JPS6354216B2 - - Google Patents
Info
- Publication number
- JPS6354216B2 JPS6354216B2 JP17285281A JP17285281A JPS6354216B2 JP S6354216 B2 JPS6354216 B2 JP S6354216B2 JP 17285281 A JP17285281 A JP 17285281A JP 17285281 A JP17285281 A JP 17285281A JP S6354216 B2 JPS6354216 B2 JP S6354216B2
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- substrate
- sih
- film
- mmhg
- 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.)
- Expired
Links
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 claims description 19
- 239000000758 substrate Substances 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 13
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 10
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 5
- 238000000576 coating method Methods 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 description 10
- 239000007789 gas Substances 0.000 description 6
- 229910052753 mercury Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 229910021417 amorphous silicon Inorganic materials 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000005469 synchrotron radiation Effects 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 108091008695 photoreceptors Proteins 0.000 description 1
- 208000017983 photosensitivity disease Diseases 0.000 description 1
- 231100000434 photosensitization Toxicity 0.000 description 1
- 239000003504 photosensitizing agent Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000005546 reactive sputtering Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
- C23C16/34—Nitrides
- C23C16/345—Silicon nitride
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/48—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating by irradiation, e.g. photolysis, radiolysis, particle radiation
- C23C16/482—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating by irradiation, e.g. photolysis, radiolysis, particle radiation using incoherent light, UV to IR, e.g. lamps
Landscapes
- Chemical & Material Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Formation Of Insulating Films (AREA)
Description
【発明の詳細な説明】 本発明は被膜形成方法に関する。[Detailed description of the invention] The present invention relates to a method for forming a film.
最近、IC回路の設計、製作関係で、絶縁膜、
表面保護膜としてシリコンナイトライド(以下
Si3N4)が注目され、その被膜形成方法が盛んに
研究されている。 Recently, insulating films,
Silicon nitride (hereinafter referred to as
Si 3 N 4 ) has attracted attention, and methods for forming its film have been actively researched.
他方、太陽電池や電子写真用感光体として、ア
モルフアスシリコン(以下a―Si)の膜が注目さ
れ、やはりその被膜形成方法の研究が盛んに行な
われている。 On the other hand, amorphous silicon (hereinafter referred to as a-Si) films are attracting attention as photoreceptors for solar cells and electrophotography, and research on methods for forming the films is also being actively conducted.
従来のこれらの被膜形成方法としては、(イ)プラ
ズマ法、(ロ)反応性スパツター法などが知られてい
るが、(イ)については、例えばSiH4を放電で分解
してSiの被膜を基体表面に形成しようとすると、
SiやHのイオンやラヂカルを被膜内に取り込むこ
とがあり、ピンホールの発生、長時間にまたがつ
て取り込まれた物質が抜けるために生ずる物性値
の経時変化の発生などの欠点があり、Si3N4の被
膜の場合にもピンホールの発生などの欠点が指摘
されている。(ロ)については、広い面積に均一に被
膜を形成することが困難なので、電子写真用に大
きなドラム、面積の広い太陽電池への利用ができ
ない等の欠点が指摘されている。 Conventional methods for forming these films include (a) plasma method and (b) reactive sputtering method, but in (a), for example, SiH 4 is decomposed by electric discharge to form a Si film. When trying to form on the substrate surface,
Si and H ions and radicals may be incorporated into the film, which has drawbacks such as the formation of pinholes and the occurrence of changes in physical properties over time due to the escape of substances that have been incorporated over a long period of time. In the case of the 3N4 coating, drawbacks such as the occurrence of pinholes have also been pointed out. As for (b), it has been pointed out that it is difficult to uniformly form a coating over a wide area, so it cannot be used for large drums for electrophotography or solar cells with a large area.
本発明は、上記事情に鑑みなされたものであつ
て、その目的は、ピンホールや経時変化のない被
膜であつて、広い面積にも均一に形成できるよう
な新規なシリコンナイトライドの被膜形成方法を
提供することにあり、その特徴は、
水銀蒸気の圧力が、1×10-4〜20mmHgの範囲
内に制御された気密容器内に基体を配置し、該基
体表面上での254±10nmの放射光強度が20μW/
cm2以上になる如く該放射光が全放射光の70%以上
の放電灯によつて該基体を照射し、該気密容器内
に、0.01〜7mmHgの圧力のSiH4と、該SiH4に
対する圧力比で
30≧圧力(N2H4)/圧力(SiH4)≧1の範囲に規定し
た
N2H4とを流入せしめて、該基体表面上に、シリ
コンナイトライドの被膜を形成することにある。 The present invention has been made in view of the above circumstances, and its purpose is to provide a novel method for forming a silicon nitride film that is free from pinholes and does not change over time and can be formed uniformly over a wide area. The feature is that the substrate is placed in an airtight container in which the pressure of mercury vapor is controlled within the range of 1 × 10 -4 to 20 mmHg, and the Radiant light intensity is 20μW/
cm 2 or more, the substrate is irradiated with a discharge lamp in which the synchrotron radiation is 70% or more of the total radiation, and SiH 4 at a pressure of 0.01 to 7 mmHg and the pressure relative to the SiH 4 are placed in the airtight container. A silicon nitride film is formed on the surface of the substrate by flowing N 2 H 4 at a ratio of 30≧Pressure (N 2 H 4 )/Pressure (SiH 4 )≧1. be.
以下、実施例とその図面を参考にしながら本発
明を説明する。 The present invention will be described below with reference to examples and drawings thereof.
第1図は、一部断面で示した、本発明被膜形成
方法を実施するための被膜形成装置の一例の説明
図であつて、ヒーターなどの加熱源とミラーなど
は省略してある。第2図は、第1図の装置のA―
A断面の説明図である。 FIG. 1 is an explanatory diagram, partially shown in cross section, of an example of a film forming apparatus for carrying out the film forming method of the present invention, and a heating source such as a heater, a mirror, etc. are omitted. Figure 2 shows the A-
It is an explanatory view of A section.
図において、1は石英製ガラスのパイプ、2
は、ゴムまたはプラスチツク性の弾性パツキング
3を介して前記パイプ1を両側から気密に保持す
る円板部材、4は、円板部材2を組み立てる支持
柱を示し、5a,5bは回転シヤフトであつて、
摩擦板6によつて夫々の先端が突き合わされ、一
方が回転すれば他方も回転するようになつたもの
で、円板部材2に対しては、例えばウイルソンシ
ールの如く、気密でかつ回動自在に係着されてい
る。そして、回転シヤフトの一方5bの外周に基
体8を保持する保持部材9を設ける。図示の例で
は、基体8は円筒状のアルミパイプである。 In the figure, 1 is a quartz glass pipe, 2
is a disc member that airtightly holds the pipe 1 from both sides through elastic packing 3 made of rubber or plastic, 4 is a support column for assembling the disc member 2, and 5a and 5b are rotating shafts. ,
The tips of each are brought into contact with each other by a friction plate 6, so that when one rotates, the other also rotates, and with respect to the disc member 2, an airtight and rotatable seal is used, such as a Wilson seal, for example. is attached to. A holding member 9 for holding the base body 8 is provided on the outer periphery of one side 5b of the rotating shaft. In the illustrated example, the base 8 is a cylindrical aluminum pipe.
7と10は、基体8をパイプ1の外部から照射
する赤外線ランプと低圧水銀蒸気放電灯であつ
て、円板部材2に対して、ランプ保持具11を介
して固定されている。このランプ保持具11は機
構を簡略にするためにミラー12の支持を兼務し
ても良い。 7 and 10 are an infrared lamp and a low-pressure mercury vapor discharge lamp that irradiate the base 8 from outside the pipe 1, and are fixed to the disc member 2 via a lamp holder 11. This lamp holder 11 may also serve as support for the mirror 12 to simplify the mechanism.
13,14は夫々、反応性気体の送入路、排出
路、15はパイプ1の内部の水銀蒸気圧を制御す
るための水銀留、16は、パイプ1内をリークし
たり、必要に応じて緩衝ガスを送入するための補
助路である。送入路13は、反応性気体の種類に
よつては複数本設けたり、或は、必要な気体をあ
らかじめ混合しておけば1本で足りる。19は、
200nm以下の光をカツトするためのフイルターで
ある。 Reference numerals 13 and 14 refer to a reactive gas inlet passage and a discharge passage, respectively; 15 a mercury reservoir for controlling the mercury vapor pressure inside the pipe 1; and 16 a mercury reservoir for controlling the mercury vapor pressure inside the pipe 1, and This is an auxiliary path for supplying buffer gas. Depending on the type of reactive gas, a plurality of inlet channels 13 may be provided, or one inlet channel 13 may be sufficient if the necessary gases are mixed in advance. 19 is
This is a filter that cuts out light of 200 nm or less.
上記装置の設計例を示すと、パイプ1は内径
120mm、基体8は直径45mm、長さ990mm、赤外線ラ
ンプは発光長1200mmの、消費電力500Wのランプ、
低圧水銀蒸気放電灯は発光長1250mm、消費電力
500Wを4本使用し、ミラーはアルミニウムを鏡
面加工したものである。この装置で、回転シヤフ
トを10回/分の速度で回転させながら、基体8の
アルミパイプの外周面の温度を約100℃、水銀蒸
気圧力を約1×10-3mmHgに保ち、SiH4とN2H4
との混合ガスを500c.c./分(圧力で大体0.2mmH
g)流すと、アルミパイプの外周面には6分程度
で厚さ1.5μmのシリコンナイトライドの層が形成
される。尚、アルミパイプ外周面での254±10nm
の強度は低圧水銀蒸気放電灯の直下で約
650μW/cm2である。 To show an example of the design of the above device, pipe 1 has an inner diameter of
120mm, the base 8 has a diameter of 45mm, a length of 990mm, an infrared lamp with an emission length of 1200mm, and a power consumption of 500W.
Low-pressure mercury vapor discharge lamp has a light emission length of 1250 mm and power consumption.
Four 500W batteries are used, and the mirror is made of mirror-finished aluminum. With this device, while rotating the rotary shaft at a speed of 10 times/min, the temperature of the outer peripheral surface of the aluminum pipe of the base 8 is maintained at approximately 100°C, the mercury vapor pressure is maintained at approximately 1 × 10 -3 mmHg, and SiH 4 and N 2 H 4
500c.c./min (approximately 0.2mmH pressure)
g) When flowing, a layer of silicon nitride with a thickness of 1.5 μm is formed on the outer peripheral surface of the aluminum pipe in about 6 minutes. In addition, 254±10nm on the outer circumferential surface of the aluminum pipe
The intensity is approximately
It is 650μW/ cm2 .
上記シリコンナイトライドの層、もしくは被膜
が形成される原理は、
Hg254±10nm
―――――――
Hg※(水銀の活性化)
SiH4+Hg※→Si+2H2+Hg
N2H4+Hg※→N2+2H2+Hg
3Si +2N2→Si3N4(シリコンナイトライド)
Si3N4→Si3N4の沈着
による。そして、N2H4とSiH4の圧力比は、
30≧圧力(N2H4)/圧力(SiH4)≧1
が良く、30より大きい範囲ではピンホールの発
生、1より小さい範囲ではSi3N4の被膜形成速度
が小さいなどの欠点が見られる。Hgはフオトセ
ンシタイザーとして機能し、圧力としては1×
10-4〜20mmHgが適している。その理由は、1×
10-4mmHgより小さいところでは、活性化された
水銀原子の密度が低すぎること及び20mmHgより
大きいところでは、水銀の自己吸収の影響が大き
く現われて来て、いづれも、被膜形成速度が遅
く、実用性に劣るからである。同様に、SiH4の
圧力としては、0.01mmHgより低いところでは被
膜形成速度が極めて遅く実用性に欠け、7mmHg
より大きいところでは、ピンホール(この場合
「す」のようなもの)などが生じて膜質が悪く、
方法として実用的かつ良質の膜は、0.01mmHgか
ら7mmHgであつた。 The principle behind the formation of the silicon nitride layer or film is as follows: Hg254±10nm ―――――――― Hg* (activation of mercury) SiH 4 +Hg*→Si+2H 2 +Hg N 2 H 4 +Hg*→N 2 +2H 2 +Hg 3Si +2N 2 →Si 3 N 4 (silicon nitride) Due to the deposition of Si 3 N 4 →Si 3 N 4 . The pressure ratio of N 2 H 4 and SiH 4 should preferably be 30≧Pressure (N 2 H 4 )/Pressure (SiH 4 )≧1; in a range larger than 30, pinholes occur, and in a range smaller than 1, Si There are drawbacks such as a slow film formation rate for 3N4 . Hg acts as a photosensitizer, and the pressure is 1×
10 -4 to 20 mmHg is suitable. The reason is 1×
Below 10 -4 mmHg, the density of activated mercury atoms is too low, and above 20 mmHg, the influence of self-absorption of mercury becomes significant, and in both cases, the film formation rate is slow. This is because it is less practical. Similarly, if the pressure of SiH 4 is lower than 0.01 mmHg, the film formation rate is extremely slow and impractical;
In larger areas, pinholes (in this case, the ones that look like "su") occur and the film quality is poor.
Practical and high-quality membranes for this method ranged from 0.01 mmHg to 7 mmHg.
補助路16を利用して導入する緩衝ガスとして
はAr,N2,等があり、これらは、Hg※の63P1や
61P1軌道の電子と衝突しても化学変化を生じせし
めることなく種々の良い効果をもたらすことがあ
り、例えば、ArやN2は、被膜形成速度が大きす
ぎる場合に適度に速度を抑制したりする。また、
フイルター19は、前記の通り200nm以下の光を
カツトするものであるが、低圧水銀蒸気放電灯か
ら放射される185±10nmの光も、254±10nmと殆
んど同様な作用効果を有するので、フイルター1
9を除くと、185±10nmの光による作用も加わ
り、更に良い結果をもたらす。 Buffer gases introduced using the auxiliary channel 16 include Ar, N 2 , etc., and these include 6 3 P 1 of Hg* and
Collisions with electrons in the 6 1 P 1 orbit can bring about various positive effects without causing chemical changes. For example, Ar and N 2 can moderately suppress the film formation rate when it is too high. I do things. Also,
As mentioned above, the filter 19 cuts out light of 200 nm or less, but the 185 ± 10 nm light emitted from a low-pressure mercury vapor discharge lamp has almost the same effect as 254 ± 10 nm, so Filter 1
If 9 is excluded, the effect of light of 185±10 nm is also added, resulting in even better results.
第3図は、第1図において、基体8に置き代つ
て配置される、絶縁基板やIC回路のチツプ(い
づれも図示せず)を載置固定するための中空支持
台17の説明図であつて、絶縁基板やチツプが昇
温しやすいように、胴体部はネツト構造18にな
つている。絶縁基板、例えばアルミナ板へのシリ
コンナイトライドの被膜形成は、前記実施例と同
じ条件で達成できる。 FIG. 3 is an explanatory diagram of a hollow support 17 for mounting and fixing an insulating substrate and an IC circuit chip (none of which are shown), which is arranged in place of the base 8 in FIG. 1. The body has a net structure 18 so that the temperature of the insulating substrate and chip can easily rise. Formation of a silicon nitride film on an insulating substrate, such as an alumina plate, can be achieved under the same conditions as in the previous example.
ところで、本発明被膜形成方法は、以下の説明
からも理解されるように、被膜形成は、主に基体
表面近傍の、光増感反応を利用して反応生成物の
沈着を利用するものであるから、基体表面上での
254±10nmの強度が大きい方が良く、少なくとも
20μW/cm2以上あつた方が良い。これより小さい
ところでは、被膜形成速度が遅く、実用性に欠け
る。したがつて、本発明は、強度を20μW/cm2以
上に、かつ広い面積を均一に照射するものである
が、低圧水銀蒸気放電灯のような水銀灯を利用す
れば、254±10nmの放射光が全方射光の70%以上
あるので、比較的簡単に設計、実施することがで
き、しかも、被膜形成速度の制御も、水銀灯の出
力を制御したり、緩衝ガスを混入せしめたりする
ことによつて容易にできるので、ピンホールや経
時変化のない被膜を、大面積にまたがつて早く均
一に形成せしめることができる。 By the way, in the film forming method of the present invention, as will be understood from the following explanation, film formation utilizes deposition of a reaction product mainly in the vicinity of the substrate surface using a photosensitization reaction. From, on the substrate surface
The higher the intensity at 254±10nm, the better, at least
It is better to be hotter than 20μW/ cm2 . If it is smaller than this, the film formation rate will be slow and it will be impractical. Therefore, although the present invention uniformly irradiates a wide area with an intensity of 20 μW/cm 2 or more, if a mercury lamp such as a low-pressure mercury vapor discharge lamp is used, radiation of 254 ± 10 nm can be achieved. Since it accounts for more than 70% of the omnidirectional light, it is relatively easy to design and implement, and the film formation rate can also be controlled by controlling the output of the mercury lamp or by mixing buffer gas. Since it can be easily formed, a coating without pinholes or deterioration over time can be quickly and uniformly formed over a large area.
本発明は、以上の説明からも理解されるよう
に、水銀蒸気の圧力が、1×10-4〜20mmHgの範
囲内に制御された気密容器内に基体を配置し、該
基体表面上での254±10nの放射光強度が20μW/
cm2以上になる如く該放射光が全放射光の70%以上
の放電灯によつて該基体を照射し、該気密容器内
に、0.01〜7mmHgの圧力のSiH4と、該SiH4に
対する圧力比で
30≧圧力(N2H4)/圧力(SiH4)≧1の範囲に規定し
た
N2H4とを流入せしめて、該基体表面上に、シリ
コンナイトライドの被膜を形成するものであるか
ら、ピンホールや経時変化のない被膜であつて、
広い面積にも均一に形成でき、したがつて、IC
回路のチツプの表面保護膜、その他の絶縁膜とし
て良好なシリコンナイトライドの被膜が提供でき
る。 As can be understood from the above explanation, the present invention provides a method for disposing a substrate in an airtight container in which the pressure of mercury vapor is controlled within the range of 1 x 10 -4 to 20 mmHg, and mercury vapor on the surface of the substrate. The radiation intensity of 254±10n is 20μW/
cm 2 or more, the substrate is irradiated with a discharge lamp in which the synchrotron radiation is 70% or more of the total radiation, and SiH 4 at a pressure of 0.01 to 7 mmHg and the pressure relative to the SiH 4 are placed in the airtight container. A film of silicon nitride is formed on the surface of the substrate by flowing N 2 H 4 at a ratio of 30≧Pressure (N 2 H 4 )/Pressure (SiH 4 )≧1. Because it is a coating that does not have pinholes or changes over time,
It can be formed uniformly over a wide area, and therefore the IC
Silicon nitride films can be provided that are good as surface protection films for circuit chips and other insulating films.
第1図及び第2図は、本発明被膜形成方法を実
行するための被膜形成装置の一例の説明図、第3
図は中空支持台の説明図であつて、図中、5a,
5bは回転シヤフト、8は基体、10は低圧水銀
蒸気放電灯、12はミラーを夫々示す。
1 and 2 are explanatory diagrams of an example of a film forming apparatus for carrying out the film forming method of the present invention;
The figure is an explanatory diagram of the hollow support stand, and in the figure, 5a, 5a,
5b is a rotating shaft, 8 is a base, 10 is a low-pressure mercury vapor discharge lamp, and 12 is a mirror.
Claims (1)
囲内に制御された気密容器内に基体を配置し、該
基体表面上での254±10nmの放射光強度が
20μW/cm2以上になる如く該放射光が全放射光の
70%以上の放電灯によつて該基体を照射し、該気
密容器内に、0.01〜7mmHgの圧力のSiH4と、該
SiH4に対する圧力比で 30≧圧力(N2H4)/圧力(SiH4)≧1の範囲に規定し
た N2H4とを流入せしめて、該基体表面上に、シリ
コンナイトライドの被膜を形成することを特徴と
する被膜形成方法。 2 更にArもしくはN2も流入せしめた第1項記
載の被膜形成方法。[Claims] 1. A substrate is placed in an airtight container in which the pressure of mercury vapor is controlled within the range of 1 × 10 -4 to 20 mmHg, and the intensity of radiated light at 254 ± 10 nm on the surface of the substrate is
The emitted light is 20 μW/cm 2 or more so that the total emitted light is
The substrate is irradiated with a discharge lamp of 70% or more, and SiH 4 at a pressure of 0.01 to 7 mmHg is added to the airtight container.
A silicon nitride coating is formed on the surface of the substrate by flowing N 2 H 4 at a pressure ratio of 30≧pressure (N 2 H 4 )/pressure (SiH 4 )≧1 to SiH 4 . A film forming method characterized by forming a film. 2. The film forming method according to item 1, wherein Ar or N 2 is also introduced.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17285281A JPS5875842A (en) | 1981-10-30 | 1981-10-30 | Forming method for film |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17285281A JPS5875842A (en) | 1981-10-30 | 1981-10-30 | Forming method for film |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5875842A JPS5875842A (en) | 1983-05-07 |
| JPS6354216B2 true JPS6354216B2 (en) | 1988-10-27 |
Family
ID=15949490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP17285281A Granted JPS5875842A (en) | 1981-10-30 | 1981-10-30 | Forming method for film |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5875842A (en) |
-
1981
- 1981-10-30 JP JP17285281A patent/JPS5875842A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5875842A (en) | 1983-05-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS61502900A (en) | Barrel reactor and photochemical vapor deposition method | |
| JPS59140365A (en) | Photochemical vapor deposition device | |
| JPS6354216B2 (en) | ||
| JPS60212220A (en) | Photochemical reaction apparatus | |
| JPH03139824A (en) | Depositing method for semiconductor device | |
| JPS5875828A (en) | Forming method for film | |
| JP2629773B2 (en) | Method of forming multilayer thin film | |
| JPS6156278A (en) | Film forming method | |
| JPH0563551B2 (en) | ||
| JPS59129770A (en) | Photochemical vapor deposition device | |
| JPH09260251A (en) | Method of manufacturing mask membrane for X-ray lithography | |
| JPS60212221A (en) | Photochemical reaction apparatus | |
| JP3010065B2 (en) | Optical excitation process equipment | |
| JPS61164640A (en) | Optical cvd apparatus | |
| JPS6152232B2 (en) | ||
| JPS60212222A (en) | Photochemical reaction apparatus | |
| JPH04105314A (en) | Manufacture of amorphous silicon | |
| JPH0563552B2 (en) | ||
| JPS61196526A (en) | Photochemical vapor deposition process and apparatus thereof | |
| JPH0621234Y2 (en) | Semiconductor manufacturing equipment | |
| JPS6150148B2 (en) | ||
| JPS6250553B2 (en) | ||
| JPS6126773A (en) | Deposited film formation method | |
| JPS63307279A (en) | Photochemical reaction treatment device | |
| JPH0626184B2 (en) | Method for producing hydrogenated amorphous silicon / carbon film |