U.S. patent number 3,929,427 [Application Number 05/357,080] was granted by the patent office on 1975-12-30 for wear-resistant surface composite materials and method for producing same.
This patent grant is currently assigned to Union Carbide Corporation. Invention is credited to Frank P. Gortsema, Henri Hatwell, Peshotan S. Kotval.
United States Patent |
3,929,427 |
Kotval , et al. |
December 30, 1975 |
Wear-resistant surface composite materials and method for producing
same
Abstract
Materials, such as metals, alloys and other products are
provided with improved wear-resistant surfaces comprised of a hard
monocarbide phase in the form of filaments within the material
matrix.
Inventors: |
Kotval; Peshotan S. (Hartsdale,
NY), Hatwell; Henri (White Plains, NY), Gortsema; Frank
P. (Croton, NY) |
Assignee: |
Union Carbide Corporation (New
York, NY)
|
Family
ID: |
26954162 |
Appl.
No.: |
05/357,080 |
Filed: |
May 4, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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270241 |
Jul 10, 1972 |
|
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|
Current U.S.
Class: |
442/148; 428/457;
428/206; 428/401; 428/539.5 |
Current CPC
Class: |
B29C
70/08 (20130101); C22C 49/00 (20130101); Y10T
428/31678 (20150401); Y10T 428/24893 (20150115); Y10T
428/298 (20150115); Y10T 442/273 (20150401) |
Current International
Class: |
C22C
49/00 (20060101); B32B 015/04 () |
Field of
Search: |
;29/195A
;161/88,89,94,95,186,213 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Rutledge; L. Dewayne
Assistant Examiner: Weise; E. L.
Attorney, Agent or Firm: Moran; William R.
Parent Case Text
This application is a continuation-in-part of U.S. application Ser.
No. 270,241 entitled "Improved Wear-Resistant Surface Composite
Materials and Method for Producing Same" filed July 10, 1972, by P.
S. Kotval, H. Hatwell and F. P. Gortsema, now abandoned.
Claims
We claim:
1. An improved wear-resistant surface composite material, the
surface of which has a duplex composite structure comprised of (a)
a matrix material of poor wear-resistance and (b) not less than
about 50 percent area fraction and up to about 90 percent area
fraction of a hard fibrous monocarbide phase, said monocarbide
phase being represented by the general formula MC wherein M is a
metal selected from the group consisting of tantalum, titanium or
tungsten and C is carbon, said monocarbide phase being in the form
of filaments between 2 and about 15 microns in diameter and being
present at the composite surface as sections of varying
orientations, the remainder of the surface being comprised of the
matrix of the said material.
2. The composite of claim 1 wherein said matrix material is
aluminum.
3. The composite material of claim 1 wherein said matrix material
is an aluminum alloy.
4. The composite material of claim 1 wherein said matrix material
is a casting grade aluminum-silicon hypereutectic alloy
composition.
5. The composite material of claim 1 wherein M of said general
formula is tantalum.
6. The composite material of claim 1 wherein M of said general
formula is titanium.
7. The composite material of claim 1 wherein M of said general
formula is tungsten.
8. The composite material of claim 1 wherein said filaments are
present as a woven fabric.
9. The composite material of claim 1 wherein said filaments are
present as a felt.
10. The composite material of claim 1 wherein said filaments are
present as chopped fibers.
11. The composite material of claim 9 wherein said woven fabric is
present as a tape.
Description
This invention relates to improved wear resistant surface composite
materials and to a method for their production. In one aspect the
invention relates to metals, particularly aluminum alloys with an
especially wear-resistant "duplex" surface comprising a large area
fraction of hard refractory metal monocarbide phases. In a further
aspect, the invention relates to the use of refractory metal
monocarbide phases in the form of fibers, felts, tapes and woven
fabrics and a method for compositing these materials in the surface
of otherwise wear-prone materials such as aluminum alloys, to
impart exceptionally high wear-resistance to the composite
surface.
As is well known, many materials such as metals, alloys and other
products exhibit poor wear properties and as a consequence, the use
of such materials is severely restricted in applications where
wear-resistance is an important requirement. In the prior art,
attempts at improving the poor wear-resistance of materials, such
as aluminum and its alloys, have been focused on two principal
methods: (a) the use of anodizing treatments which permit the
formation of a hrad oxide film on the surface of aluminum, and (b)
the use of surface coating treatments, such as plasma-spraying,
flame-plating and similar methods which involve the deposition of a
wear-resistance phase or phases on the surface of aluminum alloys.
These state-of-the-art methods go some way toward fulfilling the
requirements of improved wear-resistance for aluminum alloys.
However, both methods suffer from limitations. The films created by
anodizing treatments are mechanically weak and the enchancement of
wear-resistance is not maintained once rupture of the film occurs.
Further, there is a physical limitation of the thickness of the
films which can be created on aluminum alloys. The methods
involving the deposition of various hard phases to improve wear
behaviour suffer from the disadvantage that they are not readily
adaptable to cases where mechanical precision is necessary in the
finished part and also have the disadvantage of a propensity (under
certain conditions) toward separation of the wear-resistant coating
from the substrate.
In marked contrast to both types of the above-mentioned prior art
methods of improving wear resistance, the present invention teaches
that the entire surface of the alloy need not be covered by the
wear-improving phases. Instead, the utilization of the hard
refractory mono-carbide phases, for example in the form of a woven
tape permits the final surface to have a composite surface
structure wherein up to 80 percent of the surface area is comprised
of regions of the hard mononcarbide phase embedded within the
matrix of the alloy. the fibrous nature of the wear-improving phase
permits a continuous presence of the hard phase even in conditions
of abrasive wear. Thus, the present invention represents a marked
improvement over the prior art methods (e.g., plasma-sprayed
powders) where a particle of hard phase, once removed during
abrasive wear, ceases to provide any wear-improving role.
Accordingly, one or more of the following objects will be achieved
by the practice of this invention. It is an object of this
invention to provide improved wear resistant surface composite
materials and to a method for their production. A further object of
the invention is to provide materials with a duplex composite
surface which exhibit exceptionally improved wear resistance in
comparison to the untreated material surface. Another object of the
invention is to employ refractory metal carbides in the form of
filaments to provide a duplex composite surface having improved
wear-resistance. A still further object of this invention is to
provide aluminum alloys with improved wear-resistance surfaces.
Another object is to provide non-metallic materials such as epoxy
and phenolic resins which have improved wear-resistant surfaces.
These and other objects will readily become apparent to those
skilled in the art in the light of the teachings herein
disclosed.
In its broad aspect this invention relates to improved
wear-resistant composite materials and to a process for their
preparation. The composites are characterized by a surface which
has a duplex composite structure comprised of (a) a matrix material
of poor wear resistance and (b) not less than about 50 percent area
fraction and up to about 90 percent area fraction of a hard fibrous
monocarbide phase. The monocarbide phase is represented by the
general formula MC wherein M is a metal from the group tantalum,
titanium or tungsten and C is carbon and is in the form of
filaments of between about 2 and about 15 microns in diameter being
present at the composite surface as sections of varying
orientations, the remainder of the surface being comprised of
matrix material.
By the term "filaments" as employed throughout the specification
and appended claims is meant woven fabrics, tapes, felts, chopped
fibers, and the like composed of the metallic monocarbides. These
metallic monocarbides are prepared by the process disclosed in U.S.
Pat. No. 3,403,008.
It has been observed that a wide variety of materials which are
normally characterized by poor wear-resistance, can have their
wear-resistance markedly improved by the teachings of the instant
invention. Illustrative materials include, among others, aluminum,
silver, copper, and their alloys, non-metallic matrices, such as
epoxy and phenolic resins, and the like. For example, aluminum
alloys which normally exhibit poor wear-resistant properties
include those based on the aluminum-silicon alloy system
particularly hyper-eutectic combinations which are commonly used as
casting grade aluminum alloys. Also included are silver and silver
containing alloys such as those used for brazing applications,
copper and its alloys as well as other matrices. As previously
indicated the invention is also applicable to other non-metallic
matrices such as epoxy resins and phenolic resins.
The ability to produce the materials of this invention with
exceptionally enhanced wear-resistance results from the discovery
that when filaments of the monocarbides of the aforementioned
refractory metals are in contact with materials such as aluminum
and its alloys in the molten state, the filaments are rapidly
"wetted" by the molten metal. A feature of this wetting reaction is
the formation of intermetallic phases at the interfaces between the
individual fibers and filaments of the monocarbide phase and the
adjacent metallic matrix, the intermetallic phase providing a good
cohesive bond between the matric and the monocarbide filaments.
In those cases where the natural characteristics of the matrix
allow only limited wetting of the monocarbide phase, it may be
necessary to first create a thin metallic coating such as copper,
aluminum or nickel by electrodeposition or vapor deposition on the
surface of the filaments and thereafter to proceed with the process
of this invention with the matrix of choice.
In practice, the material of this invention can be conveniently
prepared by a variety of methods. For example, the ready
wettability of the textile form of the refractory metal
monocarbides by materials such as aluminum and its alloys lends
itself to a method of embedding the wear-resistance-imparting
monocarbide into the material directly during the casting
operation. For example, the mold can be lined with the monocarbide
filaments and the normal casting operation carried out. As
previously indicated the filaments can be employed in a variety of
forms. The particular configuration of the mold may, in part,
determine the preferred form of the filaments.
In many instances, it has been observed that filaments in the form
of tapes are convenient for lining the interior surfaces of the
mold. The thickness of the tape is not necessarily critical as long
as sufficient metallic monocarbide filaments are present to improve
the surface wear-resistant properties. In practice it has been
observed that marked improvements are obtained when the surface
composite structure is comprised of not less than about 50 percent
area fraction and up to about 90 percent area fraction of the hard
fibrous monocarbide phase.
As previously indicated the present invention can provide
mechanically precise castings which have improved wear-resistance.
Inasmuch as the metallic monocarbides are placed in the mold prior
to the matrix material, the overall configuration of the cast
article has the same dimensions as the cast article without the
monocarbides.
The filaments employed in this invention are also useful for
imparting improved wear-resistance to articles prepared by hot
pressing powdered matrix materials. For example a tape, felt, woven
fabric, or chopped fibers of the metallic monocarbide can be placed
on one or more surfaces of a die, powdered matrix material added,
and the composite hot pressed to form the desired article.
The present invention thus provides a simple and convenient
technique for imparting improved wear-resistance to surfaces of a
variety of materials. Without any complicated processing steps,
other than those involved in normal material fabrication, a
wear-resistant composite duplex surface for the material can be
directly created.
The following examples are illustrative:
EXAMPLE I
A tape of satin-weave woven fabric comprised of tantalum carbide
prepared by the process disclosed in U.S. Pat. No. 3,403,008 was
used to create a composite surface on 6061 aluminum alloy. The
filaments comprising the tape were 5.mu. in diameter.
The apparent molecular weight of the tantalum carbide was 191.4,
showing that the material of the woven fabric approximated closely
ideal stoichiometric TaC (molecular weight 192.96). A tape, 0.5
inches wide by 3.0 inches long, was placed in an alumina crucible
and a bar of 6061 aluminum alloy was placed over the tape. The
crucible and contents were held in an argon atmosphere furnace at
700.degree.C for 5 minutes. Upon cooling, the as-cast 6061 alloy
was found to have the said tape embedded fully within the lower
surface of the ingot resulting in a composite surface. Using part
of the above sample and utilizing the technique of thin foil
transmission electron microscopy, electron diffraction patterns
were obtained from the region of the interface between the TaC
filaments and the 6061 alloy matrix. The patterns revealed that in
addition to the face-centered-cubic 6061 matrix and the
face-centerd-cubic 6061 matrix and the face-centered-cubic TaC
fibers, there was a tetragonal Al.sub.3 Ta intermetallic phase
formed at the fiber/matrix interface, thus providing evidence of
good bond formation.
Blocks 1/4 inch wide .times. 5/8 inch long .times. 3/8 inch deep
were cut from the sample of 6061 alloy with the composite matrix
plus TaC fiber surface. The composite surface was tested for
wear-resistance under varying loads in a standard "Alpha" model
wear-testing machine. In this test the test surface is subject to
wear against a 4620 steel ring hardened to a hardness of R.sub.c =
58 to 63. The relative wear parameter of test material is given by
measuring the volume of the scar created on the surface by wear
test. The results obtained are set forth in Table I below:
Table I
__________________________________________________________________________
Material Lubricant Load Wear Scar Volume
__________________________________________________________________________
Cast 6061 5606 A hydraulic fluid 30 lbs. 6.5 .times. 10.sup..sup.-6
cm.sup.3 alloy with 75 area % Tac fibers 5606 A hydraulic fluid 180
lbs. 2372 .times. 10.sup..sup.-6 cm.sup.3 Untreated 5606 A
hydraulic fluid 30 lbs. 5998 .times. 10.sup..sup.-6 cm.sup.3
aluminum alloy surface 5606 A hydraulic fluid 180 lbs. too high to
measure
__________________________________________________________________________
The wear scar volumes of the composite surface of the present
invention are compared in Table I with the values for wear scar
volumes for a typical aluminum alloy. It is evident that the
composite surface of the present invention has wear characteristics
which represent a thousand-fold improvement over the wear
characteristics of conventional aluminum alloy surfaces.
EXAMPLE II
A tape of satin weave woven fabric comprising essentially of
tantalum carbide was positioned into the bottom of a mold into
which a Buehler No. 20-8133-001 Epoxy Resin was cast. Upon curing
the resultant Epoxy block was found to have one surface with a
duplex composite microstructure comprising .about. 75 area% TaC in
Epoxy matrix. Blocks 1/4 inch wide, 5/8 inch long and 4/8 inch deep
were cut from these Expoxy blocks with "matrix plus TaC fiber"
surface. The composite surface was tested for wear-resistance under
varying loads in a standard Dow-Corning Alpha model Wear-testing
Machine. In this test the test surface is subjected to wear against
a 4620 steel ring hardened to a R.sub.c = 58 to 63. The relative
wear parameters for the composite surface of an Epoxy Matrix, with
varying area fractions of the fibrous TaC phase is compared with
parameter for the bare Epoxy block in Table II.
______________________________________ Material Lubricant Load Wear
Scar Volume ______________________________________ Epoxy with Press
Fluid 30 lbs. 105 .times. 10.sup..sup.-6 cm.sup.3 75 area%. TaC
tape Epoxy with Press Fluid 30 lbs. 162 .times. 10.sup..sup.-6
cm.sup.3 60 area%. TaC tape Epoxy Press Fluid 30 lbs. 1798 .times.
10.sup..sup.-6 cm.sup.3 (untreated)
______________________________________
EXAMPLE III
Comparisons were made between the wear resistance of the surface
composite materials of this invention and known materials using
standard wear tests.
The wear data was obtained using a LFW-1 model Wear-Testing Machine
manufactured by the Dow Corning Corporation. As described in ASTM
Standard Test Method D 2714-68, all tests were carried out on
stationary rectangular (1/4 inch wide .times. 5/8 inch long .times.
3/8 inch deep) test blocks pressed, with a pre-determined load,
against a rotating ring. The wear properties measured were: (i)
Volume of Wear Scar on the test surface of wear block material;
(ii) Weight change of the mating ring; and (iii) the friction force
measured at intervals during the test. The wear data listed in
Table III were obtained under the following conditions of testing:
Mating Ring: 4620 Steel; R.sub.c =58-62; Surface finish=8-12 micro
inches Lubricant: Mobil 5606-A fluid Load: 30 lbs. Wear Speed: 180
r.p.m. (Ring diameter = 1.3775 in.) Total revs: 5400 revs.
As is evident from Table III, a Surface Composite comprising 75
area percent of TaC phase within a 6061 alloy matrix represents an
improvement of up to a thousand-fold in the measured values of wear
scar volume compared to the bare 6061 alloy. Compared to the
wear-resistance of even the hypereutectic Al-18 weight percent Si
alloy, the wear properties of Surface Composite materials represent
an increase of between 10- and 30-fold.
In the measurement of wear behavior it is necessary to take into
account the total "system" wear; i.e., the wear measured on the
test block as well as the wear measured on the "mating" rotating
member. Bearing this in mind, it is significant to compare
state-of-the-art wear-resistant materials with the Surface
Composite materials of this invention. In Table III are included
two such state-of-the-art "bulk" composite materials produced via
conventional powder metallurgy techniques: "Ferro-TiC" developed by
Chromalloy Corporation and the Al + graphite composite developed by
Toyo Kogyo Co. as a wear-resistant rotor apex seal for the "Mazda"
automobile's rotary-piston engine. The Ferro-TiC material provides
good wear-resistance but is very abrasive vis-a-vis the wear of the
mating ring. Ring weight loss values for tests with Ferro-TiC are a
factor of two higher than the comparable values for tests with
Surface Composite materials in 6061 and 2024 alloy matrices. The Al
+ graphite composite material shows higher values for both Ring
Weight Loss and Wear Scar Volume when compared to the Surface
Composite Materials thus clearly indicating the superior wear
behavior of the materials of this invention.
It should be noted that in addition to the wear properties of the
Surface Composite materials being superior to the state-of-the-art
materials, the fabrication of Surface Composite materials does not
require any major modification of either the technology or the
economics of conventional practice for casting aluminum alloys.
In contrast, the state-of-the-art wear-resistant composites
mentioned hereinbefore, are fabricated by relatively more expensive
processing involving sintering, hot pressing and the like.
Table III
__________________________________________________________________________
Material Tested Wear Scar Ring Weight Coefficient Volume Loss of
Friction
__________________________________________________________________________
(X10.sup.-.sup.6 cm.sup.3) (mg) (at 5400 revs.) 1. Surface
Composite 6 to 40 .16 - .7 .12 - .15 (75 area percent TaC satin
Weave Textile in 6061 aluminum alloy matrix). 2. Surface Composite
32 .15 .11 (75 area percent TiC bias woven tape in 6061 aluminum
alloy matrix). 3. Surface Composite 8 to 30 .12 - .25 .12 - .15 (75
percent TaC Satin Weave Textile in a 2024 alloy matrix). 4. Surface
Composite (75 4 .9 .12 area percent TaC Satin Weave textile in a
Co- Cr-Ni alloy matrix). 5. Surface Composite 9.5 .81 .11 - .12 (75
area percent TaC Satin Weave textile in Al-18w/o Si alloy matrix).
6. 6061 aluminum alloy 5998 weight gain .066 7. Al-18w/o Si alloy
380 .46 .12 8. Al + graphite 124- 131 .65-1.01 .133 composite (Toyo
Kogyo) 9. Ferro TiC (Chromalloy) 2-7 1.28 .133
__________________________________________________________________________
Although the invention has been illustrated by the preceding
examples it is not to be construed as being limited to the
materials employed therein, but rather the invention encompasses
the generic area as hereinbefore disclosed. Various modifications
and embodiments of this invention can be made without departing
from the spirit and scope thereof.
* * * * *