JPS63198316A - Tray for processing silicon wafer - Google Patents
Tray for processing silicon waferInfo
- Publication number
- JPS63198316A JPS63198316A JP31115987A JP31115987A JPS63198316A JP S63198316 A JPS63198316 A JP S63198316A JP 31115987 A JP31115987 A JP 31115987A JP 31115987 A JP31115987 A JP 31115987A JP S63198316 A JPS63198316 A JP S63198316A
- Authority
- JP
- Japan
- Prior art keywords
- maximum
- tray
- alloy
- silicon
- 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
Links
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title claims description 21
- 229910052710 silicon Inorganic materials 0.000 title claims description 18
- 239000010703 silicon Substances 0.000 title claims description 18
- 239000000956 alloy Substances 0.000 claims description 28
- 229910045601 alloy Inorganic materials 0.000 claims description 27
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 16
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 claims description 14
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 12
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- 239000010936 titanium Substances 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 239000000853 adhesive Substances 0.000 claims description 5
- 230000001070 adhesive effect Effects 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 5
- 239000011651 chromium Substances 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 claims description 5
- 229910052758 niobium Inorganic materials 0.000 claims description 5
- 239000010955 niobium Substances 0.000 claims description 5
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 5
- 229910052715 tantalum Inorganic materials 0.000 claims description 5
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 5
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- 229910052796 boron Inorganic materials 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 229910052717 sulfur Inorganic materials 0.000 claims description 4
- 239000011593 sulfur Substances 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 239000011572 manganese Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 2
- 238000003483 aging Methods 0.000 claims 2
- 238000004519 manufacturing process Methods 0.000 claims 1
- 230000005855 radiation Effects 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 230000002285 radioactive effect Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052785 arsenic Inorganic materials 0.000 description 1
- RQNWIZPPADIBDY-UHFFFAOYSA-N arsenic atom Chemical compound [As] RQNWIZPPADIBDY-UHFFFAOYSA-N 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002090 carbon oxide Inorganic materials 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- YAFQFNOUYXZVPZ-UHFFFAOYSA-N liproxstatin-1 Chemical compound ClC1=CC=CC(CNC=2C3(CCNCC3)NC3=CC=CC=C3N=2)=C1 YAFQFNOUYXZVPZ-UHFFFAOYSA-N 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- -1 persalts Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229910052711 selenium Inorganic materials 0.000 description 1
- 239000011669 selenium Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 235000012431 wafers Nutrition 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/67—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
- H01L21/67005—Apparatus not specifically provided for elsewhere
- H01L21/67011—Apparatus for manufacture or treatment
- H01L21/67098—Apparatus for thermal treatment
- H01L21/67115—Apparatus for thermal treatment mainly by radiation
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
発明の背景
半導体部品、例えば、シリコンチップの熱加工において
は、加工の1段階は、チップに特定の厚さおよび特性の
被覆物を!″i4えるためにチップを輻射電気炉中で約
593℃において加熱することを包含する。シリコンチ
ップのすべての加工は、厳しい仕様に厳格に制御される
。この特定の熱加工工程においては、各チップが一様に
加熱されること、および有害物質がチップを汚染しない
こと、が必要である。従来、これらの基準を満たすため
には、次のような合金から作られるトレー上に、熱加工
すべきチップを支持することが慣習であった。その合金
は、米国連邦政府仕様QQW390を満たし、重量%で
クロム約14〜17%、鉄約6〜10%、マンガン1%
まで、ケイ素0.5%まで、銅0,5%まで、硫黄0.
015%までを含有し、残部は本質上ニッケルからなる
もので、インコ・アロイズ・インターナショナルによっ
てインコネル(lNC0NEL :登録商標)合金60
0として販売されているものである。これらのトレーは
、暗色の固着性酸化皮膜を形成するために予め酸化され
る。この暗色の固着性酸化皮膜はチップ汚染を排除しな
がら輻射炉中でのチップの均一な加熱を可能にする。暗
色の固着性酸化皮膜並びに基板である合金は、このトレ
ーがシリコンウェーハを処理するのに使用された後、ト
レーを洗う際に使用される希フッ化水素酸(水性HF)
の作用に対しても抵抗性を有する。DETAILED DESCRIPTION OF THE INVENTION BACKGROUND OF THE INVENTION In the thermal processing of semiconductor components, such as silicon chips, one step in the processing is to provide the chip with a coating of specific thickness and characteristics. All processing of silicon chips is tightly controlled to exacting specifications. It is necessary that the chips are heated uniformly and that harmful substances do not contaminate them. Traditionally, to meet these standards, thermal processing is performed on trays made from alloys such as: The alloy meets US Federal Specification QQW390 and contains approximately 14-17% chromium, approximately 6-10% iron, and 1% manganese by weight.
Up to 0.5% silicon, up to 0.5% copper, up to 0.5% sulfur.
Inconel (lNC0NEL®) Alloy 60 is manufactured by Inco Alloys International and contains up to 15% nickel, with the remainder consisting essentially of nickel.
It is sold as 0. These trays are pre-oxidized to form a dark sticky oxide film. This dark adhesive oxide coating allows uniform heating of the chip in a radiant furnace while eliminating chip contamination. The dark adhesive oxide film and the substrate alloy are exposed to dilute hydrofluoric acid (aqueous HF) used to clean the trays after they are used to process silicon wafers.
It is also resistant to the action of
しかしながら、米国連邦政府仕様QQW390を満たす
この合金は、チップトレーに成形する時には、比較的少
ない熱加工サイクルにさらされた後に歪むであろうこと
が見出された。このような歪みは、トレーとその上に置
かれたチップとの間にギャップを生じさせやすく、この
ギャップは不均一なチップ加熱を生じさせる。このよう
なことが起こった時には、トレーは、捨てなければなら
ない。However, it has been found that this alloy, which meets US Federal Specification QQW390, will warp after being exposed to relatively few thermal processing cycles when formed into chip trays. Such distortion tends to create a gap between the tray and the chips placed thereon, which creates non-uniform chip heating. When this happens, the tray must be thrown away.
発明の概要
本発明は、重量%でニッケル最小約70%、炭素約0.
2%まで、鉄約0. 1〜約20%、ケイ素約0.05
〜約0.8%、クロム約10〜約23%、アルミニウム
約0.2〜約1.5%、チタン約1.5〜約3%、ニオ
ブとタンタルとの合51約0.1〜約3%、ジルコニウ
ム0.2%iまでおよびホウ素約0,03%までを含有
し、アルミニウムとチタンとケイ素の総和は約2〜約4
.5%である合金を含むシリコンチップ加熱用トレーで
あって、トレーの合金表面はフッ化水素酸に不溶性の詩
輻射能酸化皮膜を何することを特徴とする、シリコンチ
ップ加熱用トレーを提供するという目的を何しかつ意図
する。SUMMARY OF THE INVENTION The present invention contains a minimum of about 70% nickel and about 0.0% carbon by weight.
Up to 2%, iron approx. 0. 1 to about 20%, silicon about 0.05
- about 0.8%, about 10 to about 23% chromium, about 0.2 to about 1.5% aluminum, about 1.5 to about 3% titanium, about 0.1 to about 51 to about 51% of niobium and tantalum 3%, up to 0.2% zirconium and up to about 0.03% boron, with a total of about 2 to about 4% aluminum, titanium and silicon.
.. To provide a silicon chip heating tray containing an alloy of 5%, characterized in that the alloy surface of the tray is coated with a radioactive oxide film insoluble in hydrofluoric acid. It is intended for some purpose.
発明の好ましい態様
本発明のシリコンチップ処理用トレーを櫂供する際に、
トレーを表■に記載の組成の範囲内の合金から作ること
が有利である。Preferred Embodiments of the Invention When using the silicon chip processing tray of the present invention,
It is advantageous to make the tray from an alloy within the composition range given in Table 1.
7、・′
、/
/′
7・′
表 1
炭素 最大0.[18&大0.08マ
ンガン 最大1.0 最大1.0鉄
5〜9 5〜9硫黄
最大0.01 最大0601ケイ素
最大0.5 最大0.5銅
最大0.5 最大0.5クロム
14〜17 14〜17アルミニウム
0.4〜1.0 0.9〜1.5チタン
2.25〜2.75 2.0〜2.6二オ
ブおよびタンタル 0.7〜1.2 0.7〜1.2ニ
ッケル: 残部70 残部70表■
に記載のような合金範囲内および前記の広い合金範囲内
においては、マンガン、銅、コバルトにッケル中に含ま
れる)は、付随的元素である。硫黄、リン、ヒ素、セレ
ン、スズ、アンチモン、ビスマスなどは、不純物と考え
られ、最小実用量に維持されるべきである。少量のジル
コニウム(例えば、約0. 1%まで)は、単独でまた
は少量のホウ素(例えば、0.03%)と共に、延性の
増大を含めて各種の目的で合金に配合できる。7,・' , / /'7・' Table 1 Carbon Maximum 0. [18 & large 0.08 manganese maximum 1.0 maximum 1.0 iron
5-9 5-9 sulfur
Maximum 0.01 Maximum 0601 Silicon Maximum 0.5 Maximum 0.5 Copper
Maximum 0.5 Maximum 0.5 chrome
14-17 14-17 Aluminum 0.4-1.0 0.9-1.5 Titanium
2.25-2.75 2.0-2.6 Niobium and tantalum 0.7-1.2 0.7-1.2 Nickel: Balance 70 Balance 70 Table■
Within alloy ranges such as those described in , and within the broader alloy range described above, manganese, copper, cobalt (included in nickel) are incidental elements. Sulfur, phosphorus, arsenic, selenium, tin, antimony, bismuth, etc. are considered impurities and should be kept at minimum practical amounts. Small amounts of zirconium (eg, up to about 0.1%), alone or with small amounts of boron (eg, 0.03%), can be incorporated into the alloy for various purposes, including increasing ductility.
本発明のシリコンチップ処理用トレーの一例を図面に示
し、この図面に基づいて説明する。第1図の平面図は、
約L 3mm厚の金属から作られる長さ少なくとも約
460mm、幅少なくとも約200m+*の長方形のト
レーの表面11を示す。複数のタブ13は、トレー表面
11の両端から延出して、輻射加熱電気炉中のトレー移
動装置に係合させる手段を与える。縦方向の縁15は、
折り返して第2図に示すような下側に延出するリップ1
7を形成している。第2図は、2個のディンプル19を
通過する断面■−■における断面図である。第3図は拡
大図であり、図示のように、表面11は、金属231+
、:重畳されかつ固着している酸化皮膜21を具備する
。トレー表面11は、ディンプル19およびエンボス加
工剛化リブ20は別として、平らであり、かつ反復され
る熱サイクルを通して平らのままであることが重要であ
る。An example of the silicon chip processing tray of the present invention is shown in the drawing, and will be explained based on this drawing. The plan view in Figure 1 is
Figure 1 shows the surface 11 of a rectangular tray having a length of at least about 460 mm and a width of at least about 200 m+* made of metal about L 3 mm thick. A plurality of tabs 13 extend from opposite ends of the tray surface 11 to provide a means for engaging a tray moving device in a radiant heating electric furnace. The vertical edge 15 is
Lip 1 that is folded back and extends downward as shown in FIG.
7 is formed. FIG. 2 is a cross-sectional view taken along a cross section (■-■) passing through two dimples 19. FIG. 3 is an enlarged view, and as shown, the surface 11 is made of metal 231+
, : has an oxide film 21 that is superimposed and fixed. It is important that the tray surface 11, apart from the dimples 19 and embossed stiffening ribs 20, is flat and remains flat through repeated thermal cycling.
更に、酸化皮膜21は、金属23に永久的に固着してお
り、かつ熱の良好な吸収器および放熱器であり、かつフ
ッ化水素酸の作用に抵抗性であるような性状および厚さ
を有することが重要である。Furthermore, the oxide film 21 is permanently adhered to the metal 23 and has such properties and thickness that it is a good absorber and radiator of heat and is resistant to the action of hydrofluoric acid. It is important to have
本発明のシリコンチップトレーを作る際には、表I中の
合金のいずれか1つまたは前記の広い合金範囲内のいか
なる合金も、約1.27m1厚のシートまたはストリッ
プ形態で製造できる。次いで、金属を機械的に成形し、
例えば、所定の大きさに剪断し、トレー形状に打ち抜く
。次いで、打ち抜かれたトレーをタンプリングおよび脱
脂によって清浄にし、ビード衝撃して表面を組織化し、
最後にブラッシングする。検査後、このようにして製造
されたトレーを予め酸化して酸化皮膜21を形成する。In making the silicon chip trays of the present invention, any one of the alloys in Table I, or any alloy within the broad alloy range described above, can be manufactured in sheet or strip form approximately 1.27 ml thick. The metal is then mechanically formed,
For example, it is sheared to a predetermined size and punched into a tray shape. The punched trays are then cleaned by tamping and degreasing, bead bombarded to texture the surface, and
Brush last. After the inspection, the tray thus manufactured is oxidized in advance to form an oxide film 21.
この予備酸化に良好な条件を表■に示す。Conditions suitable for this preliminary oxidation are shown in Table (2).
表■
範 囲 有利な条件
温度(’C) 1093〜+204 115
0吸熱ガスは、メタンなどの炭化水素燃料の空気中ての
不完全燃焼生成物であり、乾燥前に容量06で窒素約4
0〜53%、水素的18〜37?6、−酸化炭素約12
〜20%、水蒸気的3゛〜12%、二酸化炭素約3%未
満および少量の未反応空気および燃料を含何する。この
吸熱ガスを、本発明の酸化シリコンチップトレーを形成
するために、金属を酸化する際に使用するためには、乾
燥して露点を10〜30℃にする。Table ■ Range Favorable conditions temperature ('C) 1093~+204 115
0 endothermic gas is the product of incomplete combustion of a hydrocarbon fuel, such as methane, in air and contains about 4
0-53%, hydrogen 18-37?6, - carbon oxide approx. 12
~20% water vapor, 3% to 12% water vapor, less than about 3% carbon dioxide and small amounts of unreacted air and fuel. This endothermic gas is dried to a dew point of 10-30° C. for use in oxidizing metal to form the silicon oxide chip tray of the present invention.
好ましくは、酸化後、酸化トレーを常温(室温)に冷却
し、平滑化操作に付す。酸化トレーが平らである時には
、次いで、約り77℃〜約732℃の温度で約1〜約8
時間実施される、空気中での時効−硬化処理に付す。有
利的には、時効は約704℃で約3時間実施する。当業
者は、他の時間と温度の組み合わせが、表Hに記載のよ
うな有利な合金および前記の広い合金範囲内の他の時効
−硬化性合金を、時効−硬化するのに使用できることを
認識するであろう。Preferably, after oxidation, the oxidation tray is cooled to normal temperature (room temperature) and subjected to a smoothing operation. When the oxidation tray is flat, it is then heated at a temperature of about 77°C to about 732°C.
It is subjected to an aging-hardening treatment in air, which is carried out for hours. Advantageously, aging is carried out at about 704°C for about 3 hours. Those skilled in the art will recognize that other time and temperature combinations can be used to age-harden advantageous alloys such as those listed in Table H and other age-hardenable alloys within the broad alloy range described above. will.
熱酸化温度に関しては、一般に、約1080℃未満の温
度で製造される酸化皮膜は薄くかつ適当な輻射能特性を
与えないので、約1080℃未満の温度は避けるべきで
ある。約1200℃よりも高い温度においては、製造さ
れる酸化物は、フッ化水素酸への抵抗性が少なくなり、
酸化皮膜がトレー表面から剥離する危険があるような厚
さにすぐなってしまう。Regarding thermal oxidation temperatures, temperatures below about 1080°C should generally be avoided since oxide films produced at temperatures below about 1080°C are thin and do not provide adequate radiative properties. At temperatures above about 1200°C, the oxides produced become less resistant to hydrofluoric acid;
The oxide film quickly becomes so thick that there is a risk of it peeling off from the tray surface.
以上の例は熱酸化の場合であるが、過酸塩、クロム酸な
どの試薬を使用して化学的に酸化し、かつ/または化学
的に/熱的に酸化することも可能である。Although the above examples are for thermal oxidation, it is also possible to oxidize chemically using reagents such as persalts, chromic acid, and/or oxidize chemically/thermally.
表1の範囲A内の合金から作られかつここに開示のよう
に処理されたトレー模擬構造物を詳細に言及したが、こ
れらの構造物は、室温と593℃との間で循環する時に
インコネル(lNC0NEI、)600合金から作られ
た構造物よりも熱的そりに、はるかに抵抗性であること
が見出された。これらの構造物上に形成された酸化皮膜
は、固着性であり、適当な輻射能特性を有し、かつフッ
化水素酸に抵抗性である。Reference has been made in detail to tray-simulating structures made from alloys within range A of Table 1 and processed as disclosed herein, which when cycled between room temperature and 593° C. It was found to be much more resistant to thermal warping than structures made from (lNC0NEI,)600 alloy. The oxide films formed on these structures are adhesive, have suitable radioactivity properties, and are resistant to hydrofluoric acid.
法令の条項に従って、本発明の特定の態様をここに例示
しかつ説明したが、当業者は、特許請求の範囲に包含さ
れる形態で変形を施すことができること、および本発明
の成る特徴が他の特徴の対応の使用なしに有利に時々使
用できることを理解するであろう。While certain aspects of the invention have been illustrated and described herein in accordance with the provisions of the statute, those skilled in the art will recognize that modifications may be made within the scope of the claims and that other features of the invention may be realized. It will be appreciated that the features of can sometimes be used advantageously without the corresponding use.
第1図および第2図は、それぞれトレーの一部分の平面
図および断面図、第3図は高輻射能酸化皮膜を有するト
レー表面の拡大図を示す。
11・・・トレー表面、21・・・酸化皮膜、23・・
・金属。1 and 2 are a plan view and a sectional view of a portion of the tray, respectively, and FIG. 3 is an enlarged view of the tray surface having a highly radioactive oxide film. 11... Tray surface, 21... Oxide film, 23...
·metal.
Claims (1)
で、鉄約0.1〜約20%、ケイ素約0.05〜約0.
8%、クロム約10〜約23%、アルミニウム約0.2
〜約1.5%、チタン約1.5〜約3%、ニオブとタン
タルとの合計約0.1〜約3%、ジルコニウム0.2%
までおよびホウ素約0.03%までを含有し、アルミニ
ウムとチタンとケイ素の総和は約2〜約4.5%である
時効硬化合金から作られるシリコンチップ処理用トレー
であって、前記トレーはその表面上に水性フッ化水素酸
の作用に抵抗性である薄い固着性高輻射能酸化皮膜を有
することを特徴とする、シリコンチップ処理用トレー。 2、下記に明記のような合金Aまたは合金Bの範囲(重
量%)を有する合金から作られる、特許請求の範囲第1
項に記載の、シリコンチップ処理用トレー。 元素:合金A:合金B 炭素:最大0.08:最大0.08 マンガン:最大1.0:最大1.0 鉄:5〜9:5〜9 硫黄:最大0.01:最大0.01 ケイ素:最大0.5:最大0.5 銅:最大0.5:最大0.5 クロム:14〜17:14〜17 アルミニウム:0.4〜1.0:0.9〜1.5チタン
:2.25〜2.75:2.0〜2.6ニオブおよびタ
ンタル:0.7〜1.2:0.7〜1.2ニッケル:残
部70:残部70 3、重量%でニッケル最小約70%、炭素約0.2%ま
で、鉄約0.1〜約20%、ケイ素約0.05〜約0.
8%、クロム約10〜約23%、アルミニウム約0.2
〜約1.5%、チタン約1.5〜約3%、ニオブとタン
タルとの合計約0.1〜約3%、ジルコニウム0.2%
までおよびホウ素約0.03%までを含有し、アルミニ
ウムとチタンとケイ素の総和は約2〜約4.5%である
時効硬化合金を、トレー構造物に機械的に成形し、前記
トレー構造物を湿った吸熱ガス中で約1093〜120
4℃の範囲内の温度で約0.25〜2時間加熱し、その
後、前記トレーの合金を時効硬化することを特徴とする
水性フッ化水素酸の作用に抵抗性である薄い固着性高輻
射能酸化被膜を有する、シリコンチップ処理用トレーの
製造法。Claims: 1. By weight, nickel minimum about 70%, carbon up to about 0.2%, iron about 0.1 to about 20%, silicon about 0.05 to about 0.
8%, chromium about 10 to about 23%, aluminum about 0.2
- about 1.5%, titanium about 1.5 to about 3%, total of niobium and tantalum about 0.1 to about 3%, zirconium 0.2%
A silicon chip processing tray made from an age-hardened alloy containing up to about 0.03% boron and about 2 to about 4.5% aluminum, titanium, and silicon, the tray comprising: 1. A tray for processing silicon chips, characterized in that it has on its surface a thin adhesive highly radiant oxide film that is resistant to the action of aqueous hydrofluoric acid. 2. Made from an alloy having a range (% by weight) of Alloy A or Alloy B as specified below:
Tray for silicon chip processing as described in section. Element: Alloy A: Alloy B Carbon: Maximum 0.08: Maximum 0.08 Manganese: Maximum 1.0: Maximum 1.0 Iron: 5-9: 5-9 Sulfur: Maximum 0.01: Maximum 0.01 Silicon : Maximum 0.5: Maximum 0.5 Copper: Maximum 0.5: Maximum 0.5 Chromium: 14-17: 14-17 Aluminum: 0.4-1.0: 0.9-1.5 Titanium: 2 .25-2.75: 2.0-2.6 Niobium and tantalum: 0.7-1.2: 0.7-1.2 Nickel: Balance 70: Balance 70 3. Nickel minimum approximately 70% in weight% , up to about 0.2% carbon, about 0.1% to about 20% iron, and about 0.05% to about 0.0% silicon.
8%, chromium about 10 to about 23%, aluminum about 0.2
- about 1.5%, titanium about 1.5 to about 3%, total of niobium and tantalum about 0.1 to about 3%, zirconium 0.2%
mechanically forming an age-hardening alloy containing up to about 0.03% boron and about 2 to about 4.5% aluminum, titanium, and silicon into a tray structure; about 1093 to 120 in a moist endothermic gas
Thin adhesive high radiation resistant to the action of aqueous hydrofluoric acid characterized by heating for about 0.25 to 2 hours at a temperature in the range of 4° C. and then age hardening the alloy of said tray. A method for manufacturing a silicon chip processing tray having a functional oxide film.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US152887A | 1987-01-08 | 1987-01-08 | |
US1528 | 2007-12-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63198316A true JPS63198316A (en) | 1988-08-17 |
Family
ID=21696503
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP31115987A Pending JPS63198316A (en) | 1987-01-08 | 1987-12-10 | Tray for processing silicon wafer |
Country Status (2)
Country | Link |
---|---|
JP (1) | JPS63198316A (en) |
GB (1) | GB2199592B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE60123016T2 (en) * | 2000-01-24 | 2007-05-03 | Inco Alloys International, Inc., Huntington | ALLOY FOR THERMAL TREATMENT AT HIGH TEMPERATURES |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4879120A (en) * | 1972-01-27 | 1973-10-24 | ||
JPS5039620A (en) * | 1973-08-13 | 1975-04-11 | ||
JPS5130529A (en) * | 1974-07-08 | 1976-03-15 | Johnson Matthey Co Ltd | |
JPS5162126A (en) * | 1974-11-29 | 1976-05-29 | Mitsubishi Metal Corp | TAINETSUSEINITSUKERUKIGOKIN |
JPS5681661A (en) * | 1979-12-06 | 1981-07-03 | Daido Steel Co Ltd | Heat resistant cast alloy |
JPS57149441A (en) * | 1981-03-12 | 1982-09-16 | Res Inst Electric Magnetic Alloys | Elinver type alloy for high temperature and preparation thereof |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2570193A (en) * | 1946-04-09 | 1951-10-09 | Int Nickel Co | High-temperature alloys and articles |
US2548092A (en) * | 1949-10-06 | 1951-04-10 | Thompson Prod Inc | Cooled hollow article |
CA1202202A (en) * | 1981-05-21 | 1986-03-25 | Stephen Floreen | Articles and parts resistant to stress corrosion cracking in reactor environments |
JPS58174538A (en) * | 1982-04-02 | 1983-10-13 | Hitachi Ltd | Ni-based alloy member and manufacture thereof |
-
1987
- 1987-12-10 JP JP31115987A patent/JPS63198316A/en active Pending
-
1988
- 1988-01-06 GB GB8800230A patent/GB2199592B/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4879120A (en) * | 1972-01-27 | 1973-10-24 | ||
JPS5039620A (en) * | 1973-08-13 | 1975-04-11 | ||
JPS5130529A (en) * | 1974-07-08 | 1976-03-15 | Johnson Matthey Co Ltd | |
JPS5162126A (en) * | 1974-11-29 | 1976-05-29 | Mitsubishi Metal Corp | TAINETSUSEINITSUKERUKIGOKIN |
JPS5681661A (en) * | 1979-12-06 | 1981-07-03 | Daido Steel Co Ltd | Heat resistant cast alloy |
JPS57149441A (en) * | 1981-03-12 | 1982-09-16 | Res Inst Electric Magnetic Alloys | Elinver type alloy for high temperature and preparation thereof |
Also Published As
Publication number | Publication date |
---|---|
GB8800230D0 (en) | 1988-02-10 |
GB2199592A (en) | 1988-07-13 |
GB2199592B (en) | 1990-09-26 |
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