[0001] This invention relates to a thermal treatment method. In particular, it relates to
a method of case hardening an article of titanium or of an alloy based on titanium.
[0002] Titanium has poor tribological properties. Various coatings can used, for example
titanium nitride, to improve the technological properties of the metal and its alloys
but even so, their use in engineering is limited by the low strength of the substrate.
Accordingly thermochemical diffusion treatments have been developed. To produce to
a layer that is sufficiently thick to support a load in a reasonable time, oxidising
and nitriding treatments are preferred at 965°C and 1050°C respectively. These high
treatment temperatures degrade the core properties of the metal or alloy to such an
extent that a further heat treatment becomes necessary after the formation of the
case.
[0003] The state of the art is illustrated by the following documents.
[0004] WO-A-96/23908 discloses a process for manufacturing a titanium article with a hardened surface
for enhanced wear resistance comprising the steps of exposing the article to an oxygen-containing
environment; heating the article to a temperature that allows oxygen to diffuse into
the article; soaking the article at the temperature for a time sufficient to oxidise
elemental metal at the surface and cooling the article to room temperature. The heating
and soaking take place at about 500°C, and the oxygen-containing environment is an
atmosphere of air.
[0005] US-A-5 316 594 relates to forming a hardened outer shell on a refractory titanium workpiece using
an argon-oxygen atmosphere containing from 1 to 3 mole percent of oxygen at a maximum
treatment temperature of 815°C.
[0006] EP-A-580 081 relates to the treatment of intermetallic compounds of titanium and aluminium in
an atmosphere containing 20% by volume of oxygen.
[0007] US-A-4 263 060 relates to the treatment of titanium articles with oxygen at a subatmospheric pressure.
[0008] WO-A-99/04055 (The University of Birmingham) discusses the need to provide engineering alloys of
titanium or zirconium with a hard case consisting of a region of relatively high hardness
maintained to a certain depth below the surface before dropping more steeply and then
gradually to the hardness of the untreated core material.
WO-A-99104055 discloses a method of case hardening an article formed of titanium, zirconium or
an alloy of titanium and/or zirconium in which the article is heat treated for a short
period of time, typically from 0.3 to 0.6 hour, in an oxidising atmosphere containing
both oxygen and nitrogen (typically air) at a temperature in the range of 700 to 1000°C
so as to form an oxide layer on the article, and then further heat treating the article
in a vacuum or in a neutral or an inert atmosphere at a temperature in the range of
700 to 1000°C so as to cause oxygen from the oxide layer to diffuse into the article.
[0009] According to
WO-A-99-04055 the case hardened article may then be surface treated by the method according to
WO-A-98/02595 (The University of Birmingham) so as to improve the tribological behaviour of the
article. This surface treatment comprises gaseous oxidation of the article at a temperature
in the range of 500 to 725°C for 0.1 to 100 hours, the temperature and time being
selected such as to produce an adherent surface component layer containing at least
50% by weight of oxides of titanium having a rutile structure and a thickness of 0.2
to 2 µm on a solid solution-strengthened diffusion zone wherein the diffusing element
is oxygen and the diffusion zone has a depth of 5 to 50 µm.
[0010] The dual step oxidation/diffusion treatment of the method according to
WO-A-99/04055 is difficult to control. A small variation in the amount of oxide formed in the first
oxidation step can result in a significant difference in the eventual hardness profile
at the end of the diffusion time in the vacuum or the neutral or inert atmosphere.
The method therefore relies entirely on empirical control, thereby causing difficulties
if it is required to treat a range of articles of different shapes and sizes.
[0011] According to
WO-A-2004/007788 there is provided a method of case hardening an article of titanium or a titanium-based
alloy, or of zirconium or a zirconium-based alloy, wherein the article is heat treated
at one or more temperatures in the range of 850°C to 900°C and at a pressure in the
order of atmospheric pressure in an oxygen diffusion atmosphere comprising (a) a carrier
gas which does not react chemically with the article in the said temperature range
and (b) molecular oxygen, wherein the concentration of oxygen in the oxygen diffusion
atmosphere is in the range of 10 volumes per million to 400 volumes per million.
[0012] The method according to
WO-A-2004/007788 is an improvement over prior methods because it enables a hard case to be formed
in a single treatment step at atmospheric pressure and is easy to control. In order
to optimise the method according to
WO-A-2004/007788 a balance has to be struck between the temperature at which the work is subjected
to the oxygen diffusion atmosphere and the duration of the treatment. In general,
temperatures in the order of 900°C favour shorter treatment times than temperatures
in the order of 800°C. We have discovered however, that at temperatures in the order
of 900 °C, some undesirable microstructural coarsening of the grains within the work
takes place. It is thus undesirable to exceed a temperature much above 850 °C. At
850 °C, we have found that total duration of the period of time throughout which the
work needs to be exposed to the oxygen diffusion for a case of adequate thickness
of some industrial uses can be unacceptably long and typically over 24 hours.
[0013] It is therefore an aim of the present invention to provide an alternative method
that is capable of ameliorating the above described difficulty when treating an article
of titanium or an alloy based on titanium.
[0014] According to the present invention there is provided a method of case hardening an
article of a metallic material selected from titanium and titanium - based alloys,
wherein the article is heat treated at a pressure in the range of 0.5 to 2 bar and
a temperature in the range of 750 to 870 °C in a diffusion atmosphere comprising (a)
carrier gas which does not react chemically with the article in the said temperature
range and (b) as active gas, wherein the concentration of the active gas in the diffusion
atmosphere is in the range of 20 to 400 volumes per million, and wherein the active
gas is carbon monoxide.
[0015] The carbon monoxide concentration in the diffusion atmosphere is preferably in the
range of 30 to 100 volumes per million. Reducing the carbon monoxide concentration
below 30 parts per million can increase the time it takes to form a hard case of given
depth. Increasing the concentration of carbon monoxide above 100 volumes per million
does not appear to increase significantly the rate of formation or the ultimate depth
of the case but it does have the effect of increasing the depth of a ceramic layer
formed on the surface of the work by virtue of the active gas. Concentrations of carbon
monoxide above 400 parts per million can result in the formation of an impermeable
surface layer that prevents the achievement of an adequate case depth.
[0016] A further advantage of the method according to the present invention is that a wear-resistant
ceramic layer can be formed at the surface of the work. We have been able to form
a uniform ceramic layer approximately 6 µm thick when subjecting a work piece of a
titanium - based alloy containing 6% by weight of aluminium and 4% by weight of varadium
as the sole alloying elements to an argon atmosphere containing 100 volumes per million
of carbon monoxide for a period of 24 hours at a temperature of 850°C. Below this
layer the upper 15 to 20 µm of the diffusion zone had a fine lamellar structure.
[0017] The term "titanium-based alloy" as used herein has its usual meaning. That is an
alloy containing more than 50% by weight of titanium. Typical alloying elements for
use in titanium-based alloys include vanadium and aluminium.
[0018] The carrier gas is preferably a noble gas such as helium, xenon, neon or argon, or
a mixture of one or more such noble gases. Argon is particularly preferred. Other
gases may be included if they do not have any marked adverse affect on the required
metallurgical engineering properties of the article. For example, traces of nitrogen
at the parts per million level are typically found in commercially available argon
and can be tolerated in the method according to the invention.
[0019] The method according to the invention is preferably performed at a pressure that
is essentially the same as the prevailing atmospheric pressure, i.e. at a pressure
in the range of 0.9 to 1.2 bar.
[0020] The duration of the heat treatment is preferably in the range of 12 to 24 hours.
[0021] The method according to the present invention is particularly useful in case hardening
engineering components or other articles formed of commercially pure grades of titanium,
of titanium-based alloys (α, α+β, or β alloys).
[0022] When the article is required to have enhanced fatigue properties, it may be subjected
after heat treatment to a mechanical surface treatment, such as shot peening.
[0023] The method according to the present invention will now be further described with
reference to the following Examples and to the accompanying drawings, in which:
Figure 1 is a graph showing the Vickers hardness profile and case depth of first samples
of titanium alloy at different carbon monoxide concentrations in case hardening treatment;
Figure 2 is a similar graph to Figure 1 but showing the relationship between case
depth and diffusion temperature for a second sample of titanium alloy.
Figure 3 is a graph comparing the hardness profiles of specimens of titanium alloy
treated in difference case hardening atmospheres:
Figure 4 is a graph comparing the dry wear properties of a specimen of a titanium
alloy case hardened according to the invention with those of a case hardened steel.
Figure 5 is a graph comparing the dry wear properties of a specimen of a titanium
alloy case hardened according to the invention with those of a case hardened steel.
Article 1. Examples
[0024] In the following examples, samples were treated in a small Boye pit furnace that
had previously been used for carburising treatments. It was therefore thoroughly burnt
out first, together with its loading jig, to ensure that no residues - particularly
carbon - were present that might affect the results. This was done by passing carbon
dioxide-free air through the furnace at 850°C for some hours while the carbon dioxide
was monitored. Burnout was considered complete when the monitored carbon dioxide concentration
began to fall.
[0025] The samples of the titanium-based alloy were in the form of polished cubes, 10mm
per side. They were placed in the pit furnace at ambient temperature. The furnace
was then heated under a flow or argon. When the processing temperature was reached,
the processing gas mixture was introduced. At the end of the processing time the atmosphere
was replaced by argon and the furnace cooled to below 150 °C before the samples were
removed.
[0026] Because of the very small flow rate of addition gas(es) required, it proved impossible
to achieve a stable addition gas concentration using pure addition gases and a Tylan
General DynaMass Flow control system. Premixed cylinders of standard gases were therefore
used to supply the addition gas to the mixer.
[0027] Preliminary screening runs at 850 °C for 24 hours to compare the method according
to the invention (using carbon monoxide as the active gas) with that that according
to
WO-A-2004/007788 (using oxygen as the active gas) were performed. In addition, experiments were performed
using carbon monoxide as the active gas and in supplementing the active gas with nitrogen
gases or mixtures of gases containing oxygen, nitrogen and carbon indicated that carbon
monoxide was found to be the most effective active gas. A range of addition levels,
treatment temperatures and times was investigated. The composition of the near surface
layers was analysed by x-ray diffraction.
[0028] The active gas level, as measured in the outlet stream, varied slightly during a
given treatment so all the results below are experienced with reference to the average
level over the treatment period.
Example 1
[0029] In this example, the effect of carbon monoxide in an argon diffusion atmosphere for
treatments carried out at a temperature of 850 °C and at atmospheric pressure (1 bar)
for 24 hours, was investigated. Results were obtained for different carbon monoxide
concentration is in the range of 30 parts by volume (volumes) per million to 80 parts
by volume per million are shown graphically in Figure 1. The case depth and hardness
were measured by conventional methods. The depth of the case was deemed to be the
thickness of the layer having a hardness above 400HV (Vickers Hardness).
[0030] It was observed that a sample treated at a carbon monoxide concentration of 78ppm
had a distinct ceramic surface layer. Such a layer confers improved wear-resistance
characteristics upon the case hardened article. No such layer was observed on the
samples treated at a carbon monoxide concentration of 45ppm or less.
[0031] The observed variations in both the hardness and the case depth are within experimental
error. Within the range of carbon monoxide concentrations investigated, the case depth
and hardness did not vary much. Forming a ceramic layer is believed to be advantageous
because it increases the wear resistance. Once the carbon monoxide concentration is
high enough to form a ceramic layer on the surface, the underlying diffusion zone
is unaffected by further increases in the carbon monoxide concentration in the treatment
atmosphere. The thickness of the ceramic layer does however increase but this is believed
not to be detrimental to at least some engineering applications even though the layer
may be brittle.
Example 2
[0032] Samples were treated for 24 and 48 hours at 800°C using a carbon monoxide concentration
of 55 volumes per million. The resultant case depths were 0.13 and 0.18mm respectively,
This variation of case depth with time is exactly in agreement with that predicted
by Fick's law.
Example 3
[0033] Samples were treated for 24 hours using a carbon monoxide concentration of 50 volumes
per million and temperatures of 750°C, 800°C and 850°C in accordance with the invention,
and 900 °C by way of comparison.
[0034] The resultant case depths obtained are shown graphically in Figure 2. Case depth
is shown to increase with temperature. The results obtained were corrected for the
small differences from the nominal 50 volumes per million carbon monoxide level in
the measured carbon monoxide concentrations.
[0035] Another effect of the treatment is to tend to cause structural coarsening. Such coarsening
was not significant for the treatment temperatures of 750 °C, 800 °C and 850 °C but
was manifest in the samples treated at 900 °C. As a result the samples treated at
900 °C would have been unsuitable for many engineering uses because the structural
coarsening inevitably lowers core strength. This would be particularly a problem for
larger engineering components that require a deeper case than in the samples produced
in accordance with this example.
Example 4
[0036] Test specimens of the T. - 6AL - 4V alloy were produced by heat treatment for 24
hours at 850 °C and atmospheric pressure in first a gas mixture of 50 parts by volume
(volumes) per million of oxygen in argon, secondly 80 parts by volume (volumes) of
carbon monoxide in argon, and thirdly 25 parts by volume carbon dioxide in argon.
The concentrations were chosen to ensure that a thin ceramic surface layer was formed
on each test specimen.
[0037] The treated specimens were subjected to dry wear tests on a pin-disc machine employing
a stationary vertical bar and a rotary disc. The heat treated specimen is attached
to the vertical bar and the disc rotated. The disc was made from a cold working tool
steel hardened and tempered to 58RC. The disc brings a high pressure (approximately
4N/mm
2 to bear on the sample. Resultant marks on the sample were then analysed by methods
well known in the art. The hardness of each specimen was also measured. The results
obtained are shown graphically in Figures 3 and 4. Figure 3 shows that the carbon
monoxide - treated samples had a significantly harder case than either the carbon
dioxide - treated sample or the oxygen - treated sample. Figure 4 shows that the wear
rate of the carbon monoxide-treated specimen is half that of the oxygen-treated specimen
with the carbon dioxide treated specimen lying between them.
Example 6
[0038] The dry wear of a carbon monoxide treated specimen of Ti-Al6-V4 produced under the
same conditions as the corresponding specimen of Figure 4 was compared to that of
an optimally carburised steel (Mn20Cr5, carburised to 0.8% by weight carbon and a
total case depth of 0.65mm, and direct oil quenched from 850 °C). The results are
shown graphically in Figure 5. The wear is an order of magnitude less for the titanium
specimen from the steel.
1. A method of case hardening an article of a metallic material selected from titanium,
and titanium-based alloys, wherein the article is a heat treated at a pressure in
the range of 0.5 to 2 bar and a temperature in the range of 750 °C to 870 °C in a
diffusion atmosphere comprising (a) carrier gas which does not react chemically with
the article in the said temperature range and (b) as active gas, wherein the concentration
of the active gas in the diffusion atmosphere is in the range of 20 to 400 volumes
per million, and wherein the active gas is carbon monoxide.
2. A method according to claim 1, wherein the carbon monoxide concentration in the diffusion
atmosphere is in the range of 30 to 100 volumes per million.
3. A method according to claim or claim 2, wherein a wear-resistant ceramic layer is
formed in the heat treatment at the surface of the article.
4. A method according to any one of the preceding claims, wherein the titanium-based
allow is an alloy of titanium with 4% by weight of vanadium and 6% by weight of aluminium.
5. A method according to any one of the preceding claims, wherein the duration of the
heat treatment is in the range of 12 to 24 hours.
6. A method according to any one of the preceding claims, wherein the article is an engineering
component.
7. A method according to any one of the preceding claims, wherein the pressure is atmospheric
pressure.
8. A method according to any one of the preceding claims, wherein the carrier gas is
argon.
9. A method according to any one of the preceding claims, wherein the carrier gas is
one or more of the following gases:
helium, neon, krypton and xeon.
10. A method according to any one of the preceding claims, wherein the diffusion atmosphere
is essentially free of molecular nitrogen.