U.S. patent number 3,622,283 [Application Number 04/639,153] was granted by the patent office on 1971-11-23 for tin-carbon fiber composites.
This patent grant is currently assigned to Union Carbide Corporation. Invention is credited to Raymond V. Sara.
United States Patent |
3,622,283 |
Sara |
November 23, 1971 |
**Please see images for:
( Certificate of Correction ) ** |
TIN-CARBON FIBER COMPOSITES
Abstract
Low-density, high-strength tin base composites are provided by
coating carbon fibers with a metallic coupling agent and then
bonding them together, preferably in a parallel or aligned manner,
by means of a tin or tin base alloy matrix. Such composites are
characterized by physical properties which are much superior to
those evidenced by the matrix material alone and find utility in
applications where the chemical properties of tin are desired but
its use is prohibited or limited due to its poor physical
properties.
Inventors: |
Sara; Raymond V. (North
Olmsted, OH) |
Assignee: |
Union Carbide Corporation
(N/A)
|
Family
ID: |
24562947 |
Appl.
No.: |
04/639,153 |
Filed: |
May 17, 1967 |
Current U.S.
Class: |
428/608; 428/367;
428/401; 428/634; 428/648; 428/656; 428/381; 428/614; 428/646;
428/926 |
Current CPC
Class: |
C22C
49/14 (20130101); B64C 1/12 (20130101); Y10T
428/12778 (20150115); Y10T 428/12708 (20150115); Y10T
428/12625 (20150115); Y10T 428/298 (20150115); Y02T
50/43 (20130101); Y10S 428/926 (20130101); Y10T
428/2944 (20150115); B64C 2001/0072 (20130101); B64C
2001/0081 (20130101); Y10T 428/12486 (20150115); Y02T
50/40 (20130101); Y10T 428/12444 (20150115); Y10T
428/12722 (20150115); Y10T 428/2918 (20150115) |
Current International
Class: |
C22C
49/00 (20060101); B64C 1/00 (20060101); C22C
49/14 (20060101); B32b 015/02 (); B32b 015/04 ();
B32b 015/14 () |
Field of
Search: |
;29/191.4,180,183.5,191,191.2,192,195 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Curtis; Allen B.
Assistant Examiner: Crutchfield; O. F.
Claims
What is claimed is:
1. A corrosion resistant composite article comprising a plurality
of carbon fibers bonded together by a tin base metal matrix, said
carbon fibers having a substantially continuous coating of a
coupling metal having a higher melting point than said tin base
metal matrix on their outer surface.
2. The corrosion resistant article of claim 1 wherein said tin base
metal matrix is essentially tin.
3. The corrosion resistant composite article of claim 1 wherein
said fibers are graphite.
4. The corrosion resistant composite article of claim 1 wherein
said carbon fibers are in yarn form.
5. The corrosion resistant composite article of claim 1 wherein
said carbon fibers are arranged in a side-by-side, parallel
relationship.
6. The corrosion resistant composite article of claim 1 wherein
said coupling metal is selected from the group consisting of
nickel, titanium and chromium.
7. The corrosion resistant composite article of claim 1 wherein
said coupling metal is nickel.
8. The corrosion resistant composite article of claim 7 wherein
said coupling metal is from 1 to 3 microns thick.
9. The corrosion resistant composite article of claim 3 wherein
said graphite fibers are in yarn form.
10. The corrosion resistant composite article of claim 3 wherein
said graphite fibers are arranged in a side-by-side, parallel
relationship.
11. The corrosion resistant composite article of claim 3 wherein
said coupling metal is selected from the group consisting of
nickel, titanium and chromium.
12. The corrosion resistant composite article of claim 3 wherein
said coupling metal is nickel.
13. The corrosion resistant composite article of claim 12 wherein
said coupling metal is from 1 to 3 microns thick.
14. The corrosion resistant composite article of claim 2 wherein
said fibers are graphite.
15. The corrosion resistant composite article of claim 14 wherein
said coupling metal is nickel.
16. The corrosion resistant composite article of claim 15 wherein
the thickness of said nickel coupling metal is from 1 to 3 microns.
Description
BACKGROUND OF INVENTION
1. Field of the Invention
The present invention relates to carbon fiber-tin composites made
up of a plurality of carbon fibers coated with a metallic coupling
agent and bonded together, preferably in a side-by-side or parallel
manner, by means of a tin base metal matrix.
2. Description of Prior Art
Tin is an element which finds wide useage in industry. One of its
most important uses is as a protective coating for stronger
materials or substrates. The use of pure tin alone as a material of
construction is limited by its inherently poor physical properties,
such as low tensile strength and modulus of elasticity. It is
presently common practice in industry to increase the tensile
strength of tin by alloying it with copper and/or antimony.
However, the resultant alloy is still quite weak.
It has been proposed to increase the tensile strength of tin by
reinforcing it with an inert fibrous material. One of the most
promising materials available today for this purpose is carbon
textiles. However, it has been discovered that strong, nonporous
carbon fiber-tin composites cannot be simply formed by bonding
carbon fibers together by means of a tin matrix. This is believed
to be due to the fact that carbon fibers are not adequately wetted
by molten tin and that when the so-coated fibers are cooled the tin
thereon, at least in part, dewets or separates from the carbon
fibers and, accordingly causes voids or weak spots to be present in
the resultant composite article.
It was discovered that this problem can be overcome by first
coating the carbon fibers with a thin but continuous metallic film
or coupling agent which has a melting point greater than tin and is
also readily wetted by tin. Carbon fiber-tin composites so-produced
not only are essentially nonporous, but they also increase the
tensile strength properties of tin to a much greater extent than
the most effective alloy additions.
SUMMARY
Broadly stated, the carbon fiber-tin composite of the invention
comprises a plurality of carbon fibers each of which is coated with
a thin layer of a coupling metal having a melting point greater
than tin which are bonded together, preferably in a side-by-side or
parallel manner, with a tin base binder or metal matrix. Generally,
this composite article may be provided by a process which comprises
coating carbon fibers with a thin but continuous film of a suitable
metal, shaping an aggregate of the so-coated fibers into the
desired form, infiltrating the voids between the individual fibers
with molten tin or tin base alloy and cooling the resultant tin
infiltrated aggregate to produce a composite article.
A graphite fiber-tin composite, containing approximately 33.5
volume percent fibers, is characterized by a density 20 percent
less than tin, a modulus of elasticity twice as great as tin, and a
tensile strength approximately 24 times greater than tin. This
composite can be formed into any desired shaped by known techniques
which will readily suggest themselves to those skilled in the art.
Its properties readily suggest its use as a material of
construction in apparatus which require strong, corrosion resistant
parts or components.
DESCRIPTION OF THE DRAWING
The sole FIGURE shown in the drawing presented herewith is a
diagrammatical illustration of a rectangular section of a carbon
fiber-metal matrix composite article produced according to the
teachings of the instant invention.
Referring now in detail to the drawing, there is shown in cross
section a rectangular composite article 1 consisting of aligned
graphite fibers 2 having disposed on their surface a continuous
2-micron thick coating of nickel 3. These so-coated fibers are
bonded together by a tin matrix 4. The graphite fibers 2 are
approximately 1 inch in length and disposed in the tin matrix 4 in
a parallel or side-by-side manner. The length dimension of the
fibers 2 is perpendicular to the surface of the drawing.
Description of the Preferred Embodiment of the Invention
Carbon textiles in any form can be employed in the practice of the
instant invention. However, it is preferred to employ carbon fibers
in yarn or monofilament form. Carbon textiles are available
commercially and are generally produced by the techniques described
in U.S. Pat. Nos. 3,107,152 and 3,116,975, among others.
The coupling metal used can be any metal which has a melting point
greater than the metal matrix which adheres to the carbon and is
readily wetted by the matrix metal without forming low melting
point alloys or brittle intermetallic phases. Metals which are
preferred as coupling agents are nickel, titanium and chromium. The
selected coupling metal can be deposited on the carbon fibers by a
variety of methods. The techniques available for accomplishing this
include electrodeposition from a suitable plating bath, thermal
decomposition of the appropriate metal halide or sputtering. The
exact deposition technique to be employed is dictated by a number
of factors. Sputtering can be used on relatively complex shapes and
results in a tenacious bond between the coupling metal and the
carbon fiber substrate. Such a bond is a highly desirable feature
in carbon fiber-metal matrix composites. Thermal decomposition of
the appropriate halide requires a heating of the carbon fiber
substrate and, accordingly, somewhat limits the type of shapes
which can be coated in this manner. Electrodeposition of a metal
from a plating solution is an ideal way of coating carbon fibers
with a thin metallic film and is the preferred coating
technique.
While the preferred binder or matrix metal is tin, it will be
readily appreciated by those skilled in the art that tin base
alloys of low melting point metals such as lead, antimony, and
bismuth may also be employed in the practice of the instant
invention.
The following example illustrates in detail the practice of the
instant invention.
A single ply of graphite yarn having an average filament diameter
of 6.9 microns and consisting of 720 monofilaments per ply was cut
into a plurality of 4-inch lengths. These 4 inch sections of
graphite yarn were then predipped into acetone to facilitate their
subsequent coating with nickel. Nickel was plated on the so-treated
graphite yarn by using a nickel anode and an electroplating plating
solution prepared by dissolving 200 grams of NiSO.sub.4 .sup..
6H.sub.2 O and 22 grams of H.sub.3 BO.sub.3 in 500 ml. of distilled
water. The plating solution temperature was maintained at
approximately 52.degree. C. The plating current varied between
about 400 to about 1000 milliamperes. A metallographic examination
of the resultant fibers showed that all monofilaments had a coating
of nickel thereon and that the average coating thickness ranged
from 1 to 3 microns. These nickel clad fibers were then cut in
approximately 1-inch lengths and placed in an aligned position (all
parallel) in a cylindrical capillary tube measuring approximately 1
inch in length and having an internal diameter of about 0.135
inches which was provided with a top and bottom closure. The
surface of the cylinder was provided with 12 randomly placed holes
or openings to facilitate the ingress of tin into the cylinder and
hence into the voids between the aligned graphite fibers. The
cylinder containing the fibers was placed into an airtight chamber
which also contained a vessel of tin. The chamber was then
evacuated to a pressure of approximately 2.times.10.sup.-6 mm. of
mercury to out gas the graphite fibers. The chamber with the tin
therein was heated to a temperature of approximately 300.degree. C.
The cylinder containing the aligned fibers was then submerged below
the surface of the molten tin. The chamber was subsequently filled
with argon gas to a pressure of about 1atmosphere to insure that
molten tin filled essentially all the voids between the aligned
graphite fibers. After about 30 seconds of pressurizing the
specimen, the capsule was withdrawn from the molten tin, cooled,
and removed from the chamber.
A metallographic examination of the resultant nickel coated
graphite fiber-tin composite showed that the nickel coating was
well bonded to the graphite fiber substrate; that the tin matrix
material had uniformly and completely wetted the so-coated fibers
without disturbing the continuity of the nickel coating; and that
no undesireable reaction zone was formed at the nickel-tin
interface.
The physical properties of a nickel clad graphite fiber-tin
composite are listed below. For comparison, similar property data
is also listed for pure tin.
Physical Properties of Tin and A Nickel Clad Graphite Fiber-Tin
Composite
---------------------------------------------------------------------------
Containing 33.5.sup.v /o Fibers
Modulus of Material Density Elasticity Tensile Strength
__________________________________________________________________________
g./cm..sup.3 .times.10.sup.6 1b./in..sup.2 lb./in..sup.2 Tin 7.05
7.8 2000 Ni clad 5.56 16.2 47,400 graphite fiber- tin composite
__________________________________________________________________________
From the foregoing data, it is observed that a composite of the
invention, containing approximately 33.5 volume percent graphite
fibers, is characterized by a density 20 percent less than tin, a
modulus of elasticity twice as great as tin, and a tensile strength
approximately 24 times greater than tin metal.
A composite so-produced, in addition to its utility as a chemical
corrosion resistant material of construction, is extremely useful
as a low density material of construction for subsonic and
supersonic aircraft, space system components, and various nuclear
devices.
While the foregoing example concerns a composite where the fibers
are positioned in a side-by-side relationship, it is readily
apparent to those skilled in the art that the graphite fibers may
be randomly orientated in the tin matrix if more isotropic physical
properties are desired without losing the benefits of the instant
invention. In addition, it is obvious that the thickness of the
metal coupling agent can be varied as desired. For example, a
thickness of only 0.1 microns has been found to be effective.
Likewise, it will be appreciated by those versed in the art that
although graphite fibers and fabrics are preferred in the practice
of the instant invention, nongraphitic carbon fibers and fabrics
may also be employed. Also, other methods of infiltrating the metal
clad carbon fibers with tin and tin base alloys will readily
suggest themselves to the skilled artisan.
As used herein and in the appended claims the term carbon is meant
to include both the nongraphitic and graphitic forms of carbon.
The foregoing example is presented for illustrative purposes only
and is not intended to unduly limit the reasonable scope of the
instant invention. The limitations of the invention are defined by
the following claims.
* * * * *