The present invention relates to a continuous casting device and a continuous casting method for titanium ingots and titanium alloy ingots capable of respectively producing titanium ingots and titanium alloy ingots by continuous casting.
Continuous casting for producing ingots made of titanium or a titanium alloy has conventionally been performed by injecting titanium or a titanium alloy melted by plasma arc melting into a bottomless mold and while solidifying it, withdrawing the resulting ingot downward. As disclosed in Patent Document 1, a molten metal obtained by melting titanium or a titanium alloy is temporarily retained in a retainer called “hearth” and the molten metal is injected into the mold from this hearth.
The hearth is usually a container made of copper and equipped, inside or outside thereof, with a forced cooling mechanism such as water cooing hole in order to prevent titanium from being contaminated. In addition, in order to prevent the molten metal from solidifying in the hearth, the surface of the molten metal in the hearth is heated. The purpose of providing such a hearth is to make the molten metal temperature uniform, prevent the raw material which has remained without being melted from entering the mold, precipitate inclusions and separate them from the molten metal, and reduce variation in the injection amount of the molten metal into the mold due to variation in a melted amount of the raw material.
When the hearth has a too large capacity or the number of the hearths is too large, however, the molten metal solidifies at the end portion of the hearth or at a channel provided between hearths. In addition to this problem, an increase in the amount of titanium which has remained in the hearth or an increase in heat loss due to heat dissipation from the hearth leads to a cost increase. A hearth suitable for raw materials or the purpose of use should therefore be employed.
When titanium ingots are produced by continuous casting, an amount of inclusions is small so that increasing the capacity of a hearth and thereby prolonging the retention time of a molten metal for the purpose of precipitating the inclusions is not necessary. Rather in this case, it is desired to decrease the capacity of the hearth to suppress heat dissipation from the hearth and reduce an electric power consumption rate by plasma arc for heating the surface of the molten metal. On the other hand, when titanium alloy ingots are produced by continuous casting, an amount of inclusions is large so that increasing the capacity of a hearth and thereby securing a sufficient retention time of a molten metal for the purpose of precipitating the inclusions is required. The term “electric power consumption rate” is an electric energy necessary per unit production amount of a product and it is an objective indicator of production efficiency.
As described above, there is a difference in the suitable shape of a hearth between continuous casting for titanium ingots and continuous casting for titanium alloy ingots. It has therefore been conventionally difficult to produce titanium ingots and titanium alloy ingots respectively in a single facility by continuous casting.
An object of the present invention is to provide a continuous casting device and a continuous casting method for titanium ingots and titanium alloy ingots capable of continuously casting and thereby producing titanium ingots and titanium alloy ingots respectively in a single facility.
In the present invention, there is provided a continuous casting device for titanium ingot and titanium alloy ingot which injects a molten metal having titanium or a titanium alloy melted therein into a bottomless mold via a plurality of hearths and while solidifying the molten metal, withdraws the resulting ingot downward, and thereby produces an ingot made of the titanium or titanium alloy by continuous casting. This device is characterized in that as at least some of the hearths, hearths for titanium to be used at the time of continuous casting for titanium ingot and hearths for titanium alloy to be used at the time of continuous casting for titanium alloy ingot can be used exchangeably. The latter hearths are greater in number and also greater in total capacity than the former hearths.
In the present invention, there is also provided a continuous casting method for titanium ingot and titanium alloy ingot including injecting a molten metal having titanium or a titanium alloy melted therein into a bottomless mold via a plurality of hearths and while solidifying the molten metal, withdrawing the resulting ingot downward. This method is characterized in that as at least some of the hearths, hearths for titanium to be used at the time of continuous casting for titanium ingot and hearths for titanium alloy to be used at the time of continuous casting for titanium alloy ingot can be used exchangeably; the latter hearths are greater in number and also in total capacity than the hearths for titanium; and the hearths for titanium alloy are exchanged with the hearths for titanium at the time of continuous casting for titanium ingot, while the hearths for titanium are exchanged with the hearths for titanium alloy at the time of continuous casting for titanium alloy ingot.
The continuous casting device and continuous casting method for titanium ingots and titanium alloy ingots according to the present invention make it possible to produce titanium ingots and titanium alloy ingots respectively in a single facility by continuous casting.
a) is a top view showing production of titanium ingots by continuous casting using a continuous casting device according to Third Embodiment and
Preferred embodiments of the present invention will hereinafter be described referring to drawings.
A continuous casting device 1 for titanium ingots and titanium alloy ingots (continuous casting device) 1 according to First Embodiment of the present invention has, as shown in
The mold 2 is equipped, inside or outside thereof, with a forced cooling mechanism such as water cooling hole and at the same time, it is a bottomless container made of copper. A molten metal 31 obtained by melting titanium (pure titanium) or a titanium alloy is injected into this container. The molten metal 31 injected into the mold 2 is solidified by cooling into an ingot 32. The mold 2 is constituted so as to be exchangeable in accordance with the shape of an ingot 32 to be produced by casting.
Since the mold 12 and the mold 22 have the same gravity center position, the peripheries of these molds 2 can be monitored in the same direction from the outside of the chamber. This facilitates monitoring of working conditions.
The plurality of hearths 3 inject the molten metal 31 into the mold 2. The hearths 3 have a raw material introduction hearth 3a into which a raw material of the ingot 32 is introduced and a molten metal transfer hearth 3b placed on the downstream side of the raw material introduction hearth 3a. Two hearths 3 adjacent to each other are linked by a channel 8. In the present embodiment, all the hearths 3 are exchangeable in accordance with the raw material of the ingot 32.
As shown in
By injecting the molten metal 31 into the mold 12 from the short side of the mold 12 having a rectangular cross-sectional shape, the high-temperature molten metal 31 is allowed to flow from the end portion, which has a greater contact area with the mold 12 and having a higher cooling rate than the center portion in the long side direction of the mold 12, toward the center portion. By injecting the high-temperature molten metal 31 into the end portion having a higher cooling rate and allowing it to flow toward the center portion having a lower cooling rate, the cooled state (temperature) of the molten metal 31 at the end portion of the mold 12 and the cooled state (temperature) of the molten metal 31 at the center portion of the mold 12 can be made uniform.
As shown in
Continuous casting for the slab 32a made of titanium can be carried out without generating a large amount of inclusions such as HDI (high-density inclusions) and LDI (low-density inclusions). It is therefore not necessary to increase the capacity of the hearth 13 for titanium and thereby prolong the retention time of the molten metal 31 for the purpose of precipitating inclusions therein. Rather, decreasing the capacity of the hearth 13 for titanium and thereby suppressing heat dissipation from the hearth 3 is preferred. On the other hand, continuous casting for the ingot 32b made of a titanium alloy is carried out while generating a large amount of inclusions. It is therefore necessary to increase the capacity of the hearth 23 for titanium alloy and thereby secure an adequate retention time of the molten metal 31 for the purpose of precipitating inclusions in the hearth. Therefore, the hearths 13 for titanium have two hearths 3, that is, the raw material introduction hearth 13a and the molten metal injection hearth 13b, while the hearths 23 for titanium alloy have three hearths 3, that is, the raw material introduction hearth 23a, the molten metal injection hearth 23b, and the flow control hearth 23c. The number of the hearths 23 for titanium alloy is greater than that of the hearths 13 for titanium. Not only the number of the hearths 23 for titanium alloy is greater but also the total capacity of them is greater than that of the hearths 13 for titanium.
Thus, at the time of continuous casting for the slab 13, the hearths 13 for titanium smaller in number and total capacity than the hearths 23 for titanium alloy are used. This makes it possible to preferably carry out continuous casting for the slab 32a while suppressing heat dissipation from the hearths 3. At the time of continuous casting for the ingot 32b, on the other hand, the hearths 23 for titanium alloy greater in number and total capacity than the hearths 13 for titanium are used. This makes it possible to preferably carry out continuous casting for the ingot 32b while securing a retention time enough for precipitating inclusions. It is to be noted that even in continuous casting for ingots made of a titanium alloy, the hearths 13 for titanium may be used when an intended quality level is not so high or the amount of inclusions is not large because a raw material to be melted has good quality.
The raw material introduction hearth 13a and the molten metal injection hearth 13b may be integrated with each other or may be separated from each other. Similarly, the raw material introduction hearth 23a, the molten metal injection hearth 23b, and the flow control hearth 23c may be integrated with one another or may be separated from one another.
A raw material introduction unit 4 introduces a raw material into the raw material introduction hearth 3a. The raw material introduction unit 4 is constituted to be exchangeable in accordance with the raw material to be used.
The raw material introduction unit 14 and the raw material introduction unit 24 introduce the raw material in the same direction so that the monitoring directions of the raw material introduction from the outside of the chamber can be made equal. This facilitates monitoring of the working condition.
A plurality of plasma torches 5 penetrating through the chamber are provided so as to be placed above the plurality of hearths 3. They heat the raw material which has been introduced into the hearths 3 and the surface of the molten metal 31 in the hearths 3 by means of plasma arc. In the present embodiment, three plasma torches 5 are provided with a predetermined interval so as to avoid mutual interference. The number of the plasma torches 5 is not limited to three. The plasma torches 5 are swingable with a support 5d (refer to
As shown in
As shown in
As described above, due to the structure that the plasma torches 5 each penetrate through the chamber, the plasma torches 5 are each placed at a fixed position.
Referring back again to
As described above, the mold 2 is exchangeable with a mold having any cross-sectional shape without changing the gravity center position. The withdrawal unit 6 is placed to withdraw the ingot 32 with the gravity center position of the mold 2 as a center. Since the ingot 32 is withdrawn with the gravity center position of the mold 2 as a center, transfer of the position of the withdrawal unit 6 is not necessary whatever cross-sectional shape the mold 2 has. In addition, since the ingot 32 is withdrawn with the gravity center position of the mold 2 as a center, a withdrawing power of the withdrawal unit 6 can be caused to act uniformly in the mold 2 whatever cross-sectional shape the mold 2 has. The ingot 32 can therefore be withdrawn without causing non-uniformity in withdrawal power or a withdrawal failure due to bending of the ingot 32.
The plasma torch 7 penetrates through the chamber so as to be placed above the mold 2 and it heats the surface of the molten metal 31 injected into the mold 2 by means of plasma arc. The plasma torch 7, similarly to the plasma torch 5, can be swung with a support as a center and it may also be moved in a vertical direction.
A titanium alloy is hard to be cast by electron beam melting in a vacuum atmosphere due to evaporation of minor components, but plasma arc melting in an inert gas atmosphere can cast not only titanium but also a titanium alloy.
Next, referring to
First, a description will be given of continuous casting for the slab 32a conducted after switching from continuous casting for the ingot 32b made of a titanium alloy to continuous casting for the slab 32a made of titanium. In this case, the mold 22 having a circular cross-sectional shape is exchanged with the mold 12 having a rectangular cross-sectional shape. In addition, the starting block 26a capable of blocking the lower-side opening portion of the mold 22 having a circular cross-sectional shape is exchanged with the starting block 16a capable of blocking the lower-side opening portion of the mold 12. The starting block 16a is supported with the withdrawal unit 6 and the lower-side opening portion of the mold 12 is blocked with the starting block 16a. Further, the hearths 23 for titanium alloy are exchanged with the hearths 13 for titanium. The raw material introduction unit 24 for continuous casting for the ingot 32b made of a titanium alloy is exchanged with the raw material introduction unit 14 for continuous casting for the slab 32a made of titanium. By swinging three plasma torches 5, the direction of each of the plasma torches 5 is adjusted so that they work for the hearths 13 for titanium.
As shown in
Then, introduction of the sponge titanium 33 from the raw material introduction unit 14 to the raw material introduction hearth 13a is started and at the same time, heating with the plasma torch 5 is started. The sponge titanium 33 introduced into the raw material introduction hearth 13a is melted by heating with the plasma torch 5a into a molten metal 31 and the molten metal fills the raw material introduction hearth 13a. The molten metal 31 overflowing from the raw material introduction hearth 13a passes through the channel 8, enters the molten metal injection hearth 13b, and gradually fills the molten metal injection hearth 13b. The molten metal 31 overflowing from the molten metal injection hearth 13b passes through the molten metal injection unit 13d, and injected into the mold 12. The molten metal 31 injected into the mold 12 is gradually solidified by cooling. The starting block 16a which has blocked the lower-side opening portion of the mold 12 is pulled down at a predetermined velocity. The slab 32a obtained by solidifying the molten metal 31 is withdrawn downward and in such a manner, continuous casting is performed.
At the time of continuous casting for the slab 32a, by using the hearths 13 for titanium while decreasing the number and the total capacity thereof compared with those of the hearths 23 for titanium alloy, continuous casting for the slab 32a can be conducted preferably while suppressing heat dissipation from the hearths 3.
Since the slab 32a is withdrawn with the gravity center position of the mold 12, which is exchangeable without changing the gravity center position, as a center, transfer of the position of the withdrawal unit 6 is not necessary whatever cross-sectional shape the mold 2 has. In addition, since the slab 32a is withdrawn with the gravity center position of the mold 12 as a center, a withdrawal power of the withdrawal unit 6 can be caused to act in the mold 2 uniformly whatever cross-sectional shape the mold 2 has. This makes it possible to withdraw the slab 32a without causing non-uniformity of a withdrawing power or a withdrawal failure due to bending of the slab 32a.
During continuous casting for the slab 32a, the plasma torch 5a heats the raw material and the surface of the molten metal 31 in the raw material introduction hearth 13a; the plasma torch 5c heats the surface of the molten metal 31 in the molten metal injection hearth 13b; and the plasma torch 5b heats the surface of the molten metal 31 in the channel 8. The plasma torch 7, on the other hand, heats the surface of the molten metal 31 injected into the mold 12.
Next, a description will be given of continuous casting for the ingot 32b made of a titanium alloy to be conducted after switching from continuous casting for the slab 32a made of titanium to continuous casting for the ingot 32b made of a titanium alloy. In this case, the mold 12 having a rectangular cross-sectional shape is exchanged with the mold 22 having a circular cross-sectional shape. The starting block 16a capable of blocking the lower-side opening portion of the mold 12 is exchanged with the starting block 26a capable of blocking the lower-side opening portion of the mold 22 having a circular cross-sectional shape. The starting block 26a is supported with the withdrawal unit 6 and the lower-side opening portion of the mold 22 is blocked with the starting block 26a. In addition, the hearth 13 for titanium is exchanged with the hearth 23 for titanium alloy. Further, the raw material introduction unit 14 for continuous casting for the slab 32a made of titanium is exchanged with the raw material introduction unit 24 for continuous casting for the ingot 32b made of a titanium alloy. Still further, by swinging three plasma torches 5, the direction of each of the plasma torches 5 is adjusted so that they work for the hearths 23 for titanium alloy.
Then, advance of the rod-like ingot 34 is started from the raw material introduction unit 24 to the raw material introduction hearth 23a and at the same time, heating with the plasma torch 5 is started. The ingot 34 placed in the raw material introduction hearth 23a is melted into titanium droplets by heating with the plasma torch 5a. The titanium droplets drop in the raw material introduction hearth 23a to be a molten metal 31 and the resulting molten metal fills the raw material introduction hearth 23a. The molten metal 31 overflowing from the raw material introduction hearth 23a passes through the channel 8, enters the flow control hearth 23c, and gradually fills the flow control hearth 23c. Further, the molten metal 31 overflowing from the flow control hearth 23c enters the molten metal injection hearth 23b and gradually fills the molten metal injection hearth 23b. Then, the molten metal 31 overflowing from the molten metal injection hearth 23b is injected into the mold 22 through the molten metal injection unit 23d. The molten metal 31 injected into the mold 22 is gradually solidified by cooling. By pulling down the starting block 26a which has blocked the lower-side opening portion of the mold 22 at a predetermined velocity, the columnar ingot 32b obtained by solidification of the molten metal 31 is withdrawn downward and in such a manner, continuous casting is performed.
At the time of continuous casting for the ingot 32b, by using the hearth 23 for titanium alloy while increasing the number and total capacity thereof compared with those of the hearth 13 for titanium, continuous casting for the ingot 32b can be conducted preferably while securing a retention time enough for precipitating inclusions.
Since the ingot 32b is withdrawn with the gravity center position of the mold 22, which is exchangeable without changing the gravity center position, as a center, transfer of the position of the withdrawal unit 6 is not required whatever cross-sectional shape the mold 2 has. In addition, since the ingot 32b is drawn with the gravity center portion of the mold 22 as a center, a withdrawing power of the withdrawal unit 6 can be caused to act uniformly in the mold 2 whatever sectional shape the mold 2 has. This makes it possible to withdraw the ingot 32b without causing non-uniformity of a withdrawing power or a withdrawal failure due to bending of the ingot 32b.
During continuous casting for the ingot 32b made of a titanium alloy, the plasma torch 5a heats the ingot 34 and the surface of the molten metal 31 in the raw material introduction hearth 23a; the plasma torch 5c heats the surface of the molten metal 31 in the molten metal injection hearth 23b; and the plasma torch 5b heats the surface of the molten metal 31 in the flow control hearth 23c. The plasma torch 7, on the other hand, heats the surface of the molten metal 31 injected into the mold 22.
As described above, in the continuous casting device 1 and the continuous casting method according to the present embodiment, the hearths 13 for titanium slab 32a smaller in both the number and total capacity than the hearths 23 for titanium alloy are used at the time of continuous casting for the slab 32 made of titanium. This enables preferable continuous casting for the slab 32a while suppressing heat dissipation from the hearths 3. The hearths 23 for titanium alloy greater in both the number and total capacity than the hearths 13 for titanium are used at the time of continuous casting for the ingot 32b made of a titanium alloy. This enables preferable continuous casting for the ingot 32b while securing a retention time enough for precipitating inclusions. Thus, the slab 32a made of titanium and the ingot 32b made of a titanium alloy can be produced respectively in a single facility by continuous casting.
By swinging each of the plasma torches 5, the surface of the molten metal 31 in the hearth 3 can be preferably heated in spite of a difference in the shape between the hearth 13 for titanium and the hearth 23 for titanium alloy. Exchange between the hearth 13 for titanium and the hearth 23 for titanium alloy therefore does not require a change in the placing position of each of the plasma torches 5 so that improvement in working efficiency can be achieved.
Since the ingot 32 is withdrawn with the gravity center position of the mold 2, which is exchangeable without changing the gravity center position, as a center, transfer of the position of the withdrawal unit 6 is not required whatever cross-sectional shape the mold 2 has. In addition, since the ingot 32 is drawn with the gravity center portion of the mold 2 as a center, a withdrawing power of the withdrawal unit 6 can be caused to act uniformly in the mold 2 whatever sectional shape the mold 2 has. This makes it possible to withdraw the ingot 32 without causing non-uniformity of a withdrawing power or a withdrawal failure due to bending of the ingot 32.
A continuous casting device 201 according to Second Embodiment of the present invention will next be described. For constituent elements similar to the constituents element described above, the same reference numbers are attached, respectively and a description on them is omitted.
At the time of continuous casting (β) for the ingot 32b made of a titanium alloy, as shown on the lower side of
At the time of continuous casting (α) for the slab 32a made of titanium, on the other hand, as shown on the upper side in
When the slab 32a made of titanium is produced by continuous casting, due to a small amount of inclusions, it is not necessary to increase the capacity of the hearths 13 for titanium and thereby increase the retention time of the molten metal 31 in order to precipitate the inclusions. The number of the hearths 13 for titanium is therefore made smaller and also the total capacity of them is made smaller than those of the hearths 23 for titanium alloy. In continuous casting for the slab 32a made of titanium, therefore, it is desired to reduce, in accordance with the total capacity of the hearths 13 for titanium or the number of the hearths 3, an electric power consumption rate by plasma arc for heating the surface of the molten metal 31. The term “electric power consumption rate” means an amount of electric power required for a unit production amount of a product and it is an indicator objectively showing production efficiency. For the hearths 23 for titanium alloy, all of the three plasma torches 5 are used, while two of the three plasma torches 5 are used for the hearths 13 for titanium. Described specifically, the number of the plasma torches 5 used at the time of continuous casting for the ingot 32b made of a titanium alloy is greater than the number of the plasma torches 5 used at the time of continuous casting for the slab 32a made of titanium. A total output, per unit melting amount, of the plasma torches 5 to be used at the time of continuous casting for the ingot 32b made of a titanium alloy is greater than a total output, per unit melting amount, of the plasma torches 5 to be used at the time of continuous casting for the slab 32a made of titanium.
Thus, at the time of continuous casting for the slab 32a made of titanium, the number and the total capacity of the hearths 13 for titanium to used are both smaller than those of the hearths 23 for titanium alloy. In addition, the number of the plasma torches 5 and the total output, per unit melting amount, of the plasma torches 5 to be used are made smaller than those at the time of continuous casting for the ingot 32b made of a titanium alloy. This enables preferable heating of the surface of the molten metal 31 in the hearths 3 while reducing the electric power consumption rate. At the time of continuous casting for the ingot 32b made of a titanium alloy, on the other hand, the number and the total capacity of the hearths 23 for titanium alloy to be used are both greater than those of the hearths 13 for titanium. In addition, the number of the plasma torches 5 and the total output, per unit melting amount, of the plasma torches 5 to be used are made greater than those at the time of continuous casting for the slab 32a made of titanium. This enables preferable heating of the surface of the molten metal 31 in the hearths 3 while suppressing the molten metal 31 from being solidified in the hearths 3.
As described above, in the continuous casting device 201 and the continuous casting method according to the present embodiment, the number and the total capacity of the hearths 13 for titanium to be used at continuous casting for the slab 32a made of titanium are smaller than those of the hearths 23 for titanium alloy. In addition, the number of the plasma torches 5 and also the total output, per unit melting amount, of the plasma torches 5 are made smaller than those to be used at the time of continuous casting for the ingot 32b made of a titanium alloy. This makes it possible to preferably heat the surface of the molten metal 31 in the hearths 3 while reducing the electric power consumption rate. On the other hand, the number and the total capacity of the hearths 23 for titanium alloy to be used at the time of continuous casting for the ingot 32b made of a titanium alloy are made greater than those of the hearths 13 for titanium. In addition, the number of the plasma torches 5 and also the total output, per unit melting amount, of the plasma torches 5 are made greater than those at the time of continuous casting for the slab 32a made of titanium. This makes it possible to preferably heat the surface of the molten metal 31 in the hearths 3 while suppressing the molten metal 31 from being solidified in the hearths 3.
A continuous casting device 301 according to Third Embodiment of the present invention will next be described. Constituent elements similar to those described above are identified by the same reference number and a description on them is omitted. A difference between the continuous casting device 301 of the present embodiment and the continuous casting device 1 of First Embodiment is that as shown in
At the time of continuous casting for the slab 32a made of titanium, as shown in
The hearths 23 for titanium alloy have the molten metal injection hearth 23b and the flow control hearth 23c and the hearth 13 for titanium has the molten metal injection hearth 13b, so that the number of the hearths 3 is greater in the former than in the latter. In addition, the hearths 23 for titanium alloy have a total capacity greater than that of the hearth 13 for titanium.
The plurality of hearths 3 have thereabove three plasma torches 5. These plasma torches 5 penetrate through a chamber. They are swingable with the support 5d (refer to
At continuous casting for the slab 32a made of titanium, as shown by the arrow in
At the time of continuous casting for the ingot 32b made of a titanium alloy, on the other hand, as shown by the arrow in
Thus, the number of the plasma torches 5 to be used at the time of continuous casting for the ingot 32b made of a titanium alloy is greater than the number of the plasma torches 5 to be used at the time of continuous casting for the slab 32a made of titanium. In addition, the total output, per unit melting amount, of the plasma torches 5 to be used at the time of continuous casting for the ingot 32b made of a titanium alloy is greater than the total output, per unit melting amount, of the plasma torches 5 to be used at the time of continuous casting for the slab 32a made of titanium.
When the mold 2, the molten metal transfer hearth 3b, and the raw material introduction hearth 3a are arranged linearly in order of mention (refer to
In addition, since the surface of the molten metal 31 in the channel 8 is also heated with the plasma torch 5, solidification of the molten metal 31 in the channel 8 can be suppressed. Further, since the surface of the molten metal 31 in the molten metal injection unit 23d is also heated with the plasma torch 7, solidification of the molten metal 31 in the molten metal injection unit 23d can be suppressed.
A shield plate (not illustrated) is preferably provided between the mold 2 and the raw material introduction hearth 3a in order to prevent a splash generated during introduction of the raw material into the raw material introduction hearth 3a from entering the mold 2.
At the time of continuous casting for the slab 32a made of titanium, a continuous casting device 401 shown in
As shown by the arrow, the plasma torch 5a placed above the raw material introduction hearth 3a is operated in an L-shape so as to travel above the channel 8 and at the same time, the plasma torch 5c placed above the molten metal injection hearth 13b is operated in an L-shape so as to travel above the molten metal injection unit 13d. The plasma torch 7 placed above the mold 12 is operated linearly along the long-side direction of the mold 12. At this time, the plasma torch 5b is in a suspended state. Being operated as described above, the plasma torch 5a heats the raw material and the surface of the molten metal 31 in the raw material introduction hearth 3a and the surface of the molten metal 31 in the channel 8; the plasma torch 5c heats the surface of the molten metal 31 in the molten metal injection hearth 13b and the surface of the molten metal 31 in the molten metal injection unit 13d; and the plasma torch 7 heats the surface of the molten metal 31 in the mold 12.
The continuous casting device 401 is constituted so that the molten metal 31 is injected from the molten metal injection unit 13d to the center portion in the long-side direction of the mold 12 having a rectangular cross-sectional shape. Further, the raw material introduction unit 14 introduces sponge titanium 33 into the raw material introduction hearth 3a in a direction different by 90 degrees from that of the continuous casting device 301 shown in
As described above, in the continuous casting devices 301 and 401 according to the present embodiment, the raw material introduction hearth 3a and the mold 2 are arranged in line in the direction C, while at least one of the raw material introduction hearth 3a and the mold 2 and the molten metal transfer hearth 3b are arranged in line in the direction D which crosses the direction C. This makes it possible to fix the position of the raw material introduction hearth 3a without being influenced by the number or size of the molten metal transfer hearth 3b. When the mold 2, the molten metal transfer hearth 3b, and the raw material introduction hearth 3a are arranged linearly or in an L-shape in order of mention, the position of the raw material introduction hearth 3a varies with the number or size of the molten metal transfer hearth 3b and the position of introducing the raw material into the raw material introduction hearth 3a also varies. By arranging the raw material introduction hearth 3a and the mold 2 in line in the direction C and fixing the position of the raw material introduction hearth 3a, the position of introducing the raw material into the raw material introduction hearth 3a can be fixed. As a result, at the time of switching between continuous casting for the slab 32a made of titanium and continuous casting for the ingot 32b made of a titanium alloy, changing the raw material introduction position is not required, making it possible to enhance the work efficiency. In addition, without necessity to needlessly increase the C-direction length of the chamber for housing the continuous casting device 301 therein, the chamber can be downsized so that a heat loss from the chamber can be reduced.
In the continuous casting devices 301 and 401 and the continuous casting method according to the present embodiment, since the plasma torch 5 also heats the surface of the molten metal 31 in the channel 8, solidification of the molten metal 31 in the channel 8 can be suppressed.
The embodiments of the present invention have each been described above, but they are only specific examples and do not particularly limit the present invention. The design of the specific constitution or the like can be changed as needed. The effects and advantages described in the embodiments of the present invention are only the most preferable effects and advantages produced by the present invention. The effects and advantages of the present invention are not limited to those described in the embodiments of the present invention.
The present application is based on Japanese Patent Application (Japanese Patent Application No. 2012-049517) filed on Mar. 6, 2012 and contents of this application are incorporated herein by reference.
Number | Date | Country | Kind |
---|---|---|---|
2012-049517 | Mar 2012 | JP | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/JP2013/056165 | 3/6/2013 | WO | 00 | 7/16/2014 |