JPH0247252A - Production of composite material film - Google Patents

Production of composite material film

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Publication number
JPH0247252A
JPH0247252A JP19581088A JP19581088A JPH0247252A JP H0247252 A JPH0247252 A JP H0247252A JP 19581088 A JP19581088 A JP 19581088A JP 19581088 A JP19581088 A JP 19581088A JP H0247252 A JPH0247252 A JP H0247252A
Authority
JP
Japan
Prior art keywords
substrate
source
composite material
gas
titanium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP19581088A
Other languages
Japanese (ja)
Inventor
Mizuaki Suzuki
瑞明 鈴木
Matsuo Kishi
松雄 岸
Kenichi Ogawa
健一 小川
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Seiko Instruments Inc
Original Assignee
Seiko Instruments Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Seiko Instruments Inc filed Critical Seiko Instruments Inc
Priority to JP19581088A priority Critical patent/JPH0247252A/en
Publication of JPH0247252A publication Critical patent/JPH0247252A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To form a TiC-SiC composite material film on a substrate at relatively low temp. by evaporating titanium by means of electron beam or hollow cathode discharge, introducing silicon compound gas and hydrocarbon gas, and ionizing and activating respective elements. CONSTITUTION:In a vacuum tank 1 in which evacuation is performed through an exhaust hole 12, Ti held in a crucible 3 is heated and evaporated by means of electron beam 8. Subsequently, a silicon compound gas, such as silane, disilane, and tetramethylsilane, as an Si source and a hydrocarbon gas, such as CH4 and C2H2, as a C source are introduced through a gas-introducing hole 7. Then, electric discharge is initiated by means of an ionization electrode 9 connected to an electric power source 13 to ionize and activate respective elements, and, at this time, a shutter 10 is opened and the above ionized and activated elements are introduced onto a substrate 2 of glass, etc. At the time ot the above treatment, a high-frequency electric power is impressed on the substrate 2, if necessary, and further the substrate 2 is heated via a heat source 11 up to the prescribed temp. By this method, the TiC-SiC composite material can be formed on the above substrate 2 without elevating ionization, activation, and substrate temps. up to >=about 200 deg.C.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明はサーマルヘッド、電子回路などに電気抵抗体と
して用いられる炭化チタン−炭化珪素(TiC−3iC
)複合材料膜の製造方法に関するものである。
Detailed Description of the Invention [Industrial Application Field] The present invention is directed to titanium carbide-silicon carbide (TiC-3iC) used as an electrical resistor in thermal heads, electronic circuits, etc.
) relates to a method for manufacturing a composite material membrane.

〔発明の概要〕[Summary of the invention]

チタン源として電子ビーム蒸発源またはホロー陰極蒸発
源を用い、珪素源として珪素化合物ガスと炭素源として
炭化水素ガスを真空槽に導入し、基板上に炭化チタン−
炭化珪素複合材料膜を低温で形成する。
Using an electron beam evaporation source or a hollow cathode evaporation source as a titanium source, a silicon compound gas as a silicon source and a hydrocarbon gas as a carbon source are introduced into a vacuum chamber, and titanium carbide is deposited on the substrate.
A silicon carbide composite film is formed at low temperature.

〔従来の技術〕[Conventional technology]

従来の技術は熱CVD法(熱化学気相成長法)と呼ばれ
る技術であり、反応容器内に材料ガスとして四塩化チタ
ン(TiC14)ガス、四塩化珪素(SiC1g)ガス
およびメタンなどの炭化水素ガスを導入し、1000″
C程度に加熱することにより熱エネルギーによって化学
反応を起こし、基板上に炭化チタン炭化珪素複合材料膜
を形成していた。
The conventional technology is a technology called thermal CVD (thermal chemical vapor deposition), which uses titanium tetrachloride (TiC14) gas, silicon tetrachloride (SiC1g) gas, and hydrocarbon gas such as methane as material gases in a reaction vessel. Introduced 1000″
By heating to about 50% Celsius, a chemical reaction was caused by the thermal energy, and a titanium carbide silicon carbide composite material film was formed on the substrate.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

上記のような従来技術では、熱エネルギーによって化学
反応を起こすために材料ガスを1000℃程度に加熱す
る必要があるため、耐熱性を存する基板上でなければ、
炭化チタン−炭化珪素複合材料膜を形成することができ
なかった。
In the conventional technology described above, it is necessary to heat the material gas to about 1000 degrees Celsius in order to cause a chemical reaction using thermal energy.
A titanium carbide-silicon carbide composite film could not be formed.

また、材料ガスである四塩化チタン、四塩化珪素は腐食
性の塩素(CI)を生じるため、反応容器や排気装置に
障害を与えてしまう。また、膜中に塩素が残留し、膜を
腐食してしまうことがある。
Furthermore, titanium tetrachloride and silicon tetrachloride, which are material gases, generate corrosive chlorine (CI), which may cause damage to the reaction vessel and the exhaust system. In addition, chlorine may remain in the film and corrode the film.

〔課題を解決するための手段〕[Means to solve the problem]

本発明は上記の問題点を解決するために、チタン源とし
て四塩化チタンなどのガスを用いずに、電子ビーム加熱
方式の金属蒸発源またはホロー陰極放電方式の金属蒸発
源を用い、珪素源としてシラン、ジシラン、テトラメチ
ルシランなどの珪素化合物ガスと炭素源としてメタン、
アセチレンなどの炭化水素ガスを真空槽に導入し、イオ
ン化電極またはホロー陰極による放電によって各元素を
イオン化、活性化、基板温度を200℃以上に上昇させ
ることなく炭化チクンー炭化珪素複合材料膜の形成を可
能とした。
In order to solve the above problems, the present invention uses an electron beam heating type metal evaporation source or a hollow cathode discharge type metal evaporation source as a silicon source instead of using a gas such as titanium tetrachloride as a titanium source. Silicon compound gas such as silane, disilane, and tetramethylsilane and methane as a carbon source,
Hydrocarbon gas such as acetylene is introduced into a vacuum chamber, and each element is ionized and activated by discharge using an ionizing electrode or hollow cathode, forming a chikum carbide-silicon carbide composite material film without raising the substrate temperature above 200°C. made possible.

〔作用〕[Effect]

電子ビー加熱方式またはホロー陰極放電方式の金属蒸発
源により、チタンを蒸発させ、導入した珪素化合物ガス
、炭化水素ガスと共にイオン化し、イオンおよび電子の
エネルギーによって元素を活性化することにより、低温
であっても炭化チタン−炭化珪素複合材料膜を基板上に
形成することができる。
Titanium is evaporated using an electron bee heating method or hollow cathode discharge method metal evaporation source, ionized together with the introduced silicon compound gas and hydrocarbon gas, and the element is activated by the energy of the ions and electrons. However, a titanium carbide-silicon carbide composite film can be formed on a substrate.

〔実施例〕〔Example〕

本発明の実施例について図面を参照して説明する。 Embodiments of the present invention will be described with reference to the drawings.

第1図は本発明の実施に用いた電子ビーム加熱方式装置
の概略図である。真空槽1内に基板2を設置し、るつぼ
3にチタンを入れ、10−’Torr以下の圧力まで排
気する。実施例では基板としてガラス板を用いた。
FIG. 1 is a schematic diagram of an electron beam heating system used in carrying out the present invention. A substrate 2 is placed in a vacuum chamber 1, titanium is placed in a crucible 3, and the crucible is evacuated to a pressure of 10-' Torr or less. In the example, a glass plate was used as the substrate.

真空槽1内に設置された基板2には切り替えスイッチ4
を介して高周波電源5または直流電a6が接続され、高
周波電圧または直流電圧を印加することができる。
A changeover switch 4 is installed on the board 2 installed in the vacuum chamber 1.
A high frequency power source 5 or a direct current power a6 is connected through the terminal, and a high frequency voltage or a direct current voltage can be applied.

まず、ガス導入ロアよりアルゴンガスを導入し、5 X
 10−’〜2 X 10−”Torr程度の圧力で基
板2に周波数13.56MHz、電力100Wの高周波
電力を印加し、アルゴンガスのグロー放電を行う。これ
によりアルゴンイオンで基板表面を衝撃し、汚染物を除
去する。充分に基板表面を清浄にした後、再び1O−5
Torr以下の圧力まで排気する。
First, introduce argon gas from the gas introduction lower, and
High frequency power of 13.56 MHz and 100 W of power is applied to the substrate 2 at a pressure of about 10-' to 2 x 10-'' Torr to cause a glow discharge of argon gas.This bombards the surface of the substrate with argon ions. Remove contaminants. After thoroughly cleaning the substrate surface, 1O-5
Evacuate to pressure below Torr.

次に、るつぼ3内のチタンを電子ビーム8で加熱、蒸発
させ、ガス導入ロアよりテトラメチルシランガス、アセ
チレンガスを導入し、5 x’to−’〜5 X 10
− ’Torrの圧力でイオン化電極9により放電を行
い、各元素をイオン化、活性化する。このとき、シャッ
ター10を開けば基板z上に炭化チタン炭化珪素複合材
料膜が形成される。チタンの蒸発量、各材料ガスの分圧
を変化させることにより、形成される膜の炭化チタンと
炭化珪素の組成比を変化させることができる。実施例で
は成膜中に基板2に周波数13.56Ml1z、電力1
00Wの高周波電力を印加した。この様に、成膜中に基
板に負の直流電圧または高周波電圧を印加することによ
り、イオンの基板への入射エネルギーが増加するため、
緻密かつ硬質な膜を基板との密着性よく形成することが
できる。
Next, the titanium in the crucible 3 is heated and evaporated with an electron beam 8, and tetramethylsilane gas and acetylene gas are introduced from the gas introduction lower, and 5 x'to-' to 5 x 10
- Discharge is performed by the ionizing electrode 9 at a pressure of Torr to ionize and activate each element. At this time, if the shutter 10 is opened, a titanium carbide silicon carbide composite material film is formed on the substrate z. By changing the amount of titanium evaporated and the partial pressure of each material gas, the composition ratio of titanium carbide and silicon carbide in the formed film can be changed. In the example, a frequency of 13.56 Ml1z and a power of 1 were applied to the substrate 2 during film formation.
A high frequency power of 00 W was applied. In this way, by applying a negative DC voltage or high frequency voltage to the substrate during film formation, the incident energy of ions to the substrate increases.
A dense and hard film can be formed with good adhesion to the substrate.

以上の方法により成膜時間10分間で膜厚約1μmの炭
化チタン−炭化珪素複合材料膜が基板上に形成された。
By the above method, a titanium carbide-silicon carbide composite material film having a film thickness of about 1 μm was formed on the substrate in a film forming time of 10 minutes.

成膜中に材料ガスとともにアルゴンガスを導入し、アル
ゴンイオンで膜を衝撃することにより、膜質を向上させ
ることができる。また、基板2を加熱する必要がある場
合は発熱#1)を使用することもできる。
The quality of the film can be improved by introducing argon gas together with the material gas during film formation and bombarding the film with argon ions. Furthermore, if it is necessary to heat the substrate 2, heating #1) can also be used.

第2図は本発明の実施に用いたホロー陰極放電方式装置
の概略図である。ホロー陰極9にアルゴンガスを導入し
、ホロー陰極放電によってチタンを加熱、蒸発させ、各
元素をイオン化する方式である以外は第1図に示した装
置と同様の装置であり、同様の炭化チタン−炭化珪素複
合材料膜を得ることができる。
FIG. 2 is a schematic diagram of a hollow cathode discharge type device used to implement the present invention. This device is similar to the device shown in FIG. 1, except that argon gas is introduced into the hollow cathode 9, and titanium is heated and evaporated by hollow cathode discharge to ionize each element. A silicon carbide composite film can be obtained.

〔発明の効果) 従来の技術のような高温は必要なく、耐熱性の劣るガラ
スなどの基板上にも炭化チタン−炭化珪素複合材料膜を
形成することができる。チタンの蒸発量、各材料ガスの
分圧などの成膜条件を変化させることにより、形成され
る膜の炭化チタンと炭化珪素の組成比を変化させること
ができる。
[Effects of the Invention] Unlike conventional techniques, high temperatures are not required, and a titanium carbide-silicon carbide composite film can be formed even on a substrate such as glass that has poor heat resistance. By changing film forming conditions such as the amount of evaporation of titanium and the partial pressure of each material gas, the composition ratio of titanium carbide and silicon carbide in the formed film can be changed.

また、材料ガスとして塩化物を使用しないため、排気ポ
ンプに障害を与えたり、膜中に塩素が残留することもな
い。
In addition, since chloride is not used as a material gas, there is no possibility of damaging the exhaust pump or leaving chlorine in the membrane.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の実施に用いた電子ビーム加熱方式装置
の概略図であり、電子ビームにより金属を加熱し、イオ
ン化電極によりイオン化する方式第2図は本発明の実施
に用いたホロー陰極放電方式装置の概略図であり、ホロ
ー陰極放電により金属を加熱、蒸発させ、イオン化する
方式である。 真空槽 基板 るつぼ 切り替えスイッチ 高周波電源 直流電源 ガス導入口 電子ビーム イオン化電極 シャッター 発熱源 排気口 イオン化電極用電源 ホロー陰極用電源 アルゴンガス導入口 出願人 セイコー電子工業株式会社 代理人 弁理士 林  敬 之 助
Figure 1 is a schematic diagram of an electron beam heating system used in the practice of the present invention, and Figure 2 shows a hollow cathode discharge system in which metal is heated by an electron beam and ionized by an ionizing electrode. This is a schematic diagram of a method device in which metal is heated, evaporated, and ionized by hollow cathode discharge. Vacuum chamber Substrate Crucible switch High frequency power supply DC power supply Gas inlet Electron beam ionization electrode shutter Heat source Exhaust port Ionization electrode power supply Hollow cathode power supply Argon gas inlet Applicant Seiko Electronic Industries Co., Ltd. Agent Patent attorney Keinosuke Hayashi

Claims (2)

【特許請求の範囲】[Claims] (1)チタン源として電子ビーム加熱方式の金属蒸発源
またはホロー陰極放電方式の金属蒸発源を用いチタンを
蒸発させ、珪素源としてシラン、ジシラン、テトラメチ
ルシランなどの珪素化合物ガスと炭素源としてメタン、
アセチレンなどの炭化水素ガスとを真空槽に導入し、イ
オン化電極またはホロー陰極などの放電によって各元素
をイオン化、活性化することにより基板上に炭化チタン
−炭化珪素複合材料膜を形成することを特徴とする複合
材料膜の製造方法。
(1) Titanium is evaporated using an electron beam heating type metal evaporation source or a hollow cathode discharge type metal evaporation source as a titanium source, and a silicon compound gas such as silane, disilane, or tetramethylsilane is used as a silicon source, and methane is used as a carbon source. ,
A titanium carbide-silicon carbide composite material film is formed on the substrate by introducing hydrocarbon gas such as acetylene into a vacuum chamber and ionizing and activating each element by electric discharge from an ionizing electrode or hollow cathode. A method for manufacturing a composite membrane.
(2)特許請求の範囲第1項において、基板上に複合材
料膜形成の際に、基板に負の直流電圧または高周波電圧
を印加することにより基板上に炭化チタン−炭化珪素複
合材料膜を形成することを特徴とする特許請求の範囲第
1項記載の複合材料膜の製造方法。
(2) In claim 1, when forming a composite material film on a substrate, a titanium carbide-silicon carbide composite material film is formed on the substrate by applying a negative DC voltage or high frequency voltage to the substrate. A method for manufacturing a composite material membrane according to claim 1, characterized in that:
JP19581088A 1988-08-05 1988-08-05 Production of composite material film Pending JPH0247252A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19581088A JPH0247252A (en) 1988-08-05 1988-08-05 Production of composite material film

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19581088A JPH0247252A (en) 1988-08-05 1988-08-05 Production of composite material film

Publications (1)

Publication Number Publication Date
JPH0247252A true JPH0247252A (en) 1990-02-16

Family

ID=16347363

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19581088A Pending JPH0247252A (en) 1988-08-05 1988-08-05 Production of composite material film

Country Status (1)

Country Link
JP (1) JPH0247252A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5442912A (en) * 1992-12-04 1995-08-22 Hitachi Construction Machinery Co., Ltd. Hydraulic recovery device
RU2502828C1 (en) * 2012-06-18 2013-12-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Национальный исследовательский Томский государственный университет" Application of antifriction wear-proof coat on titanium, alloys
GB2534519A (en) * 2013-10-31 2016-07-27 Kawasaki Heavy Ind Ltd Hydraulic shovel drive system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5442912A (en) * 1992-12-04 1995-08-22 Hitachi Construction Machinery Co., Ltd. Hydraulic recovery device
RU2502828C1 (en) * 2012-06-18 2013-12-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Национальный исследовательский Томский государственный университет" Application of antifriction wear-proof coat on titanium, alloys
GB2534519A (en) * 2013-10-31 2016-07-27 Kawasaki Heavy Ind Ltd Hydraulic shovel drive system
GB2534519B (en) * 2013-10-31 2019-12-11 Kawasaki Heavy Ind Ltd Hydraulic excavator drive system

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