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JP7600612B2 - Method for forming silicon carbide polycrystalline film and method for manufacturing silicon carbide polycrystalline substrate - Google Patents
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JP7600612B2 - Method for forming silicon carbide polycrystalline film and method for manufacturing silicon carbide polycrystalline substrate - Google Patents

Method for forming silicon carbide polycrystalline film and method for manufacturing silicon carbide polycrystalline substrate Download PDF

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JP7600612B2
JP7600612B2 JP2020176670A JP2020176670A JP7600612B2 JP 7600612 B2 JP7600612 B2 JP 7600612B2 JP 2020176670 A JP2020176670 A JP 2020176670A JP 2020176670 A JP2020176670 A JP 2020176670A JP 7600612 B2 JP7600612 B2 JP 7600612B2
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泰三 北川
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Sumitomo Metal Mining Co Ltd
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Description

本発明は、炭化珪素多結晶膜の成膜方法および炭化珪素多結晶基板の製造方法に関し、特に、化学的気相成長法(以下、「CVD法」とする場合がある)によりカーボン製支持基板上に炭化珪素(以下、「SiC」とする場合がある)多結晶膜を成膜する成膜方法と、その後、カーボン製支持基板を燃焼除去してSiC多結晶基板を得る、SiC多結晶基板の製造方法に関する。 The present invention relates to a method for forming a silicon carbide polycrystalline film and a method for manufacturing a silicon carbide polycrystalline substrate, and in particular to a method for forming a silicon carbide (hereinafter sometimes referred to as "SiC") polycrystalline film on a carbon support substrate by chemical vapor deposition (hereinafter sometimes referred to as "CVD"), and a method for manufacturing a SiC polycrystalline substrate, which subsequently burns and removes the carbon support substrate to obtain a SiC polycrystalline substrate.

SiCは珪素(以下、「Si」とする場合がある)と炭素で構成される化合物半導体材料である。SiCは、絶縁破壊電界強度がSiの10倍、バンドギャップがSiの3倍と優れているだけでなく、デバイスの作製に必要なp型、n型の制御が広い範囲で可能であることなどから、Siの限界を超えるパワーデバイス用材料として期待されている。 SiC is a compound semiconductor material composed of silicon (hereafter sometimes referred to as "Si") and carbon. Not only is SiC superior, with a dielectric breakdown field strength 10 times that of Si and a band gap three times that of Si, but it also allows for a wide range of control over the p-type and n-type required for device fabrication, making it a promising material for power devices that surpasses the limitations of Si.

しかしながら、SiC半導体は、広く普及するSi半導体と比較し、大面積のSiC単結晶基板が得られず、工程も複雑であることから、Si半導体と比較して大量生産ができず、高価であった。 However, compared to the widely used Si semiconductors, it is difficult to obtain large-area SiC single crystal substrates and the manufacturing process is complicated, making mass production of SiC semiconductors difficult and expensive compared to Si semiconductors.

SiC半導体のコストを下げるため、様々な工夫が行われてきた。例えば、特許文献1には、SiC基板の製造方法であって、少なくとも、マイクロパイプの密度が30個/cm2以下のSiC単結晶基板とSiC多結晶基板を準備し、前記SiC単結晶基板と前記SiC多結晶基板とを貼り合わせる工程を行い、その後、SiC単結晶基板を薄膜化する工程を行うことで、SiC多結晶基板上にSiC単結晶層を形成した基板を製造することが記載されている。 Various efforts have been made to reduce the cost of SiC semiconductors. For example, Patent Literature 1 describes a method for manufacturing a SiC substrate, which includes at least preparing a SiC single crystal substrate and a SiC polycrystalline substrate having a micropipe density of 30 pieces/cm2 or less, performing a step of bonding the SiC single crystal substrate and the SiC polycrystalline substrate, and then performing a step of thinning the SiC single crystal substrate, thereby manufacturing a substrate in which a SiC single crystal layer is formed on the SiC polycrystalline substrate.

更に、特許文献1には、SiC単結晶基板とSiC多結晶基板とを貼り合わせる工程の前に、SiC単結晶基板に水素イオン注入を行って水素イオン注入層を形成する工程を行い、SiC単結晶基板とSiC多結晶基板とを貼り合わせる工程の後、SiC単結晶基板を薄膜化する工程の前に、350℃以下の温度で熱処理を行い、SiC単結晶基板を薄膜化する工程を、水素イオン注入層にて機械的に剥離する工程とするSiC基板の製造方法が記載されている。 Furthermore, Patent Document 1 describes a method for manufacturing a SiC substrate in which a step of implanting hydrogen ions into the SiC single crystal substrate to form a hydrogen ion implanted layer is performed before the step of bonding the SiC single crystal substrate and the SiC polycrystalline substrate, and after the step of bonding the SiC single crystal substrate and the SiC polycrystalline substrate, and before the step of thinning the SiC single crystal substrate, a heat treatment is performed at a temperature of 350°C or less, and the step of thinning the SiC single crystal substrate is a step of mechanically peeling it off at the hydrogen ion implanted layer.

このような方法により、1つのSiC単結晶のインゴットからより多くのSiC基板が得られるようになった。 This method makes it possible to produce many more SiC substrates from a single SiC single crystal ingot.

特開2009-117533号公報JP 2009-117533 A 特開平10-251062号公報Japanese Patent Application Publication No. 10-251062

しかしながら、前記記載の方法で製造されたSiC基板は大部分が多結晶基板である。そのため、SiC単結晶基板とSiC単結晶基板とを貼り合わせたSiC基板の反りの大きさは、SiC多結晶基板の反りの大きさが支配的となる。そのため、SiC多結晶基板とSiC単結晶基板とを貼り合わせた後のデバイス製造工程において、SiC基板の反りが大きいと、フォトリソグラフィ工程におけるパターン形成不良や、イオン注入工程におけるイオン侵入深さが不均一となるなどの問題が生じる。そのため、SiC多結晶基板の反りは小さいことが求められる。 However, most SiC substrates manufactured by the above-described method are polycrystalline substrates. Therefore, the magnitude of warping of a SiC substrate formed by bonding a SiC single crystal substrate to a SiC single crystal substrate is dominated by the magnitude of warping of the SiC polycrystalline substrate. Therefore, in the device manufacturing process after bonding the SiC polycrystalline substrate to the SiC single crystal substrate, if the SiC substrate has a large warp, problems such as poor pattern formation in the photolithography process and non-uniform ion penetration depth in the ion implantation process will occur. Therefore, it is required that the SiC polycrystalline substrate has a small warp.

このようなSiC多結晶基板の反りが大きい課題に対し、例えば特許文献2においては、CVD法によるSiC多結晶膜の成膜に用いるカーボン支持基板の熱膨張係数を(3.0~5.0)×10-6(/K)の範囲とし、SiC多結晶膜の熱膨張係数(4.3~4.5)×10-6(/K)と近い熱膨張係数のカーボン支持基板を適用することで、熱膨張係数の差異によって生じ得る、SiC多結晶膜を成膜後のカーボン支持基板を冷却する過程におけるカーボン支持基板とSiC多結晶膜との体積収縮差を低減し、体積収縮差によって生じるSiC多結晶膜に生じる応力を低減することで、反りを低減させたSiC多結晶膜を得る方法が示されている。 In response to the problem of significant warping of such SiC polycrystalline substrates, for example, Patent Document 2 discloses a method of obtaining a SiC polycrystalline film with reduced warping by using a carbon support substrate used in depositing a SiC polycrystalline film by CVD with a thermal expansion coefficient in the range of (3.0 to 5.0 ) x 10-6 (/K) and using a carbon support substrate with a thermal expansion coefficient close to that of the SiC polycrystalline film, which is (4.3 to 4.5) x 10-6 (/K), thereby reducing the difference in volumetric shrinkage between the carbon support substrate and the SiC polycrystalline film during the process of cooling the carbon support substrate after depositing the SiC polycrystalline film, which may occur due to the difference in thermal expansion coefficients, and reducing the stress generated in the SiC polycrystalline film due to the difference in volumetric shrinkage.

しかしながら、SiC多結晶膜の反りを発生させる要因としては、カーボン支持基板とSiC多結晶膜の熱膨張係数の差異による、上記冷却する過程における体積収縮差だけでなく、SiC多結晶膜を構成している各結晶粒の結晶配向(例えば(0001)面の向きなど)の状態にも大きく依存することが判った。すなわち、各結晶粒の結晶配向が不均一な状態であると、カーボン支持基板側に成長したSiC多結晶膜は、上記冷却する過程において体積収縮差により受けるSiC多結晶膜の成長方向に垂直な応力を、各結晶粒内の塑性的な構造変態により低減する程度が弱くなり、結果としてSiC多結晶膜の表面よりもカーボン支持基板側に成長したSiC多結晶膜の残留応力の方が大きくなる。 However, it has been found that the factors that cause warping of the SiC polycrystalline film are not only the difference in volumetric shrinkage during the cooling process due to the difference in thermal expansion coefficient between the carbon support substrate and the SiC polycrystalline film, but also the state of the crystal orientation of each crystal grain that constitutes the SiC polycrystalline film (for example, the orientation of the (0001) plane). In other words, if the crystal orientation of each crystal grain is non-uniform, the SiC polycrystalline film grown on the carbon support substrate side is less able to reduce the stress perpendicular to the growth direction of the SiC polycrystalline film due to the difference in volumetric shrinkage during the cooling process through plastic structural transformation within each crystal grain, and as a result, the residual stress of the SiC polycrystalline film grown on the carbon support substrate side is greater than that of the surface of the SiC polycrystalline film.

一方でカーボン支持基板の体積変化に拘束され難いSiC多結晶膜の表面となる成長終端側(以下、「成長面側」とする場合がある)のSiC多結晶膜は、上記冷却する過程において体積収縮する場合に、カーボン支持基板の体積収縮による応力をカーボン支持基板側よりも受け難く、カーボン支持基板側と比較して成長面側の残留応力が小さくなる。このSiC多結晶膜におけるカーボン支持基板側と成長面側に内在する残留応力の差の大きさが、カーボン支持基板を除去後に得られるSiC多結晶膜の反りの大きさを決める主要因である。そのため、各結晶粒の結晶配向が不均一であるとカーボン支持基板を除去後のSiC多結晶膜の反りが大きくなり、その後、SiC多結晶膜をSiC多結晶基板へ加工する工程において、SiC多結晶膜に生じた粒径が変化する箇所を削り取っても、反りの程度が必要十分に小さくならないという課題があった。 On the other hand, the SiC polycrystalline film on the growth end side (hereinafter sometimes referred to as the "growth surface side"), which is the surface of the SiC polycrystalline film that is less likely to be restricted by the volumetric change of the carbon support substrate, is less susceptible to stress due to the volumetric shrinkage of the carbon support substrate than the carbon support substrate side when it shrinks in volume during the cooling process, and the residual stress on the growth surface side is smaller than that on the carbon support substrate side. The magnitude of the difference in residual stress inherent in the carbon support substrate side and the growth surface side of this SiC polycrystalline film is the main factor that determines the magnitude of warping of the SiC polycrystalline film obtained after removing the carbon support substrate. Therefore, if the crystal orientation of each crystal grain is non-uniform, the warping of the SiC polycrystalline film after removing the carbon support substrate becomes large, and thereafter, in the process of processing the SiC polycrystalline film into a SiC polycrystalline substrate, even if the areas where the grain size changes in the SiC polycrystalline film are scraped off, the degree of warping does not become sufficiently small.

また、SiC多結晶膜をSiC多結晶基板へ加工する工程において、SiC多結晶膜を所定の厚みおよび平坦度となるように整えるための面研削や面研磨の加工などにおいて、SiC多結晶膜の反りが大きいことに起因した厚み、平坦度あるいは反りの不良等の加工不良が多発するなど、SiC多結晶基板への加工工程での歩留まりを悪化させる要因ともなっていた。加えて、これらの加工不良を改善させることを目的に、例えばCVD法による成膜によってSiC多結晶膜の厚みを大きくすると、原料ガスやキャリアガス等の使用量の増加や成膜時間が長くなることにより、SiC多結晶膜の製造コストや生産性が悪化していた。 In addition, in the process of processing the SiC polycrystalline film into a SiC polycrystalline substrate, in processes such as surface grinding and surface polishing to adjust the SiC polycrystalline film to a specified thickness and flatness, processing defects such as poor thickness, flatness, or warping due to the large warping of the SiC polycrystalline film occur frequently, which is also a factor in reducing the yield in the processing process into a SiC polycrystalline substrate. In addition, if the thickness of the SiC polycrystalline film is increased by deposition using a CVD method, for example, in order to improve these processing defects, the amount of raw material gas and carrier gas used increases and the deposition time becomes longer, resulting in a deterioration in the manufacturing cost and productivity of the SiC polycrystalline film.

本発明はこのような問題点に着目してなされたもので、その課題とするところは、CVD法によってカーボン支持基板上に窒素ドーピングガスとともにSiC多結晶膜を成膜し、カーボン支持基板より分離したSiC多結晶膜の反りを緩和することで、SiC多結晶基板を加工製造する際の歩留まりやコスト、生産性が悪化するという課題を解決し、基板の反りを低減した高導電率のSiC多結晶基板を得ることのできる、炭化珪素多結晶膜の成膜方法および炭化珪素多結晶基板の製造方法を提供することにある。 The present invention was made with a focus on these problems, and its objective is to provide a method for forming a silicon carbide polycrystalline film and a method for manufacturing a silicon carbide polycrystalline substrate, which solves the problems of the deterioration of yield, cost, and productivity when processing and manufacturing a SiC polycrystalline substrate by forming a SiC polycrystalline film together with nitrogen doping gas on a carbon support substrate by a CVD method and mitigating the warping of the SiC polycrystalline film separated from the carbon support substrate, thereby obtaining a SiC polycrystalline substrate with high conductivity and reduced substrate warping.

本発明者は、上記課題を解決するため鋭意研究を行った結果、CVD法によってカーボン支持基板上に窒素ドーピングガスとともに原料ガスを導入してSiC多結晶膜を成膜する工程において、SiC成膜方向に対するカーボン製支持基板の平行方向の熱膨張係数αpと垂直方向の熱膨張係数αvの比αv/αpが所定範囲内である構造異方性が大きいカーボン材質を支持基板に用いることで、SiC多結晶膜の反りを低減させることを見出すに至った。 The inventors conducted extensive research to solve the above problems, and discovered that in the process of depositing a SiC polycrystalline film by CVD by introducing a raw material gas together with a nitrogen doping gas onto a carbon support substrate, warping of the SiC polycrystalline film can be reduced by using a carbon material with large structural anisotropy for the support substrate, in which the ratio αv/αp of the thermal expansion coefficient αp in the parallel direction of the carbon support substrate to the direction of SiC film deposition and the thermal expansion coefficient αv in the perpendicular direction is within a predetermined range.

上記課題を解決するために、本発明の炭化珪素多結晶膜の成膜方法は、化学的気相成長法により、窒素ガス、ケイ素系ガス、および炭素系ガスを用いて、厚さが300μm~10mmのカーボン製支持基板に厚さが300μm~1200μmの炭化珪素多結晶膜を成膜する成膜工程を含み、前記カーボン製支持基板は、厚さ方向に対して平行な方向の熱膨張係数をαpとし、厚さ方向に対して直交する方向の熱膨張係数をαvとした場合に、αv/αp=2.5~4.0である。 In order to solve the above problems, the method for forming a silicon carbide polycrystalline film of the present invention includes a deposition process in which a silicon carbide polycrystalline film having a thickness of 300 μm to 1200 μm is formed on a carbon support substrate having a thickness of 300 μm to 10 mm by chemical vapor deposition using nitrogen gas, silicon-based gas, and carbon-based gas, and the carbon support substrate has a thermal expansion coefficient of αv/αp = 2.5 to 4.0, where αp is the thermal expansion coefficient parallel to the thickness direction and αv is the thermal expansion coefficient perpendicular to the thickness direction.

前記αは1.0×10-6(/K)~6.0×10-6(/K)であり、前記αvは1.0×10-6(/K)~6.0×10-6(/K)であってもよい。 The α p may be in the range of 1.0×10 −6 (/K) to 6.0×10 −6 (/K), and the α v may be in the range of 1.0×10 −6 (/K) to 6.0× 10 −6 (/K).

前記成膜工程において前記炭化珪素多結晶膜を成膜する成膜温度は1200~1500℃であってもよい。 The film formation temperature for forming the silicon carbide polycrystalline film in the film formation process may be 1200 to 1500°C.

また、上記課題を解決するために、本発明の炭化珪素多結晶基板の製造方法は、上記本発明の炭化珪素多結晶膜の成膜方法により得た前記カーボン製支持基板と前記炭化珪素多結晶膜を備える積層体から、前記カーボン製支持基板を燃焼させて除去する燃焼除去工程を含む。 In order to solve the above problem, the method for producing a silicon carbide polycrystalline substrate of the present invention includes a burning and removing step of burning and removing the carbon support substrate from the laminate including the carbon support substrate and the silicon carbide polycrystalline film obtained by the method for forming a silicon carbide polycrystalline film of the present invention.

前記燃焼除去工程後、前記炭化珪素多結晶膜の表面を研磨する研磨工程を含んでもよい。 After the burning and removing process, a polishing process may be included in which the surface of the silicon carbide polycrystalline film is polished.

本発明の炭化珪素多結晶膜の成膜方法および炭化珪素多結晶基板の製造方法によれば、CVD法によってカーボン支持基板上に窒素ドーピングガスとともにSiC多結晶膜を成膜し、カーボン支持基板より分離したSiC多結晶膜の反りを緩和することで、SiC多結晶基板を加工製造する際の歩留まりやコスト、生産性が悪化するという課題を解決し、基板の反りを低減した高導電率のSiC多結晶基板を得ることができる。 According to the method for forming a silicon carbide polycrystalline film and the method for manufacturing a silicon carbide polycrystalline substrate of the present invention, a SiC polycrystalline film is formed on a carbon support substrate by CVD together with nitrogen doping gas, and warping of the SiC polycrystalline film separated from the carbon support substrate is mitigated, thereby solving the problems of deterioration in yield, cost, and productivity when processing and manufacturing SiC polycrystalline substrates, and a highly conductive SiC polycrystalline substrate with reduced substrate warping can be obtained.

本発明の炭化珪素多結晶膜の成膜方法を実施した場合のカーボン製支持基板および炭化珪素多結晶膜の側面断面を示す概略図である。1 is a schematic diagram showing a cross-sectional side view of a carbon support substrate and a silicon carbide polycrystalline film when a method for forming a silicon carbide polycrystalline film of the present invention is carried out; 本発明の炭化珪素多結晶膜の成膜方法とは異なる成膜方法を実施した場合のカーボン製支持基板および炭化珪素多結晶膜の側面断面を示す概略図である。1 is a schematic diagram showing a cross-sectional side view of a carbon support substrate and a silicon carbide polycrystalline film when a film formation method different from the silicon carbide polycrystalline film formation method of the present invention is carried out. FIG. カーボン製支持基板の一つの結晶粒とその結晶内部構造の配向を示した側面断面を示す概略図である。FIG. 2 is a schematic diagram showing a cross-sectional side view of one crystal grain of a carbon support substrate and the orientation of its internal crystal structure.

以下、本発明の実施の形態について詳細に説明するが、本発明は、この実施形態に限定されるものではない。 The following describes in detail an embodiment of the present invention, but the present invention is not limited to this embodiment.

[炭化珪素多結晶膜の成膜方法]
本発明の炭化珪素多結晶膜の成膜方法は、以下に説明する成膜工程を含む。
[Method of forming silicon carbide polycrystalline film]
The method for forming a silicon carbide polycrystalline film of the present invention includes the film forming steps described below.

〈成膜工程〉
本工程は、化学的気相成長法により、窒素ガス、ケイ素系ガス、および炭素系ガスを用いて、厚さが300μm~10mmのカーボン製支持基板に厚さが300μm~1200μmの炭化珪素多結晶膜を成膜する工程である。
<Film formation process>
This process is a process for forming a silicon carbide polycrystalline film having a thickness of 300 μm to 1200 μm on a carbon support substrate having a thickness of 300 μm to 10 mm by chemical vapor deposition using nitrogen gas, silicon-based gas, and carbon-based gas.

例えば、カーボン製支持基板を成膜装置の反応炉内に固定し、減圧状態でAr等の不活性ガスを流しながら炉内を反応温度まで昇温させる。反応温度に達したら、不活性ガスを止め、炉内にケイ素系ガスおよび炭素系ガス等の原料ガス、ドーパントガスとして窒素ガスおよびキャリアガス等を供給し、大気圧下においてカーボン製支持基板の表面や気相での化学反応を所定時間行うことにより、炭化珪素多結晶膜を成膜することができる。 For example, a carbon support substrate is fixed in the reactor of a film-forming device, and the temperature inside the reactor is raised to the reaction temperature while flowing an inert gas such as Ar under reduced pressure. When the reaction temperature is reached, the inert gas is stopped, and raw material gases such as silicon-based gas and carbon-based gas, and nitrogen gas and carrier gas as dopant gases are supplied into the reactor, and a chemical reaction is carried out on the surface of the carbon support substrate and in the gas phase at atmospheric pressure for a predetermined period of time, thereby forming a silicon carbide polycrystalline film.

(原料ガス)
原料ガスとしては、SiC多結晶膜を成膜することができれば、特に限定されず、一般的に使用されるSi系原料ガスやC系原料ガスを用いることができる。Si系原料ガスとしては、例えば、シラン(SiH4)を用いることができるほか、モノクロロシラン(SiH3Cl)、ジクロロシラン(SiH2Cl2)、トリクロロシラン(SiHCl3)、テトラクロロシラン(SiCl4)などのエッチング作用があるClを含む、塩素系Si原料含有ガス(クロライド系原料)を用いることもできる。また、C系原料ガスとしては、例えば、メタン(CH4)やプロパン(C38)アセチレン(C22)等の炭化水素ガスを用いることができる。また、上記のほか、トリクロロメチルシラン(CH3Cl3Si)、トリクロロフェニルシラン(C65Cl3Si)、ジクロロメチルシラン(CH4Cl2Si)、ジクロロジメチルシラン((CH32SiCl2)、クロロトリメチルシラン((CH3)3SiCl)等のSiとCとを両方含むガスも、原料ガスとして用いることができる。
(raw gas)
The source gas is not particularly limited as long as it can form a SiC polycrystalline film, and generally used Si-based source gas or C-based source gas can be used. As the Si-based source gas, for example, silane (SiH 4 ) can be used, and chlorine-based Si source-containing gas (chloride source) containing Cl having an etching effect, such as monochlorosilane (SiH 3 Cl), dichlorosilane (SiH 2 Cl 2 ), trichlorosilane (SiHCl 3 ), and tetrachlorosilane (SiCl 4 ), can also be used. As the C-based source gas, for example, hydrocarbon gas such as methane (CH 4 ), propane (C 3 H 8 ), and acetylene (C 2 H 2 ) can be used. In addition to the above, gases containing both Si and C, such as trichloromethylsilane ( CH3Cl3Si ), trichlorophenylsilane ( C6H5Cl3Si ) , dichloromethylsilane ( CH4Cl2Si), dichlorodimethylsilane (( CH3 ) 2SiCl2 ), and chlorotrimethylsilane (( CH3 ) 3SiCl ), can also be used as source gases.

(窒素ガス)
また、これらの原料ガスと同時に、目標とする導電率に見合う量の不純物ドーピングガスを同時に供給する。例えば、導電型をn型とする場合には窒素(N2)ガス、p型とする場合にはトリメチルアルミニウム(TMA)ガスを用いることができ、本発明では窒素ガスを用いることができる。
(Nitrogen gas)
In addition, an impurity doping gas is supplied simultaneously with these source gases in an amount appropriate for the desired conductivity. For example, nitrogen ( N2 ) gas can be used to make the conductivity type n-type, and trimethylaluminum (TMA) gas can be used to make the conductivity type p-type. In the present invention, nitrogen gas can be used.

(キャリアガス)
さらに、これらの原料ガスおよび窒素ガスと同時に、キャリアガスを用いることができる。キャリアガスとしては、炭化珪素多結晶膜の成膜を阻害することなく、原料ガスをカーボン製支持基板へ展開することができれば、一般的に使用されるキャリアガスを用いることができる。例えば、熱伝導率に優れ、炭化珪素に対してエッチング作用がある水素(H2)を用いることができる。
(Carrier gas)
Furthermore, a carrier gas can be used together with the source gas and the nitrogen gas. As the carrier gas, any commonly used carrier gas can be used as long as it can spread the source gas onto the carbon support substrate without impeding the formation of the silicon carbide polycrystalline film. For example, hydrogen (H 2 ), which has excellent thermal conductivity and an etching effect on silicon carbide, can be used.

前記成膜工程において、前記炭化珪素多結晶膜を成膜する成膜温度は、大きな反りが発生しないように炭化珪素多結晶の結晶配向が一定程度に揃った結晶粒を生成できる温度域であれば特に制限されるものではない。例えば、炭化珪素多結晶膜の反りを必要十分に抑制させるには、成長面が(111)面となる立方晶構造の炭化珪素結晶粒が生成しやすい1200~1500℃とすることが好ましい。 In the film formation process, the film formation temperature for forming the silicon carbide polycrystalline film is not particularly limited as long as it is within a temperature range in which crystal grains with a certain degree of alignment in the crystal orientation of the silicon carbide polycrystals can be produced so that significant warping does not occur. For example, in order to sufficiently suppress warping of the silicon carbide polycrystalline film, it is preferable to set the temperature at 1200 to 1500°C, at which silicon carbide crystal grains with a cubic crystal structure whose growth surface is the (111) plane are likely to be produced.

(成膜する厚み)
炭化珪素多結晶基板の規格としてその厚みが350μmである場合があり、これを考慮して、成膜工程では炭化珪素多結晶膜の厚みが300μm~1200μmとなるように成膜することができる。例えば、厚みが350μmの炭化珪素多結晶基板を得るには、研磨工程や面研削工程における研磨や研削によって厚みが薄くなることを考慮して、成膜する炭化珪素多結晶膜の厚みを400μmとすることができる。なお、厚みが300μm未満の場合には、内部応力の影響で炭化珪素多結晶膜の反りが大きくなるおそれがある。また、厚みが1200μmより厚いと、炭化珪素多結晶基板の加工や製造過程における研磨工程や面研削工程において、研磨量や研削量が多くなり、材料のロスが多くなるおそれがある。
(Thickness of film)
The silicon carbide polycrystalline substrate may have a standard thickness of 350 μm, and in consideration of this, the silicon carbide polycrystalline film may be formed to a thickness of 300 μm to 1200 μm in the film formation process. For example, to obtain a silicon carbide polycrystalline substrate having a thickness of 350 μm, the thickness of the silicon carbide polycrystalline film to be formed may be 400 μm, taking into consideration that the thickness is reduced by polishing and grinding in the polishing process and surface grinding process. If the thickness is less than 300 μm, the warping of the silicon carbide polycrystalline film may be large due to the influence of internal stress. If the thickness is greater than 1200 μm, the polishing amount and grinding amount may be large in the polishing process and surface grinding process in the processing and manufacturing process of the silicon carbide polycrystalline substrate, and the loss of material may be large.

〈カーボン製支持基板〉
以下、図1~3を参照しつつ、本発明において使用するカーボン製支持基板、成膜した炭化珪素多結晶膜に反りが発生する要因、およびその反りを本発明によって低減できる理由について、説明する。
Carbon support substrate
Hereinafter, with reference to FIGS. 1 to 3, the carbon support substrate used in the present invention, the cause of warping in the formed silicon carbide polycrystalline film, and the reason why the present invention can reduce the warping will be described.

図3に、カーボン製支持基板の一つの結晶粒とその結晶内部構造の配向を示した側面断面を示す概略図を示す。カーボンの結晶粒10の断面に付された上下方向の直線は、結晶の配向方向50を示しており、配向方向50が異なる結晶粒10が複数集まってカーボン製支持基板100や150を構成する。 Figure 3 shows a schematic diagram of a side cross section of one crystal grain of a carbon support substrate, showing the orientation of the crystal's internal structure. The vertical straight lines on the cross section of the carbon crystal grain 10 indicate the crystal orientation direction 50, and multiple crystal grains 10 with different orientation directions 50 come together to form the carbon support substrate 100 or 150.

図1に、本発明の炭化珪素多結晶膜の成膜方法を実施した場合のカーボン製支持基板および炭化珪素多結晶膜の側面断面を示す概略図を示す。矢印Aで示す方向を成膜方向として、カーボン製支持基板100に炭化珪素多結晶膜200が成膜している。カーボン製支持基板100は、配向方向50が上下方向を向く結晶粒11が最も多く、右斜め方向を向く結晶粒12や左斜め方向を向く結晶粒13が少量存在しており、上下方向の配向性が強い異方性の黒鉛を加工して得た基板である。このような異方性の黒鉛は、例えば押し出し製法等により得ることができる。 Figure 1 shows a schematic diagram of a side cross section of a carbon support substrate and a silicon carbide polycrystalline film when the silicon carbide polycrystalline film formation method of the present invention is carried out. A silicon carbide polycrystalline film 200 is formed on a carbon support substrate 100 with the direction indicated by arrow A as the film formation direction. The carbon support substrate 100 is a substrate obtained by processing anisotropic graphite with a strong vertical orientation, with the majority of crystal grains 11 having an orientation direction 50 facing up and down, and a small number of crystal grains 12 facing diagonally to the right and crystal grains 13 facing diagonally to the left. Such anisotropic graphite can be obtained, for example, by an extrusion method.

異方性の黒鉛から得られるカーボン製支持基板100は、基板の方向によって熱膨張係数が異なる。本発明では、炭化珪素多結晶膜の成膜方向Aに対して平行方向(カーボン製支持基板100の厚さ方向に対して平行な方向)の熱膨張係数をαp、成膜方向Aに対して垂直方向(カーボン製支持基板100の厚さ方向に対して直交する方向)の熱膨張係数αvの比とした場合、αv/αp=2.5~4.0の範囲となる構造異方性をもつものを、カーボン製支持基板100として用いる。 The carbon support substrate 100 obtained from anisotropic graphite has a different thermal expansion coefficient depending on the direction of the substrate. In the present invention, when the thermal expansion coefficient in a direction parallel to the deposition direction A of the silicon carbide polycrystalline film (parallel to the thickness direction of the carbon support substrate 100) is αp and the thermal expansion coefficient in a direction perpendicular to the deposition direction A (perpendicular to the thickness direction of the carbon support substrate 100) is αv, the carbon support substrate 100 used has a structural anisotropy such that αv/αp = 2.5 to 4.0.

このようなαv/αp=2.5~4.0の範囲となる構造異方性をもつカーボン材質の支持基板を用いることで、成長させる炭化珪素多結晶膜200の結晶配向210を一定方向にある程度揃えることが可能となり、図1では結晶配向210が主に成膜方向に揃っている。このように、結晶配向210が揃った炭化珪素多結晶膜200は、成膜工程後にカーボン製支持基板100と炭化珪素多結晶膜200の積層体を冷却する際に、カーボン製支持基板100の体積収縮により受ける応力を、炭化珪素多結晶膜200の結晶粒220内の塑性的な構造変態により緩和させ、炭化珪素多結晶膜200の支持基板230側と成長面240側の残留応力差を低減させることで、カーボン製支持基板100を燃焼除去後に生じる炭化珪素多結晶膜200の反りを低減させることが可能となる。 By using a carbon support substrate having such structural anisotropy in the range of αv/αp = 2.5 to 4.0, it is possible to align the crystal orientation 210 of the silicon carbide polycrystalline film 200 to a certain extent in a certain direction, and in FIG. 1, the crystal orientation 210 is aligned mainly in the film formation direction. In this way, when the laminate of the carbon support substrate 100 and the silicon carbide polycrystalline film 200 is cooled after the film formation process, the silicon carbide polycrystalline film 200 with the aligned crystal orientation 210 is able to reduce the stress caused by the volumetric contraction of the carbon support substrate 100 by the plastic structural transformation in the crystal grains 220 of the silicon carbide polycrystalline film 200, thereby reducing the residual stress difference between the support substrate 230 side and the growth surface 240 side of the silicon carbide polycrystalline film 200, thereby reducing the warping of the silicon carbide polycrystalline film 200 that occurs after the carbon support substrate 100 is burned and removed.

図2に、本発明の炭化珪素多結晶膜の成膜方法とは異なる成膜方法を実施した場合のカーボン製支持基板および炭化珪素多結晶膜の側面断面を示す概略図を示す。図1の場合と同様に、矢印Aで示す方向を成膜方向として、カーボン製支持基板150に炭化珪素多結晶膜250が成膜している。カーボン製支持基板150は、配向方向50が上下方向や右斜め方向、左斜め方向を向く結晶粒14~16が同程度に存在しており、等方性の黒鉛を加工して得た基板である。このような等方性の黒鉛は、例えば静水圧製法等により得ることができる。 Figure 2 shows a schematic diagram of a cross-sectional side view of a carbon support substrate and a silicon carbide polycrystalline film when a film formation method different from the silicon carbide polycrystalline film formation method of the present invention is carried out. As in the case of Figure 1, a silicon carbide polycrystalline film 250 is formed on a carbon support substrate 150 with the direction indicated by arrow A as the film formation direction. The carbon support substrate 150 is a substrate obtained by processing isotropic graphite, in which crystal grains 14-16 with orientation directions 50 facing up and down, right diagonal directions, and left diagonal directions are present at the same level. Such isotropic graphite can be obtained, for example, by a hydrostatic pressure method.

等方性の黒鉛から得られるカーボン製支持基板150は、カーボン製支持基板100と比較して基板の方向によって熱膨張係数が異ならない。図2ではαv/αp=2.5~4.0の範囲に該当せず、αv/αp≒1.0となる基板を、カーボン製支持基板150として用いる。 The carbon support substrate 150 obtained from isotropic graphite does not have a thermal expansion coefficient that differs depending on the direction of the substrate, as compared to the carbon support substrate 100. In FIG. 2, a substrate that does not fall within the range of αv/αp = 2.5 to 4.0 and for which αv/αp ≈ 1.0 is used as the carbon support substrate 150.

このようなカーボン製支持基板150を用いると、成長させる炭化珪素多結晶膜250の結晶配向260が一定方向に揃わず、不規則に配向する。このように、結晶配向260が揃っていない炭化珪素多結晶膜250は、成膜工程後にカーボン製支持基板150と炭化珪素多結晶膜250の積層体を冷却する際に、カーボン製支持基板150の体積収縮により受ける応力を、炭化珪素多結晶膜250の結晶粒270内の塑性的な構造変態により緩和させることが困難となり、炭化珪素多結晶膜250の支持基板280側と成長面290側の残留応力差を低減させることができないことで、カーボン製支持基板150を燃焼除去後に生じる炭化珪素多結晶膜250の反りの低減させることが困難となる。 When such a carbon support substrate 150 is used, the crystal orientation 260 of the silicon carbide polycrystalline film 250 to be grown is not aligned in a fixed direction, but is irregularly oriented. In this way, when the laminate of the carbon support substrate 150 and the silicon carbide polycrystalline film 250 is cooled after the film formation process, it is difficult to alleviate the stress caused by the volumetric shrinkage of the carbon support substrate 150 through plastic structural transformation within the crystal grains 270 of the silicon carbide polycrystalline film 250, and it is not possible to reduce the residual stress difference between the support substrate 280 side and the growth surface 290 side of the silicon carbide polycrystalline film 250, making it difficult to reduce the warping of the silicon carbide polycrystalline film 250 that occurs after the carbon support substrate 150 is burned and removed.

なお、αv/αpが4.0を超えるカーボン製支持基板100は、現状では入手できず、このような支持基板の挙動は確認することができない。 Note that carbon support substrates 100 with αv/αp exceeding 4.0 are currently unavailable, and the behavior of such support substrates cannot be confirmed.

また、本発明では、厚さが300μm~10mmのカーボン製支持基板を用いる。カーボン製支持基板の厚さが300μm未満と薄すぎると、カーボン製支持基板そのものに反りが生じることで、炭化珪素多結晶膜の反りが修正できない程度に大きくなるおそれがある。一方で、カーボン製支持基板の厚さが10mmを超えて厚すぎると、カーボン製支持基板の燃焼除去に時間がかかって炭化珪素多結晶基板の製造効率が低下する場合がある。 In addition, in the present invention, a carbon support substrate having a thickness of 300 μm to 10 mm is used. If the carbon support substrate is too thin, less than 300 μm, warping may occur in the carbon support substrate itself, causing the warping of the silicon carbide polycrystalline film to become too large to be corrected. On the other hand, if the carbon support substrate is too thick, exceeding 10 mm, it may take a long time to burn and remove the carbon support substrate, reducing the manufacturing efficiency of the silicon carbide polycrystalline substrate.

そして、カーボン製支持基板の熱膨張係数において、αは1.0×10-6(/K)~6.0×10-6(/K)であってもよい。αpがこの範囲であることにより、単結晶構造を持つ粒子で構成されるカーボン製支持基板が得られ易く、結晶配向が揃った炭化珪素多結晶膜が生成しやすい。特に、αが1.0×10-6(/K)~2.0×10-6(/K)であることで、この傾向が顕著となる。また、αpが1.0×10-6(/K)~6.0×10-6(/K)の範囲から外れると、単結晶構造を持つ粒子で構成されるカーボン製支持基板が得られ難くなるおそれがあり、結晶配向が揃った炭化珪素多結晶膜が生成し難くなる場合がある。 In addition, in the thermal expansion coefficient of the carbon support substrate, α p may be 1.0×10 −6 (/K) to 6.0× 10 −6 (/K). When α p is in this range, a carbon support substrate composed of particles having a single crystal structure is easily obtained, and a silicon carbide polycrystalline film having uniform crystal orientation is easily generated. In particular, when α p is 1.0×10 −6 (/K) to 2.0× 10 −6 (/K), this tendency becomes remarkable. Also, when α p is out of the range of 1.0×10 −6 (/K) to 6.0× 10 −6 (/K), it may be difficult to obtain a carbon support substrate composed of particles having a single crystal structure, and it may be difficult to generate a silicon carbide polycrystalline film having uniform crystal orientation.

また、αvは1.0×10-6(/K)~6.0×10-6(/K)であってもよい。αvがこの範囲であることにより、単結晶構造を持つ粒子で構成されるカーボン製支持基板が得られ易く、結晶配向が揃った炭化珪素多結晶膜が生成しやすい。特に、αvが2.5×10-6(/K)~5.0×10-6(/K)であることで、この傾向が顕著となる。また、αvが1.0×10-6(/K)~6.0×10-6(/K)の範囲から外れると、単結晶構造を持つ粒子で構成されるカーボン製支持基板が得られ難くなるおそれがあり、結晶配向が揃った炭化珪素多結晶膜が生成し難くなる場合がある。 Also, αv may be 1.0×10 −6 (/K) to 6.0× 10 −6 (/K). When αv is in this range, a carbon support substrate composed of particles having a single crystal structure is easily obtained, and a silicon carbide polycrystalline film having uniform crystal orientation is easily produced. In particular, when αv is 2.5×10 −6 (/K) to 5.0×10 −6 (/K), this tendency becomes remarkable. When αv is out of the range of 1.0×10 −6 (/K) to 6.0×10 −6 (/K), it may be difficult to obtain a carbon support substrate composed of particles having a single crystal structure, and it may be difficult to produce a silicon carbide polycrystalline film having uniform crystal orientation.

(その他の工程)
本発明の炭化珪素多結晶膜の成膜方法は、上記した成膜工程以外にも、他の工程を含むことができる。例えば、成膜装置内の基板ホルダーにカーボン製支持基板を複数枚セットする工程や、セットしたカーボン製支持基板を加熱する工程、化学蒸着前のカーボン製支持基板に、炭化珪素多結晶膜の成膜を阻害するような何らかの反応が生じないよう、基板を不活性雰囲気下とするべく、アルゴン等の不活性ガスを流通させる工程、成膜工程後に原料ガス、ドーピングガスおよびキャリアガスを停止し、成膜装置の炉内を室温まで冷却させる冷却工程等が挙げられる。
(Other processes)
The method for forming a silicon carbide polycrystalline film of the present invention may include other steps in addition to the above-mentioned film formation step, such as a step of setting a plurality of carbon support substrates on a substrate holder in a film formation apparatus, a step of heating the set carbon support substrates, a step of circulating an inert gas such as argon in order to make the substrate under an inert atmosphere so that no reaction that would inhibit the formation of a silicon carbide polycrystalline film occurs in the carbon support substrate before chemical vapor deposition, and a cooling step of stopping the supply of the source gas, doping gas, and carrier gas after the film formation step and cooling the inside of the furnace of the film formation apparatus to room temperature.

[炭化珪素多結晶基板の製造方法]
次に、本発明の炭化珪素多結晶基板の製造方法について、その一態様を説明する。かかる製造方法は、以下に説明する燃焼除去工程を含む。
[Method for manufacturing silicon carbide polycrystalline substrate]
Next, one embodiment of a method for producing a silicon carbide polycrystalline substrate of the present invention will be described. The method includes a burning and removing step as described below.

〈燃焼除去工程〉
本工程は、上記の炭化珪素多結晶膜の成膜方法により得た前記カーボン製支持基板と前記炭化珪素多結晶膜を備える積層体から、前記カーボン製支持基板を燃焼させて除去する工程である。これにより、カーボン製支持基板が消滅して、反りが抑制された炭化珪素多結晶膜が残り、これが炭化珪素多結晶基板となる。
<Combustion removal process>
This step is a step of burning and removing the carbon support substrate from the laminate including the carbon support substrate and the silicon carbide polycrystalline film obtained by the above-mentioned method for forming a silicon carbide polycrystalline film. As a result, the carbon support substrate disappears and the silicon carbide polycrystalline film with suppressed warpage remains, which becomes the silicon carbide polycrystalline substrate.

カーボン製支持基板の燃焼除去は、空気中で加熱する等の適宜な方法で行うことができる。加熱条件としては、例えば大気雰囲気下にて1000℃程度に加熱する条件が挙げられる。 The carbon support substrate can be removed by burning using an appropriate method such as heating in air. Heating conditions include, for example, heating to about 1000°C in an air atmosphere.

〈研磨工程〉
本発明の炭化珪素多結晶基板の製造方法は、燃焼除去後、前記燃焼除去工程後、前記炭化珪素多結晶膜の表面を研磨する研磨工程を含んでもよい。炭化珪素多結晶基板は、例えば半導体の製造に用いられる基板とするのであれば、半導体製造プロセスで使用できる面精度が必要となる。そこで、本工程により、炭化珪素多結晶膜の表面を平滑化することが好ましい。
<Polishing process>
The method for producing a silicon carbide polycrystalline substrate of the present invention may include a polishing step of polishing the surface of the silicon carbide polycrystalline film after the burnt removal step. If the silicon carbide polycrystalline substrate is to be used as a substrate for semiconductor manufacturing, for example, it needs to have a surface precision that can be used in the semiconductor manufacturing process. Therefore, it is preferable to smooth the surface of the silicon carbide polycrystalline film by this step.

例えば、炭化珪素多結晶膜をダイアモンドスラリーでラップ処理し、ダイアモンドとアルミナとの混合スラリーでハードポリッシュした後に、シリカスラリー(コロイダルシリカ、pH11)でポリッシュするという工程を経て、炭化珪素多結晶基板の表面を平滑化することができる。 For example, the surface of a silicon carbide polycrystalline substrate can be smoothed by lapping a silicon carbide polycrystalline film with a diamond slurry, hard polishing it with a mixed slurry of diamond and alumina, and then polishing it with a silica slurry (colloidal silica, pH 11).

(その他の工程)
本発明の炭化珪素多結晶基板の製造方法は、上記の工程以外にも、他の工程を含むことができる。例えば、炭化珪素多結晶膜によって完全に被覆されたカーボン製支持基板を燃焼除去させるため、燃焼除去工程の前にカーボン製支持基板の側面に付着した炭化珪素多結晶膜の一部を除去してカーボン製支持基板を露出させる露出工程や、研磨工程後の炭化珪素多結晶基板を洗浄する洗浄工程等が挙げられる。また、炭化珪素多結晶膜を所定の厚みへ整えるための面研削工程を含んでもよい。
(Other processes)
The method for producing a silicon carbide polycrystalline substrate of the present invention may include other steps in addition to the steps described above. For example, in order to burn and remove the carbon support substrate completely covered with the silicon carbide polycrystalline film, an exposure step of removing a part of the silicon carbide polycrystalline film attached to the side surface of the carbon support substrate to expose the carbon support substrate before the burning and removing step, and a cleaning step of cleaning the silicon carbide polycrystalline substrate after the polishing step may be included. In addition, a surface grinding step may be included to adjust the silicon carbide polycrystalline film to a predetermined thickness.

露出工程としては、具体的には、ダイアモンドやC-BN(立方晶BN)砥粒を用いたシングルワイヤソーで炭化珪素多結晶膜の外周端部の一部を切断する方法や、研磨ホイールで炭化珪素多結晶膜の外周端部の一部を削り落とすことにより、カーボン基板を露出させることができる。 Specifically, the exposure process can involve cutting off part of the outer edge of the silicon carbide polycrystalline film with a single wire saw using diamond or C-BN (cubic BN) abrasive grains, or by scraping off part of the outer edge of the silicon carbide polycrystalline film with a grinding wheel to expose the carbon substrate.

なお、本発明の炭化珪素多結晶膜の成膜方法であれば、反りの抑制された炭化珪素多結晶基板が得られる。そのため、炭化珪素多結晶基板の加工や製造過程における研磨工程や面研削工程において、炭化珪素多結晶膜の反りが大きいことに起因する厚みの均一性、平坦度あるいは反りが悪化することがなく、反りの小さな高導電率の炭化珪素多結晶基板へ加工製造することが可能となる。 The method for forming a silicon carbide polycrystalline film of the present invention makes it possible to obtain a silicon carbide polycrystalline substrate with reduced warping. Therefore, in the polishing process and surface grinding process in the processing and manufacturing of silicon carbide polycrystalline substrates, the uniformity of thickness, flatness, or warping caused by the large warping of the silicon carbide polycrystalline film does not deteriorate, making it possible to process and manufacture a silicon carbide polycrystalline substrate with low warping and high conductivity.

以下、本発明の実施例について比較例を挙げて具体的に説明する。なお、本発明はこれら実施例によって限定されるものではない。 The following describes the examples of the present invention in detail with comparative examples. Note that the present invention is not limited to these examples.

[実施例1]
(炭化珪素多結晶膜の成膜)
化学的気相成長法に用いる熱CVD装置の反応管内に、直径6インチ、厚み500μm、熱膨張係数がαp=1.0×10-6(/K)、αv=2.5×10-6(/K)、αv/αp=2.5のカーボン製支持基板100を10枚固定し、炉内へArガスを20L/分の流量で流入させながら排気ポンプにより炉内を減圧化した後、1400℃まで加熱し、その後、Arガスを停止させた。次いで、原料ガスとして、1L/分(気体換算、25℃)の流量のSiCl4、1L/分の流量のCH4、ドーピングガスとして50L/分の流量のN2、キャリアガスとして10L/分の流量のH2を、原料ガス等の流通時間を20時間としてカーボン製支持基板100へ流入させ、厚みが約1000μmの炭化珪素多結晶膜200をカーボン製支持基板100のおもて面とうら面の両面へ成膜させた。その後、原料ガス、ドーピングガスおよびキャリアガスの流入を停止し、炉内を室温まで冷却した。
[Example 1]
(Deposition of silicon carbide polycrystalline film)
Ten carbon support substrates 100 with a diameter of 6 inches, a thickness of 500 μm, and thermal expansion coefficients of αp = 1.0 × 10 -6 (/K), αv = 2.5 × 10 -6 (/K), and αv/αp = 2.5 were fixed in the reaction tube of a thermal CVD apparatus used for chemical vapor deposition, and the pressure inside the furnace was reduced using an exhaust pump while Ar gas was flowed into the furnace at a flow rate of 20 L/min.The furnace was then heated to 1400°C, and the Ar gas was then stopped. Next, SiCl4 at a flow rate of 1 L/min (gas equivalent, 25° C.), CH4 at a flow rate of 1 L/min, N2 at a flow rate of 50 L/min as a doping gas, and H2 at a flow rate of 10 L/min as a carrier gas were flowed into the carbon support substrate 100 for 20 hours to form a silicon carbide polycrystalline film 200 having a thickness of about 1000 μm on both the front and back surfaces of the carbon support substrate 100. Thereafter, the flow of the raw material gas, doping gas, and carrier gas was stopped, and the inside of the furnace was cooled to room temperature.

(炭化珪素多結晶基板の製造)
カーボン製支持基板100の側面外周に成膜した炭化珪素多結晶膜のみを研削してカーボン製支持基板100の側面を露出させ、次いで、大気雰囲気下において約1000℃の温度条件下でカーボン製支持基板100を加熱することで燃焼除去し、カーボン製支持基板100と炭化珪素多結晶膜200を分離して、20枚の炭化珪素多結晶基板を得た。
(Production of silicon carbide polycrystalline substrate)
Only the silicon carbide polycrystalline film formed on the outer periphery of the side surface of the carbon support substrate 100 was ground to expose the side surface of the carbon support substrate 100, and then the carbon support substrate 100 was heated under a temperature condition of about 1000° C. in an air atmosphere to burn and remove the silicon carbide polycrystalline film 200, and the carbon support substrate 100 and the silicon carbide polycrystalline film 200 were separated to obtain 20 silicon carbide polycrystalline substrates.

(炭化珪素多結晶基板の反りの測定)
炭化珪素多結晶基板の成長面240の表面の中心線上を、斜入射型光学測定器により測定し、得られた測定値の最大値と最小値との差を反りとした。測定は5点とし、中心、円周端部、および中心と円周端部との間にあり、中心からの距離と円周端部からの距離が同じ地点について、測定した。結果として、実施例1によって得られた炭化珪素多結晶基板の反りは、20枚の平均で100μmであった。表1に、αv/αp、炭化珪素多結晶膜の成膜温度、および炭化珪素多結晶基板の反りの測定結果を示す。
(Measurement of warpage of silicon carbide polycrystalline substrate)
The center line of the surface of the growth surface 240 of the silicon carbide polycrystalline substrate was measured by an oblique incidence type optical measuring device, and the difference between the maximum and minimum values of the obtained measurements was taken as the warpage. Measurements were performed at five points, at the center, the circumferential edge, and points between the center and the circumferential edge that were the same distance from the center and the circumferential edge. As a result, the warpage of the silicon carbide polycrystalline substrate obtained by Example 1 was 100 μm on average for 20 substrates. Table 1 shows the measurement results of αv/αp, the deposition temperature of the silicon carbide polycrystalline film, and the warpage of the silicon carbide polycrystalline substrate.

[実施例2]
熱膨張係数がαp=1.0×10-6(/K)、αv=3.2×10-6(/K)、αv/αp=3.2のカーボン支持基板を用いたこと以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例2によって得られた炭化珪素多結晶基板の反りは、80μmであった。
[Example 2]
Except for using a carbon support substrate having thermal expansion coefficients of αp=1.0× 10−6 (/K), αv= 3.2×10−6 (/K), and αv/αp=3.2, film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Example 2 was 80 μm.

[実施例3]
熱膨張係数がαp=1.0×10-6(/K)、αv=4.0×10-6(/K)、αv/αp=4.0のカーボン支持基板を用いたこと以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例3によって得られた炭化珪素多結晶基板の反りは、60μmであった。
[Example 3]
Except for using a carbon support substrate having thermal expansion coefficients of αp=1.0× 10−6 (/K), αv= 4.0×10−6 (/K), and αv/αp=4.0, film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Example 3 was 60 μm.

[実施例4]
成膜時の温度を1200℃とした以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例4によって得られた炭化珪素多結晶基板の反りは、140μmであった。
[Example 4]
Except for the temperature during film formation being 1200° C., film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Example 4 was 140 μm.

[実施例5]
成膜時の温度を1200℃とした以外は、実施例2と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例5によって得られた炭化珪素多結晶基板の反りは120μmであった。
[Example 5]
The film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 2, except that the film formation temperature was 1200° C. The warpage of the silicon carbide polycrystalline substrate obtained in Example 5 was 120 μm.

[実施例6]
成膜時の温度を1200℃とした以外は、実施例3と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例6によって得られた炭化珪素多結晶基板の反りは110μmであった。
[Example 6]
The film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 3, except that the film formation temperature was 1200° C. The warpage of the silicon carbide polycrystalline substrate obtained in Example 6 was 110 μm.

[実施例7]
成膜時の温度を1500℃とした以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例7によって得られた炭化珪素多結晶基板の反りは150μmであった。
[Example 7]
Except for the temperature during film formation being 1500° C., film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Example 7 was 150 μm.

[実施例8]
成膜時の温度を1500℃とした以外は、実施例2と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例8によって得られた炭化珪素多結晶基板の反りは130μmであった。
[Example 8]
The film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 2, except that the film formation temperature was 1500° C. The warpage of the silicon carbide polycrystalline substrate obtained in Example 8 was 130 μm.

[実施例9]
成膜時の温度を1500℃とした以外は、実施例3と同様の条件として成膜、研削、焼成および反りの測定を行った。実施例9によって得られた炭化珪素多結晶基板の反りは120μmであった。
[Example 9]
The film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 3, except that the film formation temperature was 1500° C. The warpage of the silicon carbide polycrystalline substrate obtained in Example 9 was 120 μm.

[比較例1]
熱膨張係数がαp=1.0×10-6(/K)、αv=1.0×10-6(/K)、αv/αp=1.0のカーボン支持基板を用いたこと以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。比較例1によって得られた炭化珪素多結晶基板の反りは460μmであった。
[Comparative Example 1]
Except for using a carbon support substrate having thermal expansion coefficients of αp=1.0× 10−6 (/K), αv= 1.0×10−6 (/K), and αv/αp=1.0, film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Comparative Example 1 was 460 μm.

[比較例2]
熱膨張係数がαp=2.0×10-6(/K)、αv=3.6×10-6(/K)、αv/αp=1.8のカーボン支持基板を用いたこと以外は、実施例1と同様の条件として成膜、研削、焼成および反りの測定を行った。比較例2によって得られた炭化珪素多結晶基板の反りは220μmであった。
[Comparative Example 2]
Except for using a carbon support substrate having thermal expansion coefficients of αp=2.0× 10−6 (/K), αv= 3.6×10−6 (/K), and αv/αp=1.8, film formation, grinding, firing, and warpage measurement were performed under the same conditions as in Example 1. The warpage of the silicon carbide polycrystalline substrate obtained in Comparative Example 2 was 220 μm.

Figure 0007600612000001
Figure 0007600612000001

[まとめ]
以上より、本発明であれば、炭化珪素多結晶基板を加工製造する際の歩留まりやコスト、生産性が悪化するという課題を解決し、基板の反りを低減した高導電率の炭化珪素多結晶基板を得ることができる。特に、炭化珪素多結晶基板の反りを低減することができるため、横型および縦型のダイオード用炭化珪素基板としてデバイス製造工程に供することが可能である。また、フォトリソグラフィ工程におけるパターン形成不良や、イオン注入工程におけるイオン侵入深さの不均一等を抑制することができ、歩留まりの向上が期待できる。
[summary]
As described above, the present invention solves the problems of the deterioration of yield, cost, and productivity when processing and manufacturing a silicon carbide polycrystalline substrate, and can obtain a silicon carbide polycrystalline substrate with high conductivity and reduced warpage of the substrate. In particular, since the warpage of the silicon carbide polycrystalline substrate can be reduced, it can be used in a device manufacturing process as a silicon carbide substrate for horizontal and vertical diodes. In addition, it is possible to suppress pattern formation defects in a photolithography process and non-uniformity of ion penetration depth in an ion implantation process, and thus an improvement in yield can be expected.

10 結晶粒
11 結晶粒
12 結晶粒
13 結晶粒
14 結晶粒
15 結晶粒
16 結晶粒
50 配向方向
100 カーボン製支持基板
150 カーボン製支持基板
200 炭化珪素多結晶膜
210 結晶配向
220 結晶粒
230 支持基板
240 成長面
250 炭化珪素多結晶膜
260 結晶配向
270 結晶粒
280 支持基板
290 成長面
A 矢印
10 Crystal grain 11 Crystal grain 12 Crystal grain 13 Crystal grain 14 Crystal grain 15 Crystal grain 16 Crystal grain 50 Orientation direction 100 Carbon support substrate 150 Carbon support substrate 200 Silicon carbide polycrystalline film 210 Crystal orientation 220 Crystal grain 230 Support substrate 240 Growth surface 250 Silicon carbide polycrystalline film 260 Crystal orientation 270 Crystal grain 280 Support substrate 290 Growth surface A Arrow

Claims (4)

化学的気相成長法により、窒素ガス、珪素系ガス、および炭素系ガスを用いて、厚さが300μm~10mmのカーボン製支持基板に厚さが300μm~1200μmの炭化珪素多結晶膜を成膜する成膜工程を含み、
前記カーボン製支持基板は、厚さ方向に対して平行な方向の熱膨張係数をαpとし、厚さ方向に対して直交する方向の熱膨張係数をαvとした場合に、αv/αp=2.5~4.0であり、前記αpは1.0×10-6(/K)(室温~450℃)2.0×10-6(/K)(室温~450℃)であり、前記αvは2.5×10-6(/K)(室温~450℃)~6.0×10-6(/K)(室温~450℃)である、炭化珪素多結晶膜の成膜方法。
The method includes a film formation step of forming a silicon carbide polycrystalline film having a thickness of 300 μm to 1200 μm on a carbon support substrate having a thickness of 300 μm to 10 mm by a chemical vapor deposition method using nitrogen gas, a silicon-based gas, and a carbon-based gas;
wherein the carbon support substrate has a thermal expansion coefficient αv/αp=2.5 to 4.0, where αp is a thermal expansion coefficient parallel to a thickness direction and αv is a thermal expansion coefficient perpendicular to the thickness direction, αp is 1.0×10 -6 (/K) (room temperature to 450° C.) to 2.0 ×10 -6 (/K) (room temperature to 450° C.) , and αv is 2.5×10 -6 (/K) (room temperature to 450° C.) to 6.0×10 -6 (/K) (room temperature to 450° C.) .
前記成膜工程において前記炭化珪素多結晶膜を成膜する成膜温度は1200~1500℃である、請求項1に記載の炭化珪素多結晶膜の成膜方法。 The method for forming a silicon carbide polycrystalline film according to claim 1, wherein the film forming temperature for forming the silicon carbide polycrystalline film in the film forming step is 1200 to 1500°C. 請求項1または2に記載の炭化珪素多結晶膜の成膜方法により得た前記カーボン製支持基板と前記炭化珪素多結晶膜を備える積層体から、前記カーボン製支持基板を燃焼させて除去する燃焼除去工程を含む、炭化珪素多結晶基板の製造方法。 A method for producing a silicon carbide polycrystalline substrate, comprising a burning and removing step of burning and removing the carbon support substrate from a laminate including the carbon support substrate and the silicon carbide polycrystalline film obtained by the method for forming a silicon carbide polycrystalline film according to claim 1 or 2. 前記燃焼除去工程後、前記炭化珪素多結晶膜の表面を研磨する研磨工程を含む、請求項3に記載の炭化珪素多結晶基板の製造方法。 The method for producing a silicon carbide polycrystalline substrate according to claim 3, further comprising a polishing step of polishing the surface of the silicon carbide polycrystalline film after the burning and removing step.
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