JP2003277929A - Heat- and oxidation resistant material and method for manufacturing the same, and heating element using the same - Google Patents
Heat- and oxidation resistant material and method for manufacturing the same, and heating element using the sameInfo
- Publication number
- JP2003277929A JP2003277929A JP2002086957A JP2002086957A JP2003277929A JP 2003277929 A JP2003277929 A JP 2003277929A JP 2002086957 A JP2002086957 A JP 2002086957A JP 2002086957 A JP2002086957 A JP 2002086957A JP 2003277929 A JP2003277929 A JP 2003277929A
- Authority
- JP
- Japan
- Prior art keywords
- carbon
- heat
- based coating
- resistant
- oxidation
- 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.)
- Granted
Links
- 239000000463 material Substances 0.000 title claims abstract description 122
- 238000007254 oxidation reaction Methods 0.000 title claims abstract description 74
- 230000003647 oxidation Effects 0.000 title claims abstract description 72
- 238000010438 heat treatment Methods 0.000 title claims abstract description 57
- 238000000034 method Methods 0.000 title claims abstract description 27
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 21
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 145
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 145
- 229910003460 diamond Inorganic materials 0.000 claims abstract description 32
- 239000010432 diamond Substances 0.000 claims abstract description 32
- 229910052731 fluorine Inorganic materials 0.000 claims abstract description 20
- 239000013078 crystal Substances 0.000 claims abstract description 16
- 239000003779 heat-resistant material Substances 0.000 claims abstract description 16
- 229910052801 chlorine Inorganic materials 0.000 claims abstract description 15
- 229910052740 iodine Inorganic materials 0.000 claims abstract description 15
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 11
- 239000010439 graphite Substances 0.000 claims abstract description 11
- 229910003481 amorphous carbon Inorganic materials 0.000 claims abstract description 9
- 239000011248 coating agent Substances 0.000 claims description 87
- 238000000576 coating method Methods 0.000 claims description 87
- 239000000919 ceramic Substances 0.000 claims description 14
- 239000000126 substance Substances 0.000 claims description 10
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- 239000012808 vapor phase Substances 0.000 claims description 9
- 238000005660 chlorination reaction Methods 0.000 claims description 8
- 238000009792 diffusion process Methods 0.000 claims description 8
- 230000026045 iodination Effects 0.000 claims description 8
- 238000006192 iodination reaction Methods 0.000 claims description 8
- 238000003682 fluorination reaction Methods 0.000 claims description 7
- 239000011229 interlayer Substances 0.000 claims description 6
- 239000012071 phase Substances 0.000 claims description 4
- 230000003449 preventive effect Effects 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 abstract description 44
- 229910010271 silicon carbide Inorganic materials 0.000 abstract description 32
- 239000012298 atmosphere Substances 0.000 abstract description 23
- 230000001590 oxidative effect Effects 0.000 abstract description 18
- 239000007888 film coating Substances 0.000 abstract 1
- 238000009501 film coating Methods 0.000 abstract 1
- 239000000758 substrate Substances 0.000 description 24
- 239000007789 gas Substances 0.000 description 20
- 238000006243 chemical reaction Methods 0.000 description 17
- 239000004065 semiconductor Substances 0.000 description 13
- 239000000460 chlorine Substances 0.000 description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 10
- 150000001721 carbon Chemical class 0.000 description 8
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 8
- 239000010936 titanium Substances 0.000 description 8
- 229910052719 titanium Inorganic materials 0.000 description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 7
- 230000000052 comparative effect Effects 0.000 description 7
- 238000012546 transfer Methods 0.000 description 7
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 6
- 239000003575 carbonaceous material Substances 0.000 description 6
- 238000001816 cooling Methods 0.000 description 6
- 229910052750 molybdenum Inorganic materials 0.000 description 6
- 239000011733 molybdenum Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 4
- 238000001069 Raman spectroscopy Methods 0.000 description 4
- 239000011737 fluorine Substances 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000005268 plasma chemical vapour deposition Methods 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- WKBOTKDWSSQWDR-UHFFFAOYSA-N Bromine atom Chemical compound [Br] WKBOTKDWSSQWDR-UHFFFAOYSA-N 0.000 description 3
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- 229910004298 SiO 2 Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- GDTBXPJZTBHREO-UHFFFAOYSA-N bromine Substances BrBr GDTBXPJZTBHREO-UHFFFAOYSA-N 0.000 description 3
- 229910052794 bromium Inorganic materials 0.000 description 3
- 125000004432 carbon atom Chemical group C* 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 238000011156 evaluation Methods 0.000 description 3
- 229910052736 halogen Inorganic materials 0.000 description 3
- 150000002367 halogens Chemical class 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- -1 silane compound Chemical class 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 239000002344 surface layer Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- QIJNJJZPYXGIQM-UHFFFAOYSA-N 1lambda4,2lambda4-dimolybdacyclopropa-1,2,3-triene Chemical compound [Mo]=C=[Mo] QIJNJJZPYXGIQM-UHFFFAOYSA-N 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910039444 MoC Inorganic materials 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- JNDMLEXHDPKVFC-UHFFFAOYSA-N aluminum;oxygen(2-);yttrium(3+) Chemical compound [O-2].[O-2].[O-2].[Al+3].[Y+3] JNDMLEXHDPKVFC-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000010891 electric arc Methods 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052741 iridium Inorganic materials 0.000 description 2
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 239000000395 magnesium oxide Substances 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 2
- 239000002905 metal composite material Substances 0.000 description 2
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000001179 sorption measurement Methods 0.000 description 2
- 238000004544 sputter deposition Methods 0.000 description 2
- 229910003468 tantalcarbide Inorganic materials 0.000 description 2
- VZGDMQKNWNREIO-UHFFFAOYSA-N tetrachloromethane Chemical compound ClC(Cl)(Cl)Cl VZGDMQKNWNREIO-UHFFFAOYSA-N 0.000 description 2
- 238000007740 vapor deposition Methods 0.000 description 2
- 229910019901 yttrium aluminum garnet Inorganic materials 0.000 description 2
- ZCYVEMRRCGMTRW-UHFFFAOYSA-N 7553-56-2 Chemical compound [I] ZCYVEMRRCGMTRW-UHFFFAOYSA-N 0.000 description 1
- PIGFYZPCRLYGLF-UHFFFAOYSA-N Aluminum nitride Chemical compound [Al]#N PIGFYZPCRLYGLF-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 102100033041 Carbonic anhydrase 13 Human genes 0.000 description 1
- 102100033007 Carbonic anhydrase 14 Human genes 0.000 description 1
- KZBUYRJDOAKODT-UHFFFAOYSA-N Chlorine Chemical compound ClCl KZBUYRJDOAKODT-UHFFFAOYSA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- 101000867860 Homo sapiens Carbonic anhydrase 13 Proteins 0.000 description 1
- 101000867862 Homo sapiens Carbonic anhydrase 14 Proteins 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 1
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 230000005856 abnormality Effects 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 238000010306 acid treatment Methods 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000001273 butane Substances 0.000 description 1
- 150000001722 carbon compounds Chemical class 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000005539 carbonized material Substances 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 239000011363 dried mixture Substances 0.000 description 1
- 239000012777 electrically insulating material Substances 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000010574 gas phase reaction Methods 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- IXCSERBJSXMMFS-UHFFFAOYSA-N hydrogen chloride Substances Cl.Cl IXCSERBJSXMMFS-UHFFFAOYSA-N 0.000 description 1
- 229910000041 hydrogen chloride Inorganic materials 0.000 description 1
- XMBWDFGMSWQBCA-UHFFFAOYSA-N hydrogen iodide Chemical compound I XMBWDFGMSWQBCA-UHFFFAOYSA-N 0.000 description 1
- 229910000043 hydrogen iodide Inorganic materials 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000011630 iodine Substances 0.000 description 1
- 238000007733 ion plating Methods 0.000 description 1
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical compound CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 description 1
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 1
- GVGCUCJTUSOZKP-UHFFFAOYSA-N nitrogen trifluoride Chemical compound FN(F)F GVGCUCJTUSOZKP-UHFFFAOYSA-N 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 229910000077 silane Inorganic materials 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000004611 spectroscopical analysis Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- TXEYQDLBPFQVAA-UHFFFAOYSA-N tetrafluoromethane Chemical compound FC(F)(F)F TXEYQDLBPFQVAA-UHFFFAOYSA-N 0.000 description 1
- 150000003608 titanium Chemical class 0.000 description 1
- 239000013585 weight reducing agent Substances 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/322—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
-
- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
-
- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/343—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one DLC or an amorphous carbon based layer, the layer being doped or not
Landscapes
- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Vapour Deposition (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、高温酸化性雰囲気
下においても優れた耐酸化性を有し、さらには導電性を
も兼ね備えた耐熱耐酸化性材料とその製造方法及びそれ
を用いた発熱体に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a heat and oxidation resistant material having excellent oxidation resistance even in a high temperature oxidizing atmosphere and also having electrical conductivity, a method for producing the same and heat generation using the same. It is about the body.
【0002】[0002]
【従来の技術】従来、1000℃以下の温度領域で使用
される抵抗加熱炉や熱処理装置等のヒーター等において
は、モリブデン(Mo)、タングステン(W)等の耐熱
性金属、あるいは黒鉛、無定形炭素等の炭素(C)材料
が用いられている。また、例えば1000℃を超える高
温酸化性雰囲気で使用される材料としては、酸化アルミ
ニウム(Al2O3)、窒化アルミニウム(AlN)、イ
ットリウムアルミニウムガーネット(YAG)、酸化マ
グネシウム(MgO)等の耐酸化性に優れたセラミック
スがよく用いられている。これらのセラミックスは絶縁
性及び耐熱性に優れていることから、上記の各種装置の
炉体材料、試料用のボートやセッター、絶縁基板、電気
絶縁材料等として用いられている。2. Description of the Related Art Conventionally, in a heater such as a resistance heating furnace or a heat treatment apparatus which is used in a temperature range of 1000 ° C. or less, a heat resistant metal such as molybdenum (Mo) or tungsten (W), graphite, or amorphous. A carbon (C) material such as carbon is used. Further, for example, as a material used in a high-temperature oxidizing atmosphere exceeding 1000 ° C., aluminum oxide (Al 2 O 3 ), aluminum nitride (AlN), yttrium aluminum garnet (YAG), magnesium oxide (MgO), etc. Ceramics with excellent properties are often used. Since these ceramics are excellent in insulation and heat resistance, they are used as furnace body materials for the above-mentioned various devices, boats and setters for samples, insulating substrates, electrically insulating materials and the like.
【0003】[0003]
【発明が解決しようとする課題】ところで、上述したM
o、W、C等の導電性材料においては、特に高温酸化性
雰囲気における耐酸化性が必ずしも充分ではないため
に、限定された、即ち、さほど高温でない酸化性雰囲気
下においてしか使用することができないという問題点が
あった。また、上述したセラミックスにおいては、耐熱
性に優れているものの、概ね電気伝導度が低く、高温加
熱装置のヒーター等の様に導電性が求められている部品
には使用することができないという問題点があった。By the way, the above-mentioned M
Since the conductive materials such as o, W, and C are not always sufficiently resistant to oxidation particularly in a high temperature oxidizing atmosphere, they can be used only in a limited, ie, not so high temperature oxidizing atmosphere. There was a problem. In addition, although the above-mentioned ceramics have excellent heat resistance, they have a low electric conductivity and cannot be used for parts requiring conductivity such as a heater of a high temperature heating device. was there.
【0004】本発明は、上記の課題を解決するためにな
されたものであって、高温酸化性雰囲気下においても優
れた耐酸化性を有し、さらには導電性を兼ね備えた耐熱
耐酸化性材料とその製造方法及びそれを用いた発熱体を
提供することを目的とする。The present invention has been made in order to solve the above-mentioned problems, and has a heat-resistant and oxidation-resistant material which has excellent oxidation resistance even in a high temperature oxidizing atmosphere and further has electrical conductivity. And a manufacturing method thereof and a heating element using the same.
【0005】[0005]
【課題を解決するための手段】本発明者等は、上述した
従来の技術が有する問題点を解決すべく鋭意検討した結
果、耐熱性材料の表面を特殊な炭素系被膜で被覆すれ
ば、上記課題を効率的に解決することができることを究
明した。すなわち、本発明の耐熱耐酸化性材料は、耐熱
性材料からなる基材と、この基材の少なくとも一部を被
覆する被膜とを備え、前記被膜は、主成分とされる炭素
のうち一部の炭素がC−X結合(ただし、XはF、C
l、Iから選択された1種または2種以上)を有する炭
素系被膜からなることを特徴とする。Means for Solving the Problems The inventors of the present invention have made earnest studies to solve the problems of the above-mentioned conventional techniques, and as a result, if the surface of the heat resistant material is coated with a special carbon-based coating, It was clarified that the problem can be solved efficiently. That is, the heat-resistant and oxidation-resistant material of the present invention comprises a base material made of a heat-resistant material and a coating film that covers at least a part of the base material, and the coating film is a part of carbon as a main component. Carbon is a C-X bond (where X is F, C
1 or 2 or more selected from l and I).
【0006】この耐熱耐酸化性材料では、前記被膜を、
主成分とされる炭素のうち一部の炭素がC−X結合(た
だし、XはF、Cl、Iから選択された1種または2種
以上)を有する炭素系被膜としたことにより、この炭素
系被膜は化学的に非常に安定したものとなり、高温酸化
性雰囲気下においても優れた耐酸化性を有するものとな
る。In this heat and oxidation resistant material, the coating is
A part of carbon among the main component carbon has a C-X bond (where X is one or more selected from F, Cl and I), so that this carbon is The system coating becomes chemically very stable and has excellent oxidation resistance even in a high temperature oxidizing atmosphere.
【0007】また、本発明者等は、前記耐熱性材料とし
て、導電性セラミックス、耐熱性金属、炭素のうちのい
ずれかを用いれば、廉価な材料を基材とし得て、高温酸
化性雰囲気下においても優れた耐熱耐酸化性を示すこと
は勿論のこと、優れた導電性をも兼ね備えることとな
り、耐熱耐酸化性材料を廉価に提供することができるこ
とを究明した。すなわち、前記耐熱性材料は、導電性セ
ラミックス、耐熱性金属、炭素のうちのいずれか1種で
あるのが好ましい。The inventors of the present invention have found that if any one of conductive ceramics, heat-resistant metal and carbon is used as the heat resistant material, an inexpensive material can be used as a base material in a high temperature oxidizing atmosphere. In addition to exhibiting excellent heat resistance and oxidation resistance, it has also been proved that excellent heat conductivity and oxidation resistance can be provided, and that the heat resistance and oxidation resistance material can be provided at a low price. That is, the heat resistant material is preferably any one of conductive ceramics, heat resistant metal, and carbon.
【0008】前記基材と前記炭素系被膜との間には、層
間膜を形成するのが好ましい。この層間膜を形成したこ
とにより、炭素系被膜を成膜する際に、下地層である基
材表面からの影響が阻止され、成膜される炭素系被膜
は、結晶構造の乱れや欠陥等のない所望の結晶構造とな
る。An interlayer film is preferably formed between the base material and the carbon-based coating. By forming this interlayer film, when the carbon-based coating is formed, the influence from the surface of the base material that is the underlayer is prevented, and the formed carbon-based coating has a disordered crystal structure or defects. It does not have the desired crystal structure.
【0009】前記層間膜は、炭素拡散防止膜とするのが
好ましい。この炭素拡散防止膜を形成したことにより、
炭素系被膜を構成する炭素の一部が前記基材内部に拡散
し、基材と炭素系被膜との界面に介在層を形成するのを
防止する。これにより、基材と炭素系被膜との間の密着
性が向上する。The interlayer film is preferably a carbon diffusion prevention film. By forming this carbon diffusion prevention film,
A part of carbon constituting the carbon-based coating is prevented from diffusing into the base material and forming an intervening layer at the interface between the base material and the carbon-based coating. This improves the adhesion between the base material and the carbon-based coating.
【0010】また、本発明者等は、炭素系被膜を化学気
相法によりフッ素化処理、塩素化処理またはヨウ素化処
理することにより、主成分とされる炭素のうち一部の炭
素にC−X結合(ただし、XはF、Cl、Iから選択さ
れた1種または2種以上)を導入した特殊な炭素系被膜
を備えた耐熱耐酸化性材料を廉価に提供することができ
ることを究明した。Further, the present inventors have carried out a fluorination treatment, a chlorination treatment or an iodination treatment on a carbon-based coating film by a chemical vapor phase method, so that a part of carbon as a main component is carbon-carbonized. It has been clarified that a heat-resistant and oxidation-resistant material having a special carbon-based coating having an X bond (where X is one or more selected from F, Cl and I) can be provided at a low price. .
【0011】すなわち、前記被膜は、炭素系被膜に、化
学気相法によりフッ素化処理、塩素化処理またはヨウ素
化処理を施し、前記炭素系被膜の一部の炭素を、C−X
結合(ただし、XはF、Cl、Iから選択された1種ま
たは2種以上)を有する炭素としてなることが好まし
い。That is, the carbon-based coating is subjected to a fluorination treatment, a chlorination treatment or an iodination treatment by a chemical vapor phase method so that a part of the carbon of the carbon-based coating is converted into C--X.
It is preferably a carbon having a bond (where X is one or more selected from F, Cl and I).
【0012】また、本発明者等は、前記炭素系被膜が、
ダイヤモンド単結晶体、ダイヤモンド多結晶体、ダイヤ
モンド様カーボン、グラファイト、非晶質カーボンのい
ずれか1種または2種以上を含有するものであれば、そ
の表面を化学気相法により容易にフッ素化処理、塩素化
処理またはヨウ素化処理し得て、耐酸化性をより一層向
上させ得ることを究明した。すなわち、前記炭素系被膜
は、ダイヤモンド単結晶体、ダイヤモンド多結晶体、ダ
イヤモンド様カーボン、グラファイト、非晶質カーボン
から選択された1種または2種以上を含有することが好
ましい。Further, the present inventors have found that the carbon-based coating is
As long as it contains one or more of any one of diamond single crystal, diamond polycrystal, diamond-like carbon, graphite and amorphous carbon, its surface can be easily fluorinated by chemical vapor deposition. It has been clarified that oxidization resistance can be further improved by performing chlorination treatment or iodination treatment. That is, it is preferable that the carbon-based coating contains one kind or two or more kinds selected from a diamond single crystal body, a diamond polycrystal body, diamond-like carbon, graphite, and amorphous carbon.
【0013】また、本発明者等は、基材の少なくとも一
部に、主成分とされる炭素のうち一部の炭素にC−X結
合(ただし、XはF、Cl、Iから選択された1種また
は2種以上)を導入した特殊な炭素系被膜を形成する際
に、炭素系被膜を化学気相法によりフッ素化処理、塩素
化処理またはヨウ素化処理することにより、廉価、か
つ、効率的に形成し得ることを究明した。The present inventors have also found that at least a part of the base material has a C--X bond (where X is selected from F, Cl and I) to a part of the carbons as the main component. When forming a special carbon-based coating containing one or two or more), the carbon-based coating is fluorinated, chlorinated or iodinated by a chemical vapor phase method, so that it is inexpensive and efficient. It was found that they can be formed selectively.
【0014】すなわち、本発明の耐熱耐酸化性材料の製
造方法は、耐熱性材料からなる基材と、この基材の少な
くとも一部を被覆する炭素系被膜とを備えてなる耐熱耐
酸化性材料の製造方法において、前記炭素系被膜に、化
学気相法によりフッ素化処理、塩素化処理またはヨウ素
化処理を施し、前記炭素系被膜の一部の炭素を、C−X
結合(ただし、XはF、Cl、Iから選択された1種ま
たは2種以上)を有する炭素とすることを特徴とする。That is, the method for producing a heat-resistant and oxidation-resistant material according to the present invention comprises a heat-resistant and oxidation-resistant material comprising a base material made of a heat-resistant material and a carbon-based coating covering at least a part of the base material. In the method for producing, the carbon-based coating is subjected to a fluorination treatment, a chlorination treatment, or an iodination treatment by a chemical vapor phase method, and a part of carbon in the carbon-based coating is converted into C-X.
It is characterized in that it is a carbon having a bond (however, X is one or more selected from F, Cl and I).
【0015】この製造方法では、炭素系被膜に、化学気
相法によりフッ素化処理、塩素化処理またはヨウ素化処
理を施すことで、前記炭素系被膜の一部の炭素に、C−
X結合(ただし、XはF、Cl、Iから選択された1種
または2種以上)を導入することにより、基材の少なく
とも一部に、化学的に非常に安定であり、かつ、高温酸
化性雰囲気下においても優れた耐酸化性を有する炭素系
被膜が廉価、かつ、効率的に形成される。In this manufacturing method, the carbon-based coating is subjected to a fluorination treatment, a chlorination treatment or an iodination treatment by a chemical vapor phase method, so that a part of carbon in the carbon-based coating is C-
By introducing an X bond (where X is one or more selected from F, Cl, and I), it is chemically very stable and high-temperature oxidation is at least part of the substrate. A carbon-based coating having excellent oxidation resistance even under a strong atmosphere can be formed inexpensively and efficiently.
【0016】また、本発明者等は、発熱体の本体を本発
明の耐熱耐酸化性材料により構成すれば、高温酸化性雰
囲気下においても優れた耐酸化性を有するのは勿論のこ
と、優れた導電性をも兼ね備えることにより、耐熱耐酸
化性に優れた発熱体を廉価に提供することができること
を究明した。すなわち、本発明の発熱体は、少なくとも
本体が本発明の耐熱耐酸化性材料により構成されている
ことを特徴とする。Further, the inventors of the present invention have excellent oxidation resistance even in a high temperature oxidizing atmosphere if the main body of the heating element is made of the heat and oxidation resistant material of the present invention. It has been clarified that the heat generating element having excellent heat resistance and oxidation resistance can be provided at a low price by having the conductivity as well. That is, the heating element of the present invention is characterized in that at least the main body is made of the heat and oxidation resistant material of the present invention.
【0017】[0017]
【発明の実施の形態】本発明の耐熱耐酸化性材料とその
製造方法及びそれを用いた発熱体の各実施の形態につい
て説明する。なお、本実施の形態は、発明の趣旨をより
良く理解させるために具体的に説明するものであり、特
に指定のない限り、本発明を限定するものではない。BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of a heat and oxidation resistant material of the present invention, a method for producing the same, and a heating element using the same will be described. It should be noted that the present embodiment is specifically described for better understanding of the gist of the invention, and does not limit the present invention unless otherwise specified.
【0018】「第1の実施形態」以下、本実施形態の耐
熱耐酸化性材料について説明する。本実施形態に係る耐
熱耐酸化性材料は、耐熱性材料からなる基材と、この基
材の少なくとも一部を被覆する被膜とを備えており、こ
の被膜は、主成分とされる炭素のうち一部の炭素がC−
X結合(ただし、XはF、Cl、Iから選択された1種
または2種以上)を有する炭素系被膜(以下、単にC−
X結合導入炭素系被膜と略称する)により構成されてい
る。以下、基材、C−X結合導入炭素系被膜に項分けし
て、さらに説明する。[First Embodiment] The heat and oxidation resistant material of this embodiment will be described below. The heat-resistant and oxidation-resistant material according to the present embodiment includes a base material made of a heat-resistant material and a coating film that covers at least a part of the base material. Some carbon is C-
A carbon-based coating having an X bond (where X is one or more selected from F, Cl and I) (hereinafter, simply C-
It is composed of an X bond-introduced carbon-based coating). Hereinafter, the base material and the C-X bond-introduced carbon-based coating will be further described in terms of items.
【0019】「基材」この基材を構成する耐熱性材料と
しては、特に限定されるものではないが、例えば、炭化
珪素、炭化タンタル、炭化モリブデン等の導電性セラミ
ックス、金属−セラミックス複合焼結体等の導電性金属
複合セラミックス、タングステン、モリブデン、イリジ
ウム等の耐熱性金属、グラファイト(黒鉛)、無定形炭
素等の炭素材料が適宜用いられる。"Substrate" The heat-resistant material constituting this substrate is not particularly limited, but for example, conductive ceramics such as silicon carbide, tantalum carbide, molybdenum carbide, and metal-ceramic composite sintering. A conductive metal composite ceramic such as a body, a heat resistant metal such as tungsten, molybdenum, or iridium, or a carbon material such as graphite or amorphous carbon is appropriately used.
【0020】これらの耐熱性材料のうち、炭化珪素焼結
体、炭化タンタル焼結体、炭化モリブデン焼結体等の導
電性セラミックスは、耐熱性、耐酸化性、導電性の点で
優れた材料である。特に、高純度かつ緻密な炭化珪素焼
結体は、下記のいずれかの製造方法により得ることがで
きる。Among these heat resistant materials, conductive ceramics such as a silicon carbide sintered body, a tantalum carbide sintered body and a molybdenum carbide sintered body are materials excellent in heat resistance, oxidation resistance and conductivity. Is. In particular, a highly pure and dense silicon carbide sintered body can be obtained by any of the following manufacturing methods.
【0021】(製造方法1)平均粒子径が0.1〜10
μmの炭化珪素粉末(第1の炭化珪素粉末:β型が好ま
しい)と、Ar等の非酸化性雰囲気のプラズマ中に、シ
ラン化合物またはハロゲン化珪素と炭化珪素とからなる
原料ガスを導入し、反応系の圧力を1.01×105P
a(1気圧)未満から1.33×10Pa(0.1to
rr)の範囲で制御しつつ気相反応させることにより合
成された平均粒子径が0.1μm以下の炭化珪素微粉末
(第2の炭化珪素粉末:β型が好ましい)を、所定の配
合比となるように秤量・混合し、この混合物を所定の形
状に成形し、この成形体を所定の温度で焼成し、炭化珪
素焼結体とする方法。(Production method 1) The average particle size is 0.1 to 10
Introducing a raw material gas consisting of silane compound or silicon halide and silicon carbide into plasma of a silicon carbide powder of μm (first silicon carbide powder: β type is preferable) and plasma of a non-oxidizing atmosphere such as Ar, The reaction system pressure is 1.01 × 10 5 P
less than a (1 atm) to 1.33 × 10 Pa (0.1 to
rr) and a silicon carbide fine powder having an average particle diameter of 0.1 μm or less (second silicon carbide powder: β type is preferable) synthesized by performing a gas phase reaction with a predetermined compounding ratio. A method in which the mixture is weighed and mixed so that the mixture is formed into a predetermined shape, and the formed body is fired at a predetermined temperature to obtain a silicon carbide sintered body.
【0022】(製造方法2)製造方法1における炭化珪
素微粉末(第2の炭化珪素粉末)を所定の形状に成形
し、この成形体を所定の温度で焼成し、炭化珪素焼結体
とする方法。これらの製造方法については、特許第27
26694号、特許第2732408号に開示されてお
り、容易に製造可能である。(Manufacturing Method 2) The silicon carbide fine powder (second silicon carbide powder) in Manufacturing Method 1 is molded into a predetermined shape, and this molded body is fired at a predetermined temperature to obtain a silicon carbide sintered body. Method. Regarding these manufacturing methods, see Patent No. 27.
It is disclosed in Japanese Patent No. 26694 and Japanese Patent No. 2732408, and can be easily manufactured.
【0023】これらの製造方法により得られた炭化珪素
焼結体は、1Ωcm以下、例えば、1×10-2〜1×1
0-1Ωcm程度の優れた導電性と耐熱性とを兼ね備えて
いるので、本実施形態の耐熱耐酸化性材料の基材として
好適であり、この炭化珪素焼結体を、例えば、発熱体の
本体部分に適用すれば、耐熱性及び耐酸化性に優れた発
熱体となる。The silicon carbide sintered body obtained by these manufacturing methods has a resistance of 1 Ωcm or less, for example, 1 × 10 -2 to 1 × 1.
Since it has both excellent conductivity of about 0 −1 Ω · cm and heat resistance, it is suitable as a base material for the heat and oxidation resistant material of the present embodiment. When applied to the body part, it becomes a heating element having excellent heat resistance and oxidation resistance.
【0024】これらの炭化珪素焼結体からなる基材は、
所望の形状に加工した後、大気中で熱処理を施すことで
基材表面の余分な遊離炭素を燃焼させて除去し、その
後、フッ酸への浸漬処理等により基材表面に形成された
SiO2等の不純物を溶解、除去するのが好ましい。上
記の熱処理温度は400〜1500℃、特に600〜1
000℃が好ましい。その理由は、400℃未満では、
基材表面の遊離炭素が充分に除去されず、また、150
0℃を越えると、基材の表面が酸化されて表面の一部ま
たは全部が酸化物となり、炭化珪素焼結体の純度が低下
するからである。The base material made of these silicon carbide sintered bodies is
After processing into a desired shape, excess free carbon on the surface of the base material is burned and removed by applying a heat treatment in the atmosphere, and thereafter, SiO 2 formed on the surface of the base material by dipping treatment with hydrofluoric acid or the like. It is preferable to dissolve and remove impurities such as. The heat treatment temperature is 400 to 1500 ° C., especially 600 to 1
000 ° C is preferred. The reason is that below 400 ° C,
The free carbon on the surface of the substrate is not sufficiently removed, and
This is because if the temperature exceeds 0 ° C., the surface of the base material is oxidized and part or all of the surface becomes an oxide, and the purity of the silicon carbide sintered body decreases.
【0025】上記の熱処理時間は、特に限定されるもの
ではないが、通常、1〜40時間である。ここで、1〜
40時間が好ましいとされる理由は、熱処理時間が1時
間未満では、基材表面の遊離炭素の除去効率が低く、一
方、熱処理時間が40時間を超えても、基材表面の遊離
炭素の除去効率が向上する訳ではなく無意味だからであ
る。The heat treatment time is not particularly limited, but is usually 1 to 40 hours. Where 1 ~
The reason why 40 hours is preferable is that when the heat treatment time is less than 1 hour, the removal efficiency of the free carbon on the surface of the substrate is low, while even when the heat treatment time exceeds 40 hours, the removal of the free carbon on the surface of the substrate is removed. This is because it does not improve efficiency but is meaningless.
【0026】また、基材を構成する導電性金属複合セラ
ミックスとして、Pt−Al2O3、Ag−Si−Ni−
SiO2、Mo−ZrO2等の金属−セラミックス複合焼
結体も好適に用いられる。また、基材を構成する耐熱性
材料として、タングステン、モリブデン、イリジウム等
の耐熱性金属材料も好適に用いられる。これらの耐熱性
金属材料を基材に用いる場合、この基材表面に後述する
「炭素系被膜」を成膜する際に、炭素が基材内部に拡散
し、基材と炭素系被膜との界面に介在層が形成されて密
着性が低下するおそれがある。これを防ぐためには、こ
の基材の表面に予め炭素拡散防止膜を成膜しておくのが
よい。Further, as the conductive metal composite ceramics constituting the base material, Pt-Al 2 O 3 and Ag-Si-Ni-
A metal-ceramic composite sintered body such as SiO 2 or Mo-ZrO 2 is also preferably used. Further, as the heat-resistant material forming the base material, heat-resistant metal materials such as tungsten, molybdenum, and iridium are also preferably used. When these heat-resistant metal materials are used as the base material, when the "carbon-based coating film" described later is formed on the surface of the base material, carbon diffuses inside the base material, and the interface between the base material and the carbon-based coating film. There is a possibility that an intervening layer is formed on the surface and the adhesion is reduced. In order to prevent this, it is preferable to previously form a carbon diffusion preventive film on the surface of this base material.
【0027】この炭素拡散防止膜としては、例えば、チ
タン膜、上記の耐熱性金属材料の金属成分の炭化物膜等
を例示することができる。その膜厚は、通常、0.01
〜1μm程度で充分である。なお、膜厚が0.01μm
未満になると、炭素の拡散防止効果が不十分なものとな
り、一方、膜厚が1μmを越えると、基材と炭素系被膜
との密着性が低下するおそれがある。その成膜法は、特
に制限されないが、例えば、スパッタリング法、蒸着法
等が好適に用いられる。Examples of the carbon diffusion preventive film include a titanium film and a carbide film of a metal component of the above-mentioned heat-resistant metal material. The film thickness is usually 0.01
About 1 μm is sufficient. The film thickness is 0.01 μm
If it is less than the above range, the effect of preventing carbon diffusion becomes insufficient, while if the film thickness exceeds 1 μm, the adhesion between the base material and the carbon-based coating may be deteriorated. The film forming method is not particularly limited, but for example, a sputtering method, a vapor deposition method or the like is preferably used.
【0028】また、基材を構成する耐熱性材料として、
グラファイト(黒鉛)、無定形炭素等の炭素材料も好適
に用いられる。基材としての炭素材料は、導電性セラミ
ックスや耐熱性金属と比較して加工性に優れている点で
有利である。As the heat-resistant material constituting the base material,
Carbon materials such as graphite and amorphous carbon are also preferably used. The carbon material as the base material is advantageous in that it has excellent workability as compared with conductive ceramics and heat resistant metals.
【0029】ところで、基材を構成する炭素材料は、後
述する炭素系被膜を成膜する際に用いられるプラズマに
対しては、耐性が充分でなく損耗し易い。したがって、
基材の表面が炭素系被膜で充分に被覆されるまでは、基
材の表面状態、形状、寸法等が変化する虞がある。ま
た、炭素系被膜が成膜される際に、プラズマに励起され
た炭素成分は、基材表面に沈着する際に基材の結晶構造
と同一の結晶構造を取り易く、特に、ダイヤモンド単結
晶体、ダイヤモンド多結晶体等の炭素系被膜を成膜する
際に、ダイヤモンド構造が形成されない虞がある。その
ため、耐熱性金属を基材として用いる場合と同様、基材
の表面に予めチタン膜等の中間膜(層間膜)を形成して
おくのが好ましい。By the way, the carbon material constituting the base material is not sufficiently resistant to plasma used in forming a carbon-based coating film described later and is easily worn. Therefore,
Until the surface of the base material is sufficiently covered with the carbon-based coating, the surface condition, shape, dimensions, etc. of the base material may change. In addition, when the carbon-based coating is formed, the carbon component excited by the plasma easily takes the same crystal structure as the crystal structure of the base material when deposited on the base material surface. When forming a carbon-based coating such as a diamond polycrystal, there is a possibility that a diamond structure will not be formed. Therefore, it is preferable to form an intermediate film (interlayer film) such as a titanium film in advance on the surface of the base material as in the case of using a heat resistant metal as the base material.
【0030】「C−X結合導入炭素系被膜」前記基材の
少なくとも一部、例えば表面を被覆するC−X結合導入
炭素系被膜は、例えば、炭素系被膜を、フッ素ガス、塩
素ガス、ヨウ素ガス等の臭素を除くハロゲン系腐食性ガ
スや、そのプラズマガスに曝すことでフッ素化、塩素化
またはヨウ素化し、この炭素系被膜にC−X結合(ただ
し、XはF、Cl、Iから選択された1種または2種以
上)を導入したものである。"C-X bond-introduced carbon-based coating" The C-X bond-introduced carbon-based coating covering at least a part of the substrate, for example, the surface, is, for example, a carbon-based coating formed by fluorine gas, chlorine gas or iodine. When exposed to halogen-based corrosive gases other than bromine, such as gas, or its plasma gas, it is fluorinated, chlorinated, or iodinated, and this carbon-based coating has a C—X bond (where X is selected from F, Cl, and I). One or two or more of the above mentioned) have been introduced.
【0031】上記の炭素系被膜は、特に限定されるもの
ではないが、ダイヤモンド単結晶体、ダイヤモンド多結
晶体、ダイヤモンド様カーボン、グラファイト、非晶質
カーボンから選択された1種または2種以上を含有する
ことが好ましく、例えば、ダイヤモンド単結晶体、ダイ
ヤモンド多結晶体、ダイヤモンド様カーボン、グラファ
イト、非晶質カーボンのいずれか1種、あるいはダイヤ
モンド様カーボンおよび/またはカーボンを含むダイヤ
モンド多結晶体が好適に用いられる。これらの材料は、
プラズマCVD法、イオンプレーティング法等を用いて
基材表面に容易に成膜することができるので好適であ
る。とりわけ、ダイヤモンド単結晶体やダイヤモンド多
結晶体は、導電性の他、優れた耐磨耗性をも併せ持つの
で好適である。The above-mentioned carbon-based coating is not particularly limited, but may be one or more selected from a diamond single crystal body, a diamond polycrystal body, diamond-like carbon, graphite and amorphous carbon. It is preferable to contain, for example, any one of diamond single crystal, diamond polycrystal, diamond-like carbon, graphite and amorphous carbon, or diamond polycrystal containing diamond-like carbon and / or carbon is suitable. Used for. These materials are
It is preferable because a film can be easily formed on the surface of the substrate by using a plasma CVD method, an ion plating method, or the like. Above all, a diamond single crystal body and a diamond polycrystal body are preferable because they have not only conductivity but also excellent abrasion resistance.
【0032】なお、上記のダイヤモンド様カーボンおよ
び/またはカーボンを含むダイヤモンド多結晶体とは、
ダイヤモンド結晶粒子間、あるいは基材とダイヤモンド
結晶粒子との間(粒界)に、ダイヤモンド様カーボンお
よび/またはカーボンが偏析したものである。The diamond-like carbon and / or the diamond polycrystal containing carbon is as follows.
The diamond-like carbon and / or carbon is segregated between the diamond crystal grains or between the base material and the diamond crystal grains (grain boundaries).
【0033】上記の炭素系被膜の厚みも特に限定される
ものではないが、通常、1〜100μmの範囲が好まし
い。その理由は、厚みが1μm未満であると、基材の表
面が完全には被覆されず、耐酸化性が不十分となるから
であり、一方、100μmを超えると、基材の表面形状
が変化し、不具合が生じる虞、例えば、基材表面に形成
された凹凸や溝までが被膜によって埋没してしまうとい
う不具合が生じる虞があり、さらに、成膜に多大な時間
を要するために、製造コストの上昇を招き、経済的でな
いからである。The thickness of the above-mentioned carbon-based coating is not particularly limited, but is usually preferably in the range of 1 to 100 μm. The reason is that if the thickness is less than 1 μm, the surface of the base material is not completely covered and the oxidation resistance becomes insufficient, while if it exceeds 100 μm, the surface shape of the base material changes. However, there is a risk that defects may occur, for example, irregularities and grooves formed on the surface of the base material may be buried by the coating film. This is because it is not economical.
【0034】上記の基材の表面に、このような炭素系被
膜を形成する方法としては、特に限定されるものではな
いが、例えば、プラズマ気相法等の化学気相法は、緻密
な膜が形成可能であり、また、ダイヤモンド単結晶体や
ダイヤモンド多結晶体からなる炭素系皮膜を成膜し得る
ので好適に用いられる。炭素系被膜の成膜に用いられる
原料としては、例えば、メタン、エタン、プロパン、ブ
タン、一酸化炭素、二酸化炭素、アルコール類等、その
構造中に炭素原子を含み、容易に気相種とすることがで
きる炭素化合物を用いる。プラズマ励起源としては、マ
イクロ波、直流グロー放電、直流アーク放電、高周波、
熱フィラメント等、いずれも好適に用いられる。The method for forming such a carbon-based coating on the surface of the above-mentioned substrate is not particularly limited, but, for example, a chemical vapor deposition method such as a plasma vapor deposition method is used to form a dense film. Can be formed, and a carbon-based coating composed of a diamond single crystal body or a diamond polycrystal body can be formed. Examples of the raw material used for forming the carbon-based film include methane, ethane, propane, butane, carbon monoxide, carbon dioxide, alcohols, etc., which contain carbon atoms in the structure and are easily converted into vapor phase species. A carbon compound that can be used is used. As a plasma excitation source, microwave, DC glow discharge, DC arc discharge, high frequency,
A hot filament or the like is preferably used.
【0035】上記の化学気相法としては、特に、マイク
ロ波プラズマCVD法が好適に用いられる。このマイク
ロ波プラズマCVD法は、既に開示されている公知の方
法で、プラズマ反応チャンバー内に基材を配置し、マイ
クロ波をプラズマ反応チャンバー内に印加することで、
このチャンバー内に定在波を形成させ、炭素原子を含む
原料ガスを予め加熱してある前記基材表面上で分解、プ
ラズマ化させ、該基材表面上に炭素系被膜を成膜する方
法である。As the above chemical vapor deposition method, a microwave plasma CVD method is particularly preferably used. This microwave plasma CVD method is a known method that has already been disclosed, in which a substrate is placed in a plasma reaction chamber and microwaves are applied to the plasma reaction chamber,
In this method, a standing wave is formed in this chamber, and a source gas containing carbon atoms is decomposed and plasmatized on the surface of the substrate that has been heated in advance, and a carbon-based coating film is formed on the surface of the substrate. is there.
【0036】上記の炭素原子を含む原料ガスとしては、
炭素原子を含み、容易に気相種とすることができる化合
物であればよく、例えば、メタン、水素の混合ガスが好
ましく、より好ましく、はメタンと水素との混合比率が
CH4:0.1〜10.0v/v%、H2:99.9〜9
0.0v/v%である混合ガスがダイヤモンド単結晶体
やダイヤモンド多結晶体からなる炭素系被膜を成膜し得
る他、余分な炭素成分が反応チャンバー内壁に付着しな
いので好適である。As the above-mentioned source gas containing carbon atoms,
Any compound containing a carbon atom and capable of easily forming a gas phase species may be used, and for example, a mixed gas of methane and hydrogen is preferable, and a mixture ratio of methane and hydrogen is preferably CH 4 : 0.1. ˜10.0 v / v%, H 2 : 99.9-9
A mixed gas of 0.0 v / v% is preferable because it can form a carbon-based coating film composed of a diamond single crystal body or a diamond polycrystal body, and an excess carbon component does not adhere to the inner wall of the reaction chamber.
【0037】原料ガスの流量は、通常1〜500scc
m、好ましくは10〜200sccmである。その理由
は、原料ガスの流量が1sccm未満であると反応効率
が低下し、成膜時のレートが低下するからであり、一
方、500sccmを超えるとプラズマ反応チャンバー
内でガスの強制対流が生じ、プラズマを安定に保てなく
なるからである。また、反応圧力は、通常7.5×10
-4Pa〜4Pa、好ましくは7.5×10-3Pa〜1.
5Paである。反応圧力が7.5×10-4Pa未満で
は、例えば、ダイヤモンド単結晶体やダイヤモンド多結
晶体等の成膜速度が遅くなるからで、一方、4Paを超
えるとプラズマが消失してしまうからである。The flow rate of the source gas is usually 1 to 500 scc
m, preferably 10 to 200 sccm. The reason is that if the flow rate of the raw material gas is less than 1 sccm, the reaction efficiency decreases, and the rate at the time of film formation decreases. On the other hand, if it exceeds 500 sccm, forced convection of gas occurs in the plasma reaction chamber, This is because the plasma cannot be kept stable. The reaction pressure is usually 7.5 × 10.
-4 Pa to 4 Pa, preferably 7.5 x 10 -3 Pa to 1.
It is 5 Pa. When the reaction pressure is less than 7.5 × 10 −4 Pa, for example, the film forming rate of a diamond single crystal body or a diamond polycrystalline body becomes slow, while when it exceeds 4 Pa, plasma disappears. is there.
【0038】次いで、上記の炭素系被膜にC−F結合を
導入する。炭素系被膜は、その最表面の炭素原子にC−
X(ただし、XはF、Cl、Iから選択された1種また
は2種以上)結合を導入することによって、耐酸化性を
付与することができる。このようなC−X結合を導入す
る方法としては、炭素系被膜で被覆された基材を、フッ
化窒素、フッ化炭素、フッ素ガス、四塩化炭素、塩化水
素、ヨウ化水素等、臭素以外のハロゲン元素を含む気体
物質の存在の下で、定圧で励起した、臭素以外のハロゲ
ン元素を含有するプラズマに暴露する方法等を例示する
ことができる。Then, a C--F bond is introduced into the carbon-based coating. The carbon-based coating has C- on the outermost carbon atom.
Oxidation resistance can be imparted by introducing an X (where X is one or more selected from F, Cl and I) bond. As a method of introducing such a C—X bond, a base material coated with a carbon-based film is prepared by using nitrogen fluoride, carbon fluoride, fluorine gas, carbon tetrachloride, hydrogen chloride, hydrogen iodide, etc. other than bromine. The method of exposing to plasma containing a halogen element other than bromine, which is excited at a constant pressure in the presence of a gaseous substance containing a halogen element, can be exemplified.
【0039】このような炭素系被膜の表面改質は、炭素
系被膜が成膜された直後にチャンバー内のガスをフッ素
系ガスと入れ替え、再度プラズマを発生させて行っても
よく、あるいは、炭素系被膜が被覆された基材を一旦系
外へ取り出し、検査、確認した後に、別途に行っても良
い。Such surface modification of the carbon-based coating may be carried out by replacing the gas in the chamber with a fluorine-based gas immediately after the carbon-based coating is formed and generating plasma again. The base material coated with the system coating may be taken out of the system once, inspected and confirmed, and then separately performed.
【0040】この表面改質に用いられるプラズマ励起源
発生方法としては、マイクロ波、直流グロー放電、直流
アーク放電、高周波等のいずれの方法も用いることがで
きるが、これらの方法に限定されず、放電によってプラ
ズマを発生し、炭素系被膜の表面を改質することができ
る方法であれば何れの方法でも良い。また、反応圧力
は、通常7.5×10-4Pa〜4Pa、好ましくは7.
5×10-3Pa〜1.5Paである。反応圧力が7.5
×10-4Pa未満では、炭素系被膜の表面改質の効果が
低く、一方、4Paを越えるとプラズマが不安定となる
からである。また、反応温度は300〜500℃が好ま
しい。反応温度がこの範囲を外れると、表面改質の効率
が低下するからである。As a method for generating a plasma excitation source used for this surface modification, any method such as microwave, direct current glow discharge, direct current arc discharge, and high frequency can be used, but the method is not limited to these methods. Any method may be used as long as plasma can be generated by electric discharge and the surface of the carbon-based coating can be modified. The reaction pressure is usually 7.5 × 10 −4 Pa to 4 Pa, preferably 7.
It is 5 × 10 −3 Pa to 1.5 Pa. Reaction pressure is 7.5
If it is less than × 10 -4 Pa, the effect of surface modification of the carbon-based coating is low, while if it exceeds 4 Pa, plasma becomes unstable. The reaction temperature is preferably 300 to 500 ° C. This is because when the reaction temperature is out of this range, the efficiency of surface modification is reduced.
【0041】このようにして形成されたC−X結合導入
炭素系被膜は、102Ωm〜103Ωm程度の体積固有抵
抗値を有し、導電性に優れている。そのため、このC−
X結合導入炭素系被膜により導電性の基材表面を被覆し
ても、基材の導電性を大きく損なうことはない。したが
って、導電性の良好な材料を基材に用いると、得られる
被覆型の耐熱耐酸化性材料は導電性を備えた材料とな
り、この耐熱耐酸化性材料を、例えば、発熱体の本体部
分に適用すれば、高温酸化性雰囲気の下で用いられるヒ
ーター材料として好適なものとなる。The C—X bond-introduced carbon-based coating film thus formed has a volume resistivity value of about 10 2 Ωm to 10 3 Ωm and is excellent in conductivity. Therefore, this C-
Even if the surface of the conductive base material is covered with the X-bond-introduced carbon-based coating, the conductivity of the base material is not significantly impaired. Therefore, when a material having good conductivity is used for the base material, the obtained coating-type heat-resistant and oxidation-resistant material becomes a material having conductivity, and this heat-resistant and oxidation-resistant material is applied to, for example, the body portion of the heating element. When applied, it is suitable as a heater material used under a high temperature oxidizing atmosphere.
【0042】「第2の実施形態」図1は、本発明の第2
の実施形態の炭化珪素ヒーターを示す平面図、図2は図
1のA−A線に沿う断面図であり、この炭化珪素ヒータ
ー(発熱体)1は、中心から平面上外方へ六方向に突出
した略円板状のヒーターエレメント(発熱体の本体)2
と、ヒーターエレメント2の中心を挟んで対称となる一
対の突片の先端部各々に設けられたモリブデンからなる
電極3、3とにより構成されている。このヒーターエレ
メント2は、第1の実施形態の耐熱耐酸化性材料を用い
て作製されたもので、炭化珪素焼結体からなる基材の表
面がC−X結合導入炭素系被膜により被覆されている。[Second Embodiment] FIG. 1 shows a second embodiment of the present invention.
2 is a plan view showing the silicon carbide heater of the embodiment of FIG. 2, and FIG. 2 is a cross-sectional view taken along the line AA of FIG. 1. The silicon carbide heater (heating element) 1 is arranged in six directions from the center outward in the plane. Protruding substantially disk-shaped heater element (main body of heating element) 2
And electrodes 3 made of molybdenum provided on the respective tip portions of a pair of protrusions which are symmetrical with respect to the center of the heater element 2. This heater element 2 is manufactured using the heat and oxidation resistant material of the first embodiment, and the surface of the base material made of a silicon carbide sintered body is covered with a C—X bond-introduced carbon-based film. There is.
【0043】本実施形態の炭化珪素ヒーター1によれ
ば、発熱体の本体部分であるヒーターエレメント2に第
1の実施形態の耐熱耐酸化性材料を用いたので、このヒ
ーターエレメント2は化学的に非常に安定したものとな
り、高温酸化性雰囲気下においても優れた耐酸化性を有
するものとなる。したがって、耐熱耐酸化性に優れた炭
化珪素ヒーター1を提供することができる。According to the silicon carbide heater 1 of this embodiment, since the heat resistant and oxidation resistant material of the first embodiment is used for the heater element 2 which is the main body portion of the heating element, this heater element 2 is chemically It becomes very stable and has excellent oxidation resistance even in a high temperature oxidizing atmosphere. Therefore, it is possible to provide the silicon carbide heater 1 having excellent heat resistance and oxidation resistance.
【0044】「第3の実施形態」図3は、本発明の第3
の実施形態の半導体チップ実装ボード製造用のパルスヒ
ーターを示す断面図であり、このパルスヒーター11
は、発熱体12と、発熱体12からの熱を断熱するため
のベース材13と、発熱体12に通電して発熱体12を
所定の温度に昇温させるための電極14とを備えてい
る。この発熱体12は、第1の実施形態の耐熱耐酸化性
材料を用いて作製されたもので、炭化珪素焼結体からな
る基材の表面がC−X結合導入炭素系被膜により被覆さ
れている。[Third Embodiment] FIG. 3 shows the third embodiment of the present invention.
FIG. 11 is a sectional view showing a pulse heater for manufacturing a semiconductor chip mounting board of the embodiment of FIG.
Includes a heating element 12, a base material 13 for insulating heat from the heating element 12, and an electrode 14 for energizing the heating element 12 to raise the heating element 12 to a predetermined temperature. . The heating element 12 is manufactured using the heat and oxidation resistant material of the first embodiment, and the surface of the base material made of a silicon carbide sintered body is covered with a C—X bond-introduced carbon-based coating. There is.
【0045】この発熱体12及びベース材13には、半
導体チップを吸着するための吸着孔15及び伝熱板吸着
用吸着孔16が、これらを貫通するように形成されてい
る。このベース材13には、さらに、発熱体12を強制
冷却して降温させるための冷却孔17が複数形成されて
いる。これら電極14、14には、リード線18がそれ
ぞれ接続されている。Adsorption holes 15 for adsorbing the semiconductor chips and adsorption holes 16 for adsorbing the heat transfer plate are formed on the heating element 12 and the base material 13 so as to penetrate them. The base material 13 is further formed with a plurality of cooling holes 17 for forcibly cooling the heating element 12 to lower the temperature. Lead wires 18 are connected to the electrodes 14 and 14, respectively.
【0046】このパルスヒーター11を用いて半導体チ
ップの実装ボードを製造するには、図4に示すように、
まず、パルスヒーター11の発熱体12に伝熱板21を
固定したパルスヒーターを用意し、このパルスヒーター
を、基板22上に導電性ボンディング材23を介して配
置された半導体チップ24上に配置し、このパルスヒー
ターを受圧板25に押圧しつつ、基板22と導電性ボン
ディング材23と半導体チップ24とを、発熱体12に
より伝熱板21を介して加熱し、導電性ボンディング材
23を溶融する。In order to manufacture a semiconductor chip mounting board using this pulse heater 11, as shown in FIG.
First, a pulse heater in which the heat transfer plate 21 is fixed to the heating element 12 of the pulse heater 11 is prepared, and this pulse heater is arranged on the semiconductor chip 24 arranged on the substrate 22 via the conductive bonding material 23. While pressing the pulse heater against the pressure receiving plate 25, the substrate 22, the conductive bonding material 23, and the semiconductor chip 24 are heated by the heating element 12 via the heat transfer plate 21, and the conductive bonding material 23 is melted. .
【0047】次いで、冷却孔17に冷却用の空気を送り
込み、発熱体12及び伝熱板21を所定の温度、例え
ば、導電性ボンディング材23の凝固温度以下まで冷却
し、導電性ボンディング材23を固化させ、半導体チッ
プ24と基板22とを導電性ボンディング材23により
ボンディングする。Next, cooling air is sent to the cooling holes 17 to cool the heating element 12 and the heat transfer plate 21 to a predetermined temperature, for example, to the solidification temperature of the conductive bonding material 23 or less, and the conductive bonding material 23 is removed. After being solidified, the semiconductor chip 24 and the substrate 22 are bonded by the conductive bonding material 23.
【0048】本実施形態のパルスヒーターによれば、発
熱体12に、第1の実施形態の耐熱耐酸化性材料を用い
たので、この発熱体12は化学的に非常に安定したもの
となり、高温酸化性雰囲気下においても優れた耐酸化性
を有するものとなる。したがって、耐熱耐酸化性に優れ
たパルスヒーターを提供することができる。According to the pulse heater of the present embodiment, the heat-resistant and oxidation-resistant material of the first embodiment is used for the heating element 12, so that the heating element 12 becomes chemically very stable and high temperature. It has excellent oxidation resistance even in an oxidizing atmosphere. Therefore, it is possible to provide a pulse heater having excellent heat resistance and oxidation resistance.
【0049】[0049]
【実施例】以下、実施例及び比較例を挙げ、本発明をさ
らに詳しく説明する。EXAMPLES The present invention will be described in more detail with reference to Examples and Comparative Examples.
【0050】「実施例1」市販の平均粒子径が1.1μ
mのβ型炭化珪素粉末(第1の炭化珪素粉末)95重量
部に、モノシランとメタンとを原料ガスとしてプラズマ
CVD法により気相合成して得た平均粒子径0.02μ
mのβ型炭化珪素微粉末(第2の炭化珪素粉末)を5重
量部添加し、これをメタノール中にて分散せしめ、さら
にボールミルで12時間混合し、この混合物を乾燥させ
た。Example 1 Commercially available average particle size is 1.1 μm.
An average particle diameter of 0.02μ obtained by vapor-phase synthesis of 95 parts by weight of β-type silicon carbide powder of m (first silicon carbide powder) using monosilane and methane as raw material gases by a plasma CVD method.
5 parts by weight of β-type silicon carbide fine powder of m (second silicon carbide powder) was added, dispersed in methanol, and further mixed by a ball mill for 12 hours, and this mixture was dried.
【0051】次いで、この乾燥した混合物を内径210
mmの黒鉛製モールドに充填し、ホットプレス装置に
て、アルゴン雰囲気下、プレス圧400Kg/cm2、
焼結温度2200℃の条件で90分間加圧焼成し、円板
状の炭化珪素焼結体を得た。得られた炭化珪素焼結体の
密度は3.22g/cm3であり、また、ガード電極を
備えた抵抗測定装置を用いて体積固有抵抗値を測定した
ところ、この炭化珪素焼結体の体積固有抵抗値は8×1
0-2Ωcmであった。The dried mixture is then heated to an inner diameter of 210
mm graphite mold and filled with a hot press machine under an argon atmosphere at a pressing pressure of 400 Kg / cm 2 ,
Pressure sintering was performed for 90 minutes under a sintering temperature of 2200 ° C. to obtain a disc-shaped silicon carbide sintered body. The density of the obtained silicon carbide sintered body was 3.22 g / cm 3 , and the volume specific resistance value was measured using a resistance measuring device equipped with a guard electrode. Specific resistance value is 8 × 1
It was 0 -2 Ωcm.
【0052】次いで、上記の炭化珪素焼結体を大気中8
00℃で15時間、加熱処理して表面の炭素分を除去し
た後、45℃のフッ酸水溶液で5時間、フッ酸処理し、
表層のSiO2分を溶解し、炭化珪素基板とした。この
炭化珪素基板をプラズマ反応チャンバー内に載置し、基
板温度900℃、反応圧力0.6Paの条件下で、この
チャンバー内に2モル%のCH4を含むH2ガスを導入
し、5時間、マイクロ波出力600Wでプラズマを形成
しつつ、前記炭化珪素基板上に炭素系被膜を成膜した。Next, the above-mentioned silicon carbide sintered body was placed in the atmosphere 8
After heat treatment at 00 ° C. for 15 hours to remove the carbon content on the surface, hydrofluoric acid treatment at 45 ° C. for 5 hours was performed on the hydrofluoric acid,
The SiO 2 portion of the surface layer was dissolved to obtain a silicon carbide substrate. This silicon carbide substrate was placed in a plasma reaction chamber, and H 2 gas containing 2 mol% CH 4 was introduced into this chamber under the conditions of a substrate temperature of 900 ° C. and a reaction pressure of 0.6 Pa for 5 hours. While forming plasma with a microwave output of 600 W, a carbon-based coating film was formed on the silicon carbide substrate.
【0053】この炭素系被膜の厚みを走査型電子顕微鏡
(SEM)で観察したところ、その膜厚は中心部、外周
部ともに2μmと均一であった。また、上記の炭素系被
膜の組成及び構造をラマン分光分析法にて分析したとこ
ろ、1333cm-1に現れるダイヤモンドのラマンシフ
トの半価幅(半値幅)は6cm-1であり、1550cm
-1を中心とするダイヤモンド様カーボンのラマンシフト
と1333cm-1を中心とするダイヤモンドのラマンシ
フトの強度比Isp 2/sp3が0.1の良質なダイヤモンド
多結晶体からなる炭素系被膜であった。When the thickness of this carbon-based coating was observed with a scanning electron microscope (SEM), the thickness was uniform at 2 μm in both the central portion and the outer peripheral portion. Furthermore, analysis of the composition and structure of the carbon-based coating film in Raman spectroscopy, the half width of the Raman shift of diamond appearing at 1333 cm -1 (half-width) is 6 cm -1, 1550 cm
-1 is a carbon-based coating composed of a high-quality diamond polycrystal having a Raman shift of diamond-like carbon centered at -1 and a Raman shift of diamond centered at 1333 cm -1 I sp 2 / sp3 of 0.1. It was
【0054】次いで、このダイヤモンド多結晶体からな
る炭素系被膜で被覆された炭化珪素焼結体を、プラズマ
反応チャンバー内に載置し、100%NF3ガスを20
sccmの流速で流動させながら、雰囲気圧力を7.6
×10-4Paとし、この状態で高周波電力RFを500
W印加して発生させたプラズマで10分間処理(反応温
度:400℃)することにより、ダイヤモンド多結晶体
からなる炭素系被膜の表層にC−F結合を形成し、実施
例1の耐熱耐酸化性材料を得た。Next, the silicon carbide sintered body coated with the carbon-based coating composed of this diamond polycrystal is placed in the plasma reaction chamber, and 100% NF 3 gas is added thereto for 20 minutes.
Atmospheric pressure of 7.6 while flowing at a flow rate of sccm
× and 10 -4 Pa, a high frequency power RF in this state 500
By treatment with plasma generated by applying W for 10 minutes (reaction temperature: 400 ° C.), a C—F bond is formed in the surface layer of the carbon-based coating composed of diamond polycrystal, and the heat-resistant and oxidation-resistant property of Example 1 is obtained. I obtained the material.
【0055】この炭素系被膜の被膜構造をESCA(el
ectron spectroscopy for chemicalanalysis)により評
価したところ、フッ素と炭素の原子数比F/Cが0.9
であり、被膜の表層にC−F結合を形成していることが
確認された。また、上記のガード電極を備えた抵抗測定
装置を用いて体積固有抵抗値を測定したところ、この炭
素系被膜の体積固有抵抗値は4×102Ωcmであっ
た。The coating structure of this carbon-based coating is ESCA (el
ectron spectroscopy for chemical analysis), the atomic ratio F / C of fluorine and carbon was 0.9.
It was confirmed that a C—F bond was formed on the surface layer of the coating. When the volume resistivity value was measured using the resistance measuring device equipped with the guard electrode, the volume resistivity value of this carbon-based coating was 4 × 10 2 Ωcm.
【0056】「実施例2」実施例1にて用いたβ型炭化
珪素微粉末(第2の炭化珪素粉末)を、実施例1と同一
の条件で加圧焼成して、円板状の炭化珪素焼結体を得
た。得られた炭化珪素焼結体の密度を測定したところ、
3.2g/cm3であり、また、体積固有抵抗値は2×
10-2Ωcmであった。次いで、この炭化珪素焼結体の
表面に、実施例1に準じてC−F結合を有する炭素系被
膜を形成し、実施例2の耐熱耐酸化性材料を得た。[Example 2] The β-type silicon carbide fine powder (second silicon carbide powder) used in Example 1 was pressure-fired under the same conditions as in Example 1 to obtain a disc-shaped carbonized material. A silicon sintered body was obtained. When the density of the obtained silicon carbide sintered body was measured,
3.2 g / cm 3 , and the volume resistivity value is 2 ×
It was 10 -2 Ωcm. Then, a carbon-based coating having a C—F bond was formed on the surface of this silicon carbide sintered body according to Example 1 to obtain the heat-resistant and oxidation-resistant material of Example 2.
【0057】「実施例3」市販のモリブデン金属板の表
面に、スパッタリング法を用いてチタン膜(膜厚:0.
1μm)を被覆し、このチタン被膜付きモリブデン金属
板を基材とした。このチタン膜はモリブデン金属板への
炭素の拡散を抑止するための炭素拡散防止膜である。次
いで、実施例1に準じて、上記のチタン膜上にC−F結
合を有する炭素系被膜を形成し、実施例3の耐熱耐酸化
性材料を得た。Example 3 On the surface of a commercially available molybdenum metal plate, a titanium film (film thickness: 0.
1 μm), and this molybdenum metal plate coated with titanium was used as a base material. This titanium film is a carbon diffusion preventing film for suppressing the diffusion of carbon into the molybdenum metal plate. Then, according to Example 1, a carbon-based coating film having a C—F bond was formed on the titanium film to obtain a heat and oxidation resistant material of Example 3.
【0058】「実施例4」市販の炭素材料(無定形炭
素)の表面に、スパッタリング法を用いてチタン膜(膜
厚0.1μm)を被覆し、このチタン膜付き炭素材料を
基材とした他は、実施例1に準じて実施例4の耐熱耐酸
化性材料を得た。Example 4 The surface of a commercially available carbon material (amorphous carbon) was coated with a titanium film (film thickness: 0.1 μm) by the sputtering method, and this carbon material with a titanium film was used as a base material. Others were the same as in Example 1, and the heat-resistant and oxidation-resistant material of Example 4 was obtained.
【0059】「評価」実施例1〜4の耐熱耐酸化性材料
の炭素系被膜を形成した面における耐酸化性及び加熱処
理後の表面状態を評価した。また、比較例として、モリ
ブデン(比較例1)、高密度炭素(黒鉛:比較例2)、
窒化アルミニウム焼結体(比較例3)、及び実施例1に
おけるフッ化処理前のダイヤモンド被膜付き炭化珪素焼
結体(比較例4)を用い、これらの耐酸化性及び加熱処
理後の表面状態も併せて評価した。"Evaluation" The heat resistance and oxidation resistance of Examples 1 to 4 were evaluated for the oxidation resistance and the surface condition after heat treatment on the surface on which the carbon-based coating was formed. As comparative examples, molybdenum (Comparative Example 1), high-density carbon (graphite: Comparative Example 2),
Using the aluminum nitride sintered body (Comparative Example 3) and the diamond-coated silicon carbide sintered body before the fluorination treatment in Example 1 (Comparative Example 4), the oxidation resistance and the surface state after the heat treatment were also obtained. It was evaluated together.
【0060】耐酸化性及び加熱処理後の表面状態各々の
評価方法は、次のとおりである。
「耐酸化性」赤外線集光炉内に試料を配置し、圧力1.
33×10Pa、酸素(100%)雰囲気下、昇温速
度:5℃/secで600℃まで昇温させ、前記試料を
この温度に30分間保持することで加熱処理を行った。
耐酸化性(消耗速度)は、試料の重量減少量、炭素系被
膜の密度、試料の表面積から消耗膜厚を算出し、この消
耗膜厚を加熱処理時間で除して算出した。なお、表1に
おいては「消耗速度」で示した。The evaluation methods of the oxidation resistance and the surface condition after the heat treatment are as follows. "Oxidation resistance" Place the sample in an infrared concentrator and set the pressure to 1.
In a 33 × 10 Pa, oxygen (100%) atmosphere, the temperature was raised to 600 ° C. at a temperature rising rate of 5 ° C./sec, and the sample was held at this temperature for 30 minutes for heat treatment.
The oxidation resistance (wear rate) was calculated by calculating the wear film thickness from the weight reduction amount of the sample, the density of the carbon-based coating, and the surface area of the sample, and dividing this wear film thickness by the heat treatment time. It should be noted that in Table 1, it is shown by "consumption rate".
【0061】「加熱処理後の表面状態」加熱処理後の表
面状態を目視にて観察すると共に、X線回析法にて酸化
物相生成の有無を確認した。評価結果を表1に示す。"Surface condition after heat treatment" The surface condition after heat treatment was visually observed and the presence or absence of oxide phase formation was confirmed by X-ray diffraction. The evaluation results are shown in Table 1.
【0062】[0062]
【表1】 [Table 1]
【0063】表1によれば、実施例1〜4では、炭素系
被膜の消耗が全く認められず、また、加熱処理後の表面
状態についても何ら変化が認められず、高温酸化性雰囲
気下においても優れた耐酸化性を有することが分かっ
た。一方、比較例1〜4では、炭素系被膜の消耗が認め
られ、また、加熱処理後の表面状態についても、酸化物
相の生成、酸化物膜の剥離、CO2ガス発生等が認めら
れ、膜質が劣化していることが明らかとなった。したが
って、高温酸化性雰囲気下における耐酸化性が極めて悪
いことが分かった。According to Table 1, in Examples 1 to 4, no consumption of the carbon-based coating film was observed, and no change was observed in the surface condition after the heat treatment. Was also found to have excellent oxidation resistance. On the other hand, in Comparative Examples 1 to 4, consumption of the carbon-based coating film was observed, and regarding the surface state after the heat treatment, generation of an oxide phase, peeling of the oxide film, generation of CO 2 gas, etc. were observed. It became clear that the film quality was deteriorated. Therefore, it was found that the oxidation resistance in a high temperature oxidizing atmosphere was extremely poor.
【0064】「実施例5」図1及び図2に示すようなヒ
ータエレメント2を実施例1の耐熱耐酸化性材料を用い
て作製し、更に、モリブデンからなる電極3を取り付
け、炭化珪素ヒーター1とした。この炭化珪素ヒーター
1を酸化加熱炉に取り付け、印加電圧を一定にして5A
の電流を流したところ、炭化珪素ヒーター1の表面は約
10℃/分の速度で昇温し、80分後には設定温度であ
る800℃となった。次いで、この加熱を10時間続け
たところ、炭化珪素ヒーター1の消耗は全く認められ
ず、さらに、この加熱試験を10回繰り返した後におい
ても異常は全く認められなかった。[Embodiment 5] A heater element 2 as shown in FIGS. 1 and 2 is manufactured using the heat and oxidation resistant material of Embodiment 1, and further an electrode 3 made of molybdenum is attached to the silicon carbide heater 1. And This silicon carbide heater 1 was attached to an oxidation heating furnace and the applied voltage was kept constant at 5 A.
When the current was applied, the temperature of the surface of the silicon carbide heater 1 was raised at a rate of about 10 ° C./min, and after 80 minutes, it reached the set temperature of 800 ° C. Next, when this heating was continued for 10 hours, the silicon carbide heater 1 was not consumed at all, and no abnormality was recognized even after repeating this heating test 10 times.
【0065】「実施例6」図3に示すような発熱体12
を実施例1の耐熱耐酸化性材料を用いて作製し、この発
熱体12を用いてパルスヒーター11を作製した。次い
で、図4に示すように、この発熱体12の上面(図4で
は下面)に伝熱板21を設け、半導体チップ24と導電
性ボンディング材23と基板22とを、伝熱板21を介
して発熱体12により大気雰囲気中で加熱加圧し、半導
体チップ24と基板22とを導電性ボンディング材23
によりボンディングした。[Embodiment 6] A heating element 12 as shown in FIG.
Was produced using the heat and oxidation resistant material of Example 1, and the pulse heater 11 was produced using this heating element 12. Next, as shown in FIG. 4, the heat transfer plate 21 is provided on the upper surface (lower surface in FIG. 4) of the heating element 12, and the semiconductor chip 24, the conductive bonding material 23, and the substrate 22 are interposed via the heat transfer plate 21. The semiconductor chip 24 and the substrate 22 are electrically conductively bonded to each other by heating and pressurizing the semiconductor chip 24 and the substrate 22 in the atmosphere by the heating element 12.
Bonded by.
【0066】加熱パターンは、室温から450℃まで2
秒間で昇温し、450℃に10秒間保持して導電性ボン
ディング材23を加熱・溶融した後、冷却孔17から冷
却空気を吹き付けで室温まで降温させることとした。降
温に伴い、溶融した導電性ボンディング材23が固化
し、ボンディングが完了した。このような半導体実装ボ
ードの製造を連続して10,000回繰り返したとこ
ろ、発熱体12の消耗は全く認められなかった。The heating pattern is from room temperature to 450 ° C.
The temperature was raised in 2 seconds and the temperature was kept at 450 ° C. for 10 seconds to heat and melt the conductive bonding material 23, and then cooling air was blown from the cooling holes 17 to lower the temperature to room temperature. As the temperature dropped, the molten conductive bonding material 23 solidified and the bonding was completed. When the production of such a semiconductor mounting board was repeated 10,000 times in succession, the heating element 12 was not consumed at all.
【0067】[0067]
【発明の効果】以上説明したように、本発明の耐熱耐酸
化性材料によれば、耐熱性材料からなる基材の少なくと
も一部を被覆する被膜を、主成分とされる炭素のうち一
部の炭素がC−X結合(ただし、XはF、Cl、Iから
選択された1種)を有する炭素系被膜としたので、耐熱
性は勿論のこと、高温酸化性雰囲気下においても優れた
耐酸化性を奏することができる。As described above, according to the heat-resistant and oxidation-resistant material of the present invention, a coating for covering at least a part of a base material made of a heat-resistant material is used as a main component of a part of carbon. Since the carbon is a carbon-based coating having a C—X bond (where X is one selected from F, Cl, and I), it has excellent acid resistance not only in heat resistance but also in a high temperature oxidizing atmosphere. It is possible to achieve chemical conversion.
【0068】また、前記耐熱性材料として、導電性セラ
ミックス、耐熱性金属、炭素のうちのいずれかを用いれ
ば、高温酸化性雰囲気下においても優れた耐熱耐酸化性
を示すことは勿論のこと、優れた導電性をも兼ね備える
ことができ、耐熱耐酸化性材料を廉価に提供することが
できる。Further, if any one of conductive ceramics, heat-resistant metal and carbon is used as the heat-resistant material, it goes without saying that excellent heat-oxidation resistance is exhibited even in a high temperature oxidizing atmosphere. It can also have excellent conductivity and can provide a heat resistant and oxidation resistant material at a low price.
【0069】本発明の耐熱耐酸化性材料の製造方法によ
れば、炭素系被膜に、化学気相法によりフッ素化処理、
塩素化処理またはヨウ素化処理を施し、前記炭素系被膜
の一部の炭素を、C−X結合(ただし、XはF、Cl、
Iから選択された1種または2種以上)を有する炭素と
するので、耐熱性、及び高温酸化性雰囲気下においても
優れた耐酸化性を有する炭素系被膜を廉価、かつ、効率
的に形成することができる。According to the method for producing a heat-resistant and oxidation-resistant material of the present invention, a carbon-based coating is fluorinated by a chemical vapor phase method,
Chlorination treatment or iodination treatment is performed, and a part of carbon of the carbon-based coating is converted into C—X bond (where X is F, Cl,
Since carbon having one or more selected from I) is used, a carbon-based coating film having heat resistance and excellent oxidation resistance even in a high temperature oxidizing atmosphere can be formed inexpensively and efficiently. be able to.
【0070】本発明の発熱体によれば、少なくとも本体
部分を本発明の耐熱耐酸化性材料により構成したので、
高温酸化性雰囲気下における耐熱耐酸化性は勿論のこ
と、優れた導電性をも兼ね備えた発熱体を廉価に提供す
ることができる。According to the heating element of the present invention, at least the main body is made of the heat and oxidation resistant material of the present invention.
It is possible to provide at low cost a heating element which has excellent conductivity as well as heat and oxidation resistance in a high temperature oxidizing atmosphere.
【図1】 本発明の第2の実施形態の炭化珪素ヒーター
を示す平面図である。FIG. 1 is a plan view showing a silicon carbide heater according to a second embodiment of the present invention.
【図2】 図1のA−A線に沿う断面図である。FIG. 2 is a cross-sectional view taken along the line AA of FIG.
【図3】 本発明の第3の実施形態の半導体チップ実装
ボード製造用のパルスヒーターを示す断面図である。FIG. 3 is a sectional view showing a pulse heater for manufacturing a semiconductor chip mounting board according to a third embodiment of the present invention.
【図4】 本発明の第3の実施形態のパルスヒーターを
用いて半導体チップの実装ボードを製造する様を示す側
面図である。FIG. 4 is a side view showing how a mounting board for a semiconductor chip is manufactured using a pulse heater according to a third embodiment of the present invention.
1 炭化珪素ヒーター(発熱体) 2 ヒーターエレメント(発熱体の本体) 3 電極 11 パルスヒーター 12 発熱体 13 ベース材 14 電極 18 リード線 21 伝熱板 22 基板 23 導電性ボンディング材 24 半導体チップ 25 受圧板 1 Silicon carbide heater (heating element) 2 Heater element (main body of heating element) 3 electrodes 11 pulse heater 12 heating element 13 Base material 14 electrodes 18 lead wire 21 heat transfer plate 22 Substrate 23 Conductive bonding material 24 semiconductor chips 25 Pressure plate
───────────────────────────────────────────────────── フロントページの続き (72)発明者 小西 幹郎 東京都千代田区六番町6番地28 住友大阪 セメント株式会社内 Fターム(参考) 4K030 AA09 AA17 BA24 BA27 BA28 CA02 CA05 DA02 FA01 HA04 LA11 4K044 AA01 AA13 AB10 BA18 BA20 BB03 BC11 CA13 CA14 ─────────────────────────────────────────────────── ─── Continued front page (72) Inventor Mikio Konishi 28 Sumitomo Osaka, 6-6 Rokubancho, Chiyoda-ku, Tokyo Inside Cement Co., Ltd. F-term (reference) 4K030 AA09 AA17 BA24 BA27 BA28 CA02 CA05 DA02 FA01 HA04 LA11 4K044 AA01 AA13 AB10 BA18 BA20 BB03 BC11 CA13 CA14
Claims (8)
少なくとも一部を被覆する被膜とを備え、 前記被膜は、主成分とされる炭素のうち一部の炭素がC
−X結合(ただし、XはF、Cl、Iから選択された1
種または2種以上)を有する炭素系被膜からなることを
特徴とする耐熱耐酸化性材料。1. A base material made of a heat-resistant material, and a coating film covering at least a part of the base material, wherein the coating film contains a part of carbon as a main component of carbon.
-X bond (where X is 1 selected from F, Cl and I)
A heat-resistant and oxidation-resistant material, characterized in that it comprises a carbon-based coating having one or more kinds.
ス、耐熱性金属、炭素のうちのいずれか1種であること
を特徴とする請求項1記載の耐熱耐酸化性材料。2. The heat and oxidation resistant material according to claim 1, wherein the heat resistant material is any one of conductive ceramics, heat resistant metal, and carbon.
間膜を形成してなることを特徴とする請求項1または2
記載の耐熱耐酸化性材料。3. The interlayer film is formed between the base material and the carbon-based coating film.
The heat resistant and oxidation resistant material described.
とを特徴とする請求項3記載の耐熱耐酸化性材料。4. The heat and oxidation resistant material according to claim 3, wherein the interlayer film is a carbon diffusion preventive film.
によりフッ素化処理、塩素化処理またはヨウ素化処理を
施し、前記炭素系被膜の一部の炭素を、C−X結合(た
だし、XはF、Cl、Iから選択された1種または2種
以上)を有する炭素としてなることを特徴とする請求項
1ないし4のいずれか1項記載の耐熱耐酸化性材料。5. The carbon-based coating is subjected to a fluorination treatment, a chlorination treatment or an iodination treatment by a chemical vapor phase method so that a part of the carbon of the carbon-based coating is converted to C—X bond (however, , X is a carbon having one or more selected from F, Cl and I). The heat and oxidation resistant material according to any one of claims 1 to 4, wherein
体、ダイヤモンド多結晶体、ダイヤモンド様カーボン、
グラファイト、非晶質カーボンから選択された1種また
は2種以上を含有することを特徴とする請求項5記載の
耐熱耐酸化性材料。6. The carbon-based coating comprises a diamond single crystal body, a diamond polycrystal body, diamond-like carbon,
The heat and oxidation resistant material according to claim 5, which contains one or more selected from graphite and amorphous carbon.
少なくとも一部を被覆する炭素系被膜とを備えてなる耐
熱耐酸化性材料の製造方法において、 前記炭素系被膜に、化学気相法によりフッ素化処理、塩
素化処理またはヨウ素化処理を施し、前記炭素系被膜の
一部の炭素を、C−X結合(ただし、XはF、Cl、I
から選択された1種または2種以上)を有する炭素とす
ることを特徴とする耐熱耐酸化性材料の製造方法。7. A method for producing a heat-resistant and oxidation-resistant material, comprising: a base material made of a heat-resistant material; and a carbon-based coating film covering at least a part of the base material. Fluorination treatment, chlorination treatment, or iodination treatment is performed by the phase method, and a part of carbon of the carbon-based coating is converted into C—X bond (where X is F, Cl, I).
1. A method for producing a heat-resistant and oxidation-resistant material, comprising: carbon having one or more selected from
ずれか1項記載の耐熱耐酸化性材料により構成されてい
ることを特徴とする発熱体。8. A heating element, characterized in that at least a main body is made of the heat-resistant and oxidation-resistant material according to any one of claims 1 to 6.
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| JP2002086957A JP4056774B2 (en) | 2002-03-26 | 2002-03-26 | Heating element and manufacturing method thereof |
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| JP2002086957A JP4056774B2 (en) | 2002-03-26 | 2002-03-26 | Heating element and manufacturing method thereof |
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| JP2003277929A true JP2003277929A (en) | 2003-10-02 |
| JP4056774B2 JP4056774B2 (en) | 2008-03-05 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005257137A (en) * | 2004-03-10 | 2005-09-22 | Osaka Gas Co Ltd | Member for stove trivet and stove trivet |
| JP2008019464A (en) * | 2006-07-11 | 2008-01-31 | Sumitomo Electric Ind Ltd | Diamond coating and method for producing the same |
| EP1691938A4 (en) * | 2003-11-14 | 2010-04-14 | Lam Res Corp | Silicon carbide components of semiconductor substrate processing apparatuses treated to remove free-carbon |
| US7759618B2 (en) | 2003-07-16 | 2010-07-20 | Sandvik Materials Technology Uk Limited | Silicon carbide heating elements |
| US10129931B2 (en) | 2008-06-06 | 2018-11-13 | Sandvik Materials Technology Uk Limited | Electrical resistance heating element |
-
2002
- 2002-03-26 JP JP2002086957A patent/JP4056774B2/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7759618B2 (en) | 2003-07-16 | 2010-07-20 | Sandvik Materials Technology Uk Limited | Silicon carbide heating elements |
| EP1691938A4 (en) * | 2003-11-14 | 2010-04-14 | Lam Res Corp | Silicon carbide components of semiconductor substrate processing apparatuses treated to remove free-carbon |
| JP2005257137A (en) * | 2004-03-10 | 2005-09-22 | Osaka Gas Co Ltd | Member for stove trivet and stove trivet |
| JP2008019464A (en) * | 2006-07-11 | 2008-01-31 | Sumitomo Electric Ind Ltd | Diamond coating and method for producing the same |
| US10129931B2 (en) | 2008-06-06 | 2018-11-13 | Sandvik Materials Technology Uk Limited | Electrical resistance heating element |
Also Published As
| Publication number | Publication date |
|---|---|
| JP4056774B2 (en) | 2008-03-05 |
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