TECHNICAL FIELD
[0001] This invention refers to a method for producing a high speed steel with the composition
according to the preamble of claim 1.
BACKGROUND
[0002] New materials suitable for applications involving elevated temperatures and wear
are needed today. Such application areas may include, hot forging tools for metal
forming, combustion engine parts etc.
[0003] Several different special alloys suitable for high temperature use exist, for example
FeCrAl-alloys, NiCrAl-alloys, Ni-base alloys, Co-base alloys and special stainless
steels. However, the FeCrAl- NiCrAl- and Ni- alloys are too soft to be used in the
aforementioned areas of applications. Some Co-base alloys are sufficiently hard but
too expensive to be a practical alternative for most applications.
[0004] High speed steel (HSS) offers good hardness at room temperature and is able to maintain
that hardness up to 600°C. However, for some applications it is desirable to maintain
the room temperature hardness at temperatures well above 600°C.
[0005] In the art it is known that alloying the high speed steel with cobalt improves its
hardness at higher temperatures.
[0006] Several different ways to improve high speed steel usability in high temperature
applications exists in the art.
[0007] It is known in the art that adding alloying elements such as cobalt (Co) in combination
with strong carbide-forming elements which act through the base mass or matrix increase
the high speed steel's hardness at high-temperature and thereby the wear resistance.
[0008] It is also known in the art that adding alloying elements such as tungsten, molybdenum
and vanadium increases the high speed steel's ability to withstand high-temperature,
i.e their hot hardness and high temperature wear, thanks to formation of carbides
based on said alloying elements.
[0009] It is also known in the art that an increase of the formed amount of carbides by
alloying with carbide forming elements such as chromium, molybdenum, tungsten and
vanadium positively contributes to the wear resistance of the high speed steel.
[0010] A large amount of alloying elements makes the high speed steel difficult to produce
by standard casting techniques. The resulting microstructure suffers problems from
severe segregation with very coarse carbides which results in very poor toughness
and strength of the high speed steel. In applications in which the steel is subjected
to forging after the casting thereof, some of these problems are overcome as a result
of the effect that such deformation has on the microstructure of the material.
[0011] For alloys that in addition to high temperature and wear needs to withstand an oxidative/corrosive
environment some new demands arise due to synergy effects. For materials that are
simultaneously exposed to corrosion/oxidation and wear, the behaviour of the material
is of utter importance. The oxidation kinetics as well as oxide scale mechanical properties
and adhesion become important factors for the use of the alloy.
[0012] By depositing special coatings on the high speed steel, it's oxidation behaviour
can be altered (
Reduction of wear in critical engine components using ion-beam-assisted deposition
and ion implantation, J.H. Arps et al., Surface and Coatings Technology 84 1996 p579-583). However, such coatings are of limited use in applications with heavy wear, since
they only bring a thin protective coating (in the micrometer range) to the steel.
In applications in which the wear can be expected to be in the millimetre range, steel
products with this type of coating will require subsequent, further coating as the
initial coating would wear down. This would increase the cost of the product considerably
over its expected lifetime. Another feasible solution would be to utilize surface
modification of the high speed steel, such as ion-implantation (
Ion beam modification of metals, G. Dearnley, Nuclear Instruments and Methods in Physics
Research B50 1990 p358-367). However, a problem with ionimplantation is the Gaussian distribution of ions, which
causes depth varying material characteristics. Ionimplantation also implies a limited
useful thickness of the modified layer; therefore it is not suited for use in the
aforementioned applications.
[0013] US Patent No. 5989491 to Isamoto et al. discloses a method that uses oxide dispersion strengthening for a powder metallurgy
alloy. The inventors behind this patent noted that fine dispersion of particles of
an oxide in an oxide dispersion strengthened heat resisting powder metallurgy alloy
enhanced creep rupture strength in addition to fundamental heat resisting properties
inherent to heat resisting alloys. However, the alloy disclosed in
US5989491 is not suitable for mechanical applications involving wear such as those aforementioned,
since the wear resistance of the end product will not be affected by the addition
of fine particles of an oxide.
[0014] Several patents disclose the use of rare-earth elements in high speed steels in connection
with applications at elevated temperatures, for example see:
JP1142055A,
JP63213641A,
CN101037760A,
JP1159349A,
JP1142056A,
CN101078090A,
JP6299298A,
CN1693527A,
JP57143468A,
JP2005281839A,
CN101831590A,
JP8041592A,
JP57143471A,
JP2003253396A, and
JP1008252A. However, all of these alloys are cumbersome to produce with standard casting techniques.
The level of alloying some of these high speed steels exhibits, likely causes problems
with segregation of alloying elements during solidification and form coarse carbide
structures. Therefore, it is cumbersome to manufacture a high speed steel, with high
levels of alloying elements and rare-earth elements, and simultaneously achieve uniform
material properties and a well controlled microstructure.
[0015] JP57085952A (abstract) discloses an alloy with a composition corresponding to the composition
according to the preamble of claim 1 of the present invention. It must be assumed
that the document in question also discloses casting as the method of producing the
alloy. It must be assumed that the steel disclosed therein has a microstructure that
results in poor strength of the material and therefore makes it less usable as a wear
part.
THE OBJECT OF THE INVENTION
[0016] The object of this invention is to present a method by means of which the above mentioned
problems associated with manufacturing of high speed steel comprising of rare earth
element Y for applications that involve wear at elevated temperatures, are reduced
or solved.
[0017] The present invention also aims at providing a manufacturing method which increases
the ability of high speed steel to withstand wear at elevated temperatures.
[0018] Thus, the present invention is based on the insight of the problems of segregation
and coarse carbide structures associated with casting and the addition of yttrium
into conventional high speed steel.
SUMMARY
[0019] The object of the invention is achieved by a method for producing a high speed steel
that with reference to its chemical composition consists of the following elements,
in weight%: Carbon (C) 1-3, Chromium (Cr) 3-6, Molybdenum (Mo) 0-7, Tungsten (W) 0-15,
Vanadium (V) 3-14, Cobalt (Co) 0-10, Niobium (Nb) 0-3, Nitrogen (N) 0-0.5, Yttrium
(Y) 0.2-1, and remainder consisting of iron (Fe) and unavoidable impurities and wherein
Mo+0,5W = 2-10" said method being characterised in that the method comprises the steps
of: providing a powder comprising the elements of said high speed steel, forming a
body of said powder, and subjecting said body to elevated heat (temperature) and elevated
pressure such that a consolidation of the powder thereof is achieved. This step may
be referred to as the consolidation step or a hot isostatic pressure (HIP) step.
[0020] During said consolidation step, the steel is in solid state, i.e. non-molten state.
Preferably the temperature during said step of elevated temperature is within the
range of 950-1200 °C, wherein lower temperatures may be required for alloys with relatively
high content of C and low content of alloying elements such as Mo, W, Co, Y, etc and
wherein higher temperatures within said range is required for alloys with relatively
low content of C and high content of said further alloying elements. If the temperature
is too low, the final result will be a porous material, and if the temperature is
too high, the material might start to melt, which should be avoided.
[0021] The pressure during the consolidation step is dependent on the temperature that is
chosen for each respective steel composition. A relatively low temperature may be
compensated for by means of a higher pressure. Preferably, for the compositions within
the scope of the invention, as defined in claim 1 and also in the dependent claims,
and for the mentioned temperature range of the consolidation step, the pressure should
be in the range of 800-1500 bar. In general, higher content of alloying elements will
require a higher pressure for a specific chosen temperature.
[0022] According to a preferred embodiment, the body of consolidated powder, that now has
a very low porosity level or no porosity at all, is then subjected to soft annealing.
The soft annealing is performed in order to facilitate subsequent machining of the
alloy. Preferably, the maximum temperature of the soft annealing step is the temperature
of the foregoing consolidation step, while the minimum temperature is the temperature
at which the steel undergoes softening and carbides in the steel spheroidize and the
martensite transforms to ferrite. In any case, the temperature must not be so high
that it results in severe coarsening of the carbide grain size.
[0023] The selected soft annealing temperature will depend on the composition of the alloy.
Generally, higher contents of alloying elements will require a higher annealing temperature.
Accordingly, for the compositions within the scope of the present invention, the soft
annealing temperature will preferably be from 600 to 900 °C. The duration of the soft
annealing should be sufficiently long to reach ferrite content in the material that
is sufficiently high. Preferably, after soft annealing the ferrite-austenite ratio
should be at least 95/5. The steel is cooled relatively slowly, in order to avoid
formation of martensite, or bainite in the alloy. Preferably, the cooling rate is
within the range of 5-20°C/hour, depending on the composition of the alloy. Cooling
with this rate is performed down to a temperature below which the cooling rate will
no longer affect the formation of bainite, martensite. Below that temperature, the
cooling may be natural, and the cooling rate may depend only on the outer conditions
reigning. For the alloys within the scope of the invention, this temperature may be
in the range of 600-700°C.
[0024] The body is thereafter preferably subjected to machining if necessary and thereafter
heat treated with a hardening (austenizing) step at a temperature in the range of
950-1200°C, depending on the specific composition of the steel that is hardened. After
hardening, there will be some remaining austenite in the steel, the main part of the
steel now being martensite. This austenite is removed by means of subsequent annealing
steps. During the first step remaining austenite is transformed into martensite. However,
this martensite being very brittle will require a further annealing step in order
to become sufficiently ductile. Depending on the composition and the amount of austenite
that remains in the steel after hardening, the number and duration of the annealing
steps may vary. According to a preferred embodiment of the invention, annealing steps
are performed until the level of remaining austenite is maximum 5%, preferably maximum
2%.
[0025] The technical effect of the inventive method is that the rare earth element yttrium
is evenly distributed in the powder. If the high speed steel according to the inventive
concept would have been produced by a conventional casting method, the highly reactive
element yttrium would segregate and not be evenly distributed. An even distribution
of yttrium in the high speed steel base-matrix causes an oxide scale that is formed
to adhere effectively to the high speed steel. The added yttrium also changes the
growth kinetics of the oxide scale so that the scale quickly grows to a saturation
thickness. The growth rate of the oxide scale is drastically reduced above this saturation
thickness. The beneficial technical effect on the wear resistance, at elevated temperatures,
due to the fine dispersion of yttrium in the base-matrix of the high speed steel is
unexpectedly good. This technical effect is beyond what a person skilled in the art
would expect from an addition of yttrium using a powder metallurgy method. In fact
the gain in technical effect is so high that it, unexpectedly, compensates for the
higher costs related to the use of powder metallurgy as the method of producing this
steel, making the steel very useful in any application in which it is subjected to
severe wear conditions. In particular, the steel will have a mean carbide particle
size which is much lower than that of a corresponding material made using casting
method. According to the invention, the steel should have a mean carbide particle
size of <3µm, something it will have if the method of the invention is being used
for the production thereof. As a result of the production method of the invention,
the steel will also have an isotropic microstructure, which is also advantageous for
its wear properties. In other words, the invention teaches that the consolidation
step and the subsequent heat treating steps shall be performed such that the steel
obtains a mean carbide particle size which is <3µm and an isotropic microstructure.
[0026] The properties of the formed oxide scale are extremely important in applications
that besides high temperature and wear also include oxidation/corrosion. In oxidative/corrosive
applications it is of great importance that damages in the oxide scale are quickly
repaired by a fast growth of the oxide scale itself, and this is achievable by using
the material produced by the inventive method.
[0027] According to a preferred embodiment of the inventive method, the provision of the
powder mixture comprises the step of argon-atomisation of molten metal comprising
said elements into said powder. By using argon-atomisation of the molten metal the
amount of nitrides is minimized compared to using nitrogen-atomisation wherein the
use of nitrogen gas causes the nitrides to form.
[0028] According to the invention the yttrium content of the high speed steel is within
the range 0.20 to 1.0 weight%. It is preferred that the yttrium content of the high
speed steel is more than 0.40 weight%, and less than 0.70 weight% more preferably
less than 0.60 weight%. In a particularly preferred embodiment, the Yttrium content
is with the range of 0.45-0.60 weight%.
[0029] The yttrium content defined in the interval above gives the aforementioned positive
effects on the oxide scale. Especially the yttrium content in the range of 0.45-0.60
weight% gives a very good increase in the ability of the high speed steel to withstand
high temperature wear. The lower limit 0.20% of the interval defines a starting point
from where a significant positive effect of yttrium on the high temperature wear can
be identified. The higher limit of 1% indicates the end of the interval from where
a significant positive effect of yttrium on the high temperature wear can be identified.
[0030] According to a preferred embodiment of the inventive method the carbon (C) content
of said high speed steel is in the range of 1.1-1.4 weight%. The amount of carbon
should be sufficient to form the carbides necessary for the wear resistance of the
high speed steel. Preferably the amount of carbon should be enough to produce a high
speed steel with sufficient hardenability. The lower limit of 1.1% defines a minimum
carbon content in order to form a high speed steel with the desired carbides and hardenability.
The higher limit of 1.4% defines maximum carbon content in this embodiment, above
which austenite may be formed.
[0031] According to a preferred embodiment of the inventive method the chromium (Cr) content
is in the range of 3.0-6.0 weight%. This interval causes good hardenability as well
as the necessary forming of carbides. However, too much chromium causes formation
of residual austenite and increased risk for over-tempering; therefore the upper limit
of Cr must not be exceeded. According to yet another preferred embodiment, the Cr
content is within the range of 4.0-5.0 weight%.
[0032] According to a preferred embodiment of the inventive method the molybdenum (Mo) content
is in the range of 4.5-5.5 weight%. This interval causes secondary hardening by precipitation
of carbides that will increase the hot hardness and wear resistance of the high speed
steel.
[0033] According to a preferred embodiment of the inventive method the tungsten (W) content
is in the range of 6.0-7.0 weight%. This interval causes secondary hardening by precipitation
of carbides that will increase the hot hardness and wear resistance of the high speed
steel.
[0034] It is a well-known fact that Mo and W have similar effects on this kind of steel
and that they are therefore to a large extent replaceable with each other. According
to claim 1, Mo+0.5W = 2-10 weight%. According to a preferred embodiment, Mo+0.5W=
5-8.5 weight%.
[0035] According to a preferred embodiment of the inventive method the vanadium (V) content
is in the range of 3.0-5.0 weight%. This interval causes secondary hardening by precipitation
of carbides that will increase the hot hardness and wear resistance of the high speed
steel. However, too much vanadium causes the high speed steel to become brittle and
therefore, the upper limit must not be exceeded. According to yet another preferred
embodiment the V content is in the range of 3.0-3.5 weight%.
[0036] According to another preferred embodiment of the inventive method the cobalt (Co)
content of said high speed steel is in the range of 8.0-9.0 weight%. The alloying
of high speed steel with cobalt improves the tempering resistance and hot hardness,
both of which are of great importance for the high speed steel to be used in a high
temperature wear application. The amount of cobalt also has an effect on the hardness
of the high speed steel by affecting the amount of retained austenite, causing said
retained austenite to easily be converted to martensite during tempering. The selected
interval for cobalt is a suitable interval for a high speed steel of this composition
wherein the upper level is more an economic compromise than a scientific constraint.
Alternatively, if cobalt is not to be used in the above-defined range, the cobalt
content is 0% or at an impurity level.
[0037] Powder metallurgical high speed steel produced by the inventive method possesses
properties such as very good resistance to high temperature wear even in oxidative/corrosive
environments.
BRIEF DESCRIPTIONS OF THE DRAWINGS
[0038] The inventive concept will now be further explained using reference figures in connection
with attached drawings and graphs, in which
Figure 1 is a schematic figure of a "pin on disc" test equipment,
Figure 2 shows a cross section of a typical groove obtained from a "pin on disc" evaluation,
perpendicular to the longitudinal direction,
Figure 3 is a diagram showing the groove depth at room temperature and 650°C for the
alloys A, B and C in the "pin on disc" experiment,
Figure 4 is a diagram showing the volume loss per meter at 650°C for the alloys A,
B and C in the "pin on disc" experiment, and
Figure 5 shows the hardness in HRC for alloy A, B and C.
DETAILED DESCRIPTION
[0039] The industrial production of semi-finished products, components and cutting tools
based on powder metallurgical high speed steel started 35 years ago. The first powder
metallurgical production of high speed steel was based on hot isostatic pressing (HIP)
and consolidation of atomized powders. The HIP step was normally followed by hot forging
of the hipped billets. This method of production is still the dominating powder metallurgical
method to produce high speed steel.
[0040] The original objective for research and development on powder metallurgical processing
of high speed steel was to improve its functional properties and performance in demanding
applications. The main advantages from the powder metallurgical manufacturing process
are no segregation and uniform and isotropic microstructure. The well known problems
with coarse and severe carbide segregation in conventional cast steel and forged steel
are thus avoided in powder metallurgical high speed steel.
[0041] Thus, the powder metallurgical manufacturing method of a high speed steel with sufficient
amount of carbon and carbide forming elements, results in a disperse distribution
of carbides that to a large extent solves the problem of low strength and toughness
associated with conventionally produced high speed steel.
[0042] The present invention refers to a method for producing a high speed steel. The inventive
method comprises the step of providing a powder consisting of the elements: 1-3 wt-%
carbon (C), 3-6 wt-% chromium (Cr), 0-7 wt-% molybdenum (Mo), 0-15 wt-% tungsten (W),
3-14 wt-% vanadium (V), 0-10 wt-% cobalt (Co), 0-3 wt-% niobium (Nb),0-0.5 wt-% nitrogen
(N), 0.2-1 wt-% yttrium (Y), and remainder iron (Fe) and unavoidable impurities, wherein
Mo+0.5W = 2-10 weight%. It should be pointed out that the elements having a lower
limit of 0 % are optional.
[0043] In a preferred embodiment of the invention, the provision of the powder mixture comprises
the step of argon gas-atomisation of molten metal comprising said elements into said
powder. In a preferred embodiment of the invention, the argon gas-atomisation of the
molten high speed steel causes high speed steel particles of a maximum size of 160
µm to be formed.
[0044] After the provision of the powder a body is formed from said powder. This forming
may for example comprise pouring said powder into a capsule. The capsule is then evacuated,
e.g. by being subjected to a negative pressure of below 0.004 mbar for 24 hours in
order to evacuate said capsule. The capsule is then sealed in order to maintain said
negative pressure in the capsule. The consolidation of the powder is achieved by subjecting
the capsule to an elevated temperature, e.g. about 1150°C, and an elevated pressure,
e.g. about 1000 bar, for a long period of time, e.g. two hours. This last consolidation
step is called hot isostatic pressing, HIP.
[0045] A soft annealing step follows the HIP step, preferably the soft annealing step is
performed at 900°C followed by a temperature decrease to 700°C at a cooling rate of
10°C/hour, from thereon the body is allowed to naturally cool down to room temperature.
[0046] After soft annealing the body may be subjected to machining and preferably a hardening
(austenizing) step at 1100°C and three subsequent annealing steps at 560°C for 60
minutes each, with natural cooling to room temperature there between.
[0047] The resulting material from these subsequent steps exhibits a very good uniformity
without the aforementioned segregations and coarse carbide structure, and the most
important effect is that the yttrium element is evenly distributed in the base-matrix
of the high speed steel.
Table 1
Alloy |
Carbon (C) wt-% |
Chromium (Cr) wt-% |
Molybdenum (Mo) wt-% |
Vanadium (V) wt-% |
Tungsten (W) wt-% |
Yttrium (Y) wt-% |
A |
1.28 |
4.2 |
5 |
3.1 |
6.4 |
- |
B |
1.18 |
4.2 |
5 |
3.1 |
6.4 |
0.5 |
C |
1.19 |
4.2 |
5 |
3.1 |
6.4 |
1 |
[0048] In order to demonstrate the superior properties of the inventive method a high speed
steel was designed without the optional elements, see table 1. The exclusion of the
optional elements gives a clear and concise demonstration of the improved high-temperature
wear due to the method. A simple evaluation method "pin-on-disc" for high-temperature
wear is described below.
[0049] Table 1 shows the elements of the high speed steel used in the experiment. Smelts
were produced with the elements in table 1, and from these smelts powders were produced
by means of gas atomisation using argon. The powders of alloy B and C in table 1 have
a particle size of <160 µm, while the powder of alloy A has a particle size of <500
µm.
[0050] In the following description a performed experiment will be described in detail.
[0051] The preparation of samples continued with a filling of the capsules with powder,
said capsules were made from spiral welded tubes with a diameter of 73 mm. The capsules
were then exposed to an pressure below 0.004 mbar for 24 hours; the capsules were
then sealed in order to maintain said pressure.
[0052] In order to consolidate the powder in the capsules a hot isostatic pressing operation
was performed at 1150°C and 1000 bar for 2 hours. The samples were then subjected
to a soft annealing step at 900°C followed by a temperature decrease to 700°C at a
cooling rate of 10°C/hour, from thereon the samples were allowed to naturally cool
down to room temperature.
[0053] The samples were then machined and heat treated with a hardening (austenizing) step
at 1100°C and three subsequent annealing steps at 560°C for 60 minutes each, with
natural cooling to room temperature there between.
[0054] The final preparation step comprises stepwise grinding and polishing of the sample
in automatic grinding/polishing equipment. During the final polishing step a 1 µm
diamond suspension was used.
[0055] Figure 1 shows a simplified test set-up used for the tribological testing; this set-up
is known in the art and has been referred to as "pin on disc". The principle for the
"pin on disc" tribological testing is as follows; a sample 1 is rotated around an
axis 5 with a speed ω for a number of revolutions. Simultaneous with the rotation
of the sample 1 a force F is applied to a pin 2 that in its turn applies the same
force F to a ball 3. The ball 3 is made of Al
2O
3 and has a diameter of 6 mm. The rotation of the sample 1 and the force F on the ball
3 causes a groove 6 to be formed in the sample 1.
[0056] In order to evaluate the wear behaviour at elevated temperatures the lower part of
the "pin on disc" set-up is accommodated in a furnace 4. Thus, the furnace 4 can heat
the sample 1, the ball 3 and the lower part of the pin 2 to the desired operating
temperature.
[0057] Figure 2 shows a cross section of the groove 6 perpendicular to the longitudinal
direction of the groove 6. The depth d measured from the polished surface of the sample
to the bottom of the groove 6 is used as a measure of the wear resistance of the sample.
Another figure of the wear resistance is the cross-sectional area 7, which is defined
as the cross-sectional area of the groove 6 below the polished surface of the sample
1 perpendicular to the longitudinal direction of the groove 6. The profile and depth
d of the groove 6 was estimated using a Veeco Wyko NT9100 white light interferometer.
[0058] A series of samples according to the description above were produced and tested according
to the "pin on disc" procedure outlined above. The "pin on disc" result is presented
in figure 3, the linear speed in this test was 20 cm/s, the applied force F was 5N
and 20N, respectively, and the samples were rotated 20000 revolutions.
[0059] As can be seen in figure 3 the addition of yttrium causes the depth of the groove
to decrease at 650°C; see alloy A with a groove depth d equal to 5.7 µm, alloy B with
a groove depth d equal to 1,9 µm and alloy C with a groove depth d equal to 3.7 µm.
This indicates the anticipated increased wear resistance at elevated temperatures
for alloys produced by the inventive method. The addition of 0.5 % yttrium to the
high speed steel (Alloy B) caused a reduction of the groove depth d of roughly three
times compared to the high speed steel without yttrium (Alloy A). Also the addition
of 1% yttrium to the high speed steel (Alloy C) caused a reduction of the groove depth
d at 650°C.
[0060] A more representative measure of the wear resistance is the volume loss per meter
(mm
3/m). The calculation of the volume loss per meter is performed by integrating the
cross sectional area 7 over the longitudinal direction of the track and divide by
the circumference of the groove. In figure 4 the volume loss per meter is presented;
volume loss for alloy A is 4.6x10
-5 mm
3/m, volume loss for alloy B is 1.8×10
-5 mm
3/m and finally the volume loss for alloy C is 4×10
-5 mm
3/m. The relation between the yttrium content of the high speed steel and the volume
loss per meter thereof is illustrated in figure 4. From figure 4 one can conclude
that the yttrium content of 0.5 % clearly results in the lowest volume loss per meter.
A higher yttrium content than 1% also has a beneficial effect on the volume loss per
meter. This relation implies that the yttrium content of 0.5% gives a superior increase
in the implied wear resistance of the high speed steel.
[0061] According to the invention the yttrium content of the high speed steel is within
the range 0.2 to 1 weight%. It is preferred that the yttrium content of the high speed
steel is more than 0.4 weight%, and less than 0.7 weight% more preferably less than
0.6 weight%, most preferably 0.5 weight%.
[0062] In figure 5 the hardness of the samples is presented. The hardness is 63 HRC for
alloy A, the hardness is 57 HRC for alloy B and the hardness is 56 HRC for alloy C.
The conclusion from figure 5 is that the hardness is reduced with the addition of
yttrium. One possible explanation for this reduction is that less carbon is available
in the alloys that contain yttrium, thereby reducing the hardness. This illustrates
the theory that the wear rate of the high speed steel, in figure 3, at room temperature
is primarily dominated by the hardness of the high speed steel. At room temperature
the wear rate increases with decreasing hardness. However, at elevated temperatures
other mechanisms are dominating the wear, such as the growth kinetics and the mechanical
properties of the oxide scale.
1. A method for producing a high speed steel that with reference to its chemical composition
consists of the following elements, in weight%:
1-3 |
Carbon (C) |
3-6 |
Chromium (Cr) |
0-7 |
Molybdenum (Mo) |
0-15 |
Tungsten (W) |
3-14 |
Vanadium (V) |
0-10 |
Cobalt (Co) |
0-3 |
Niobium (Nb) |
0-0.5 |
Nitrogen (N) |
0.2-1 |
Yttrium (Y), and |
remainder iron (Fe) and unavoidable impurities, wherein Mo+0.5W = 2-10 weight%,
characterised in that the method comprises the steps of:
- providing a powder comprising the elements of said high speed steel,
- forming a body of said powder, and
- subjecting said body to elevated heat and elevated pressure such that a consolidation
of the powder thereof is achieved.
2. A method for producing a high speed steel according to claim 1, characterised in that the provision of the powder mixture comprises the step of argon-atomisation of molten
metal comprising said elements into said powder.
3. A method for producing a high speed steel according to claim 1 or 2, characterized in that the yttrium (Y) content of said high speed steel is more than 0.4 weight%.
4. A method for producing a high speed steel according to any of claims 1-3, characterized in that the yttrium (Y) content of said high speed steel is 0.7 weight% or less.
5. A method for producing a high speed steel according to any of claims 1-4, characterized in that the yttrium (Y) content of said high speed steel is within the range of 0.45-0.60
weight%.
6. A method for producing a high speed steel according to any one of claims 1-5, characterised in that the carbon (C) content of said high speed steel is in the range of 1.1-1.4 weight%
7. A method for producing a high speed steel according to any one of claims 1-6, characterised in that the chromium (Cr) content of said high speed steel is in the range of 3.0-6.0 weight%.
8. A method for producing a high speed steel according to any one of claims 1-7, characterised in that the chromium (Cr) content of said high speed steel is in the range of 4.0-5.0 weight%.
9. A method for producing a high speed steel according to any one of claims 1-7, characterised in that the Molybdenum (Mo) content of said high speed steel is in the range of 4.5-5.5 weight%.
10. A method for producing a high speed steel according to any one of claims 1-9, characterised in that the tungsten (W) content of said high speed steel is in the range of 6-7 weight%
11. A method for producing a high speed steel according to any one of claims 1-10, characterised in that Mo+0,5W = 5.0-8.5 weight%.
12. A method for producing a high speed steel according to any one of claims 1-11, characterised in that the Vanadium (V) content of said high speed steel is in the range of 3.0-5.0 weight%.
13. A method for producing a high speed steel according to any one of claims 1-12, characterised in that the Vanadium (V) content of said high speed steel is in the range of 3.0-3.5 weight%.
14. A method for producing a high speed steel according to any of claims 1-13, characterised in that the Cobalt (Co) content of said high speed steel is in the range of 8.0-9.0 weight%.
15. A high speed steel obtained by the method according to any one of claims 1-14, characterised in that it has a mean carbide particle size <3µm.
16. A high speed steel according to claim 15, characterised in that it has an isotropic microstructure.