This application is the U.S. national stage application of International Patent Application No. PCT/KR2011/000682, filed Feb. 1, 2011, which claims priority to Korean Application Nos. 10-2010-0074423, filed Jul. 30, 2010 and 10-2010-0108913, filed Nov. 3, 2010, the disclosures of each of which are incorporated herein by reference in their entirety.
The disclosure relates to a heat treatment container for a vacuum heat treatment apparatus.
A vacuum heat treatment apparatus, as an apparatus of manufacturing a desired material by heat-treating a raw material in a crucible, has an advantage of preventing pollution from the surroundings from generating by performing a heat treatment in a vacuum state. In the vacuum heat treatment apparatus, a insulating member is positioned in a chamber maintained in the vacuum state and a heat is positioned in the insulating member so as to heat the raw material.
However, a material generated by reacting with the crucible and the raw material during the reaction may be attached on an inner wall of the crucible. Since the generated material is different from the crucible, a heat stress is applied to the crucible due to a difference of heat expansion coefficients between different materials. In a serious case, the crucible may be broken by the heat stress during the reaction. Accordingly, a replacement cost of the crucible is extremely generated, such that productivity may be deteriorated.
The present invention had been made in an effort to provide a heat treatment container for a vacuum heat treatment apparatus capable of preventing breakage due to a heat stress.
An exemplary embodiment of the present invention provides a heat treatment container for a vacuum heat treatment apparatus including: a bottom portion and a sidewall, and a support protruding inward.
The support may elongate in a depth direction of the heat treatment container.
The support may be positioned the sidewall.
The support may be formed at each sidewall by a single or in plural.
The support may have a rectangular or round cross-section.
The support may be integrally formed to the heat treatment container.
The heat treatment container may be for manufacturing of silicon carbide.
Another exemplary embodiment of the present invention provides a heat treatment container for a vacuum heat treatment apparatus including a plan shape having a curve-shaped portion.
The plan shape of the heat treatment container may be curved.
The plan shape of the heat treatment container may be circular or ellipse.
The heat treatment container may have a inner space and an opened one side, and may further include a cover member covering the heat treatment container, wherein the cover member may include a first portion having a first thickness and contacting the heat treatment container and a second portion having a second thickness larger than the first thickness and corresponding to the inner space.
A side of the second portion adjacent to the first portion may be inclined or rounded with respect to a cover surface of the cover member.
An exhaust passage may be formed at an adjacent portion to the cover member in the heat treatment container.
The heat treatment container may be for manufacturing of silicon carbide.
According to an exemplary embodiment, the vacuum heat treatment apparatus can prevent the heat treatment container form being modified due to the heat stress at a high temperature by forming a support in the heat treatment container. In this case, the support is formed to elongate in a depth direction of the heat treatment container, to thereby making it possible to prevent efficiently the modification of the heat treatment container.
The vacuum heat treatment apparatus can prevent the modification and the breakage of the heat treatment container by optimizing a shape of the heat treatment container to minimize the heat stress applied to the heat treatment container. Further, the vacuum heat treatment apparatus can prevent breakage due to a collision between a container part and a cover member by optimizing a shape of the cover member.
In describing embodiments, it will be understood that when layers (films), regions, patterns, or structures are referred to as being “on” or “under” a substrate, layers (films), regions, pads, or patterns, “on” and “under” include “directly” or “indirectly”.
In the drawings, since the thicknesses or sizes of layers (films), regions, patterns, or structures may be modified for clear description, their actual sizes are not fully reflected.
Hereinafter, an exemplary embodiment of the present invention will be described in detail with reference to accompanying drawings.
Referring to
An atmosphere gas is injected into the chamber 10 through an atmosphere gas supplying pipe (not shown). The atmosphere gas may use an inert gas such as argon (Ar), helium (He), or the like.
The insulating member 20 in the chamber 10 insulates the heat treatment container part 30 so as to maintain at a proper temperature for the reaction. The insulating member 20 may include graphite so as to withstand a high temperature.
The heat treatment container part 30, in which raw materials are filled and a desired material is generated by reacting with the raw materials, is positioned in the insulating member 20. The heat treatment container part 30 may include graphite so as to withstand a high temperature. The gas generated during the reaction or a non-reacted gas may be discharged through an outlet 12 connected to the heat treatment container part 30.
The heating member 40 heating the heat treatment container part 30 is positioned between the insulating member 20 and the heat treatment container part 30. The heating member 40 may supply the heat to the heat treatment container part 30 by various methods. For example, the heating member 40 may generate the heat by apply voltage to graphite.
The heat treatment container part 30 of the vacuum heat treatment apparatus 100 is a crucible which contains the raw material and applies the heat to manufacture the desired material and it will be described below with reference to
The vacuum heat treatment apparatus 100 may be used as, for example, a manufacturing apparatus of silicon carbide in which silicon carbide is manufactured by heating a mixed raw material including a carbon source and a silicon source.
That is, the mixed raw material including the carbon source and the silicon source is contained in the heat treatment container part 30 of the vacuum heat treatment apparatus 100 and heated together by the heating member 40.
In the exemplary embodiment, the silicon source may include various materials capable of supplying silicon. For example, the silicon source may include silica. The silicon source may be a silica power, a silica sol, a silica gel, a quartz powder, or the like. However, the exemplary embodiment is not limited thereto and an organic silicon compound including silicon may be used as the silicon source.
The carbon source may include a solid carbon source or an organic carbon compound.
The solid carbon source may be graphite, carbon black, carbon nano tube (CNT), fullerene (C60), or the like.
The organic carbon compound may be penol, franc, xylene, polyimide, polyunrethane, polyvinyl alcohol, polyacrylonitrile, poly vinyl acetate, or the like. In addition, the organic carbon compound may be cellulose, sugar, pitch, tar, or the like.
The silicon source and the carbon source are mixed.
Further, when the organic carbon compound is used as the carbon source, it is required to use approximately two times more carbon source than the solid carbon source. However, it may have a little difference depending on the carbon amount generated in the carbonization process. When the organic carbon compound is used as the carbon source, the carbon source in the mixed material is carbonized by heating the mixed material of the silicon source and the carbon source. The carbonization is preferably maintained at a temperature of 700° C. to 1200° C., more preferably, 900° C. to 1100° C. However, in the case where the carbon source is not the organic carbon compound, the carbonization may be omitted.
Thereafter, when the mixed material of the carbon source and the silicon source is contained and heated in the heat treatment container part 30, the silicon carbide is manufactured by a carbothermal reaction according to the following reaction formula 1 to 3.
SiO2(s)+C(s)−>SiO(g)+CO(g) [Reaction Formula 1]
SiO(g)+2C(s)−>SiC(s)+CO(g) [Reaction Formula 2]
SiO2(s)+3C(s)−>SiC(s)+2CO(g) [Reaction Formula 3]
The heating may be performed in the argon (Ar) or vacuum atmosphere. The degree of a vacuum may be more than 0.03 torr to 0.5 torr or less, preferably, more than 0.03 torr to 0.1 torr or less. In the case of the degree of a vacuum of 0.03 torr or less, since a mechanical load is mostly generated in the mass-produced equipment, additional equipment is required, such that maintenance of the equipment is difficult and the cost is increased.
The heating temperature may be 1300° C. to 1900° C., preferably, 1600° C. to 1900° C. Here, the heating time may be about 3 hours, but is not limited thereto.
As such, the vacuum heat treatment apparatus 100 according to the exemplary embodiment may be used for manufacturing silicon carbide, but is not limited thereto. The vacuum heat treatment apparatus 100 may be used for manufacturing various materials in which the heat treatment is required in the synthesis.
Referring to
Referring to
The heat treatment container 150 includes a bottom and a sidewall which are integrally formed and has a space portion filled by the raw material. In addition, referring to
The vacuum heat treatment apparatus used as an apparatus of manufacturing silicon carbide will be described as an example. The carbon source and the silicon source are filled in the heat treatment container 150 and then silicon carbide is generated by the reaction at the high temperature. In this case, since the heat treatment container 150 is made of graphite in order to withstand the high temperature, a silicon carbide layer may be formed in the heat treatment container 150 by reacting with graphite of the heat treatment container 150 and the silicon source. Thereafter, since the silicon carbide layer which is a different material is formed in the heat treatment container 150 made of graphite, a middle portion C of the heat treatment container 150 may be curved toward the outside as compared with the peripheral portion.
In the exemplary embodiment, since the support 152 capable of keeping a curved force is formed at the sidewall of the heat treatment container 150, the modification of the heat treatment container 150 can be prevented.
The support 152 is formed in the inner wall of the heat treatment container 150 as shown in the drawing, but the exemplary embodiment is not limited thereto. Accordingly, the support 152 may be formed at the outer wall of the heat treatment container 150.
The support 152 may elongate in a depth direction of the heat treatment container 150. Accordingly, the modification of the heat treatment container 150 can be prevented.
Referring to
Referring back to
Referring back to
Further, in a modified example as shown in
Hereinafter, a heat treatment container part according to another exemplary embodiment of the present invention will be described with reference to
Referring to
The carbon source and the silicon source are filled in the heat treatment container part 30 and silicon carbide is generated by the reaction at a high temperature. At this time, the heat treatment container part 30 is made of graphite in order to the high temperature in order to withstand the high temperature, a silicon carbide layer may be formed in the heat treatment container part 30 by reacting with graphite of the heat treatment container part 30 and the silicon source. Accordingly, the silicon carbide layer which is different material may be formed in the heat treatment container part 30 made of graphite. Since a heat expansion coefficient of silicon carbide is larger than that of graphite constituting the heat treatment container part 30 in the related art, the middle portion of the heat treatment container part 30 is expanded. However, in the exemplary embodiment, since the plan shape of the heat treatment container part 30 has the curve-shaped portion, a force applied to the heat treatment container part 30 can be minimized by using directivity between the heat stresses applied to the heat treatment container part 30. Accordingly, the modification and the breakage of the heat treatment container can be prevented.
At this time, since the plan shape of the heat treatment container part 30 is curved, the force applied to the heat treatment container part 30 may be close to almost zero. For example, the plan shape of the heat treatment container part 30 may be circular or ellipse.
In the exemplary embodiment, the heat treatment container part 30 has a inner space and may include heat treatment container 32 having an opened one side and a cover member 34 covering the heat treatment container 32.
The heat treatment container 32 includes an inner space filled with the raw material for the reaction. in addition, an exhaust passage 322 is formed in the heat treatment container 32 so that a gas flows between the cover member 34 and the heat treatment container 32. The gases generated in the heat treatment may be discharged through the exhaust passage 322. The exhaust passage 322 may be formed in the heat treatment container of the first exemplary embodiment (reference numeral 150 of
The cover member 34 may include a first portion 341 formed at the outer area so as to contact the heat treatment container 32 and a second portion 342 formed at the central area so as to correspond to the space of the heat treatment container 32. At this time, a second thickness T2 of the second portion 342 is larger than a first thickness T1 of the first portion 341 such that the heat treatment container 32 and the cover member 34 can be firmly fixed.
A side 343 of the second portion 342 adjacent to the first portion 341 is inclined with respect to a cover surface of the cover member 34. as such, since the side 343 is inclined, the breakage due to the collision of the heat treatment container 32 and the cover member 34 can be efficiently prevented. The side 343 of the second portion 342 may have various shapes and for example, as shown in
The cover member 34 may be applied to the first exemplary embodiment described above. In addition, in the exemplary embodiment, as shown in
The features, structures, effects, and the like described in the exemplary embodiments are included in at least one exemplary embodiment and are not particularly limited to only one exemplary embodiment. Furthermore, the features, structures, effects, and the like described in the exemplary embodiments can be applied to other exemplary embodiments through combination and modification by those skilled in the art to which the exemplary embodiments belong. Therefore, it should be appreciated that contents related with the combination and modification are included in the scope of the present invention.
As described above, the preferred embodiments have been described and illustrated in the drawings and the specification. Herein, specific terms have been used, but are just used for the purpose of describing the present invention and are not used for defining the meaning or limiting the scope of the present invention, which is disclosed in the appended claims. Therefore, it will be appreciated to those skilled in the art that various modifications are made and other equivalent embodiments are available. Accordingly, the actual technical protection scope of the present invention must be determined by the spirit of the appended claims.
Number | Date | Country | Kind |
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10-2010-0074423 | Jul 2010 | KR | national |
10-2010-0108913 | Nov 2010 | KR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/KR2011/000682 | 2/1/2011 | WO | 00 | 4/9/2013 |
Publishing Document | Publishing Date | Country | Kind |
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WO2012/015132 | 2/2/2012 | WO | A |
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Number | Date | Country | |
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20130196278 A1 | Aug 2013 | US |