FIELD OF THE INVENTION
[0001] The present invention relates to a titanium plate, and more particularly to a titanium
plate excellent in workability.
RELATED ART
[0002] Conventionally, titanium materials such as titanium alloys and pure titanium have
been widely used for sports and leisure equipment, medical devices, various members
for plants, aviation and space related equipment, and the like because titanium materials
are generally light and high in strength compared with iron-based materials such as
iron and alloys thereof.
In addition, since titanium materials are also excellent in corrosion resistance and
the like, they are used, for example, for plate materials of plate heat exchangers,
muffler members of motorcycles, and the like.
For producing such products, a plate formed from a titanium material (titanium plate)
is subjected, for example, to various workings involving plastic deformation such
as bending and drawing.
Therefore, a titanium plate is required to have excellent workability in fabrication
such as drawing, in order to be subjected to such various applications.
[0003] However, recently, as a result of requirements for the reduction in the thickness
of a titanium plate to reduce material cost or the like, improvement in strength has
increasingly been required.
That is, simultaneously satisfying formability and strength, which are the properties
in a trade-off relation, is increasingly required.
[0004] Titanium sponge used as a raw material of the titanium plate or the like is produced
by the Kroll process, and for example, pure titanium is produced by a method of subjecting
the titanium sponge obtained by the Kroll process to arc melting or the like to obtain
an ingot.
Pure titanium is classified according to the content of elements other than titanium
such as iron and oxygen in the Japanese Industrial Standard (JIS), in which JIS class
1, JIS class 2, JIS class 3, JIS class 4, and the like are specified.
With respect to the material properties thereof, JIS class 1 titanium in which the
content of iron and the like is low has the lowest strength and excellent formability.
It is known that JIS class 2 titanium has higher strength than JIS class 1 titanium,
and JIS class 3 titanium has higher strength than JIS class 2 titanium.
On the other hand, JIS class 2 titanium has lower formability than JIS class 1 titanium,
and JIS class 3 titanium has lower formability than JIS class 2 titanium, and it is
not easy to obtain a good formed article by subjecting a titanium plate of JIS class
2 or 3 to drawing or the like.
[0005] With respect to the above subject, the following Patent Documents 1 to 3 describe
that formability is improved by controlling the content of components other than titanium
such as iron in a titanium material to the range below a predetermined level.
However, sufficient strength cannot be expected in the titanium materials described
in these Patent Documents.
Further, since the reduction reaction in the Kroll process as described above is typically
performed discontinuously (batch wise) in a carbon steel or iron alloy vessel, the
resultant titanium sponge contains higher amount of iron in the region close to the
wall of the vessel than in the region close to the central part of the vessel.
Because of this, if the iron content is limited, for example, to a range of 0.035%
to 0.100% as described in Patent Document 3, the titanium in the central part of the
vessel must be used, which limits a material to be used and poses a risk of cost increase.
[0006] Note that in the following Patent Documents 4 and 5, a higher content of iron is
permitted compared with the inventions described in Patent Documents 1 to 3, but it
cannot be said that the materials in Patent Documents 4 and 5 have sufficient formability.
PRIOR ART DOCUMENT
PATENT DOCUMENT
[0007]
Patent Document 1: Japanese Patent Application Laid-open No. Sho-63-60247
Patent Document 2: Japanese Patent Application Laid-open No. Hei-9-3573
Patent Document 3: Japanese Patent Application Laid-open No. 2006-316323
Patent Document 4: Japanese Patent Application Laid-open No. 2008-127633
Patent Document 5: Japanese Patent Application Laid-open No. 2002-180166
DISCLOSURE OF THE INVENTION
PROBLEMS TO BE SOLVED BY THE INVENTION
[0008] An object of the present invention is to provide a titanium plate having high strength
and excellent workability.
MEANS FOR SOLVING PROBLEMS
[0009] As a result of extensive and intensive investigations to achieve the above-described
object, the present inventors have found that a titanium plate having high strength
and excellent workability can be formed by forming the titanium plate so that it may
have a predetermined content of iron and oxygen and crystal grains may be in a predetermined
state, and such a finding has resulted in completion of the present invention.
[0010] Specifically, the present invention related to a titanium plate for achieving the
above object is
characterized in that the titanium plate has, by mass, an iron content of more than 0.10% and less than
0.60%, an oxygen content of more than 0.005% and less than 0.10%, a carbon content
of less than 0.015%, a nitrogen content of less than 0.015%, a hydrogen content of
less than 0.015%, with the balance being titanium and unavoidable impurities, wherein
a two-phase structure of an α-phase and a β-phase are formed, and the β-phase is formed
so as to have a circle-equivalent average grain size of 3 µm or less.
ADVANTAGES OF THE INVENTION
[0011] The present invention can provide a titanium plate having high strength and excellent
workability.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012]
Figure 1 is a photomicrograph showing the microstructure of the titanium plate of
Example 7.
Figure 2 is a graph showing the relationship between the circle-equivalent average
grain size of the β-phase and the Erichsen value.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0013] Hereinafter, a preferred embodiment of the present invention will be described.
The titanium plate in the present embodiment is formed from a titanium material containing
the following components, wherein a two-phase structure of an α-phase and a β-phase
is formed, and the β-phase is formed so as to have a circle-equivalent average grain
size of 3 µm or less.
The titanium material has, by mass, an iron (Fe) content of more than 0.10% and less
than 0.60%, an oxygen (O) content of more than 0.005% and less than 0.10%, a carbon
(C) content of less than 0.015%, a nitrogen (N) content of less than 0.015%, a hydrogen
(H) content of less than 0.015%, with the balance being titanium (Ti) and unavoidable
impurities.
[0014] As described above, the iron (Fe) is contained in the titanium material in a content,
by mass, of more than 0.10% and less than 0.60%.
Fe is a β-stabilizing element, and although a part of Fe forms a solid solution, most
of Fe forms a β-phase.
Further, it is known that Fe is present as TiFe by heat treatment or the like, which
suppresses crystal grain growth.
Therefore, it has been conventionally believed that when the Fe content in a titanium
material is increased, the crystal grain size in the α-phase formed in the titanium
plate is reduced, which can improve the strength of the titanium material and the
workability of polishing work, but reduces an index showing ductility (formability)
such as the Erichsen value.
[0015] However, as described below in detail, even if the Fe content in a titanium plate
is increased, the reduction in ductility can be suppressed and the improvement in
strength can be achieved by setting the O content to a predetermined value and adjusting
the size of a β-phase to a predetermined value.
[0016] The Fe content of the titanium material forming the titanium plate of the present
embodiment is more than 0.10% and less than 0.60% by mass because if the Fe content
is 0.10% or less, it may be impossible to impart sufficient strength to the resultant
titanium plate.
On the other hand, if the content is 0.60% or more, a reduction in ductility may occur
even if the O content in the titanium material is set to a predetermined value, which
may lead to reduction in the formability of the titanium plate.
[0017] Note that in the Kroll process, the titanium material having an iron content of 0.60%
or more is generally formed only in a small region near the vessel.
Therefore, in the present embodiment, most of the titanium sponge obtained by the
Kroll process can be used as the raw material because, in the titanium plate of the
present embodiment, the upper limit of the iron content as its component is set to
0.60% by mass.
That is, the titanium plate of the present embodiment can be said to be suitable as
a consumption material used for forming a formed article in that the raw material
can be easily acquired.
[0018] The oxygen (O) is contained in the titanium material in a content by mass of more
than 0.005% and less than 0.10%.
The O content of the titanium material forming the titanium plate of the present embodiment
is more than 0.005% and less than 0.10% by mass because if the O content is 0.10%
or more, the strength of the titanium plate may be excessively increased, and as a
result, good formability may not be achieved even if the β-phase is adjusted.
[0019] Further, it is important that carbon (C), nitrogen (N), and hydrogen (H) are each
contained in a content corresponding to JIS class 2 or less for the purpose of ensuring
good workability in fabrication.
More specifically, it is important that the contents of C, N, and H are each less
than 0.015% by mass.
Further, it is preferred that the content of C be 0.01% or less, the content of N
be 0.01% or less, and the content of H be 0.01% or less.
Although a lower limit is not to be set for the above contents of C, N, and H from
the point of view of the workability of a titanium plate, the production cost of the
titanium plate may be significantly increased if the content is intended to be extremely
reduced.
From the point of view of preventing such cost increase, the C content is preferably
0.0005% or more, the N content is preferably 0.0005% or more, and the H content is
preferably 0.0005% or more.
[0020] Conventionally, a titanium plate for which good workability is required in fabrication
generally includes only an α-phase because such a titanium plate is made from a titanium
material having a low iron content corresponding to JIS class 1 or JIS class 2.
Since the larger the α-grain size, the better the workability, it is important that
the titanium plate in the present embodiment has a two-phase structure of α + β, in
which the β-phase has a circle-equivalent average grain size of 3 µm or less.
An index which shows workability, such as the Erichsen value, can be improved by forming
a titanium plate so as to have such a structure.
[0021] If the circle-equivalent average grain size of the β-phase exceeds 3 µm, workability
could be reduced with the Erichsen value lowered, for example, to less than 10 mm.
This is because cracks are likely to occur at the boundary of the coarsened β-phase
and the α-phase due to stress concentration, which reduces the workability of the
titanium plate.
Although the lower limit of the circle-equivalent average grain size of the β-phase
is not particularly specified, but it is preferably 0.05 µm or more because the production
cost will be significantly increased in obtaining a titanium plate having a circle-equivalent
average grain size of less than 0.05 µm.
Note that the circle-equivalent average grain size of the β-phase can be determined
by a method described in "Examples" to be described below.
[0022] Note that these findings have been found by the inventors of the present application
by the following methods.
That is, cold-rolled plates each having a thickness of 0.5 mm were prepared on an
experimental basis in a small-sized vacuum arc melting furnace using plural types
of titanium materials each having a different iron content while changing annealing
conditions. Then, the resultant cold-rolled plates (titanium plates) were evaluated
for formability by the Erichsen test (details will be described in "Examples" to be
described below).
Then, it was found that the grain size of the β-phase is increased by, for example,
increasing the annealing time, and that the more the grain size of the β-phase is
increased, the smaller the Erichsen value becomes.
A crack was discovered at the interface between the coarse β-grain and the α-phase
by detailed investigation of the structure and fracture surface. Then, annealing conditions
were changed to reduce the grain size of the β-phase, and it was found that the reduction
in the grain size of the β-phase has increased the Erichsen value, indicating improvement
in formability.
In particular, it has been found that a circle-equivalent average grain size of the
β-phase of 3 µm is considered as a boundary, and that when the circle-equivalent average
grain size of the β-phase is 3 µm or less, a high strength titanium plate excellent
in workability can be obtained.
[0023] As shown in the description of the process for obtaining this finding, the grain
size of the β-phase can be adjusted by the iron content of the titanium material,
the final annealing temperature and the final annealing time during the titanium plate
production, and the like.
[0024] Hereinafter, these conditions in the method for producing a titanium plate will be
described.
Referring now to the conditions of the final annealing temperature and the final annealing
time during the titanium plate production, the crystal grain size can be reduced by
suppressing the growth of β-grains by decreasing the final annealing temperature.
Further, the crystal grain size can be reduced by suppressing the growth of crystal
grains by reducing the final annealing time.
[0025] More specifically, if the final annealing temperature is less than 550°C, the worked
structure after cold rolling may not be recrystallized, reducing formability.
On the other hand, if the temperature exceeds 800°C, the diffusion rate of iron in
titanium may be increased, coarsening the crystal grains of the β-phase.
Accordingly, the final annealing temperature is preferably any temperature in the
range of 550°C or more and 800°C or less.
[0026] Further, the final annealing time is determined by the above final annealing temperature,
the thickness of a titanium plate, the capacity of an annealing furnace, and the like.
Specifically, when the final annealing temperature is 650°C or more and 800°C or less,
the final annealing time is preferably longer than 0 minute and 15 minutes or less.
Note that since the structure is recrystallized during heating even in the case where
the final annealing is completed immediately after the temperature of the titanium
plate reached the above final annealing temperature, a risk of reducing formability
is low if the final annealing time exceeds at least 0 minute.
On the other hand, the upper limit value of the final annealing time is defined as
15 minutes in the above final annealing temperature because if the final annealing
is performed longer than 15 minutes, the crystal grains of the β-phase may be coarsened,
reducing the workability of the titanium plate.
[0027] Note that when the final annealing temperature is 550°C or more and less than 650°C,
the final annealing is preferably performed so that the following expression (1) may
be satisfied, wherein t (min) represents the annealing time and T (°C) represents
the annealing temperature.

(wherein, 550 ≤ T < 650)
[0028] A certain amount of time is required for recrystallization because recrystallization
proceeds only at a slow rate in such a temperature range.
Thus, improvement in the formability by recrystallization can be achieved by selecting
the conditions which satisfy the above expression (1).
[0029] However, if long-time annealing is performed in the case where the final annealing
temperature is more than 630°C and less than 650°C, the crystal grains of the β-phase
may be coarsened, reducing the workability of a titanium plate.
Therefore, it is preferred to perform the final annealing so that the following expression
(2) may be satisfied in this temperature region.

(wherein, 630 < T < 650)
[0030] Further, the annealing time is preferably 300 minutes or less in the case where the
final annealing temperature is in a temperature range of 550°C or more and 630°C or
less.
By selecting such conditions, it is possible to suppress the coarsening of the β-phase
in the structure to be formed in the titanium plate and impart good workability to
the titanium plate.
Note that if a final annealing time exceeding 300 minutes is provided in this temperature
range, the crystal grains of the β-phase may be coarsened, reducing the workability
of the titanium plate.
[0031] By employing the production conditions illustrated in the above, the grain size of
the β-phase in the titanium plate can be adjusted to a predetermined level or less,
thus obtaining a titanium plate excellent in strength and workability.
[0032] Note that although not described in detail here, known matters in conventional titanium
plates and titanium plate production methods can be employed in the titanium plate
of the present embodiment within the range which does not significantly impair the
effect of the present invention.
Examples
[0033] Next, the present invention will be described in more detail with reference to Examples,
but the present invention is not limited to these.
(Examples 1 to 22, Comparative Examples 1 to 3)
(Preparation of test pieces)
[0034] An ingot (140 mm in diameter) was prepared by small-sized vacuum arc melting, and
the ingot was heated to 1150°C and then forged to prepare a slab having a thickness
of 50 mm.
The slab was hot-rolled at 850°C to a thickness of 5 mm and then annealed at 750°C,
and the scale on the surface of the annealed slab was cut to prepare a plate material
having a thickness of 4 mm.
The plate material was further cold-rolled to prepare a plate-shaped sample (titanium
plate) having a thickness of 0.5 mm.
The titanium plate having a thickness of 0.5 mm was subjected to final annealing in
a vacuum atmosphere to prepare a test piece for evaluation.
In the final annealing, the crystal grain size of the test piece was adjusted by adjusting
the temperature (550°C or more and 800°C or less) and time (300 minutes or less).
(Measurement of components)
[0035] The amounts of iron and oxygen contained in the titanium plate were measured using
the plate material having a thickness of 4 mm from which the surface scale was cut.
The iron content was measured according to JIS H1614 and the oxygen content was measured
according to JIS H1620.
(Measurement of tensile strength)
[0036] Further, the tensile strength of the test piece (titanium plate) in which the crystal
grain size has been adjusted as described above was measured according to JIS Z 2241.
(Evaluation of workability)
[0037] Furthermore, the Erichsen value of the test piece (titanium plate) in which the crystal
grain size has been adjusted as described above was measured according to JIS Z2247
to evaluate the workability of the titanium plate.
(Investigation of structure)
[0038] The state of the microstructure of the titanium plate that was observed with a photomicrograph
is shown in Figure 1 (the microstructure of Example 7).
Since the β-phase appears black and the α-phase appears white in this structural photograph,
the photograph was subjected to binarization processing using image analysis software
to determine the average area of the β-phase, and the diameter of a circle having
the same area as the average area was determined by calculation to define a circle-equivalent
average grain size.
The results of the above are shown in Table 1.
[0039]
[Table 1]
|
Iron content (mass%) |
Oxygen content (mass%) |
Tensile strength (MPa) |
Erichsen value (mm) |
β-phase circle-equivalent average grain size (µm) |
Example 1 |
0.131 |
0.055 |
390 |
12.4 |
0.7 |
Example 2 |
0.131 |
0.055 |
400 |
12.1 |
0.9 |
Examples 3 |
0.131 |
0.055 |
375 |
11.9 |
1.1 |
Example 4 |
0.131 |
0.055 |
367 |
11.7 |
1.8 |
Comparative Example 1 |
0.131 |
0.055 |
434 |
9.5 |
3.3 |
Example 5 |
0.223 |
0.060 |
402 |
11.7 |
1.5 |
Example 6 |
0.223 |
0.060 |
417 |
11.5 |
1.4 |
Example 7 |
0.223 |
0.060 |
392 |
10.9 |
1.5 |
Example 8 |
0.223 |
0.060 |
383 |
11.2 |
2.4 |
Example 9 |
0.223 |
0.060 |
395 |
11.4 |
1.5 |
Comparative Example 2 |
0.223 |
0.060 |
434 |
9.0 |
3.5 |
Example 10 |
0.253 |
0.038 |
361 |
12.3 |
1.2 |
Example 11 |
0.253 |
0.038 |
371 |
12.1 |
0.9 |
Example 12 |
0.253 |
0.038 |
349 |
11.4 |
1.3 |
Example 13 |
0.253 |
0.038 |
332 |
11.2 |
2.0 |
Example 14 |
0.253 |
0.038 |
354 |
12.0 |
1.1 |
Example 15 |
0.377 |
0.066 |
424 |
11.7 |
2.0 |
Example 16 |
0.377 |
0.066 |
429 |
11.3 |
1.9 |
Example 17 |
0.377 |
0.066 |
420 |
10.8 |
2.1 |
Example 18 |
0.377 |
0.066 |
411 |
10.5 |
2.5 |
Comparative Example 3 |
0.377 |
0.066 |
450 |
7.9 |
3.9 |
Example 19 |
0.520 |
0.047 |
459 |
11.3 |
2.2 |
Example 20 |
0.520 |
0.047 |
471 |
11.0 |
2.0 |
Example 21 |
0.520 |
0.047 |
445 |
10.6 |
2.5 |
Example 22 |
0.520 |
0.047 |
435 |
10.3 |
2.8 |
[0040] In Table 1, the iron content and the oxygen content in Examples 1 to 4 are the same
as those in Comparative Example 1, but the circle-equivalent average grain size of
the β-phase was adjusted by the difference between the annealing conditions, and the
smaller the circle-equivalent average grain size of the β-phase, the larger the Erichsen
value.
In addition, the same tendency is observed in the other Examples and Comparative Examples,
and it is understood that the present invention can provide a titanium plate having
high strength and excellent workability also from Figure 2 showing the relationship
between the circle-equivalent average grain size of the β-phase and the Erichsen value
in Table 1.