BACKGROUND OF THE INVENTION
1. Field of the Invention
[0001] The present invention relates to a method of improving physical properties of titanium
alloys and, more specifically, a method of increasing thermal conductivity and reducing
electrical resistivity of articles made of titanium-based compositions.
2. Description of the Background Art
[0002] Titanium alloys offer attractive physical and mechanical property combinations that
provide significant weight savings in various industries such as aerospace and space.
Thermal conductivity of titanium alloys, however, is low compared to other structural
metals such as steel and aluminum. Low thermal conductivity of titanium alloys affects
heating rates and obtainable cooling rates after processing and heat treatments. Another
drawback of titanium alloys is their high electrical resistivity compared to steel
and aluminum. High electrical resistivity limits the use of titanium alloys as electrical
conductors. There is a need, therefore, for a new and improved method of increasing
thermal conductivity and reducing electrical resistivity of conventional titanium
alloys such as Ti-6AI-4V without debits in mechanical properties, specifically tensile
elongation and fatigue. The method of the present invention meets this need.
BRIEF SUMMARY OF THE INVENTION
[0003] In accordance with the new and improved method of the present invention, titanium
boride (TiB) precipitates are incorporated into a titanium alloy and the alloy is
then subjected to controlled deformation to orient the TiB precipitates in the direction
of interest to achieve improvements in thermal and electrical properties. The controlled
deformation of the alloy to orient the TiB precipitates is accomplished by hot metalworking.
[0004] The boron is introduced into the titanium alloy composition to produce TiB precipitates
by any suitable method, such as casting, cast-and-wrought processing, powder metallurgy
techniques such as gas atomization and blended elemental approach. Hot metalworking
operations such as forging, rolling and extrusion can be used to accomplish alignment
of the TiB precipitates along the direction of metal flow.
[0005] As an illustrative example, the method of the present invention may be used to increase
thermal conductivity and reduce electrical resistivity of multi-component titanium
alloys such as Ti-6AI-4V (Ti-64) and Ti-6Al-2Sn-4Zr-2Mo(Ti-6242).
BRIEF DESCRIPTION OF THE DRAWINGS
[0006]
FIGURE 1 is a pre-alloyed powder metallurgy process flowchart for fabrication of TiB
incorporated titanium alloy articles;
FIGURE 2a is a microstructure of Ti-6A1-4V-1B showing a cross-section of as-atomized
pre-alloyed powder particle;
FIGURE 2b is a microstructure of Ti-6A1-4V-1B after powder consolidation via hot isostatic
pressing;
FIGURE 3 shows microstructures of Ti-6A1-4V-1B forging article at different locations;
FIGURE 4a is a microstructure of an extrusion article made out of pre-alloyed powder
of Ti-6A1-4V-1B revealing TiB precipitates (dark phase) aligned along the extrusion
axis.
FIGURE 4b is a transverse micrograph of FIGURE 4a showing hexagonal cross-sections
of TiB precipitates;
FIGURE 5 is a graph comparing the thermal conductivity of Ti-6A1-4V-1B (labeled as
nano Ti-64) forging and extrusion articles with that of a Ti-6A1-4V article;
FIGURE 6 is a graph comparing the thermal conductivity of Ti-6A1-2Sn-4Zr-2Mo-1B forging
article with that of the baseline Ti-6A1-2Sn-4Zr-2Mo article;
FIGURE 7 is a graph comparing the electrical resistivity of Ti-6A1-4V-1B (labeled
as nano Ti-64) forging article with that of a Ti-6A1-4V article; and
FIGURE 8 is a graph comparing the electrical resistivity of Ti-6A1-2Sn-4Zr-2Mo-1B
forging article with that of the baseline Ti-6A1-2Sn-4Zr-2Mo article.
DETAILED DESCRIPTION OF THE INVENTION
[0007] Methods of increasing thermal conductivity and reducing electrical resistivity of
multi-component titanium alloys such as Ti-6AI-4V (Ti-64) and Ti-6Al-2Sn-4Zr-2Mo (Ti-6242)
are described hereinafter. These methods encompass two important elements:
- 1) Incorporation of TiB precipitates into the titanium alloy matrix; and
- 2) Alignment of TiB precipitates in the direction of interest via hot metalworking.
[0008] Introduction of boron into the titanium alloy composition to produce TiB precipitates
can be accomplished by several different methods, such as casting, cast-and-wrought
processing, powder metallurgy techniques such as gas atomization and blended elemental
approach. The boron may be added to the titanium alloy in the liquid state, wherein
the boron is completely dissolved in the liquid titanium alloy. The boron may be added
to the titanium alloy through intermixing of solid powders, as by powder metallurgy.
Regardless of the process used to add the boron to the titanium alloy, the boron may
be added as elemental boron, TiB2 or as any appropriate master alloy containing boron.
The boron may be added in amounts in the range from 0.01 % to 18.4%, by weight. More
preferably, the boron is added to the titanium alloy in amounts ranging from 0.01%
to 2%, by weight, depending on titanium alloy composition.
[0009] Hot metalworking operations such as forging, rolling, and extrusion can be used to
accomplish alignment of TiB precipitates along the direction of metal flow.
[0010] The present method can be practiced by the gas atomization powder metallurgy process
flowchart shown in Figure 1. The boron is added to the molten titanium alloy and the
liquid melt is inert gas atomized to obtain titanium alloy powder. Each powder particle
contains needle-shaped TiB precipitates distributed uniformly and in random orientations.
An example microstructure of Ti-6AI-4V-1B powder particle cross-section which contains
6 vol. % of TiB (dark phase) is shown in Figure 2a. Titanium alloy powder is consolidated
using a conventional technique such as hot isostatic pressing (HIP) to obtain a fully
dense powder compact. In as-compacted condition, the TiB precipitates are still in
random orientations distributed uniformly in the titanium alloy matrix. An example
microstructure of Ti-6A1-4V-1B powder after HIP is shown in Figure 2b.
[0011] The powder compact is then subjected to a metalworking operation such as forging,
rolling, or extrusion. Hot working parameters commonly practiced for producing titanium
alloy articles were found to produce the desired alignment of TiB precipitates along
the direction of metal flow. As an illustrative example, the hot working parameters
are as follows:
Micrographs at different locations of a Ti-6A1-4V-1B article made via forging of a
powder compact of 16" height × 3.5" diameter into a disk of 3" height × 8" diameter
in the temperature range 1750 - 2200°F and a ram speed of 40 inch/min are shown in
Figure 3. Alignment of TiB needle-shaped precipitates (dark phase) along the radial
orientation after forging is evident in Figure 3. Another example microstructure of
a Ti-6AI-4V-IB article that was produced by extrusion processing of a 3" diameter
powder compact into a bar of 0.75" diameter at 2000°F and a ram speed of 100 inch/min
is shown in Figure 4, which reveals alignment of TiB precipitates (dark phase) along
the extrusion axis.
[0012] Thermal and electrical properties of several TiB incorporated titanium alloy articles
(chemical compositions given in Table 1) were evaluated. Identical testing was performed
on titanium alloys without TiB precipitates for comparison. Thermal conductivity testing
was performed in accordance with the standard test method ASTM E1461 and electrical
resistivity was determined per the standard method ASTM B84.
Table 1: Chemical compositions (in weight percent) of titanium alloy articles tested.
| |
|
|
Composition in Weight Percent |
| |
|
|
|
|
|
|
|
|
|
|
|
|
|
| 1 |
Ti-64 |
Bar |
6.05 |
<0.005 |
0.004 |
0.153 |
0.0033 |
0.0031 |
0.115 |
|
|
|
|
4.18 |
|
balance |
| 2 |
NanoTi-64 |
Forging |
6.04 |
0.91 |
0.051 |
0.05 |
0.011 |
0.009 |
0.139 |
|
|
|
|
3.8 |
|
balance |
| 3 |
Nano Ti-64 |
Extrusion |
6.1 |
1.06 |
0,046 |
0.051 |
0.0042 |
0.016 |
0.122 |
|
|
|
|
4.2 |
|
balance |
| 4 |
Ti-6242 |
Bar |
6.1 |
<0.005 |
0.019 |
0.048 |
0.0051 |
0.021 |
0.132 |
2.08 |
0.031 |
0.066 |
1.16 |
|
4.16 |
balance |
| 5 |
Nano Ti-6242 |
gorging |
6.11 |
1.03 |
0.109 |
0.046 |
0.0049 |
0.0068 |
0.108 |
2.11 |
0.045 |
0.1 |
1.88 |
|
4,43 |
balance |
[0013] Thermal conductivity of Ti-64-1B (labeled as nano Ti-64) forging and extrusion articles
is compared with that of Ti-64 article in Figure 5. Higher thermal conductivity of
nano Ti-64 forging in the radial orientation and nano Ti-64 extrusion in the axial
orientation is evident compared to the baseline Ti-64 in the temperature range 70-1250°F.
[0014] Thermal conductivity data of Ti-6242-1B forging article is compared with that of
the baseline Ti-6242 article in Figure 6. Increased thermal conductivity compared
to the baseline is evident in this material system also. Increase in thermal conductivity
by up to 35% was recorded in articles with the TiB precipitates aligned along the
test direction.
[0015] Electrical resistivity of Ti-64-1B (labeled as nano Ti-64) forging article is compared
with that of Ti-64 article in Figure 7. Reduced electrical resistivity of nano Ti-64
forging in the radial orientation compared to the baseline Ti-64 in the temperature
range 70-1500°F is evident. Electrical resistivity data of Ti-6242-1B forging article
is compared with that of the baseline Ti-6242 article in Figure 8. Reduced electrical
resistivity compared to the baseline is evident in this material system also. Reduction
in thermal conductivity by up to 20% was recorded in articles with the TiB precipitates
aligned along the test direction.
[0016] In addition to the improvements in thermal and electrical properties, TiB incorporated
titanium alloys offer several benefits in mechanical properties without debits in
ductility and fatigue. For example, room temperature tensile properties of boron-modified
titanium alloy articles (referred to as nano version) are compared with those of baseline
titanium alloys in Table 2. In nano titanium alloys, the tensile yield strength and
ultimate strength were higher by 25%, modulus of elasticity is higher by 20%, while
maintaining tensile elongations equivalent to their baseline titanium alloys.
[0017] Table 2: Typical room temperature tensile properties of boron-modified titanium alloy articles
referred to as nano alloys. TYS: Tensile Yield Strength, UTS: Ultimate Tensile Strength,
TE: Tensile Elongation, and TM: Tensile Modulus (modulus of elasticity in tension).
| 1 |
Ti-64 |
Bar |
Axial |
120 |
130 |
13 |
16.9 |
| 2 |
Nano Ti-64 |
Forging |
Radial |
140 |
154 |
13 |
18.6 |
| 3 |
Nano Ti-64 |
Extrusion |
Axial |
152 |
163 |
10 |
19.9 |
| 4 |
Ti-6242 |
Bar |
Axial |
131 |
141 |
13 |
16.5 |
| 5 |
Nano Ti-6242 |
Forging |
Radial |
161 |
170 |
9 |
19.1 |
[0018] While the invention has been described in connection with what is presently considered
to be the most practical and preferred embodiments, it is to be understood that the
invention is not to be limited to the disclosed embodiments, but on the contrary,
is intended to cover various modifications and equivalent arrangements included within
the spirit and scope of the appended claims.
1. A method of increasing thermal conductivity and decreasing electrical resistivity
of a titanium alloy comprising:
introducing boron into the titanium alloy to produce TiB precipitates, and
aligning the TiB precipitates in a direction of metal flow by hot metalworking.
2. The method of claim 1 wherein the TiB precipitates are produced by casting, cast-and-wrought
processing, or powder metallurgy techniques.
3. The method of claim 1 wherein the hot metalworking is forging, rolling or extrusion.
4. The method of claim 1 wherein the titanium alloy is a multi-component material such
as Ti-6AI-4V or Ti-6Al-2Sn-4Zr-2Mo.
5. The method of claim 1 wherein the boron is approximately 0.01% to 18.4% by weight
of the titanium alloy.
6. The method of claim 1 wherein the boron is added to a molten titanium alloy, and the
resulting liquid melt is inert gas atomized to produce a titanium alloy powder containing
needle shaped TiB precipitates distributed uniformly and in random orientations.
7. The method of claim 6 wherein the titanium alloy powder is consolidated by hot isostatic
pressing.
8. The method of claim 3 wherein the hot metalworking is forging of a powder compact
at a temperature of approximately 1750-2000°F and a ram speed of approximately 40
inch./min.
9. The method of claim 3 wherein the hot metalworking is extrusion processing of a powder
compact at a temperature of approximately 2000°F and a ram speed of approximately
100 inch./min.
10. The method of claim 1 wherein there is no degradation of the ductility or fatigue
of the titanium alloy.