U.S. patent number 3,655,365 [Application Number 05/033,990] was granted by the patent office on 1972-04-11 for high speed tool alloys and process.
This patent grant is currently assigned to IIT Research Institute. Invention is credited to Frederick C. Holtz, Jr..
United States Patent |
3,655,365 |
Holtz, Jr. |
April 11, 1972 |
HIGH SPEED TOOL ALLOYS AND PROCESS
Abstract
Compositions suitable for tool use and containing from about 10
to about 40% of a material selected from the group consisting of
tungsten and molybdenum and mixtures thereof; from about 0.5 to
about 4% carbon; at least one reactive metal selected from the
group consisting of chromium, vanadium, niobium, tantalum, silicon
and manganese; the balance a mixture of iron and cobalt. The alloy
is formed by the hot consolidation of pre-alloyed powders and
results in an alloy having a uniformly dispersed carbide phase of a
grain size less than 3 microns.
Inventors: |
Holtz, Jr.; Frederick C.
(Evanston, IL) |
Assignee: |
IIT Research Institute
(Chicago, IL)
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Family
ID: |
21873645 |
Appl.
No.: |
05/033,990 |
Filed: |
May 1, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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518181 |
Jan 3, 1966 |
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435733 |
Feb 26, 1965 |
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Current U.S.
Class: |
75/245; 76/101.1;
148/410; 419/15; 420/453; 30/350; 148/404; 148/513; 419/23 |
Current CPC
Class: |
C22C
27/04 (20130101); C22C 29/06 (20130101); C22C
38/12 (20130101); C22C 19/07 (20130101); C22C
32/0052 (20130101) |
Current International
Class: |
C22C
29/06 (20060101); C22C 32/00 (20060101); C22C
27/04 (20060101); C22C 38/12 (20060101); C22C
27/00 (20060101); C22C 19/07 (20060101); C22c
039/08 (); C22c 039/50 (); C21d 007/14 () |
Field of
Search: |
;75/.5BB,.5BC,123,203,226,170,126 ;148/126,11.5F,11.5R,12.1 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Bizot; Hyland
Assistant Examiner: Stallard; W. W.
Parent Case Text
This patent application is a continuation-in-part of application
Ser. No. 518,181 filed Jan. 3, 1966, and now abandoned which
application in turn is a continuation-in-part of application Ser.
No. 435,733 filed Feb. 26, 1965, both previous applications having
the same inventor and being assigned to the assignee of the present
invention.
Claims
We claim:
1. An alloy formed by the consolidation of pre-alloyed powders to a
fully dense condition and adapted for high speed cutting
operations, said pre-alloyed powder having a composition by weight
consisting essentially of from about 10 to about 40% of a material
selected from the group consisting of tungsten and molybdenum and
mixtures thereof; from about 0.5 to about 4% carbon; at least one
reactive metal selected from the group consisting of from 0 to
about 25% chromium, from 0 to about 10% vanadium, from 0 to about
5% niobium, from 0 to about 10% tantalum, from 0 to about 5%
silicon and from 0 to about 5% manganese; the balance of the alloy
being a mixture of iron and cobalt wherein cobalt constitutes from
about 25 to about 50% and iron constitutes about 20 to about 48% of
the total composition, said alloy being characterized by a
substantially uniformly dispersed carbide phase in a fine-grained
major phase matrix, and by substantially all of said carbide phase
having a grain size less than 3 microns, said alloy further being
characterized by a hardness in excess of 60 Rockwell C.
2. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 25% chromium.
3. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 10 % vanadium.
4. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 5% niobium.
5. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 10% tantalum.
6. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 5% silicon.
7. A composition as set forth in claim 1 wherein said reactive
metal consists of from about 1 to about 5% manganese.
8. An alloy composition as set forth in claim 1 wherein the
composition by weight consists essentially of from about 15 to
about 25% chromium; from about 7 to about 12% tungsten; from about
4 to about 8% molybdenum; from about 2 to about 4% carbon; the
balance being a mixture of cobalt and iron wherein cobalt
constitutes from about 25 to about 30% of the total
composition.
9. An alloy as set forth in claim 1 wherein the composition
consists essentially of about 20% chromium, about 9% tungsten,
about 3% carbon, about 6% molybdenum, about 27% cobalt and about
35% iron with incidental impurities.
10. An alloy as set forth in claim 1 wherein the composition
consists essentially of about 10% tungsten, about 10% chromium,
about 1.8% carbon, about 40% cobalt, balance iron.
11. An alloy as set forth in claim 1 wherein the composition
consists essentially of about 14% tungsten, about 5% vanadium,
about 1.3% carbon, about 40% cobalt, balance iron.
12. The method of making a solid alloy composition characterized by
a substantially uniformly dispersed carbide phase in the major
phase matrix, said carbide phase having a grain size predominantly
of less than 3 microns which comprises the steps of: atomizing an
alloy charge comprising from 25 to 30% cobalt, from 15 to 25%
chromium, from 7 to 12% tungsten, from 4 to 8% molybdenum, from 2
to 4% carbon, balance iron with incidental impurities, rapidly
quenching said atomized material and consolidating said material
into solid metal stock without the formation of deleterious
oxides.
13. The method of making a fully dense alloy composition suitable
for tool use and having a Rockwell C hardness of at least 60 and a
substantially uniformly dispersed carbide phase in the major phase
matrix, said carbide phase having a grain size predominantly of
less than 3 microns which comprises the steps of atomizing an alloy
charge comprising from about 10 to about 40% of a material selected
from the group consisting of tungsten and molybdenum and mixtures
thereof; from about 0.5 to about 4% carbon; a reactive metal
selected from the group consisting of chromium, vanadium, niobium,
tantalum, silicon and manganese, said reactive metals being in
amounts as follows, chromium from 0 to about 25%, vanadium from 0
to about 10%, niobium from 0 to about 5%, tantalum from 0 to about
10%, silicon from 0 to about 5% and manganese from 0 to about 5%;
the balance of the alloy being a mixture of iron and cobalt wherein
cobalt constitutes from about 25 to about 50% and iron constitutes
about 20 to about 48% of the total composition, rapidly quenching
said atomized material to form a pre-alloyed powder, and hot
consolidating said pre-alloyed powder into fully dense stock
suitable for tool use.
Description
The present invention relates to iron-cobalt base alloys and to the
process of their fabrication into cutting tools. More specifically,
the present invention is directed to iron-cobalt base alloys formed
from pre-alloyed powders which include minor additions of reactive
metals, defined hereinafter, which provide improved cutting
performance in high speed, steady state cutting operations.
Co-pending application Ser. Nos. 743,921, now abandoned, and
743,922, filed July 11, 1968, and assigned to the assignee of the
present invention, disclose alloy tool steels which are free of
reactive metals such as chromium, vanadium, niobium, tantalum,
silicon, manganese, titanium and aluminum. As discussed in these
previous applications, the presence of these reactive metals tends
to impair some of the qualities of the disclosed alloys for cutting
purposes as they readily react with oxygen in the ambient air to
form oxide films on the pre-alloyed powders. The presence of this
oxide film may result in impaired fabricability and reduced
strength of the alloy when consolidated from a powder for tool use.
Consequently, the presence of reactive metals results in higher
cost due to special atomizing methods for the powder production or
of special oxide reduction treatments of the finished alloy.
It has subsequently been learned that, while the so-called oxide
free or reactive metal free tool steel alloys exhibit very good
tool life properties when tools formed therefrom are utilized in
discontinuous, e.g., milling, cutting operations or low speed
operations such as must be employed in the cutting or boring of
difficult to machine alloys, tools formed from oxide free alloys
exhibit less satisfactory tool life when employed in high speed,
continuous cutting of relatively soft steels, e.g., lathe turning
or boring. It is believed that the lesser tool life that has been
found to occur when tools formed from oxide free alloys are used in
continuous cutting of soft steel is caused in part by a welding of
the workpiece to the cutting point of the tool which causes tearing
away of the tool material. The net result is a tool life not much
better than conventional tool steels when employed in the
continuous cutting of relatively soft steel. It is believed that
the tendency of the workpiece material and the tip of the oxide
free tool to weld together is primarily due to the inability to
apply lubricants in sufficient quantities at the tip of the tool in
high speed continuous cutting operations because of the speed of
the operation and the inaccessability of the tool tip. The present
invention avoids this shortcoming of the oxide free alloys by the
inclusion of small amounts of reactive metals to provide a
lubricating factor to the alloys of the present invention.
It is an object of the present invention to provide an alloy
suitable for fabrication into a tool having increased life in high
speed steady state cutting of metals.
It is a further object of the present invention to provide an alloy
suitable for fabrication into a tool having increased life in high
speed steady state cutting of metals and characterized by the
carbide phase of the alloy being substantially uniformly dispersed
in a fine grained major phase with substantially all of the carbide
phase having a grain size below 3 microns.
These and other objects and advantages of the present invention
will become apparent in connection with the following detailed
description together with the accompanying drawings in which:
FIG. 1 schematically illustrates an atomizing chamber for use in
the manufacture of the alloys of the present invention;
FIG. 2 is an enlarged view which schematically illustrates
atomizing apparatus of FIG. 1;
FIG. 3 is a photomicrograph at a magnification of 2,000 of atomized
particles of one embodiment of the invention;
FIG. 4 is a photomicrograph at 2,000 magnification showing a
consolidated and annealed alloy of the present invention; and
FIG. 5 is a graph comparing the cutting test data of one embodiment
of the invention with a commercially available high speed cutting
steel.
Briefly, the present invention relates to iron-cobalt alloys
containing tungsten and/or molybdenum, carbon and a reactive metal.
As indicated the disclosed alloys are particularly suited for
fabrication into tools for use in high speed cutting operations on
relatively soft materials, particularly high speed continuous
cutting, for example lathe turning and boring, in which the cutting
edge of the tool is continually in contact with the workpiece.
Continuous cutting operations require less maximum strength of the
tool alloy than milling operations due to a lack of impact loading
on the tool.
Alloys suitable for the aforementioned use, as described in detail
hereinafter, have a composition, by weight, of from about 10 to
about 40% of a material selected from the group consisting of
tungsten, molybdenum and mixtures thereof, from about 0.5 to about
4% carbon, a minor addition of one or more reactive metals selected
from the group consisting of chromium, vanadium, niobium, tantalum,
silicon, manganese and mixtures thereof and the balance a mixture
of iron and cobalt wherein cobalt constitutes from about 25 to
about 50% and iron constitutes from about 20 to about 48% of the
total composition. The amount of each of these reactive metal
additions which can be added to the alloy composition while
retaining a suitable tool material varies with the specific
reactive metal employed.
The preferred ranges of reactive metal additions for the present
invention are as follows, each range being given in percent by
weight of the total composition: chromium from 0 to about 25%;
vanadium from 0 to about 10%; niobium from 0 to about 5%; tantalum
from 0 to about 10%; silicon from 0 to about 5%; and manganese from
0 to about 5%. It has been found that when these ranges are
exceeded by any substantial amount excess oxide is formed and
maintaining suitable strength for tool steel is not feasible.
The ranges specified above are for additions of a single reactive
metal to the basic composition. It is also contemplated that
mixtures of reactive metals be employed in the same
composition.
When more than one reactive metal is employed the specified ranges
are no longer valid. An addition of a second reactive metal results
in a lowering of the limits for both reactive metals employed. In
the case of mixing niobium with silicon or manganese, each of which
has an upper limit of about 5%, the substitution would be linear.
That is, any mixture would be suitable so long as the total
reactive metals constitute no more than 5% of the total
composition. The same linear relationship holds for the mixing of
vanadium and tantalum, each of which has an upper limit of about
10% of the total composition. However, when mixing reactive metals
having different upper limits the relationship changes. Rather than
a linear decrease of the metal having the higher limit, the limit
is reduced by a percentage equal to the percentage of the limit
employed for the lower limit metal. For example, when mixing
chromium with vanadium which have respective limits of 25% and 10%
when employed alone, a 2% addition of vanadium (constituting 20% of
the 10% limit) reduces the allowable limit for chromium to about
20% (a decrease of 20% of the original limit for chromium).
Correspondingly, a 4% addition of vanadium (40% of the limit)
reduces the allowable limit for chromium to about 15% (a 40%
decrease in the chromium limit). Expressed in different terms, if
the limit for each reactive metal when used alone is regarded as
100% for that metal, the total of the two or more metals mixed
should not exceed 100% treating the portion of each metal as a
percentage of its own 100% limit.
The alloys of the present invention are characterized by a carbide
phase substantially uniformly dispersed in a fine grained major
phase with substantially all of the carbide phase having a grain
size below 3 microns. This structure is achieved by the hot
consolidation of pre-alloyed powders by the method described
hereinafter. It is this structure which results in the required
hardness and strength properties for use of the alloys of the
present invention for tool steel purposes.
Referring again to the drawings, FIGS. 1 and 2 schematically
illustrate one apparatus suitable for the atomizing of powders. An
appropriate alloy charge of the desired composition is first
weighed and melted in a suitable crucible. Then the molten alloy is
poured through an orifice 21 at the top of an atomizing chamber 22.
In such a chamber the molten stream is first broken up into fine
droplets and then quickly quenched by a high pressure stream of gas
or liquid entering the chamber 22 through a gas inlet port 23 and a
manifold 29 which surrounds the orifice 21. At the lower end of the
orifice 21 a refractory lined cone 27 is provided extending into
the manifold for the atomizing medium. As the molten material exits
the lower end of the cone 27 the atomizing medium strikes the
molten metal stream to break the stream into fine particles. In
addition, this impact quenches the molten particles so that they
are solidified even before final cooling in the water reservoir 24
described below.
A water reservoir 24 is positioned at the bottom of the atomizing
chamber 22, and the chamber walls and bottom are fabricated of a
steel shell which is water cooled. In the illustrated embodiment
the chamber is approximately 3 feet in diameter and approximately 4
feet in height; however, other dimensions and geometries may be
employed without departing from the scope of the invention. The
bottom wall of the chamber is slightly conical and tapers downward
to the center at which a capped opening 25 is provided for removal
of the quenched metal powder and water.
An inert gas such as argon is supplied through the inlet port 23 at
reasonably high pressure, for example, 350 psi. A tundish 26 is
also provided above the orifice 21 to hold the molten metal charge
before it flows into the atomizing chamber 22. The argon is
permitted to exit from the atomizing chamber at an exhaust port 28
provided in the side wall. Atomization in the described apparatus
results in powders approximately 75 - 85% of which are finer than
80 mesh and from 15 - 30% finer than 325 mesh.
Consolidation of the alloyed powders into fully dense solid stock
can be accomplished by a number of different methods. One of these
methods involves the canning of the powders in Inconel cylinders
lined with molybdenum foil to permit easy stripping of the canning
material from the hot worked ingot. Consolidation of the powders is
accomplished by hammer forging and hot rolling at temperatures of
the order of 2,150.degree. F. An optional step in the process
involves the evacuation of the Inconel can prior to sealing it in
order to prevent additional oxidation of the powder particles. For
the particular compositions disclosed and claimed herein, however,
the evacuation of the can does not produce significant improvements
in the consolidated product. Additional details of the
consolidation process applied to powders generally are set forth in
co-pending application Ser. No. 435,733, filed Feb. 26, 1965. After
consolidation the alloys are heat treated by standard procedures
set forth in more detail hereinafter. ##SPC1##
Table I indicates the composition and hardness of several alloys
formed in accordance with the present invention and consolidated
for tool purposes. It should be noted from Table I that the
additions of reactive materials are quite small in most cases with
the exception of chromium which has been added in amounts up to 20%
by weight of the finished product. It has been discovered that
small additions of a reactive metal greatly improved the high speed
cutting properties of the finished tool alloy over those of an
oxide free or reactive metal free alloy. In addition, the disclosed
alloys have been compared with available commercial steels for high
speed cutting. The results of such tests are set forth in Table II
and in FIG. 5, and show that the alloys tested were equal or
superior to the commercial steels in all tests. ##SPC2##
Compositions within the scope of the present invention which
exhibited particularly good cutting properties on AISI 4340 steel
involved the addition of relatively high amounts of chromium, from
15 to 25%, to a basic alloy comprising from about 25 to about 30%
cobalt, from about 7 to about 12% tungsten, from about 4 to about
8% molybdenum, from about 2 to about 4% carbon, balance iron with
incidental impurities. Of these compositions alloy A 36 consisting
of 20% chromium, 27% cobalt, 9% tungsten, 6% molybdenum, 3% carbon
and 35% iron with incidental impurities exhibited a tool life twice
that of commercial high speed steel in machining AISI 4340 of Rc 50
at a speed of 60 surface feet per minute.
Also the importance of having sufficient carbon is illustrated by
comparing alloys A 148 and A 166 which contain 1.3% and 1.8% carbon
respectively and are otherwise similar. The result of the added
carbon in A 166 is an increase in hardness from 67.9 to 71.0
Rockwell C. This increase was achieved by forming added carbides
without sacrificing the fine grained structure. Cutting data for A
166 shows a tool life approximately five times that of M 43
commercial steel when cutting AISI 4150 steel of Rc 32
hardness.
It is also interesting to note in referring to the cutting data and
the compositions of alloys A 180 and A 181 that while A 181 is of a
lower hardness and in all probability possesses a lower transverse
rupture strength than the alloy of A 180 due to an additional 3% of
vanadium, the lubricating effect is quite pronounced and the tool
life of the higher vanadium content alloy A 181 is almost double
that of alloy A 180 which was roughly comparable to the
commercially available alloy for cutting at the speed indicated and
on the material indicated. All cutting tests in Table II were
conducted on a 40 Horsepower engine lathe with universally
adjustable speed. Each tool was ground to standard positive rake
with a feed of 0.010 inches per revolution a depth of cut of 0.0625
inches. The tool life was based on a flank wearland of 0.060 inches
measured optically, the only exception being the tests conducted on
AISI 1045 in which the cutting was based on a flank wearland of
0.040 inches due to the long tool life and a shortage of stock
material.
The selection of the particular group of metals termed herein
reactive metals is based on what is commonly termed the negative
free energy of formation of the particular metals involved. The
negative free energy of formation is a commonly used measure of the
ease with which metal oxides are formed and the degree of
difficulty in reducing the oxide, once formed, to the free metal
form. The metals listed have been selected from common alloying
elements based on a negative free energy of formation having values
ranging from -58 to -72 K cal/gm - atom at 1,500.degree. K. It has
been found that the amount of each metal which can be employed
varies from one metal to another. The variation is believed to be
at least in part related to the negative free energy of formation
and the atomic weight of the particular metal. It has also been
found that chromium can be employed in amounts up to about 25%
while retaining tool properties. The reason for this higher limit
for chromium is not known.
Other common alloying agents such as Ti, Al, Zr and Mg having
negative free energies of formation ranging from -91 to -101 K
cal/gm - atom at 1,500.degree. K are not suitable additions because
they tend to form a much greater proportion of oxide even for small
additions than do the reactive metals in the preferred range of
negative free energy of formation. Additionally, the oxides of Ti,
Al, Zr and Mg once formed are proportionately more difficult to
reduce than the preferred metals. Thus additions of these metals
even in small amounts weaken the alloy sufficiently that tool use
is not practical.
The addition of the preferred reactive metals also results in a
somewhat reduced transverse rupture strength over that exhibited by
the same composition without the addition of the reactive metal.
However, for the high speed, steady state, cutting of steels,
having a Rockwell C value up to about 50, the addition of small
amounts of the reactive metals results in a greatly improved tool
life over that exhibited by the oxide free alloys. As mentioned
earlier, it is believed that the improved tool life is at least
partially the result of a lubricating factor caused by the addition
of one or more of the reactive metals. This lubricating property is
particularly important in the high speed cutting operations
described earlier in which the relative speed between the tool and
the workpiece might be as high as 140 surface feet per minute. At
such speeds it is very difficult to reach the cutting surface of
the tool with conventional liquid lubricants. The additions of
reactive metals to tools to be utilized in the high speed, steady
state cutting environment has resulted in an elimination of the
welding phenomenon of the workpiece to the tool tip exhibited by
the oxide free alloys.
While the addition of these materials to the alloy produces an
unexpected increase in tool life for a particular type of cutting
operation, a consideration of the metallurgy involved indicates
that the amount of reactive metal addition must be kept relatively
a small part of the total alloy. As stated earlier, each of these
reactive metals tends to form an oxide on the metal powder, which
oxide is relatively difficult to reduce to the pure metal state
after the alloy powder has been formed. During the atomizing
process a thin film of oxide forms on each alloy droplet. This
oxide is a mixture of the oxides of all of the metallic alloy
constituents including the easily reduced oxides of iron, cobalt,
tungsten and molybdenum as well as of the reactive metal additions.
This does not mean, however, that all of the reactive metal
additive forms an oxide. Some of the reactive metal additive
partitions, one portion uniting with carbon to form the carbide
phase such as vanadium carbide, and the other portion remaining in
solution in the alloy matrix.
When the powders are jacketed in the Inconel can and heated to
2,000.degree. to 2,100.degree. F. for approximately 45 minutes
prior to consolidation, the oxides on the surface of the powder
react with the carbon in the alloy and much of the oxide is reduced
during the consolidation. It has been found that for very small
additions such as 2.5% chromium there are no deleterious oxides
remaining in the alloy after consolidation. For higher percentages
of chromium, in excess of 10%, removal of all oxides formed by the
chromium is impractical since the ingot would require soaking for
several hours within the specified temperature range or for a
shorter time at a much higher temperature range. Thus, for chromium
contents in excess of 10% by weight and for additives of the other
specified reactive metals even in much smaller amounts, some oxide
will remain in the finished alloy after consolidation. During the
heating and hot working of the ingot the oxides which are on the
outside of the individual powder particles and are not reduced by
the carbon in the alloy are dispersed into fine particles of oxide
due to the mechanical working of the alloy. In this form the oxide,
which would substantially reduce the strength of the alloy if left
as a continuous film on the powder particles, results in only a
moderate reduction of strength. However, the reduction of strength
is not sufficient to impair the steady state metal cutting
performance of the alloy at high speeds.
It is not clear whether the beneficial lubricating properties of
the reactive metals are achieved only from the metal which has been
reduced to the free state or which has formed carbides or whether
the oxide form also contributes to the lubricating feature. It is
known, however, that as the oxide content increases due to presence
of the reactive metals beyond the ranges specified herein, the
strength of the alloy rapidly becomes lower and the achievement of
the required hardness for tool use also becomes increasingly
difficult. The balance in each alloy is between adding sufficient
reactive metal to lubricate without weakening the structure too
much for tool use.
There are, of course, other advantages due to the addition of the
reactive metals to the alloys, some of which are already known.
Chromium, for example, is known to impart hardenability and
oxidation resistance to the finished alloy, that is, oxidation
resistance of the tool point due to contact with the workpiece
during cutting. This property is to be distinguished from the
tendency to form oxides on the powder during atomizing as set forth
herein. Vanadium is added to some of the tool steels of the present
invention to form very hard carbides for wear resistance. One
particular advantage of the small additions of the reactive metals
in the preatomized and consolidated type of alloy is the ability in
many of the compositions to adequately harden the material for tool
use by employing a solutionizing temperature of the order of
1,700.degree. F. In standard commercial high speed steels
temperatures considerably above 2,000.degree. F. are required to
obtain hardness values approaching the Rockwell C 70. 1,700.degree.
F. is sufficiently low to permit brazing of tool alloys to low cost
steels and solutionizing without melting the brazing metal. The
ability to utilize the lower hardening temperature also results in
less scaling of the tool material and in much finer structure in
the finished alloy, both in terms of the ultrafine carbide
dispersion and the crystal growth within the alloy matrix itself.
In this connection it should be noted that the solutionizing
temperature of 2,200.degree. F. employed for some of the alloys in
Table I was not necessary to achieve desired properties.
Conventionally processed tool steels and other ferrous alloys are
melted and then poured into ingot molds which are of such a size,
shape and are characterized by such a thermal conductivity that the
metal requires at least several minutes before solidification is
complete. During this time interval the carbide phase nucleates and
grows to appreciable size. Subsequent hot working of the ingots
causes some break-up of the carbides but they remain relatively
coarse and tend to be aligned in the direction of hot working. On
the other hand the alloys which are made as taught in the present
invention are cooled from the molten state in the form of fine
spherical droplets (mostly less than 0.007 inches in diameter)
which solidify into particles in a fraction of a second. These
particles have a finely dispersed high volume of carbides (FIG. 3)
of a diameter predominantly less than 3 microns. The extremely
short time interval for solidification does not permit the carbide
phase to grow appreciably. The atomized powders are then heated for
consolidation and for subsequent heat treatment. It should be noted
that this heating is done at a temperature (about 2,150.degree. F.)
below that at which there is an undue coarsening or agglomeration
of the carbide phase. As can be seen by comparing FIGS. 3 and 4
there is only a slight growth in the size of the carbides during
consolidation. Because of the extra fineness of the hard carbide
particles, the atomized and consolidated alloys of the present
invention may be hot worked at temperatures similar to, or even
lower than, those used for conventionally produced tool steels and
the alloys do not contain large carbide particles which would act
as sites for crack initiation and propagation. Thus, another
advantage of the present alloys and the herein described method of
making them is that greater carbide volumes may be had without
impairing alloy workability. It should be appreciated also that
consolidation of the powders into wrought stock was accomplished in
the present case without resorting to conventional sintering
techniques and without adding carbon in any manner to the powders.
The amount of carbon desired in the particular alloy is selected
prior to atomization and substantially this exact amount will be
uniformly distributed in the final wrought stock. This amount is
important to the formation of the carbide phase and to the hardness
achieved as can be seen from alloys A 148 and A 166 in Table I. The
carbon content if too low will prevent the alloy from reaching
required tool hardness.
As briefly mentioned above, the atomized and consolidated alloys of
the present invention may be heat treated by methods commonly
employed for conventional tool and die steels. After hot working
the consolidated alloys may be rendered more readily machinable by
heating to temperatures of 1,500.degree. or 1600.degree. F.
followed by slow cooling such as furnace cooling. After the
appropriate finished shape has been fabricated from the stock, it
may then be hardened by standard commercial practices.
The hardening or austenitizing is most readily accomplished by
first heating the alloy to a tmmperature of approximately
1,700.degree. to 2,200.degree. F. depending on the particular
composition involved, holding at this temperature for a sufficient
length of time to permit adequate solution of carbides into the
matrix, then cooling by immersion in oil or by air cooling.
Following this quenching the alloys are then tempered by reheating
to a temperature near 1,000.degree. F. for several hours. This
tempering treatment may be performed two or three times cooling to
room temperatures between each heating cycle to impart additional
toughness to the alloy.
It should be noted that the heat treatments employed during
annealing, austenitizing and tempering are conducted at
temperatures which do not permit excessive growth or agglomeration
of the carbide phase during the heating periods used for such
atomized and consolidated alloys.
While the present invention has been described with respect to
particular compositions within the specified range, it will be
understood that various modifications and variations may be
effected without departing from the spirit or scope of the
invention as set forth in the following claims.
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