The present invention relates to susceptors and methods for manufacturing the same.
Conventionally, it is known to use, in a semiconductor manufacturing process or the like, a susceptor whose surface layer is made of silicon carbide. However, in cases such as where silicon carbide or the like is epitaxially grown on a wafer, the wafer and the susceptor are exposed to high temperatures, for example, over 1500° C. Thus, there arises a problem of adhesion of silicon carbide forming the surface layer of the susceptor to the wafer.
To solve the above problem, Patent Literature 1 proposes a susceptor in which a portion for placing a wafer thereon is formed of a detachable member made of tantalum carbide and a peripheral portion around the portion for placing a wafer thereon is formed of a detachable silicon carbide-coated graphite member.
Patent Literature 1: JP-A-2006-60195
However, since the susceptor disclosed in Patent Literature 1 is formed of a plurality of members, if has the problem of its manufacturing process being complicated and the problem of being difficult to handle.
To solve these problems, it may be conceivable to coat the entire surface of the susceptor with tantalum carbide. However, the coating of the entire surface of the susceptor with tantalum carbide causes the problem that when a silicon carbide film or the like is deposited on a wafer, the silicon carbide film deposited on the tantalum carbide layer peels off, so that resultant silicon carbide particles adhere to the wafer. Furthermore, because there is a difference in coefficient of thermal expansion (CTE) between the tantalum carbide layer and graphite forming the base material, this presents the problem of the entire susceptor warping.
An object of the present invention is to provide a susceptor that, in forming a thin film on a wafer, can reduce impurities or the like adhering to the wafer and a method for manufacturing the same.
A susceptor according to the present invention includes a base material with a recess, a tantalum carbide layer formed directly on a bottom surface of the recess, and a silicon carbide layer formed on a surface of the base material except for the recess.
In the present invention, the tantalum carbide layer may also be formed directly on a side surface of the recess.
The base material is preferably made of a carbon material and more preferably made of graphite.
A method for manufacturing a susceptor according to a first aspect of the present invention includes the steps of: preparing an original base material in which a recess is yet to be formed; forming a silicon carbide layer on a surface of the original base material; forming the recess in the original base material and removing a region of the silicon carbide layer corresponding to the recess; and forming a tantalum carbide layer on a bottom surface of the recess.
A method for manufacturing a susceptor according to a second aspect of the present invention includes the steps of: preparing a base material with a recess formed therein; forming a silicon carbide; layer on a surface of the base material except for the recess; and forming a tantalum carbide layer on a bottom surface of the recess.
In the second aspect of the present invention, the step of forming a silicon carbide layer may include the steps of: placing a masking member in the recess; forming a silicon carbide layer on a surface of the base material on which the masking member is placed; and removing the masking member from the recess after forming the silicon carbide layer.
In the manufacturing methods according to the first and second aspects of the present invention, the step of forming a tantalum carbide layer may include the steps of: forming a metal tantalum layer on a bottom surface of the recess; and subjecting the metal tantalum layer to a carburization treatment to form a tantalum carbide layer.
In the manufacturing methods according to the first and second aspects of the present invention, the step of forming a tantalum carbide layer may include the steps of: providing a masking jig to cover the surface of the base material except for the recess; and forming a tantalum carbide layer after providing the masking jig.
In the manufacturing methods according to the first and second aspects of the present invention, the tantalum carbide layer may be concurrently formed on the bottom surface and a side surface of the recess.
In the manufacturing methods according to the first and second aspects of the present invention, in order that in forming a tantalum carbide layer, the tantalum carbide layer is prevented from being formed to penetrate between the masking jig and the base material, an expandable graphite sheet is preferably placed between the masking jig and the base material.
According to the present invention, it can be reduced that in forming a thin film on a wafer, impurities or the like adhere to the wafer.
A description will be given below of preferred embodiments. However, the following embodiments are merely illustrative and the present invention is not limited by the following embodiments. Furthermore, throughout the drawings, members having substantially the same functions may be referred to by the same references.
The base material 10 is preferably made of a carbon material and more preferably made of graphite. Furthermore, the base material 10 is preferably made of a material having a coefficient of thermal expansion (CTE) comparable with that of the silicon carbide layer 20 formed thereon. From these viewpoints, the base material 10 is preferably made of a material having a coefficient of thermal expansion (CTE) of 4 to 6.5/° C. (350 to 450° C.). Also from such viewpoints, the base material 10 is preferably made of a carbon material, such as graphite.
The silicon carbide layer 20 can be formed, for example, by a CVD process. The thickness of the silicon carbide layer 20 is preferably within a range from 50 μm to 300 μm and more preferably within a range from 80 μm to 160 μm.
The tantalum carbide layer 22 can be formed, for example, by forming a metal tantalum layer by a CVD process and then subjecting the metal tantalum layer to a carburization treatment. Such a formation of a tantalum carbide layer is described in, such as, for example, Published Japanese Patent Application No. 2011-153070. The thickness of the tantalum carbide layer 22 is, but not particularly limited to, preferably, for example, within a range from 10 μm to 30 μm.
In this embodiment, the tantalum carbide layer 22 is formed on the inside of the recess 11 on which a wafer is to be placed, and the wafer can be placed on the tantalum carbide layer 22. Therefore, it is avoided that silicon carbide adheres to the underside of the wafer. Furthermore, the silicon carbide layer 20 is formed on the surface of the base material 10 except for the recess 11. For this reason, even if silicon carbide is deposited on the silicon carbide layer 20 while silicon carbide is epitaxially grown on the wafer, the deposited silicon carbide does not peel off. Therefore, it can be prevented that the deposited silicon carbide peels into particles and the particles adhere to the surface of the wafer. Hence, in this embodiment, it can be reduced that in forming a thin film on a wafer, impurities or the like adhere to the wafer.
Furthermore, in this embodiment, the tantalum carbide layer 22 is formed directly on the bottom surface 11a and the side surface 11b of the recess 11. Therefore, the tantalum carbide layer 22 can be formed with good adhesiveness on the base material 10. It may foe conceivable that after the silicon carbide layer 20 is formed on the entire surface of the base material 10, inclusive of the inside of the recess 11, the tantalum carbide layer 22 is formed on the inside of the recess 11. In this case, the tantalum carbide layer 22 on the inside of the recess 11 is formed on the silicon carbide layer 20. In the case where, as in this embodiment, the tantalum carbide layer 22 is formed directly on the base material 10, the tantalum carbide layer 22 can be formed with good adhesiveness as compared with the case where the tantalum carbide layer 22 is formed on the silicon carbide layer 20. In addition, if the tantalum carbide layer 22 is formed on the silicon carbide layer 20, thickness variations or irregularities of the silicon carbide layer 20 make it difficult to provide high dimensional accuracy. In the case where the tantalum carbide layer 22 is formed directly on the base material 10, a coating thickness of the tantalum carbide layer 22 only is added onto the base material 10, which can increase the dimensional accuracy of the recess 11. In the case of placing a wafer within the recess 11, the recess 11 is often required to have high dimensional accuracy, which is a great advantage in use as a susceptor.
Moreover, in this embodiment, since the silicon carbide layer 20 having a coefficient of thermal expansion close to that of the base material 10 is formed on the stir face of the base material 10 except for the recess 11, this can prevent the susceptor 1 from warping.
The susceptor 1 according to the embodiment shown in
As shown in
As shown in
After the recess 11 is formed, the silicon carbide layer 20 and a portion of the base material 10 exposed in the recess 11 are preferably subjected to a purification treatment. For example, the purification treatment can be performed by a heat treatment using chlorine gas and hydrogen gas, chlorine trifluoride gas or the like. It is preferred to reduce the ash content of the portion of the base material 10 exposed in the recess 11 to 20 ppm or less by the purification treatment.
As shown in
As shown in
However, excessive suppression of penetration of a metal tantalum layer 22 in forming the metal tantalum layer 21 may cause a lack of the thickness of the tantalum carbide layer in the recess 11. In the case where a tantalum carbide layer having a sufficient thickness is formed, the tantalum carbide layer formed to slightly penetrate and protrude onto a susceptor top surface of the silicon carbide layer 20 does not cause any significant inconvenience. The protrusion of the tantalum carbide layer onto the susceptor top surface of the silicon carbide layer 20 is preferably controlled to 5 mm or less and more preferably 3 mm or less.
In the above manner, as shown in
Next, the metal tantalum layer 21 formed on the inside of the recess 11 is subjected to a carburization treatment to form a tantalum carbide layer 22. The carburization treatment can be performed, for example, by a method described in Published Japanese Patent Application No. 2011-153070.
In the manner as thus far described, the susceptor 1 according to the embodiment shown in
First, as shown in
Next, as shown in
Next, a silicon carbide layer 20 is formed on the surface of the base material 10. The silicon carbide layer 20 is formed by a CVD process. Although the silicon carbide layer 20 is also formed on the masking member 12, a state shown in
Next, like the first aspect, as shown in
Next, like the first aspect, the metal tantalum layer 21 formed on the inside of the recess 11 is subjected to a carburization treatment to form a tantalum carbide layer 22.
In the above manner, the susceptor 1 according to the embodiment shown in
Furthermore, in the case where a material having a linear expansion coefficient approximating that of the silicon carbide layer 20 is selected as the base material 10, if the tantalum carbide layer 22 is formed at, for example, 1800° C. and then cooled to room temperature, a difference in linear expansion coefficient between silicon carbide and tantalum carbide may cause production of fine cracks in the tantalus carbide layer 22. Because the base material 10 is exposed in the cracks, its contact with a reaction gas may cause, for example, corrosion of graphite of the base material 10. However, when the susceptor 1 is used as a susceptor for SiC epitaxial growth, the reaction temperature rises to about 1500° C. to about 1700° C. Thus, the extended cracks are filled during the reaction by the tantalum carbide layer 22 having expanded, so that the corrosion of the base material 10 can be prevented.
By applying the usage as described above, regardless of the linear expansion coefficient relation between the base material 10 and the tantalum carbide layer 22, an appropriate material can be selected for the base material 10 to form a susceptor.
In this usage, the difference between the formation temperature and the service temperature of the tantalum carbide layer is preferably not higher than 300° C. and more preferably not higher than 200° C.
Although the description of the method for manufacturing a susceptor according to the present invention has been given by taking as examples the method according to the first aspect shown in
Furthermore, although the description of the susceptor according to the present invention has been given by taking as an example the susceptor according to the embodiment shown in
Number | Date | Country | Kind |
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2014-128957 | Jun 2014 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2015/065763 | 6/1/2015 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2015/198798 | 12/30/2015 | WO | A |
Number | Name | Date | Kind |
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9824911 | Ohno | Nov 2017 | B2 |
20080035632 | Fujita | Feb 2008 | A1 |
20090266300 | Iizuka | Oct 2009 | A1 |
20120301723 | Kondo | Nov 2012 | A1 |
20130327274 | Ohno et al. | Dec 2013 | A1 |
20150321966 | Shinohara | Nov 2015 | A1 |
20170175262 | Kawada | Jun 2017 | A1 |
Number | Date | Country |
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101001978 | Jul 2007 | CN |
101374973 | Feb 2009 | CN |
103484837 | Jan 2014 | CN |
10 2013 204566 | Dec 2013 | DE |
1 790 757 | May 2007 | EP |
11-269646 | Oct 1999 | JP |
2004-84057 | Mar 2004 | JP |
2006-041358 | Feb 2006 | JP |
2006-60195 | Mar 2006 | JP |
4252944 | Apr 2009 | JP |
2009-252969 | Oct 2009 | JP |
2011-153377 | Aug 2011 | JP |
2012-222284 | Nov 2012 | JP |
2013-254853 | Dec 2013 | JP |
2014123036 | Aug 2014 | WO |
Entry |
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Office Action dated Jul. 18, 2017, issued in counterpart Japanese Application No. 2014-128957, with English machine translation. (7 pages). |
Office Action dated Jul. 30, 2018, issued in counterpart Chinese Application No. 201580032799.5, with English translation. (13 pages). |
International Search Report dated Aug. 18, 2015, issued in counterpart of International Application No. PCT/JP2015/065763 (2 pages). |
Extended Search Report dated Dec. 19, 2017, issued in counterpart European Application No. 15812047.7 (6 pages). |
Notification of Transmittal of Translation of the International Preliminary Report on Patentability (Form PCT/IB/338) issued in counterpart International Application No. PCT/JP2015/065763 dated Jan. 5, 2017, with Forms PCT/IB/373 and PCT/ISA/237. (8 pages). |
Number | Date | Country | |
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20170162425 A1 | Jun 2017 | US |