JPS63186865A - Crucible for vapor deposition - Google Patents
Crucible for vapor depositionInfo
- Publication number
- JPS63186865A JPS63186865A JP1935587A JP1935587A JPS63186865A JP S63186865 A JPS63186865 A JP S63186865A JP 1935587 A JP1935587 A JP 1935587A JP 1935587 A JP1935587 A JP 1935587A JP S63186865 A JPS63186865 A JP S63186865A
- Authority
- JP
- Japan
- Prior art keywords
- crucible
- polycarbosilane
- molten
- vapor deposition
- graphite
- 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
Links
- 238000007740 vapor deposition Methods 0.000 title claims abstract description 18
- 229920003257 polycarbosilane Polymers 0.000 claims abstract description 13
- 239000011148 porous material Substances 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims abstract description 7
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052753 mercury Inorganic materials 0.000 claims abstract description 6
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 10
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 10
- 239000007770 graphite material Substances 0.000 claims description 4
- 229920001558 organosilicon polymer Polymers 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 abstract description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 8
- 229910002804 graphite Inorganic materials 0.000 abstract description 8
- 239000010439 graphite Substances 0.000 abstract description 8
- 229910052751 metal Inorganic materials 0.000 abstract description 7
- 239000002184 metal Substances 0.000 abstract description 7
- 238000000576 coating method Methods 0.000 abstract description 6
- 230000008021 deposition Effects 0.000 abstract description 6
- VLKZOEOYAKHREP-UHFFFAOYSA-N n-Hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 abstract description 6
- 239000011248 coating agent Substances 0.000 abstract description 5
- 150000002739 metals Chemical class 0.000 abstract description 3
- 238000001035 drying Methods 0.000 abstract description 2
- 230000007774 longterm Effects 0.000 abstract description 2
- 229910052709 silver Inorganic materials 0.000 abstract description 2
- 239000002904 solvent Substances 0.000 abstract description 2
- 238000010438 heat treatment Methods 0.000 abstract 1
- 230000035515 penetration Effects 0.000 abstract 1
- 238000007665 sagging Methods 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 13
- 238000006243 chemical reaction Methods 0.000 description 5
- 238000000151 deposition Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000005470 impregnation Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- 230000008020 evaporation Effects 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 238000002459 porosimetry Methods 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- 238000001771 vacuum deposition Methods 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/243—Crucibles for source material
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用性)
本発明は、アルミニウム或いは銀などの熔融金属を高温
、高真空下で蒸発させ、フィルムもしくはシート状物な
どの材料表面にこれらの金属を沈着させる、いわゆる金
属蒸着の際に用いられるルツボ(以下蒸着ルツボという
)の発明に関するものである。[Detailed Description of the Invention] (Industrial Applicability) The present invention evaporates molten metal such as aluminum or silver at high temperature and under high vacuum, and deposits these metals on the surface of a material such as a film or sheet. This invention relates to a crucible used in so-called metal vapor deposition (hereinafter referred to as a vapor deposition crucible).
(従来の技術とその問題)
このような目的を果し得る蒸着用ルツボとしては、例え
ばアルミニウム蒸着の場合、1200 ’C〜1500
℃の高温で−Elッ10−’〜10−’m m Hgの
高真空下での使用に耐える材料てなければならないのて
、通常は種々の処理、例えば酸化アルミニウムの含浸等
をした黒鉛質の材料が用いられていた。この黒鉛質の蒸
着ルツボを繰り返し使用していくとその内部、特に底側
部か侵蝕され、遂には穴がおいてその使用が不可源とな
ることかあった。(Prior art and its problems) For example, in the case of aluminum vapor deposition, a vapor deposition crucible that can achieve such a purpose is 1200'C to 1500'C.
Since the material must be able to withstand use under high vacuum conditions of -10-' to 10-' mm Hg at high temperatures of -10-' to 10-' mm Hg, it is usually graphite that has undergone various treatments, such as impregnation with aluminum oxide. materials were used. When this graphite vapor deposition crucible is used repeatedly, its interior, especially the bottom side, becomes corroded, and eventually holes are formed, making it impossible to use.
それゆえ、多くの場合は熔融アルミニウムか、その使用
中にh端部へ這い上り或いは上端面に沈積し、これらが
蒸着ルツボの外側面部へ垂れ下り、ここで熔融アルミニ
ウムと黒鉛との化学反応が起って、この部分が侵蝕され
、側面部の肉厚が減少もしくは割れを生じて、遂にはそ
の使用が不可能となる。Therefore, in many cases, molten aluminum creeps up to the h-end or deposits on the upper end surface during its use, and this drips down to the outer surface of the deposition crucible, where a chemical reaction between the molten aluminum and graphite occurs. As a result, this portion becomes eroded, the wall thickness of the side wall decreases, or cracks occur, eventually making it impossible to use.
したかって、アルミニウムの蒸着ルツボ側面部への垂れ
下がりは、前述のように蒸着ルツボや。Therefore, the hanging of aluminum on the side of the deposition crucible is caused by the deposition crucible as described above.
カーボンファイバー等からなる断熱材の寿命(使用回数
)を短くし、そのコスト高をきたすのみならず、蒸着用
ルツボに割れを生じた場合には、高温の熔融アルミニウ
ムが流出して高価な真空蒸着装置を汚したり、さらにこ
れが著しい場合には、かかる装置を損傷することもあり
、安全1−でも好ましくない。Not only does this shorten the lifespan (number of uses) of heat insulating materials such as carbon fibers and increase their cost, but if the crucible for deposition cracks, high-temperature molten aluminum flows out, resulting in expensive vacuum deposition. Safety 1- is not preferable because the equipment may be contaminated or, if this is significant, the equipment may be damaged.
このような蒸着ルツボの破損に伴って製品としての、フ
ィルムやシートも蒸着が完全に行われないために、その
商品価値を失い多大の損失をきたすことになる。If the vapor deposition crucible is damaged, the film or sheet as a product will not be completely vapor-deposited, and will lose its commercial value, resulting in a large amount of loss.
(問題点を解決するための手段及び作用)本発明者らは
、上記の問題点を解決すべく永年研究の結果、従来のも
のに比較し耐久性にすぐれた蒸着用ルツボを工夫するに
至り本発明を完成するに至った。(Means and effects for solving the problems) As a result of long-term research in order to solve the above problems, the present inventors have devised a crucible for vapor deposition that is more durable than conventional crucibles. The present invention has now been completed.
すなわち、本発明は、水銀圧入法により測定さめる割合
が25%以してあり、かつその気孔率を15%以下に調
整した黒鉛材からなる蒸着ルツボの一部又は全部に溶媒
に溶かしたポリカルボシラ Hn
は含浸し、200〜350℃で空気中乾燥した後、不活
性雰囲気中800℃〜1500℃で加熱することにより
、基材表面あるいは、空隙部に被覆されたポリカルボシ
ランか熱分解により炭化珪素被膜を形成(以下、SiC
化という)して熔融金属の這いヒリ、又は、ルツボの侵
蝕を防+hしてその使用回数を向上させようとするもの
である。That is, the present invention provides polycarbosila Hn dissolved in a solvent in part or all of a vapor deposition crucible made of graphite material whose porosity is adjusted to 15% or less and whose proportion is 25% or more as determined by mercury porosimetry. is impregnated, dried in the air at 200 to 350°C, and then heated at 800 to 1500°C in an inert atmosphere to form silicon carbide by thermal decomposition of the polycarbosilane coated on the surface of the substrate or in the voids. Forming a film (hereinafter referred to as SiC
The aim is to increase the number of times the metal can be used by preventing creeping of molten metal or corrosion of the crucible.
本発明者らによれば、蒸着用ルツボの表層あるいは、空
隙部又は基材自体をSiC化してなる構造にすると、熔
融アルミニウムとのなじみが極めて少ないために、これ
を乗り越えて外側部へ進行することができず、もとのル
ツボ内へ戻されて外側面に垂れ下がることは、はとんど
無くなることか判明している。一方、従来のSiC化の
方法には、(1)コンバージョン法と(2) S i
C−CVDコーティング法とかある。その生成条件はき
わめて困難を伴うものてあり、多大の経験と設備を必要
とし°Cいた。According to the present inventors, if the surface layer of the crucible for vapor deposition, the voids, or the base material itself is made of SiC, the compatibility with molten aluminum is extremely low, so that molten aluminum will overcome this and proceed to the outside. It has been found that the cases where the crucible cannot be removed and is returned to its original crucible and hangs down on the outer surface are almost completely eliminated. On the other hand, conventional SiC conversion methods include (1) conversion method and (2) SiC conversion method.
There is also a C-CVD coating method. The conditions for its production were extremely difficult and required a great deal of experience and equipment.
これに対し、本発明におけるポリカルボシランは、20
0〜350℃の空気乾燥、800〜15 Hn
CH4+)(2のごとく容易にSiC化に転化すること
かでき、しかも溶液濃度を10〜20%とすることによ
り効果的に良く処理かできる。On the other hand, the polycarbosilane in the present invention has 20
Air drying at 0 to 350°C, 800 to 15 Hn CH4+) (2) can be easily converted to SiC, and can be effectively treated by setting the solution concentration to 10 to 20%.
濃度か10%以下の時は生成するSiC化のせか少ない
ため効率は悪く、また溶液濃度か20%を越えると粘度
か高くなり、塗布又は、含浸が不均一になるという問題
が発生する。溶液濃度が10〜20%の場合には、ルツ
ボ表層部への塗布あるいは、ボア部への含浸は、スムー
スに行われ、1〜数回の処理で充分耐久性にすぐれた蒸
着用ルツボとなり、濃度管理は非常に重要なポイントで
あることを見い出した。When the concentration is less than 10%, the efficiency is poor because only a small amount of SiC is produced, and when the concentration of the solution exceeds 20%, the viscosity becomes high, causing the problem of uneven coating or impregnation. When the solution concentration is 10 to 20%, the coating on the surface layer of the crucible or impregnation into the bore part is performed smoothly, and a crucible for vapor deposition with excellent durability can be obtained with one to several treatments. We found that concentration control is a very important point.
また、蒸着用ルツボの黒鉛材を水銀圧入法によ気孔の占
める割合を25%以上、かつその気孔率を15%以下に
調整することにより、効率よくポリカルボシラン溶液の
塗布及び含浸を行うことができ、耐久性の飛曜的効果か
現れるものである。In addition, by adjusting the proportion of pores in the graphite material of the crucible for vapor deposition to 25% or more and 15% or less using the mercury intrusion method, the polycarbosilane solution can be applied and impregnated efficiently. This results in a dramatic effect on durability.
合が25%以下、あるいは、気孔率が15%以上となる
と、ポリカルボシラン溶液のくり返し処理が必要である
と共にSiC化の後も空隙が残る状態となり、耐久性の
大きな向トは望めないものである。If the porosity is less than 25% or the porosity is more than 15%, repeated treatments of the polycarbosilane solution are required, and voids remain even after conversion to SiC, making it impossible to expect great durability. It is.
(実施例) 以下本発明の実施例について説明する。(Example) Examples of the present invention will be described below.
実施例1
水銀圧入法による気孔径の内、50Å〜6000Aの気
孔の占める割合か65%であり、気孔率か7%の蒸着用
ルツボに、ポリカルボシランをn−ヘキサンに溶かした
15%溶液を含浸し、空気中250°Cで乾燥した後1
200°Cに加熱処理し、アルミニウム蒸着の実用試験
に供したところ、平均使用回数60回で外側面の模倣は
軽微であったか、内面下部の模倣か進み肉厚か薄くなっ
たため使用を中止した。Example 1 A 15% solution of polycarbosilane dissolved in n-hexane was placed in a deposition crucible with a porosity of 7% and a porosity of 50 Å to 6000 A accounting for 65% of the pore diameter determined by mercury porosimetry. After impregnating and drying at 250°C in air 1
When it was heat-treated to 200°C and subjected to a practical test for aluminum vapor deposition, after an average of 60 uses, the imitation of the outer surface was slight, or the imitation of the lower part of the inner surface progressed and the wall became thick or thin, so use was discontinued.
実施例岐
水銀圧入法による気孔径の内、50Å〜6000Aの気
孔の占める割合が50%であり、気孔率が11%のaR
用シルツボ、ポリカルボシランなn−ヘキサンに溶かし
た18%溶液を含浸し、さらに這い上り防+)効果を増
すため、同溶液を上端部に塗布した後、空気中250℃
で乾燥し1200′Cに加熱しC、アルミニウム蒸着の
実用試験に供したところ平均使用回数は、58回で外側
面の模倣はほとんど無かったが、内面下部の模倣か進ん
だため中IIニジた。Example: Of the pore diameters obtained by mercury intrusion method, the proportion of pores of 50 Å to 6000 A accounts for 50%, and the porosity is 11%.
Impregnated with a 18% solution of polycarbosilane dissolved in n-hexane, and to further increase the anti-climb effect, after applying the same solution to the upper end, the pot was heated at 250°C in air.
It was dried at 1,200'C and subjected to a practical test for aluminum vapor deposition.The average number of times it was used was 58, and there was almost no imitation of the outer surface, but the imitation of the lower part of the inner surface was advanced, so it was graded as medium II. .
(比較例)
気孔率が18%、50Å〜6000Aの気孔の占める割
合が20%の蒸着用ル:ンボに酸化アルミニウムを含浸
処理して得られたルツボを、アルミニウム蒸着の実用試
験に供したところ、モ均使用回数が25回でその外側面
が、アルミニウムに模倣され使用不可能となった。(Comparative example) A crucible obtained by impregnating a crucible with aluminum oxide was subjected to a practical test for aluminum evaporation. After using it 25 times, its outer surface imitated aluminum and became unusable.
(発明の効果)
以トのごとく本発明は、気孔径及び気孔率を調整した黒
鉛材からなる蒸着用ルツボに、ポリカルボシラン溶液を
塗布あるいは含浸して容易にSiC化に転化することに
より、アルミ蒸着用ルツボの耐久性の向上に、絶大な効
果を現し、極めて有用なものである。(Effects of the Invention) As described above, the present invention can easily convert into SiC by coating or impregnating a polycarbosilane solution on a vapor deposition crucible made of graphite material with adjusted pore size and porosity. It is highly effective and extremely useful in improving the durability of crucibles for aluminum evaporation.
以 上that's all
Claims (1)
00Åの気孔の占める割合が25%以上であり、かつそ
の気孔率が15%以下である黒鉛材からなる蒸着用ルツ
ボの一部又は全部に有機ケイ素重合体であるポリカルボ
シランを塗布又は含浸し、前記ポリカルボシランより炭
化珪素の被膜を形成したことを特徴とする蒸着用ルツボ
。Of the pore diameter measured by mercury intrusion method, 50 Å to 60
Polycarbosilane, which is an organosilicon polymer, is coated or impregnated on part or all of a vapor deposition crucible made of graphite material in which the proportion of 00 Å pores is 25% or more and the porosity is 15% or less. . A vapor deposition crucible, characterized in that a silicon carbide film is formed from the polycarbosilane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1935587A JPS63186865A (en) | 1987-01-28 | 1987-01-28 | Crucible for vapor deposition |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1935587A JPS63186865A (en) | 1987-01-28 | 1987-01-28 | Crucible for vapor deposition |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63186865A true JPS63186865A (en) | 1988-08-02 |
Family
ID=11997070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1935587A Pending JPS63186865A (en) | 1987-01-28 | 1987-01-28 | Crucible for vapor deposition |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63186865A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000046418A1 (en) * | 1999-02-05 | 2000-08-10 | Applied Films Gmbh & Co. Kg | Device for coating substrates with a vaporized material under low pressure or in a vacuum using a vaporized material source |
WO2007015550A1 (en) * | 2005-08-03 | 2007-02-08 | Ibiden Co., Ltd. | Jig for silicon carbide firing and method for producing porous silicon carbide body |
-
1987
- 1987-01-28 JP JP1935587A patent/JPS63186865A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000046418A1 (en) * | 1999-02-05 | 2000-08-10 | Applied Films Gmbh & Co. Kg | Device for coating substrates with a vaporized material under low pressure or in a vacuum using a vaporized material source |
WO2007015550A1 (en) * | 2005-08-03 | 2007-02-08 | Ibiden Co., Ltd. | Jig for silicon carbide firing and method for producing porous silicon carbide body |
JPWO2007015550A1 (en) * | 2005-08-03 | 2009-02-19 | イビデン株式会社 | Silicon carbide firing jig and method for producing porous silicon carbide body |
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