JP2021066624A - Manufacturing method of silicon carbide polycrystalline substrate - Google Patents

Manufacturing method of silicon carbide polycrystalline substrate Download PDF

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JP2021066624A
JP2021066624A JP2019192013A JP2019192013A JP2021066624A JP 2021066624 A JP2021066624 A JP 2021066624A JP 2019192013 A JP2019192013 A JP 2019192013A JP 2019192013 A JP2019192013 A JP 2019192013A JP 2021066624 A JP2021066624 A JP 2021066624A
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silicon carbide
carbide polycrystalline
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泰三 北川
Taizo Kitagawa
泰三 北川
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Sumitomo Metal Mining Co Ltd
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Abstract

To provide a manufacturing method of a silicon carbide polycrystalline substrate, for manufacturing a silicon carbide polycrystalline substrate having small warp, by suppressing generation of large warp on the silicon carbide polycrystalline substrate.SOLUTION: A manufacturing method of a silicon carbide polycrystalline substrate includes a first silicon carbide polycrystalline film deposition step for depositing a first silicon carbide polycrystalline film at the temperature of 1,400°C-1,500°C on a support substrate by a chemical vapor growth method, and a second silicon carbide polycrystalline film deposition step for depositing a second silicon carbide polycrystalline film on the first silicon carbide polycrystalline film, at the temperature of 1,200°C-1,300°C, namely, at a lower temperature by 100°C-200°C than a deposition temperature of the first silicon carbide polycrystalline film.SELECTED DRAWING: Figure 2

Description

本発明は、炭化ケイ素多結晶基板の製造方法に関する。 The present invention relates to a method for producing a silicon carbide polycrystalline substrate.

炭化ケイ素は、ケイ素と炭素で構成される、化合物半導体材料である。炭化ケイ素は、絶縁破壊電界強度がケイ素の10倍で、バンドギャップがケイ素の3倍であり、半導体材料として優れている。さらに、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、ケイ素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。 Silicon carbide is a compound semiconductor material composed of silicon and carbon. Silicon carbide has an dielectric breakdown electric field strength 10 times that of silicon and a band gap 3 times that of silicon, and is excellent as a semiconductor material. Furthermore, since it is possible to control the p-type and n-type required for manufacturing devices in a wide range, it is expected as a material for power devices that exceeds the limit of silicon.

しかしながら、炭化ケイ素半導体は、従来広く普及しているケイ素半導体と比較して、大面積の炭化ケイ素単結晶基板を得ることが難しく、製造工程も複雑である。これらの理由から、炭化ケイ素半導体は、ケイ素半導体と比較して大量生産が難しく、高価であった。 However, in the silicon carbide semiconductor, it is difficult to obtain a silicon carbide single crystal substrate having a large area as compared with the silicon semiconductor which has been widely used in the past, and the manufacturing process is complicated. For these reasons, silicon carbide semiconductors are more difficult to mass-produce and more expensive than silicon semiconductors.

これまでにも、炭化ケイ素半導体のコストを下げるために、様々な工夫が行われてきた。例えば、特許文献1には、炭化ケイ素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/cm以下の炭化ケイ素単結晶基板と炭化ケイ素多結晶基板を準備し、前記炭化ケイ素単結晶基板と前記炭化ケイ素多結晶基板とを貼り合わせる工程を行い、その後、単結晶基板を薄膜化する工程を行い、多結晶基板上に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。 So far, various measures have been taken to reduce the cost of silicon carbide semiconductors. For example, Patent Document 1 describes a method for manufacturing a silicon carbide substrate, wherein at least a silicon carbide single crystal substrate and a silicon carbide polycrystalline substrate having a micropipe density of 30 pieces / cm 2 or less are prepared, and the silicon carbide is described. It is described that a step of laminating a single crystal substrate and the silicon carbide polycrystalline substrate is performed, and then a step of thinning the single crystal substrate is performed to produce a substrate having a single crystal layer formed on the polycrystalline substrate. ing.

更に、特許文献1には、単結晶基板と多結晶基板とを貼り合わせる工程の前に、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、単結晶基板と多結晶基板とを貼り合わせる工程の後、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、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炭化ケイ素基板の製造方法が記載されている。 Further, in Patent Document 1, before the step of bonding the single crystal substrate and the polycrystalline substrate, a step of injecting hydrogen ions into the single crystal substrate to form a hydrogen ion injection layer is performed, and the single crystal substrate and the polycrystalline substrate are combined. After the step of bonding with the crystal substrate and before the step of thinning the single crystal substrate, the step of performing heat treatment at a temperature of 350 ° C. or lower to thin the single crystal substrate is mechanically performed by the hydrogen ion injection layer. Describes a method for manufacturing a silicon carbide substrate as a step of peeling.

このような方法により、1つの炭化ケイ素単結晶インゴットからより多くの炭化ケイ素貼り合わせ基板が得られるようになった。 By such a method, more silicon carbide bonded substrates can be obtained from one silicon carbide single crystal ingot.

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

特許文献1の方法で製造された炭化ケイ素貼り合わせ基板の大部分が、多結晶基板である。よって、多結晶基板と単結晶基板を貼り合わせた、炭化ケイ素貼り合わせ基板の反りの大きさは、多結晶基板の反りの大きさによる影響が支配的となる。炭化ケイ素貼り合わせ基板を用いたデバイス製造工程において、炭化ケイ素貼り合わせ基板の反り量が大きいと、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ため、炭化ケイ素貼り合わせ基板に用いる多結晶基板の反りは小さいことが求められる。 Most of the silicon carbide bonded substrates produced by the method of Patent Document 1 are polycrystalline substrates. Therefore, the size of the warp of the silicon carbide bonded substrate, which is obtained by bonding the polycrystalline substrate and the single crystal substrate, is dominated by the influence of the warp size of the polycrystalline substrate. In the device manufacturing process using the silicon carbide bonded substrate, if the amount of warpage of the silicon carbide bonded substrate is large, there are problems such as poor pattern formation in the photolithography process and non-uniform ion implantation depth in the ion implantation process. Therefore, the warpage of the polycrystalline substrate used for the silicon carbide bonded substrate is required to be small.

以上のような、炭化ケイ素多結晶基板の反りについての課題に対して、特許文献2においては、化学的気相成長法による炭化ケイ素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3.0×10−6/K〜5.0×10−6/Kの範囲とすることが記載されている。炭化ケイ素多結晶膜の熱膨張係数(およそ4.3×10−6/K〜4.5×10−6/K)と近い熱膨張係数のカーボン支持基板を用いることで、カーボン支持基板と炭化ケイ素多結晶膜との熱膨張係数の差異による、炭化ケイ素多結晶膜を成膜した後に冷却する時の体積収縮差を低減し、炭化ケイ素多結晶膜に生じる応力を低減することで、反りを低減させた炭化ケイ素多結晶膜を得る方法が示されている。
しかしながら、炭化ケイ素多結晶膜の反りを発生させる要因は、上記の要因だけではない。炭化ケイ素多結晶膜とは異なる材質のカーボン支持基板上へ炭化ケイ素多結晶膜を成膜することにより、炭化ケイ素多結晶膜が成膜する初期には炭化ケイ素多結晶の粒径が小さく、その後、炭化ケイ素多結晶膜の成膜が進むと形成される炭化ケイ素多結晶の粒径が大きくなる。これにより、成膜した炭化ケイ素多結晶膜内の炭化ケイ素多結晶の粒径に差が生じることに起因して、炭化ケイ素多結晶膜内の内部応力に差が生じることも、炭化ケイ素多結晶膜の反りを大きくする一因となっている。支持基板を除去して炭化ケイ素多結晶膜を炭化ケイ素多結晶基板へ加工する工程において、炭化ケイ素達結晶膜において粒径が変化する箇所を削り取っても、炭化ケイ素多結晶基板の反りが十分に小さくならないという課題があった。
In response to the above-mentioned problems related to the warp of the silicon carbide polycrystalline substrate, Patent Document 2 describes the coefficient of thermal expansion of the carbon support substrate used for forming the silicon carbide polycrystalline film by the chemical vapor deposition method. it is described that in the range of 3.0 × 10 -6 /K~5.0×10 -6 / K . By using a carbon support substrate of the thermal expansion coefficient (approx. 4.3 × 10 -6 /K~4.5×10 -6 / K ) and thermal expansion coefficient near the silicon carbide polycrystal film, a carbon support substrate carbide Warpage is reduced by reducing the difference in volume shrinkage when the silicon carbide polycrystalline film is formed and then cooled due to the difference in the coefficient of thermal expansion from that of the silicon carbide polycrystalline film, and by reducing the stress generated in the silicon carbide polycrystalline film. A method for obtaining a reduced silicon carbide polycrystalline film has been shown.
However, the above-mentioned factors are not the only factors that cause the warp of the silicon carbide polycrystalline film. By forming a silicon carbide polycrystalline film on a carbon support substrate made of a material different from that of the silicon carbide polycrystalline film, the particle size of the silicon carbide polycrystalline film is small at the initial stage when the silicon carbide polycrystalline film is formed, and then As the film formation of the silicon carbide polycrystalline film progresses, the particle size of the silicon carbide polycrystalline film formed increases. This causes a difference in the particle size of the silicon carbide polycrystalline film in the formed silicon carbide polycrystalline film, which causes a difference in the internal stress in the silicon carbide polycrystalline film. It contributes to increasing the warp of the film. In the process of removing the support substrate and processing the silicon carbide polycrystalline film into the silicon carbide polycrystalline substrate, the warp of the silicon carbide polycrystalline substrate is sufficient even if the portion of the silicon carbide crystal film where the particle size changes is scraped off. There was a problem that it did not become smaller.

また、炭化ケイ素多結晶膜を炭化ケイ素多結晶基板へ加工する工程においては、炭化ケイ素多結晶膜を所定の厚さおよび平坦度へ整えるために、面研削や面研磨の加工などを行うことがある。これらの加工において、炭化ケイ素多結晶膜の反りが大きいことに起因して、厚さや平坦度あるいは反りの不良が発生することがあり、炭化ケイ素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なっていた。加えて、これらの加工不良を改善することを目的として、例えば炭化ケイ素を成膜するときに炭化ケイ素多結晶膜の厚さを大きくすることがある。炭化ケイ素多結晶膜の厚さを大きくするために、ガス使用量が増加することや成膜時間が長くなることにより、製造コストや生産性が悪化するという問題があった。 Further, in the process of processing the silicon carbide polycrystalline film into the silicon carbide polycrystalline substrate, surface grinding or surface polishing may be performed in order to adjust the silicon carbide polycrystalline film to a predetermined thickness and flatness. is there. In these processes, poor thickness, flatness, or warpage may occur due to the large warpage of the silicon carbide polycrystalline film, which deteriorates the yield in the processing process for the silicon carbide polycrystalline substrate. It was a factor. In addition, for the purpose of improving these processing defects, for example, when forming a silicon carbide film, the thickness of the silicon carbide polycrystalline film may be increased. In order to increase the thickness of the silicon carbide polycrystalline film, there is a problem that the manufacturing cost and productivity are deteriorated due to an increase in the amount of gas used and a long film formation time.

よって、本発明は、炭化ケイ素多結晶基板に大きな反りが発生することを抑制して、反りの小さい炭化ケイ素多結晶基板を製造する、炭化ケイ素多結晶基板の製造方法を提供することを目的とする。 Therefore, an object of the present invention is to provide a method for manufacturing a silicon carbide polycrystalline substrate, which suppresses the occurrence of a large warp in the silicon carbide polycrystalline substrate and manufactures the silicon carbide polycrystalline substrate with a small warp. To do.

本発明の炭化ケイ素多結晶基板の製造方法は、化学的気相成長法によって支持基板上に第1炭化ケイ素多結晶膜を、1400℃〜1500℃の温度で成膜する、第1炭化ケイ素多結晶膜成膜工程と、前記第1炭化ケイ素多結晶膜の上に、第2炭化ケイ素多結晶膜を、1200℃〜1300℃、かつ、前記第1炭化ケイ素多結晶膜の成膜温度よりも100℃〜200℃低い温度で成膜する、第2炭化ケイ素多結晶膜成膜工程と、を含む。 In the method for producing a silicon carbide polycrystalline substrate of the present invention, a first silicon carbide polycrystalline film is formed on a support substrate by a chemical vapor phase growth method at a temperature of 1400 ° C to 1500 ° C. Crystal film forming step and the second silicon carbide polycrystalline film on the first silicon carbide polycrystalline film at 1200 ° C to 1300 ° C and higher than the film forming temperature of the first silicon carbide polycrystalline film. It includes a second silicon carbide polycrystalline film forming step of forming a film at a temperature lower than 100 ° C. to 200 ° C.

本発明の炭化ケイ素多結晶基板の製造方法であれば、炭化ケイ素多結晶基板に大きな反りが発生することを抑制して、反りの小さい炭化ケイ素多結晶基板を製造することができる。 According to the method for producing a silicon carbide polycrystalline substrate of the present invention, it is possible to suppress the occurrence of a large warp in the silicon carbide polycrystalline substrate and produce a silicon carbide polycrystalline substrate with a small warp.

本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法において、化学的気相成長法(CVD法)により炭化ケイ素多結晶膜を成膜する成膜装置の一例を模式的に示す断面図である。Cross-sectional view schematically showing an example of a film forming apparatus for forming a silicon carbide polycrystalline film by a chemical vapor deposition method (CVD method) in the method for producing a silicon carbide polycrystalline substrate according to an embodiment of the present invention. Is. 本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法において、各工程における支持基板、炭化ケイ素多結晶膜、および、炭化ケイ素多結晶基板の側面を模式的に示す断面図である。It is sectional drawing which shows typically the side surface of the support substrate, the silicon carbide polycrystalline film, and the silicon carbide polycrystalline substrate in each step in the manufacturing method of the silicon carbide polycrystalline substrate which concerns on one Embodiment of this invention. 従来の炭化ケイ素多結晶基板の製造方法において、各工程における支持基板、炭化ケイ素多結晶膜、および、炭化ケイ素多結晶基板の側面を模式的に示す断面図である。It is sectional drawing which shows typically the side surface of the support substrate, the silicon carbide polycrystalline film, and the silicon carbide polycrystalline substrate in each step in the conventional method of manufacturing the silicon carbide polycrystalline substrate. 従来の炭化ケイ素多結晶基板の製造方法により得られた、支持基板と炭化ケイ素多結晶膜との積層体における、炭化ケイ素多結晶の粒径の分布を模式的に示す断面図である。It is sectional drawing which shows typically the distribution of the particle diameter of the silicon carbide polycrystalline film in the laminated body of the support substrate and the silicon carbide polycrystalline film obtained by the conventional manufacturing method of the silicon carbide polycrystalline substrate. 本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法により得られた、支持基板と炭化ケイ素多結晶膜との積層体における、炭化ケイ素多結晶の粒径の分布を模式的に示す断面図である。A cross section schematically showing the distribution of the particle size of the silicon carbide polycrystalline film in the laminate of the support substrate and the silicon carbide polycrystalline film obtained by the method for producing the silicon carbide polycrystalline substrate according to the embodiment of the present invention. It is a figure.

本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法について、図面を参照して説明する。なお、本発明は、以下の実施形態に限定されるものではない。 A method for manufacturing a silicon carbide polycrystalline substrate according to an embodiment of the present invention will be described with reference to the drawings. The present invention is not limited to the following embodiments.

図1は、本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法において、化学的気相成長法により炭化ケイ素多結晶膜を成膜する成膜装置の一例である成膜装置1000を模式的に示す断面図である。図2は、本発明の一実施形態にかかる炭化ケイ素多結晶基板の製造方法において、各工程におけるカーボン支持基板、炭化ケイ素多結晶膜、積層体、および、炭化ケイ素多結晶基板の断面を模式的に示す図である。図2(A)は支持基板100を示す図であり、図2(B)は第1炭化ケイ素多結晶膜成膜工程により得られた積層体400Aを示す図であり、図2(C)は第2炭化ケイ素多結晶膜成膜工程により得られた積層体400Bを示す図であり、図2(D)は積層体400Bを支持基板100の除去工程に供して得られた炭化ケイ素多結晶基板500を示す図である。 FIG. 1 shows a film forming apparatus 1000 which is an example of a film forming apparatus for forming a silicon carbide polycrystalline film by a chemical vapor deposition method in the method for producing a silicon carbide polycrystalline substrate according to an embodiment of the present invention. It is sectional drawing which shows typically. FIG. 2 schematically shows a cross section of a carbon support substrate, a silicon carbide polycrystalline film, a laminate, and a silicon carbide polycrystalline substrate in each step in the method for manufacturing a silicon carbide polycrystalline substrate according to an embodiment of the present invention. It is a figure shown in. FIG. 2 (A) is a diagram showing a support substrate 100, FIG. 2 (B) is a diagram showing a laminate 400A obtained by the first silicon carbide polycrystalline film forming step, and FIG. 2 (C) is a diagram. It is a figure which shows the laminated body 400B obtained by the 2nd silicon carbide polycrystalline film film forming process, and FIG. 2 (D) is the silicon carbide polycrystalline substrate obtained by subjecting the laminated body 400B to the removal step of the support substrate 100. It is a figure which shows 500.

本実施形態の炭化ケイ素多結晶基板の製造方法は、化学的気相成長法によって支持基板100上に第1炭化ケイ素多結晶膜200を、1400℃〜1500℃の温度で成膜する、第1炭化ケイ素多結晶膜成膜工程と、第1炭化ケイ素多結晶膜200の上に、第2炭化ケイ素多結晶膜300を、1200℃〜1300℃、かつ、第1炭化ケイ素多結晶膜200の成膜温度よりも100℃〜200℃低い温度で成膜する、第2炭化ケイ素多結晶膜成膜工程と、を含む。本発明者は、このような本実施形態の炭化ケイ素多結晶基板の製造方法により、製造された炭化ケイ素多結晶基板500の反りを低減することができることを見出すに至った。 The method for producing a silicon carbide polycrystalline substrate of the present embodiment is a first method in which a first silicon carbide polycrystalline film 200 is formed on a support substrate 100 at a temperature of 1400 ° C. to 1500 ° C. by a chemical vapor phase growth method. The silicon carbide polycrystalline film forming step and the formation of the second silicon carbide polycrystalline film 300 on the first silicon carbide polycrystalline film 200 at 1200 ° C. to 1300 ° C. and the first silicon carbide polycrystalline film 200. It includes a second silicon carbide polycrystalline film forming step of forming a film at a temperature 100 ° C. to 200 ° C. lower than the film temperature. The present inventor has found that the warpage of the manufactured silicon carbide polycrystalline substrate 500 can be reduced by the method for producing the silicon carbide polycrystalline substrate of the present embodiment.

次に、各工程について、第1炭化ケイ素多結晶膜成膜工程、第2炭化ケイ素多結晶膜成膜工程、支持基板100の除去工程の順に説明する。以下の説明は本実施形態の炭化ケイ素多結晶基板500の製造方法の一例であり、問題のない範囲で温度、圧力、ガス雰囲気等の各条件や、手順等を変更してもよい。また、以下においては、支持基板100の両面を成膜対象として第1炭化ケイ素多結晶膜200を成膜して炭化ケイ素多結晶基板500を製造する場合について説明する。なお、カーボン支持基板の片面を成膜対象として炭化ケイ素多結晶膜を成膜して炭化ケイ素多結晶基板を製造してもよい。成膜対象をカーボン支持基板の片面とするか、両面とするかは、炭化ケイ素多結晶基板の製造計画や蒸着炉の構造等の条件により適宜決定すればよい。 Next, each step will be described in the order of a first silicon carbide polycrystalline film forming step, a second silicon carbide polycrystalline film forming step, and a step of removing the support substrate 100. The following description is an example of the method for manufacturing the silicon carbide polycrystalline substrate 500 of the present embodiment, and each condition such as temperature, pressure, gas atmosphere, and the procedure may be changed within a range where there is no problem. Further, in the following, a case where the first silicon carbide polycrystalline film 200 is formed on both sides of the support substrate 100 as a film forming target to manufacture the silicon carbide polycrystalline substrate 500 will be described. A silicon carbide polycrystalline substrate may be produced by forming a silicon carbide polycrystalline film on one side of the carbon support substrate as a film forming target. Whether the target of film formation is one side or both sides of the carbon support substrate may be appropriately determined depending on the conditions such as the production plan of the silicon carbide polycrystalline substrate and the structure of the vapor deposition furnace.

(第1炭化ケイ素多結晶膜成膜工程)
第1炭化ケイ素多結晶膜成膜工程は、化学的気相成長法によって支持基板100上に第1炭化ケイ素多結晶膜200を、1400℃〜1500℃の温度で成膜する工程である。第1炭化ケイ素多結晶膜成膜工程は、例えば、図1に示した成膜装置1000を用いて行うことができる。
(First Silicon Carbide Polycrystal Film Filming Step)
The first silicon carbide polycrystalline film forming step is a step of forming the first silicon carbide polycrystalline film 200 on the support substrate 100 by a chemical vapor deposition method at a temperature of 1400 ° C. to 1500 ° C. The first silicon carbide polycrystalline film film forming step can be performed, for example, by using the film forming apparatus 1000 shown in FIG.

成膜装置1000は、化学的気相成長法によって、支持基板100に第1炭化ケイ素多結晶膜200を成膜するために用いることができる。成膜装置1000は、成膜装置1000の外装となる筐体1100と、支持基板100に第1炭化ケイ素多結晶膜200を成膜させる成膜室1010と、成膜室1010より排出された原料ガスやキャリアガスを後述のガス排出口1030へ導入する排出ガス導入室1040と、排出ガス導入室1040を覆うボックス1050と、ボックス1050の外部より成膜室1010内を加温する、カーボン製のヒーター1060と、成膜室1010の下部に設けられ、成膜室1010に原料ガスやキャリアガスを導入するガス導入口1020と、ガス排出口1030と、支持基板100を保持する基板ホルダー1070を有する。また、基板ホルダー1070は、2つの柱1071と、支持基板100を水平に載置する、柱1071に設けられた載置部1072を有する。 The film forming apparatus 1000 can be used to form the first silicon carbide polycrystalline film 200 on the support substrate 100 by the chemical vapor deposition method. The film forming apparatus 1000 includes a housing 1100 which is an exterior of the film forming apparatus 1000, a film forming chamber 1010 for forming the first silicon carbide polycrystal film 200 on the support substrate 100, and a raw material discharged from the film forming chamber 1010. A carbon-made film forming chamber 1010 that heats the inside of the film forming chamber 1010 from the outside of the exhaust gas introduction chamber 1040 that introduces gas or carrier gas into the gas discharge port 1030 described later, the box 1050 that covers the exhaust gas introduction chamber 1040, and the box 1050. It has a heater 1060, a gas introduction port 1020 provided below the film formation chamber 1010 for introducing a raw material gas or a carrier gas into the film formation chamber 1010, a gas discharge port 1030, and a substrate holder 1070 for holding a support substrate 100. .. Further, the substrate holder 1070 has two pillars 1071 and a mounting portion 1072 provided on the pillar 1071 on which the support substrate 100 is horizontally mounted.

第1炭化ケイ素多結晶膜200の成膜時において、原料ガスやキャリアガス等は、成膜室1010に設けられたガス導入口1020から導入され、成膜室1010の下部から排出ガス導入室1040に排出され、さらに、ガス排出口1030から成膜装置1000の外部に排出される。 At the time of film formation of the first silicon carbide polycrystal film 200, the raw material gas, carrier gas, etc. are introduced from the gas introduction port 1020 provided in the film formation chamber 1010, and the exhaust gas introduction chamber 1040 is introduced from the lower part of the film formation chamber 1010. Is discharged to the outside of the film forming apparatus 1000 from the gas discharge port 1030.

また、支持基板100の厚さや成膜対象面の大きさ等の形状は特に限定されず、所望の炭化ケイ素多結晶基板500に合わせたものを用いることができる。支持基板100としては、例えば、カーボン製の支持基板を用いることができる。 Further, the shape such as the thickness of the support substrate 100 and the size of the surface to be formed is not particularly limited, and a material suitable for the desired silicon carbide polycrystalline substrate 500 can be used. As the support substrate 100, for example, a carbon support substrate can be used.

次に、成膜装置1000を用いて、化学的気相成長法により、支持基板100上に第1炭化ケイ素多結晶膜200を成膜させる手順を説明する。 Next, a procedure for forming the first silicon carbide polycrystalline film 200 on the support substrate 100 by a chemical vapor deposition method using the film forming apparatus 1000 will be described.

支持基板100(図2(A))を載置部1072に載置し、減圧状態で、Ar等の不活性ガス雰囲気下で、成膜の反応温度まで、ヒーター1060により支持基板100を加熱する。成膜の反応温度まで達したら、不活性ガスの供給を止めて、温度を維持して、成膜室1010内に第1炭化ケイ素多結晶膜200の成分を含む原料ガスやキャリアガスを供給する。支持基板100の成膜対象面や気相での化学反応により、加熱した支持基板100の両面に第1炭化ケイ素多結晶膜200を成膜させることができる。その後、室温まで冷却することで、図2(B)に示すように、支持基板100に第1炭化ケイ素多結晶膜200が成膜された、積層体400Aが得られる。 The support substrate 100 (FIG. 2 (A)) is placed on the mounting portion 1072, and the support substrate 100 is heated by the heater 1060 in a reduced pressure state under an inert gas atmosphere such as Ar to the reaction temperature of the film formation. .. When the reaction temperature of the film formation is reached, the supply of the inert gas is stopped, the temperature is maintained, and the raw material gas or carrier gas containing the component of the first silicon carbide polycrystalline film 200 is supplied into the film formation chamber 1010. .. The first silicon carbide polycrystalline film 200 can be formed on both surfaces of the heated support substrate 100 by a chemical reaction on the surface of the support substrate 100 to be formed or in the gas phase. Then, by cooling to room temperature, as shown in FIG. 2B, a laminated body 400A in which the first silicon carbide polycrystalline film 200 is formed on the support substrate 100 is obtained.

原料ガスとしては、第1炭化ケイ素多結晶膜200を成膜させることができれば、特に限定されず、一般的に炭化ケイ素多結晶膜の成膜に使用されるSi系原料ガス、C系原料ガスを用いることができる。例えば、Si系原料ガスとしては、シラン(SiH)を用いることができるほか、モノクロロシラン(SiHCl)、ジクロロシラン(SiHCl)、トリクロロシラン(SiHCl)、テトラクロロシラン(SiCl)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)を用いることができる。C系原料ガスとしては、例えば、メタン(CH)、プロパン(C)、アセチレン(C)等の炭化水素を用いることができる。上記のほか、トリクロロメチルシラン(CHClSi)、トリクロロフェニルシラン(CClSi)、ジクロロメチルシラン(CHClSi)、ジクロロジメチルシラン((CHSiCl)、クロロトリメチルシラン((CHSiCl)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。 The raw material gas is not particularly limited as long as the first silicon carbide polycrystalline film 200 can be formed, and the Si-based raw material gas and the C-based raw material gas generally used for forming the silicon carbide polycrystalline film are not particularly limited. Can be used. For example, as the Si-based raw material gas, silane (SiH 4 ) can be used, monochlorosilane (SiH 3 Cl), dichlorosilane (SiH 2 Cl 2 ), trichlorosilane (SiHCl 3 ), tetrachlorosilane (SiCl 4). ) And other chlorine-based Si raw material-containing gas (chloride-based raw material) containing Cl having an etching action can be used. As the C-based raw material gas, for example, hydrocarbons such as methane (CH 4 ), propane (C 3 H 8 ), and acetylene (C 2 H 2 ) can be used. In addition to the above, trichloromethylsilane (CH 3 Cl 3 Si), trichlorophenylsilane (C 6 H 5 Cl 3 Si), dichloromethylsilane (CH 4 Cl 2 Si), dichlorodimethylsilane ((CH 3 ) 2 SiCl 2) ), Chlorotrimethylsilane ((CH 3 ) 3 SiCl) and other gases containing both Si and C can also be used as the raw material gas.

また、キャリアガスとしては、炭化ケイ素多結晶膜の成膜を阻害することなく、原料ガスを支持基板100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、炭化ケイ素に対してエッチング作用があるHガスをキャリアガスとして用いることができる。また、これら原料ガスおよびキャリアガスと同時に、第3のガスとして、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こともできる。例えば、炭化ケイ素多結晶基板500の導電型をn型とする場合には窒素(N)、p型とする場合にはトリメチルアルミニウム(TMA)を用いることができる。 Further, as the carrier gas, a commonly used carrier gas can be used as long as the raw material gas can be developed on the support substrate 100 without inhibiting the formation of the silicon carbide polycrystalline film. For example, an H 2 gas having excellent thermal conductivity and having an etching action on silicon carbide can be used as a carrier gas. Further, at the same time as these raw material gas and carrier gas, as a third gas, an impurity doping gas in an amount commensurate with the target conductivity can be simultaneously supplied. For example, nitrogen (N 2 ) can be used when the conductive type of the silicon carbide polycrystalline substrate 500 is n-type, and trimethylaluminum (TMA) can be used when the conductive type is p-type.

第1炭化ケイ素多結晶膜200を成膜させる際には、上記のガスを適宜混合して供給することができる。また、上記のガスを混合せずに、個別に供給してもよい。また、所望の炭化ケイ素多結晶膜の性状に応じて、第1炭化ケイ素多結晶膜成膜工程の途中でガスの混合割合を変更してもよい。 When forming the first silicon carbide polycrystalline film 200, the above gas can be appropriately mixed and supplied. Moreover, you may supply individually without mixing the said gas. Further, the mixing ratio of the gas may be changed during the process of forming the first silicon carbide polycrystalline film, depending on the desired properties of the silicon carbide polycrystalline film.

また、本実施形態における、第1炭化ケイ素多結晶膜200の成膜温度は、1400℃〜1500℃とする。また、第1炭化ケイ素多結晶膜200の厚さは、例えば、50μm〜150μm程度とすることができる。 The film formation temperature of the first silicon carbide polycrystalline film 200 in the present embodiment is 1400 ° C to 1500 ° C. The thickness of the first silicon carbide polycrystalline film 200 can be, for example, about 50 μm to 150 μm.

以上の第1炭化ケイ素多結晶膜成膜工程により、支持基板100と第1炭化ケイ素多結晶膜200の積層体400Aが得られる。積層体400Aは、第2炭化ケイ素多結晶膜成膜工程に供される。 By the above-mentioned first silicon carbide polycrystalline film forming step, a laminate 400A of the support substrate 100 and the first silicon carbide polycrystalline film 200 can be obtained. The laminate 400A is subjected to the second silicon carbide polycrystalline film forming step.

(第2炭化ケイ素多結晶膜成膜工程)
次に、第2炭化ケイ素多結晶膜成膜工程を行う。第2炭化ケイ素多結晶膜成膜工程は、第1炭化ケイ素多結晶膜200の上に、第2炭化ケイ素多結晶膜300を、1200℃〜1300℃、かつ、第1炭化ケイ素多結晶膜200の成膜温度よりも100℃〜200℃低い温度で成膜する工程である。第2炭化ケイ素多結晶膜成膜工程は、例えば、図1に示した成膜装置1000を用いて、後述する降温工程を介して、第1炭化ケイ素多結晶膜成膜工程に連続して行うこともできるし、積層体400Aを室温程度まで冷却したのちに第2炭化ケイ素多結晶膜成膜工程に供してもよい。
(Second silicon carbide polycrystalline film film forming process)
Next, a second silicon carbide polycrystalline film forming step is performed. In the second silicon carbide polycrystalline film forming step, the second silicon carbide polycrystalline film 300 is placed on the first silicon carbide polycrystalline film 200 at 1200 ° C. to 1300 ° C. and the first silicon carbide polycrystalline film 200. This is a step of forming a film at a temperature 100 ° C. to 200 ° C. lower than the film forming temperature of. The second silicon carbide polycrystal film forming step is continuously performed in the first silicon carbide polycrystal film forming step through, for example, the film forming apparatus 1000 shown in FIG. 1 through a temperature lowering step described later. Alternatively, the laminate 400A may be cooled to about room temperature and then subjected to the second silicon carbide polycrystal film forming step.

第2炭化ケイ素多結晶膜成膜工程を第1炭化ケイ素多結晶膜成膜工程に連続して行う場合には、原料ガス、ドーピングガス、キャリアガスの供給を停止して、成膜室1010内の温度を第2炭化ケイ素多結晶膜300の成膜温度、すなわち、1200℃〜1300℃、かつ、第1炭化ケイ素多結晶膜200の成膜温度よりも100℃〜200℃低い温度まで降温させる(降温工程)。所定の温度になったら、温度を維持して、原料ガス、ドーピングガス、キャリアガスの供給を再開して、所定の厚さの第2炭化ケイ素多結晶膜300を形成させる。第2炭化ケイ素多結膜成膜工程の成膜条件は、温度条件以外は第1炭化ケイ素多結晶膜成膜工程と同様にしてもよいし、ガスの混合割合等の条件を変更してもよい。なお、降温工程において原料ガス等の供給を停止した際に、成膜室1010内のガス体積が収縮しない程度に、H等のキャリアガスやAr等の不活性ガスを供給することが好ましい。 When the second silicon carbide polycrystal film forming step is continuously performed in the first silicon carbide polycrystal film forming step, the supply of the raw material gas, the doping gas, and the carrier gas is stopped, and the inside of the film forming chamber 1010 is stopped. Is lowered to the film formation temperature of the second silicon carbide polycrystal film 300, that is, 1200 ° C. to 1300 ° C., and 100 ° C. to 200 ° C. lower than the film formation temperature of the first silicon carbide polycrystal film 200. (Temperature lowering process). When the temperature reaches a predetermined temperature, the temperature is maintained and the supply of the raw material gas, the doping gas, and the carrier gas is restarted to form the second silicon carbide polycrystalline film 300 having a predetermined thickness. The film forming conditions of the second silicon carbide polycrystalline film forming step may be the same as those of the first silicon carbide polycrystalline film forming step except for the temperature condition, or the conditions such as the gas mixing ratio may be changed. .. Incidentally, when stopping the supply of the source gas or the like in the cooling step, to the extent that the gas volume of the film forming chamber 1010 does not shrink, it is preferable to supply the inert gas of the carrier gas and Ar such as H 2.

第2炭化ケイ素多結晶膜成膜工程における成膜温度は、第1炭化ケイ素多結晶膜200と第2炭化ケイ素多結晶膜300における内部応力差を小さくするために、第1炭化ケイ素多結晶膜200の炭化ケイ素多結晶の結晶粒の大きさと第2炭化ケイ素多結晶膜300の炭化ケイ素多結晶の結晶粒の大きさの差が小さくなるように設定する。例えば、第1炭化ケイ素多結晶膜200の結晶粒の大きさと、第2炭化ケイ素多結晶膜300の成膜初期の結晶粒の大きさが同程度であり、第2炭化ケイ素多結晶膜300内において、厚さ方向に結晶粒の大きさの差が小さいことが好ましい。各工程の成膜温度の設定方法としては、例えば、予備試験を行って種々の温度条件で炭化ケイ素多結晶基板を製造して、得られた炭化ケイ素多結晶基板の断面を走査型電子顕微鏡(SEM)を用いて観察し、各膜の炭化ケイ素多結晶の結晶粒の大きさの分布を確認して、大きさの差が小さい温度条件を採用することができる。また、第2炭化ケイ素多結晶膜の厚さは、製造する炭化ケイ素多結晶基板500の厚さや第1炭化ケイ素多結晶膜200の厚さを考慮して適宜設定すればよく、例えば、300μm〜800μm程度とすることができる。所定の厚さの第2炭化ケイ素多結晶膜300が形成されたのち、原料ガス等の供給を停止する。以上の第2炭化ケイ素多結晶膜成膜工程により、図2(C)の積層体400Bが得られる。積層体400Bは、室温程度まで冷却されたのちに、支持基板100の除去工程に供される。
(除去工程)
次に、第2炭化ケイ素多結晶膜成膜工程により得られた積層体400Bを、積層体400Bから支持基板100を除去する除去工程に供する。
The film formation temperature in the second silicon carbide polycrystalline film forming step is the first silicon carbide polycrystalline film in order to reduce the internal stress difference between the first silicon carbide polycrystalline film 200 and the second silicon carbide polycrystalline film 300. The difference between the size of the crystal grains of the 200 silicon carbide polycrystals and the size of the crystal grains of the silicon carbide polycrystal of the second silicon carbide polycrystal film 300 is set to be small. For example, the size of the crystal grains of the first silicon carbide polycrystalline film 200 and the size of the crystal grains at the initial stage of film formation of the second silicon carbide polycrystalline film 300 are about the same, and the inside of the second silicon carbide polycrystalline film 300 It is preferable that the difference in crystal grain size in the thickness direction is small. As a method for setting the film formation temperature in each step, for example, a preliminary test is performed to manufacture a silicon carbide polycrystalline substrate under various temperature conditions, and a cross section of the obtained silicon carbide polycrystalline substrate is scanned with a scanning electron microscope ( By observing using SEM), the distribution of the size distribution of the crystal grains of the silicon carbide polycrystalline of each film can be confirmed, and the temperature condition in which the difference in size is small can be adopted. The thickness of the second silicon carbide polycrystalline film may be appropriately set in consideration of the thickness of the silicon carbide polycrystalline substrate 500 to be manufactured and the thickness of the first silicon carbide polycrystalline film 200, for example, from 300 μm to 300 μm. It can be about 800 μm. After the second silicon carbide polycrystalline film 300 having a predetermined thickness is formed, the supply of the raw material gas and the like is stopped. By the above-mentioned second silicon carbide polycrystalline film forming step, the laminate 400B shown in FIG. 2C is obtained. The laminate 400B is cooled to about room temperature and then subjected to a step of removing the support substrate 100.
(Removal process)
Next, the laminated body 400B obtained by the second silicon carbide polycrystalline film forming step is subjected to a removing step of removing the support substrate 100 from the laminated body 400B.

支持基板100の除去工程は、積層体400Bから、支持基板100の除去を行い、炭化ケイ素多結晶基板500を得る工程である。まず、積層体400Bにおいて、支持基板100が露出していない場合には、支持基板100の外周端部に積層した炭化ケイ素多結晶膜(第1炭化ケイ素多結晶膜200および第2炭化ケイ素多結晶膜300)を、ダイヤ砥石等を用いて研削して、支持基板100の少なくとも一部を露出させる。支持基板100としてカーボン製の支持基板を用いた場合には、例えば、積層体400Bを数百度(例えば800℃〜1000℃程度)に加熱して、支持基板100を燃焼させることにより除去することができる。燃焼による支持基板100の除去工程は、例えば、二珪化モリブデン製のヒーターを備える燃焼炉等を用いることができる。積層体400Bを燃焼炉内に保持して、燃焼炉内にOや空気等の酸化性ガスを供給しながら、常圧または減圧状態で、ヒーターにより燃焼炉内を加熱する。加熱により、支持基板100のみが燃焼して、図2(D)に示すように、炭化ケイ素多結晶基板500が得られる。なお、得られた炭化ケイ素多結晶基板500の反りをなくしたり、所望の厚さにしたりするために、必要に応じて、支持基板100を除去したのちに、さらに研削加工や研磨加工を行ってもよい。 The step of removing the support substrate 100 is a step of removing the support substrate 100 from the laminate 400B to obtain the silicon carbide polycrystalline substrate 500. First, in the laminated body 400B, when the support substrate 100 is not exposed, the silicon carbide polycrystalline film (first silicon carbide polycrystalline film 200 and second silicon carbide polycrystalline film 200) laminated on the outer peripheral end of the support substrate 100 The film 300) is ground using a diamond grindstone or the like to expose at least a part of the support substrate 100. When a carbon support substrate is used as the support substrate 100, for example, the laminate 400B can be removed by heating the laminate 400B to several hundred degrees (for example, about 800 ° C. to 1000 ° C.) and burning the support substrate 100. it can. For the step of removing the support substrate 100 by combustion, for example, a combustion furnace equipped with a heater made of molybdenum disilicate can be used. The laminate 400B is held in the combustion furnace, and while supplying an oxidizing gas such as O 2 or air to the combustion furnace, the inside of the combustion furnace is heated by a heater under a normal pressure or a reduced pressure state. By heating, only the support substrate 100 is burned to obtain the silicon carbide polycrystalline substrate 500 as shown in FIG. 2 (D). In addition, in order to eliminate the warp of the obtained silicon carbide polycrystalline substrate 500 and to obtain a desired thickness, if necessary, after removing the support substrate 100, further grinding or polishing is performed. May be good.

以上の炭化ケイ素多結晶基板の製造方法により得られた炭化ケイ素多結晶基板500は、例えば、反り量が100μm以下である。よって、本実施形態の炭化ケイ素多結晶基板の製造方法により、反りの小さい炭化ケイ素多結晶基板500を得ることができる。 The silicon carbide polycrystalline substrate 500 obtained by the above method for producing a silicon carbide polycrystalline substrate has, for example, a warp amount of 100 μm or less. Therefore, the silicon carbide polycrystalline substrate 500 having a small warp can be obtained by the method for producing the silicon carbide polycrystalline substrate of the present embodiment.

(結晶粒の大きさの分布)
次に、従来の炭化ケイ素多結晶基板の製造方法と本実施形態の炭化ケイ素多結晶基板の製造方法において、炭化ケイ素多結晶膜における炭化ケイ素多結晶の結晶粒の大きさの分布を比較して説明する。
(Distribution of crystal grain size)
Next, in the conventional method for producing a silicon carbide polycrystalline substrate and the method for producing a silicon carbide polycrystalline substrate of the present embodiment, the distribution of the grain size of the silicon carbide polycrystalline film in the silicon carbide polycrystalline film is compared. explain.

従来の炭化ケイ素多結晶基板の製造方法は、図3(A)に示す支持基板100に所望の厚さの炭化ケイ素多結晶膜700を成膜して、積層体800(図3(B))を得たのち、支持基板100を除去して、炭化ケイ素多結晶基板700A(図3(C))を得て、例えば図3(C)の線Aの部分まで研削することにより、反りを低減した炭化ケイ素多結晶基板900(図3(D))を得るというものである。従来の炭化ケイ素多結晶基板の製造方法では、1400℃よりも低い温度で炭化ケイ素多結晶膜700を成膜することが多い。 In the conventional method for manufacturing a silicon carbide polycrystalline substrate, a silicon carbide polycrystalline film 700 having a desired thickness is formed on the support substrate 100 shown in FIG. 3 (A) to form a laminate 800 (FIG. 3 (B)). After obtaining the above, the support substrate 100 is removed to obtain a silicon carbide polycrystalline substrate 700A (FIG. 3 (C)), and the warp is reduced by, for example, grinding to the portion of line A in FIG. 3 (C). The silicon carbide polycrystalline substrate 900 (FIG. 3 (D)) is obtained. In the conventional method for manufacturing a silicon carbide polycrystalline substrate, the silicon carbide polycrystalline film 700 is often formed at a temperature lower than 1400 ° C.

ここで、従来の炭化ケイ素多結晶基板の製造方法で得られた積層体800(図3(B))においては、炭化ケイ素多結晶の結晶粒の分布は図4のようになる。すなわち、支持基板100に近いほど結晶粒が小さく(例えば平均粒径が10μm程度)、炭化ケイ素多結晶膜700の厚さが増すにしたがって炭化ケイ素多結晶の結晶粒が大きくなる(例えば平均粒径が50μm程度)。反りを低減した炭化ケイ素多結晶基板900を得るために必要な厚さの炭化ケイ素多結晶膜700を成膜すると、炭化ケイ素多結晶膜700内で厚さ方向における炭化ケイ素多結晶のサイズの差が大きくなって内部応力差が大きくなり、このような積層体800から支持基板100を除去して得られた炭化ケイ素多結晶基板700A(図3(C))は、支持基板100に接していた面から炭化ケイ素多結晶基板700Aの厚さ方向外方に向かって凸状に大きく反りが発生し得る。よって、例えば、炭化ケイ素単結晶基板との貼り合わせ基板を製造する用途に用いる際に、炭化ケイ素多結晶基板700Aに発生した反りの部分を研削、研磨して所定の平坦度、所定の厚さとして反りを低減した炭化ケイ素多結晶基板900(図3(D))に加工する手間が大きく、歩留まり、コスト、生産性が悪化するという課題があった。 Here, in the laminate 800 (FIG. 3 (B)) obtained by the conventional method for producing a silicon carbide polycrystalline substrate, the distribution of crystal grains of the silicon carbide polycrystalline substrate is as shown in FIG. That is, the closer to the support substrate 100, the smaller the crystal grains (for example, the average particle size is about 10 μm), and as the thickness of the silicon carbide polycrystalline film 700 increases, the crystal grains of the silicon carbide polycrystalline film become larger (for example, the average particle size). Is about 50 μm). When the silicon carbide polycrystalline film 700 having the thickness required to obtain the silicon carbide polycrystalline substrate 900 with reduced warpage is formed, the difference in the size of the silicon carbide polycrystalline film 700 in the thickness direction within the silicon carbide polycrystalline film 700. The silicon carbide polycrystalline substrate 700A (FIG. 3 (C)) obtained by removing the support substrate 100 from the laminate 800 was in contact with the support substrate 100. A large convex warp may occur from the surface toward the outside of the silicon carbide polycrystalline substrate 700A in the thickness direction. Therefore, for example, when used for manufacturing a substrate bonded to a silicon carbide single crystal substrate, a warped portion generated in the silicon carbide polycrystalline substrate 700A is ground and polished to have a predetermined flatness and a predetermined thickness. As a result, it takes a lot of time and effort to process the silicon carbide polycrystalline substrate 900 (FIG. 3 (D)) with reduced warpage, and there is a problem that the yield, cost, and productivity are deteriorated.

一方、本実施形態の炭化ケイ素多結晶基板の製造方法は、化学的気相成長法によって支持基板100上に第1炭化ケイ素多結晶膜200を、1400℃〜1500℃の温度で成膜する、第1炭化ケイ素多結晶膜成膜工程と、第1炭化ケイ素多結晶膜200の上に、第2炭化ケイ素多結晶膜300を、1200℃〜1300℃、かつ、第1炭化ケイ素多結晶膜200の成膜温度よりも100℃〜200℃低い温度で成膜する、第2炭化ケイ素多結晶膜成膜工程と、を含む。 On the other hand, in the method for producing a silicon carbide polycrystalline substrate of the present embodiment, the first silicon carbide polycrystalline film 200 is formed on the support substrate 100 by a chemical vapor phase growth method at a temperature of 1400 ° C to 1500 ° C. The first silicon carbide polycrystalline film forming step and the second silicon carbide polycrystalline film 300 on the first silicon carbide polycrystalline film 200 at 1200 ° C. to 1300 ° C. and the first silicon carbide polycrystalline film 200. Includes a second silicon carbide polycrystalline film film forming step of forming a film at a temperature 100 ° C. to 200 ° C. lower than the film forming temperature of.

第1炭化ケイ素多結晶膜200においては、図5に示すように、従来の炭化ケイ素多結晶基板の製造方法における炭化ケイ素多結晶膜の一般的な成膜温度より高いため、炭化ケイ素多結晶の結晶粒の大きさが大きくなりやすい(例えば平均粒径50μm程度)。従来の炭化ケイ素多結晶基板の製造方法のように、同じ温度で成膜を続けると、厚さが増すに従って形成される炭化ケイ素多結晶の結晶粒のサイズが大きくなる。そこで、本実施形態の炭化ケイ素多結晶基板の製造方法では、第2炭化ケイ素多結晶膜製造工程として、1200℃〜1300℃、かつ、第1炭化ケイ素多結晶膜200の成膜温度よりも100℃〜200℃低い温度で第2炭化ケイ素多結晶膜300を成膜する。これにより、第2炭化ケイ素多結晶膜300の成膜初期における炭化ケイ素多結晶の結晶粒の大きさは、成膜温度が低いものの、第1炭化ケイ素多結晶膜200の炭化ケイ素多結晶の結晶粒の大きさの影響を受けて大きくなる傾向にある(例えば平均粒径50μm程度)。また、図5に示すように、第2炭化ケイ素多結晶膜300の成膜温度が低いことから、第2炭化ケイ素多結晶膜300の厚さが増しても炭化ケイ素多結晶の結晶粒の大きさが大きくなりにくく、第1炭化ケイ素多結晶膜200の炭化ケイ素多結晶の結晶粒の大きさと、第2炭化ケイ素多結晶膜300成膜過程後期に形成された炭化ケイ素多結晶の結晶粒の大きさとの差が小さくなる。すなわち、本実施形態の炭化ケイ素多結晶基板の製造方法により得られた炭化ケイ素多結晶基板500においては、厚さ方向において炭化ケイ素多結晶の結晶粒の大きさの差が小さくなる。 In the first silicon carbide polycrystalline film 200, as shown in FIG. 5, since the film formation temperature of the silicon carbide polycrystalline film in the conventional method for producing a silicon carbide polycrystalline substrate is higher than the general film formation temperature, the silicon carbide polycrystalline film 200 is used. The size of crystal grains tends to be large (for example, the average particle size is about 50 μm). If the film formation is continued at the same temperature as in the conventional method for manufacturing a silicon carbide polycrystalline substrate, the size of the crystal grains of the silicon carbide polycrystalline substrate to be formed increases as the thickness increases. Therefore, in the method for producing a silicon carbide polycrystalline substrate of the present embodiment, the second silicon carbide polycrystalline film manufacturing step is 1200 ° C. to 1300 ° C., which is 100 higher than the film formation temperature of the first silicon carbide polycrystalline film 200. The second silicon carbide polycrystalline film 300 is formed at a low temperature of ° C. to 200 ° C. As a result, the size of the crystal grains of the silicon carbide polycrystalline film at the initial stage of film formation of the second silicon carbide polycrystalline film 300 is the crystal of the silicon carbide polycrystalline film of the first silicon carbide polycrystalline film 200, although the film formation temperature is low. It tends to increase due to the influence of grain size (for example, the average particle size is about 50 μm). Further, as shown in FIG. 5, since the film formation temperature of the second silicon carbide polycrystalline film 300 is low, the size of the crystal grains of the silicon carbide polycrystalline film 300 is large even if the thickness of the second silicon carbide polycrystalline film 300 is increased. The size of the crystal grains of the silicon carbide polycrystalline film 200 of the first silicon carbide polycrystalline film 200 and the crystal grains of the silicon carbide polycrystalline film formed in the latter half of the film forming process of the second silicon carbide polycrystalline film 300 The difference from the size becomes small. That is, in the silicon carbide polycrystalline substrate 500 obtained by the method for producing the silicon carbide polycrystalline substrate of the present embodiment, the difference in the size of the crystal grains of the silicon carbide polycrystalline substrate becomes small in the thickness direction.

以上のことから、本実施形態の炭化ケイ素多結晶基板の製造方法では、厚さ方向における炭化ケイ素多結晶の結晶粒のサイズの差が小さく、内部応力差が小さくなるため、支持基板100を除去した際に、炭化ケイ素多結晶基板500に大きな反りが発生することを抑制して、従来の製造方法よりも反りが小さい炭化ケイ素多結晶基板500を得ることができる。これにより、炭化ケイ素多結晶基板の加工製造における、所定の厚みおよび平坦度へ整えるための面研削や面研磨の加工などにおいて、炭化ケイ素多結晶基板の反りが大きいことに起因する厚さ、平坦度あるいは反りが悪化することなく、反りの小さな炭化ケイ素多結晶基板へ加工製造することが可能となる。また、製造された炭化ケイ素多結晶基板500の反りが小さいことで、炭化ケイ素多結晶基板として用いる厚さよりも大幅に厚い炭化ケイ素多結晶膜を成膜する必要がなくなり、炭化ケイ素多結晶基板としての反りをなくすための研削加工、研磨加工の負担や、材料の無駄を減らして、コストの削減、歩留まりや生産性を向上させることができる。 From the above, in the method for producing a silicon carbide polycrystalline substrate of the present embodiment, the difference in the size of the crystal grains of the silicon carbide polycrystalline substrate in the thickness direction is small and the difference in internal stress is small, so that the support substrate 100 is removed. At that time, it is possible to suppress the occurrence of a large warp in the silicon carbide polycrystalline substrate 500 and obtain the silicon carbide polycrystalline substrate 500 having a smaller warp than the conventional manufacturing method. As a result, in the processing and manufacturing of the silicon carbide polycrystalline substrate, the thickness and flatness due to the large warp of the silicon carbide polycrystalline substrate in the surface grinding and surface polishing for adjusting to a predetermined thickness and flatness. It is possible to process and manufacture a silicon carbide polycrystalline substrate having a small warp without deteriorating the degree or warpage. Further, since the manufactured silicon carbide polycrystalline substrate 500 has a small warp, it is not necessary to form a silicon carbide polycrystalline film that is significantly thicker than the thickness used as the silicon carbide polycrystalline substrate, and the silicon carbide polycrystalline substrate can be used. It is possible to reduce the burden of grinding and polishing to eliminate warpage and waste of materials, reduce costs, and improve yield and productivity.

また、特に、本実施形態の炭化ケイ素多結晶基板の製造方法であれば、高導電率(例えば、0.1Ω・cm程度以上の)の炭化ケイ素多結晶基板を製造する場合であっても、炭化ケイ素中の窒素原子が表面より脱離し難い温度域(例えば2200℃より高い温度等の高温域)で加熱処理等せずに、高い導電率を損なうことなく炭化ケイ素多結晶基板の反りを低減できる。よって、本実施形態の製造方法で製造された炭化ケイ素多結晶基板を、横型に加えて、縦型のダイオード用炭化ケイ素基板として、デバイス製造工程に供することが可能となり、炭化ケイ素多結晶基板の反り量が小さいことで、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などが少なくなり、歩留まりの向上が期待できる。 Further, in particular, according to the method for producing a silicon carbide polycrystalline substrate of the present embodiment, even in the case of producing a silicon carbide polycrystalline substrate having high conductivity (for example, about 0.1 Ω · cm or more), Warpage of silicon carbide polycrystalline substrate is reduced without heat treatment in a temperature range where nitrogen atoms in silicon carbide are difficult to desorb from the surface (for example, a high temperature range such as a temperature higher than 2200 ° C.) without impairing high conductivity. it can. Therefore, the silicon carbide polycrystalline substrate manufactured by the manufacturing method of the present embodiment can be used in the device manufacturing process as a vertical silicon carbide substrate for a diode in addition to the horizontal type, and the silicon carbide polycrystalline substrate can be used. Since the amount of warpage is small, poor pattern formation in the photolithography process and non-uniformity of the ion penetration depth in the ion injection process are reduced, and an improvement in yield can be expected.

その他、本発明を実施するための最良の構成、方法などは、以上の記載で開示されているが、本発明は、これに限定されるものではない。すなわち、本発明は、主に特定の実施形態に関して特に説明されているが、本発明の技術的思想及び目的の範囲から逸脱することなく、以上述べた実施形態に対し、形状、材質、数量、その他の詳細な構成において、当業者が様々な変形を加えることができるものである。従って、上記に開示した形状、材質などを限定した記載は、本発明の理解を容易にするために例示的に記載したものであり、本発明を限定するものではないから、それらの形状、材質などの限定の一部、もしくは全部の限定を外した部材の名称での記載は、本発明に含まれるものである。 In addition, the best configuration, method, and the like for carrying out the present invention are disclosed in the above description, but the present invention is not limited thereto. That is, although the present invention has been particularly described mainly with respect to a specific embodiment, the shape, material, quantity, and the shape, material, quantity, etc. In other detailed configurations, those skilled in the art can make various modifications. Therefore, the description that limits the shape, material, etc. disclosed above is merely an example for facilitating the understanding of the present invention, and does not limit the present invention. Therefore, those shapes, materials, etc. The description by the name of the member which removes a part or all of the limitation such as is included in the present invention.

以下、本発明の実施例及び比較例によって、本発明をさらに詳細に説明するが、本発明は、これらの実施例によって何ら限定されることはない。 Hereinafter, the present invention will be described in more detail with reference to Examples and Comparative Examples of the present invention, but the present invention is not limited to these Examples.

[炭化ケイ素多結晶基板の製造、および、炭化ケイ素多結晶基板の評価]
(実施例1)
前述した実施形態の成膜装置1000を用いて、炭化ケイ素多結晶膜の成膜を行った。まず、成膜装置1000の基板ホルダー1070に、直径6インチ、厚み500μmのカーボン支持基板を固定した。成膜室1010内へArガスを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、1400℃に達した後Arガスの供給を停止した。原料ガスとして、SiCl、CHを用い、ドーピングガスとしてN、キャリアガスとしてHを用いた。第1炭化ケイ素多結晶膜成膜工程においては、これらのガスの混合比をSiCl:CH:H:N=1:1:10:20として、総流入量を22slm(standard L/min)として、1400℃で2時間の成膜を実施した。厚さが100μmの第1炭化ケイ素多結晶膜をカーボン支持基板の両面に成膜させて、カーボン支持基板と前記炭化ケイ素多結晶膜の積層体を得た。
[Manufacturing of silicon carbide polycrystalline substrate and evaluation of silicon carbide polycrystalline substrate]
(Example 1)
The silicon carbide polycrystalline film was formed using the film forming apparatus 1000 of the above-described embodiment. First, a carbon support substrate having a diameter of 6 inches and a thickness of 500 μm was fixed to the substrate holder 1070 of the film forming apparatus 1000. The pressure inside the furnace was reduced by an exhaust pump while flowing Ar gas into the film forming chamber 1010, and then heated to 1400 ° C., and after reaching 1400 ° C., the supply of Ar gas was stopped. SiCl 4 and CH 4 were used as the raw material gas, N 2 was used as the doping gas, and H 2 was used as the carrier gas. In the first silicon carbide polycrystal film forming step, the mixing ratio SiCl of these gases 4: CH 4: H 2: N 2 = 1: 1: 10: as 20, the total inflow 22 slm (standard L / As min), film formation was carried out at 1400 ° C. for 2 hours. A first silicon carbide polycrystalline film having a thickness of 100 μm was formed on both sides of the carbon support substrate to obtain a laminate of the carbon support substrate and the silicon carbide polycrystalline film.

次に、第2炭化ケイ素多結晶膜成膜工程を行った。第1炭化ケイ素多結晶膜を成膜したあと、原料ガス、ドーピングガスの供給を停止して、キャリアガスのみを供給しながら成膜室内を1200℃まで降温させたのち、温度を維持して、第1炭化ケイ素多結晶膜成膜工程と同じ条件でガスを供給して、厚さ400μmの第2炭化ケイ素多結晶膜の成膜を行った。以上により、カーボン支持基板と炭化ケイ素多結晶膜との積層体を得て、積層体を室温まで冷却したのちに支持基板の除去工程を行った。積層体の外周端部に積層した炭化ケイ素多結晶膜を、ダイヤ砥石を用いて研削して、カーボン支持基板の側面を全周に亘って露出させた。次に、二珪化モリブデン製のヒーターを備える燃焼炉を用いて、大気雰囲気下で温度1000℃、100時間加熱してカーボン支持基板を燃焼除去した。これにより、炭化ケイ素多結晶基板を得た。 Next, a second silicon carbide polycrystalline film forming step was performed. After forming the first silicon carbide polycrystal film, the supply of the raw material gas and the doping gas was stopped, the temperature of the film forming chamber was lowered to 1200 ° C. while supplying only the carrier gas, and then the temperature was maintained. Gas was supplied under the same conditions as in the first silicon carbide polycrystal film forming step to form a second silicon carbide polycrystal film having a thickness of 400 μm. As described above, a laminate of the carbon support substrate and the silicon carbide polycrystalline film was obtained, the laminate was cooled to room temperature, and then the support substrate was removed. The silicon carbide polycrystalline film laminated on the outer peripheral end of the laminate was ground with a diamond grindstone to expose the side surface of the carbon support substrate over the entire circumference. Next, using a combustion furnace equipped with a heater made of molybdenum disilicate, the carbon support substrate was burnt off by heating at a temperature of 1000 ° C. for 100 hours in an air atmosphere. As a result, a silicon carbide polycrystalline substrate was obtained.

次に、得られた炭化ケイ素多結晶基板の反り量を測定した。炭化ケイ素多結晶基板の成膜された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量とした。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。反り量が、100μmより大きいとき、製造した炭化ケイ素多結晶基板について、デバイス等の製造工程で問題の生じ得る反りが有ると判定した。反り量の測定結果を、表1に示した。 Next, the amount of warpage of the obtained silicon carbide polycrystalline substrate was measured. The center line of the film-deposited surface of the silicon carbide polycrystalline substrate was measured with an obliquely incident optical measuring instrument, and the difference between the maximum value and the minimum value of the obtained measured values was defined as the amount of warpage. The measurement was performed at 5 points, and the measurement was performed at the center, the circumferential end, and the point between the center and the circumferential end, where the distance from the center and the distance from the circumferential end are the same. When the amount of warpage is larger than 100 μm, it was determined that the manufactured silicon carbide polycrystalline substrate has warpage that may cause a problem in the manufacturing process of the device or the like. The measurement results of the amount of warpage are shown in Table 1.

(実施例2、実施例3、比較例1〜比較例4)
第1炭化ケイ素多結晶膜成膜工程、第2炭化ケイ素達結晶膜成膜工程の温度を種々変更したこと以外は、実施例1と同様にして炭化ケイ素多結晶基板を製造した。第1炭化ケイ素多結晶膜工程の成膜温度は、実施例2、比較例1、比較例2は1400℃、実施例3、比較例3、比較例4は1500℃とした。第2炭化ケイ素多結晶膜工程の成膜温度は、実施例2、実施例3は1300℃、比較例1は1350℃、比較例2、比較例4は1100℃、比較例3は1400℃とした。得られた炭化ケイ素多結晶基板について、実施例1と同様に反り量の測定を行い、測定結果を表1に示した。
(Example 2, Example 3, Comparative Example 1 to Comparative Example 4)
A silicon carbide polycrystalline substrate was produced in the same manner as in Example 1 except that the temperatures of the first silicon carbide polycrystalline film forming step and the second silicon carbide reaching crystal film forming step were variously changed. The film formation temperature in the first silicon carbide polycrystalline film step was 1400 ° C. for Example 2, Comparative Example 1, and Comparative Example 2, and 1500 ° C. for Example 3, Comparative Example 3, and Comparative Example 4. The film formation temperature of the second silicon carbide polycrystalline film step was 1300 ° C. in Example 2 and Example 3, 1350 ° C. in Comparative Example 1, 1100 ° C. in Comparative Example 2 and Comparative Example 4, and 1400 ° C. in Comparative Example 3. did. The amount of warpage of the obtained silicon carbide polycrystalline substrate was measured in the same manner as in Example 1, and the measurement results are shown in Table 1.

Figure 2021066624
Figure 2021066624

[評価結果の考察]
以上の評価結果により、本発明の例示的態様である実施例1〜実施例3において、比較例1〜比較例4と比べて、製造された炭化ケイ素多結晶基板の反り量が小さく、反り量は60μm〜80μmであった。比較例1、比較例2のように、第1炭化ケイ素多結晶膜成膜工程と第2炭化ケイ素多結晶膜成膜工程との温度差が小さいと、第1炭化ケイ素多結晶膜と第2炭化ケイ素多結晶膜における粒径の差が実施例ほど小さくならずに、反り量が大きくなると考えられた。また、比較例2、比較例4のように、第2炭化ケイ素多結晶膜成膜工程の温度を大きく下げると、第2炭化ケイ素多結晶膜内の炭化ケイ素多結晶の粒径が第1炭化ケイ素多結晶膜内の炭化ケイ素多結晶の粒径よりも小さくなり、粒径の差が生じて、反り量が大きくなると考えられた。以上の実施例、比較例の結果より、本発明の炭化ケイ素多結晶膜の製造方法により、大きな反りが発生することを抑制して、反りの小さい炭化ケイ素多結晶基板を製造することができることが示された。
[Discussion of evaluation results]
Based on the above evaluation results, in Examples 1 to 3 which are exemplary embodiments of the present invention, the amount of warpage of the produced silicon carbide polycrystalline substrate is smaller than that of Comparative Examples 1 to 4, and the amount of warpage is small. Was 60 μm to 80 μm. When the temperature difference between the first silicon carbide polycrystalline film forming step and the second silicon carbide polycrystalline film forming step is small as in Comparative Example 1 and Comparative Example 2, the first silicon carbide polycrystalline film and the second It was considered that the difference in particle size in the silicon carbide polycrystalline film was not as small as in the examples, and the amount of warpage was large. Further, as in Comparative Examples 2 and 4, when the temperature of the second silicon carbide polycrystalline film forming step is significantly lowered, the particle size of the silicon carbide polycrystalline film in the second silicon carbide polycrystalline film becomes the first carbide. It was considered that the particle size was smaller than that of the silicon carbide polycrystalline in the silicon polycrystalline film, a difference in particle size was generated, and the amount of warpage was large. From the results of the above Examples and Comparative Examples, it is possible to produce a silicon carbide polycrystalline substrate having a small warp by suppressing the occurrence of a large warp by the method for producing a silicon carbide polycrystalline film of the present invention. Shown.

100 支持基板
200 第1炭化ケイ素多結晶膜
300 第2炭化ケイ素多結晶膜
400A、400B 積層体
500 炭化ケイ素多結晶基板
100 Support substrate 200 1st silicon carbide polycrystalline film 300 2nd silicon carbide polycrystalline film 400A, 400B Laminated product 500 Silicon carbide polycrystalline substrate

Claims (1)

化学的気相成長法によって支持基板上に第1炭化ケイ素多結晶膜を、1400℃〜1500℃の温度で成膜する、第1炭化ケイ素多結晶膜成膜工程と、
前記第1炭化ケイ素多結晶膜の上に、第2炭化ケイ素多結晶膜を、1200℃〜1300℃、かつ、前記第1炭化ケイ素多結晶膜の成膜温度よりも100℃〜200℃低い温度で成膜する、第2炭化ケイ素多結晶膜成膜工程と、を含む、炭化ケイ素多結晶基板の製造方法。
A first silicon carbide polycrystalline film forming step of forming a first silicon carbide polycrystalline film on a support substrate at a temperature of 1400 ° C. to 1500 ° C. by a chemical vapor deposition method.
On the first silicon carbide polycrystalline film, the second silicon carbide polycrystalline film is placed at a temperature of 1200 ° C. to 1300 ° C., which is 100 ° C. to 200 ° C. lower than the film formation temperature of the first silicon carbide polycrystalline film. A method for producing a silicon carbide polycrystalline substrate, which comprises a second silicon carbide polycrystalline film forming step.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114075699A (en) * 2021-11-21 2022-02-22 无锡华鑫检测技术有限公司 Double-layer composite silicon carbide substrate and preparation method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05295546A (en) * 1992-04-20 1993-11-09 Sumitomo Metal Ind Ltd Production of ceramic film laminated material
JPH10167861A (en) * 1996-12-16 1998-06-23 Tokai Carbon Co Ltd Antioxidation treatment of carbon material reinforced carbon fiber
JPH11292645A (en) * 1998-04-16 1999-10-26 Tokai Carbon Co Ltd Oxidation resistant c/c composite material and its production
JP2003034867A (en) * 2001-07-27 2003-02-07 Tokai Carbon Co Ltd TUBULAR SiC-COMPACT AND MANUFACTURING METHOD THEREFOR
JP2012136376A (en) * 2010-12-24 2012-07-19 Toyo Tanso Kk Unit for liquid phase epitaxial growth of single crystal silicon carbide, and method for liquid phase epitaxial growth of single crystal silicon carbide
WO2017047509A1 (en) * 2015-09-15 2017-03-23 信越化学工業株式会社 MANUFACTURING METHOD OF SiC COMPOSITE SUBSTRATE

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05295546A (en) * 1992-04-20 1993-11-09 Sumitomo Metal Ind Ltd Production of ceramic film laminated material
JPH10167861A (en) * 1996-12-16 1998-06-23 Tokai Carbon Co Ltd Antioxidation treatment of carbon material reinforced carbon fiber
JPH11292645A (en) * 1998-04-16 1999-10-26 Tokai Carbon Co Ltd Oxidation resistant c/c composite material and its production
JP2003034867A (en) * 2001-07-27 2003-02-07 Tokai Carbon Co Ltd TUBULAR SiC-COMPACT AND MANUFACTURING METHOD THEREFOR
JP2012136376A (en) * 2010-12-24 2012-07-19 Toyo Tanso Kk Unit for liquid phase epitaxial growth of single crystal silicon carbide, and method for liquid phase epitaxial growth of single crystal silicon carbide
WO2017047509A1 (en) * 2015-09-15 2017-03-23 信越化学工業株式会社 MANUFACTURING METHOD OF SiC COMPOSITE SUBSTRATE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114075699A (en) * 2021-11-21 2022-02-22 无锡华鑫检测技术有限公司 Double-layer composite silicon carbide substrate and preparation method thereof
CN114075699B (en) * 2021-11-21 2024-04-12 苏州晶瓴半导体有限公司 Double-layer composite silicon carbide substrate and preparation method thereof

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