04B 41/4529 (20130101); C04B
41/455 (20130101); C04B 41/507 (20130101); C04B
41/4529 (20130101); C04B 41/455 (20130101); C04B
41/5061 (20130101); C04B 41/009 (20130101); C04B
35/522 (20130101); C04B 41/009 (20130101); C04B
14/386 (20130101); Y10S 428/902 (20130101); Y10T
428/2918 (20150115); Y10T 428/12465 (20150115); Y10T
428/2958 (20150115); Y10S 428/938 (20130101); Y10T
428/2916 (20150115); Y10T 428/12486 (20150115) |
Current International
Class: |
C22C
49/14 (20060101); C23C 16/38 (20060101); C23C
16/56 (20060101); C04B 41/50 (20060101); C04B
41/45 (20060101); C04B 41/87 (20060101); C22C
49/00 (20060101); C23c 011/08 (); C23c
001/00 () |
Field of
Search: |
;117/71R,16C,16R,228 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Weiffenbach; Cameron K.
Assistant Examiner: Varndell; Ralph E.
Attorney, Agent or Firm: Schiller & Pandiscio
Parent Case Text
This is a division of U.S. Pat. application Ser. No. 343,650 filed
Mar. 22, 1973 now U.S. Pat. No. 3,860,443.
Claims
What is claimed is:
1. A composite product comprising a plurality of carbon fibers each
have a coating of a material selected from the group consisting of
titanium boride, and a mixture of titanium boride and titanium
carbide said fibers being disposed in a substantially solid matrix
of metal selected from the group consisting of magnesium, lead,
zinc, copper, aluminum, tin and alloys of said metals.
2. A composite as defined in claim 1 wherein said fibers are
substantially graphite.
3. A composite as defined in claim 1 wherein the thickness of said
coating is in the range of between about 100 to 10000
Angstroms.
4. A composite as defined in claim 2 wherein said metal comprises
aluminum.
5. A composite as defined in claim 2 wherein said metal comprises
copper.
6. A composite as defined in claim 2 wherein said metal comprises
lead.
Description
The present invention relates to composite materials, and more
specifically to composites of carbon fibers embedded in a metallic
matrix, and the method of making same.
High strength, low weight structures can be formed of composites of
filaments embedded or bound in a matrix. Particularly, carbon
fibers have high tensile strength and a high modulus of elasticity,
so that composites formed of a metal matrix containing such fibers
aligned in the direction of maximum expected stress can be readily
used for components requiring high strength-to-density and high
modulus-to-density ratios over a wide range of temperatures.
Metal-graphite composites also combine the lubricating properties
of graphite with the toughness of the metal to provide a material
with a low coefficient of friction and wear resistance. Composites
of graphite with materials such as aluminum and copper, exhibit
great strength and high electrical conductivity.
A number of metals in molten form, such as aluminum and the like,
do not readily wet graphite. It has been suggested that the
graphite can be wetted by molten aluminum if a layer of aluminum
carbide is first provided at the interface between the metal and
fiber, but that such aluminum carbide phase cannot be tolerated due
to its thermochemical and mechanical instability. In U.S. Pat. No.
3,553,820 issued to R. V. Sara, it is taught that aluminum graphite
fiber composites can be formed by first coating the fibers with a
tantalum film by electrodeposition from a fused salt bath,
outgassing the fibers by pumping them down to a very low pressure
and submerging the outgassed fibers into a pressurized molten
aluminum bath to fill the interstices of the fibers. A similar
process is described in U.S. Pat. No. 3,571,901 issued to R. V.
Sara, in which the carbon fibers are first coated with silver or a
silver aluminum alloy by electrodeposition from the plating
solution, then the fibers are contacted with aluminum foil and the
combined foil-fiber is heated while under pressure to the solidus
temperature of the foil. In both of these systems, it is also
suggested that the metal coating can be applied by sputtering or by
reduction of salts of the metal. Whether using silver or tantalum,
it is difficult to obtain uniform thin coatings on the fibers, and
in any event, the resulting composites contain substantial amounts
of expensive, heavy material such as silver and tantalum.
Electrodeposition and chemical deposition techniques have also been
used to deposit the matrix material directly around graphite
fibers, the coated fibers being subsequently hot-pressed to form
composites. The major disadvantage of forming composites with such
deposition techniques is that for the most part, the matrix
material is usually limited to a rather pure metal, which for many
purposes has markedly inferior properties compared to alloys.
A principal object of the present invention is therefore to provide
a simple, unique process for forming metal/graphite fiber
composites without resort to high pressures or temperatures.
Another object of the present invention is to provide a unique
metal/graphite composite in which the composition of the matrix
material may be varied over a wide margin. Yet other objects of the
present invention will in part appear obvious and will in part
appear hereinafter.
The invention accordingly comprises the process and the several
steps and the relation of one or more of such steps with respect to
each of the others, and the products and compositions possessing
the features, properties and relation of elements which are
exemplified in the following detailed disclosure and the scope of
the invention all of which will be indicated in the claims.
Generally to effect the foregoing and other objects the present
invention involves a thin, substantially uniform coating of a
wetting agent on carbon fibers, the wetting agent being titanium
boride, titanium carbide or a mixture of both, the interstices
between the coated fibers being filled with a metal infiltrated
initially as a liquid under ambient pressure. Because it is not
considered possible to account for the formulae generally of
borides in terms of ordinary conceptions of valency, the term
"boride" as used herein is not to be considered limited to any
particular stoichiometric relation unless specifically
indicated.
For a fuller understanding of the nature and objects of the present
invention, reference should be had to the following detailed
description taken in connection with the accompanying drawing
wherein there is shown a diagramatic illustration, in
cross-section, of a carbon-fiber metal composite produced according
to the teachings of the invention.
Although graphite fibers are preferred in the practice of the
instant invention it is intended that the term "carbon fibers"
should include both graphitic and non-graphitic carbon fibers. The
carbon fibers used in the invention may be made from any of a large
number of precursors such as pitch, rayon, polyacrylonitrile or the
like in the form of yarn, tow, webs which are woven, knitted,
felted, and the like. In a preferred form, the fibers are graphite
derived from rayon in uniaxial yarn form, of seven micron average
fiber diameter, containing approximately 11,000 fibers in the yarn.
Such carbon fibers and textiles are well known and available
commerically, and the method of producing same is well known in the
art.
The composite of the invention comprises, as shown in the drawing,
a plurality of graphite fibers 20 each having a substantially
continuous surface coating 21 of a wetting agent which is titanium
boride, titanium carbide or a mixture of both. Typically, the fiber
diameter is about 7 microns and the coating thickness is as thin as
100 A, so that for the sake of clarity the relative thickness of
the coating in the drawing has been exagerated. The fibers are
embedded in a solid metallic matrix 22 which may be aluminum,
magnesium, copper, lead, zinc, tin and various alloys of these
metals such as aluminum/silicon and the like.
In order for infiltration or investment of a bundle of fibers to
occur on immersion in a liquid, the liquid must wet the fiber
surfaces. As previously noted, molten metals such as aluminum and
copper do not readily wet graphite. Consequently, the present
invention provides on the surfaces of the graphite fibers a coating
of a wetting agent. This coating is a substantially uniform layer,
preferably in the range between 100 to 10,000 A in thickness, of
titanium boride, titanium carbide, or a mixture thereof. While
there are many techniques for coating fibers, the preferred method
in the present invention involves a vapor phase deposition whereby
the material of the coatings is deposited as a consequence of the
simultaneous reduction of a mixture of a gaseous compound of
titanium and a gaseous compound of boron. Vapor deposition
techniques to form coatings are well known in the art and usually
are carried out at temperatures between about 900 to 1400.degree.C.
For example, it is known that intermetallic compounds, such as
hafnium boride, can be deposited as a coating from a mixture of
gaseous hafnium chloride and boron trichloride reduced by hydrogen
gas.
In the process of the present invention, the preferred vapor
deposition process involves a comparatively low temperature
reduction of a mixture of titanium tetrachloride and boron
trichloride with zinc metal vapor as the reducing agent. It is
postulated that the use of the zinc metal which serves as a "slow"
reducing agent permits a wide variety of reactions to occur whereby
better control will be obtained over the process.
For example, if the relative weight ratio of boron trichloride to
titanium tetrachloride of the mixture thereof is low (i.e. less
than about one-third the coating on the fiber will constitute a
mixture of titanium carbide and a boride which has an approximate
composition expressed substantially as TiB. At higher weight ratios
the composition of the deposited coat approaches TiB.sub.2.
The foregoing can be explained on the basis of the following series
of postulated reactions that are believed to occur in the gas phase
and at the graphite fiber surfaces during the deposition process.
It is believed that the first two equations express the reduction
processes which are occurring.
1. TiCl.sub.4 + Zn .fwdarw. TiCl.sub.2 + ZnCl.sub.2
2. 2BCl.sub.3 + 3Zn .fwdarw. 2B + 3ZnCl.sub.2
It is believed then that the boron thus produced and the carbon of
the fibers react with the titanium dichloride somewhat as
follows:
3. 2TiCl.sub.2 + XB .fwdarw. TiB.sub.X + TiCl.sub.4
4. 2TiCl.sub.2 + C .fwdarw. TiC + TiCl.sub.4
From equation (3), it appears that if there is enough of the boron
halide to provide a relative excess of boron so that X in equation
(3) is around the value of 2, the form of titanium boride formed
will closely approximate TiB.sub.2.
This latter consideration can be important because to achieve a
satisfactory composite, it is not only desirable that the fiber
coat promote wetting by the matrix metal, but that it also provides
a chemically stable interface between the fiber and the metal of
the matrix. For example, if the metal of the matrix is copper, a
coating which is a mixture of TiC and TiB is satisfactory. On the
other hand, if the metal of the matrix is aluminum or an alloy with
a high percentage of aluminum, it has been found that the coating
composition should be substantially TiB.sub.2.
Fibers with the requisite coat are then drawn through a bath
containing the molten metal matrix and because the fibers are
wetted, infiltration of the interstices between the fibers will
occur. The entire infiltration process can be carried out at
ambient pressure preferably under an inert atmosphere such as argon
or the like. The metal-fiber mass is then allowed to cool below the
solidus temperature of the metal, thereby forming a solid
composite. The composites, which can be originally made in the form
of wires, rods, tapes or sheets, can be pressed together at a
temperature above the melting point of the matrix to give bulk
composites of various shapes such as bars, angle sections and
panels. If desired, during the pressing of such shapes, any excess
metal may be expressed from the composite in order to increase the
volume percentage of the fibers.
The following examples illustrate more clearly the manner in which
carbon fiber composites are produced according to the invention.
The invention however should not be construed as being limited to
the particular embodiments set forth in the examples.
EXAMPLE I
Graphite yarn containing approximately 11,000 individual fibers of
50 .times. 10.sup.6 modulus was exposed to a vapor reaction mixture
formed of 0.38 percent TiCl.sub.4, 0.21% BCl.sub.3, and 0.80% Zn,
the balance being argon (all percentages being by weight). The gas
mixture was maintained at a temperature of 650.degree.C for 30
minutes to provide a coating of about 200.degree.A, believed to be
substantially TiB.sub.2 on the yarn fibers. The coated fibers were
transferred under argon to a molten bath containing 13 percent by
weight of silicon-aluminum alloy and kept immersed in the bath at
650.degree.C for 2 minutes. The resulting metal-fiber composite was
removed from the bath and then allowed to cool below the solidus
temperature of the alloy. A section taken across the long axis of
the fibers through the composite appears substantially as shown in
the drawing.
A number of sections of the composite described in this Example I
were hot pressed in a graphite die under vacuum at 600.degree.C for
5 minutes to form a composite plate 6 inches long by 0.5 inches
wide by 0.05 inches thick.
EXAMPLE II
The graphite yarn similar to that used in Example I was exposed to
a similar gas mixture in which however the composition was as
follows: 0.38 wt.% TiCl.sub.4, 0.14 wt.% BCl.sub.3 and 0.80 wt.%
Zn, the balance being argon. The fibers were exposed to that gas
mixture at 650.degree.C for 30 minutes and transferred under argon
to a molten bath containing a bronze alloy of about 90 wt.% Cu and
10 wt.% Sn at about 980.degree.C for one minute. The composite was
removed from the bath and allowed to cool to form a solid
article.
EXAMPLE III
Coated graphite fibers were prepared as in Example I, and
tansferred under argon to a molten bath containing a lead alloy
(0.4% Ca, 99.6% Pb) held at about 550.degree. C. The fibers were
kept in the bath for 10 minutes, and the composite was then removed
and allowed to cool below the solidus temperature of the alloy. The
resulting composite could be hot pressed to form bearings.
Since certain changes may be made in the above process and product
without departing from the scope of the invention herein involved,
it is intended that all matter contained in the above description
or shown in the accompanying drawing shall be interpreted in an
illustrative and not in a limiting sense.
* * * * *