JPH0531469B2 - - Google Patents
Info
- Publication number
- JPH0531469B2 JPH0531469B2 JP25771586A JP25771586A JPH0531469B2 JP H0531469 B2 JPH0531469 B2 JP H0531469B2 JP 25771586 A JP25771586 A JP 25771586A JP 25771586 A JP25771586 A JP 25771586A JP H0531469 B2 JPH0531469 B2 JP H0531469B2
- Authority
- JP
- Japan
- Prior art keywords
- adhesive
- graphite
- carbon
- adherend
- group
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 62
- 239000000853 adhesive Substances 0.000 claims description 59
- 230000001070 adhesive effect Effects 0.000 claims description 59
- 229910002804 graphite Inorganic materials 0.000 claims description 35
- 239000010439 graphite Substances 0.000 claims description 35
- 229910052799 carbon Inorganic materials 0.000 claims description 27
- 239000012790 adhesive layer Substances 0.000 claims description 26
- 239000000203 mixture Substances 0.000 claims description 24
- -1 polycyclic aromatic compound Chemical class 0.000 claims description 19
- 229920005989 resin Polymers 0.000 claims description 19
- 239000011347 resin Substances 0.000 claims description 19
- 239000003431 cross linking reagent Substances 0.000 claims description 14
- 229920001187 thermosetting polymer Polymers 0.000 claims description 14
- 125000003118 aryl group Chemical group 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 13
- 238000004519 manufacturing process Methods 0.000 claims description 12
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 11
- 239000003377 acid catalyst Substances 0.000 claims description 11
- 229910052717 sulfur Inorganic materials 0.000 claims description 11
- 239000011593 sulfur Substances 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 10
- 230000001590 oxidative effect Effects 0.000 claims description 10
- 239000002243 precursor Substances 0.000 claims description 10
- 238000006243 chemical reaction Methods 0.000 claims description 9
- 125000000524 functional group Chemical group 0.000 claims description 9
- 238000010438 heat treatment Methods 0.000 claims description 9
- 239000012298 atmosphere Substances 0.000 claims description 8
- 229910052736 halogen Inorganic materials 0.000 claims description 8
- 150000002367 halogens Chemical class 0.000 claims description 8
- 239000003245 coal Substances 0.000 claims description 7
- 239000000295 fuel oil Substances 0.000 claims description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 5
- 125000004970 halomethyl group Chemical group 0.000 claims description 5
- 125000004029 hydroxymethyl group Chemical group [H]OC([H])([H])* 0.000 claims description 5
- 229910052760 oxygen Inorganic materials 0.000 claims description 5
- 239000001301 oxygen Substances 0.000 claims description 5
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 4
- VSCWAEJMTAWNJL-UHFFFAOYSA-K aluminium trichloride Chemical compound Cl[Al](Cl)Cl VSCWAEJMTAWNJL-UHFFFAOYSA-K 0.000 claims description 4
- MWPLVEDNUUSJAV-UHFFFAOYSA-N anthracene Chemical class C1=CC=CC2=CC3=CC=CC=C3C=C21 MWPLVEDNUUSJAV-UHFFFAOYSA-N 0.000 claims description 4
- 239000007795 chemical reaction product Substances 0.000 claims description 4
- WDECIBYCCFPHNR-UHFFFAOYSA-N chrysene Chemical class C1=CC=CC2=CC=C3C4=CC=CC=C4C=CC3=C21 WDECIBYCCFPHNR-UHFFFAOYSA-N 0.000 claims description 4
- VPUGDVKSAQVFFS-UHFFFAOYSA-N coronene Chemical class C1=C(C2=C34)C=CC3=CC=C(C=C3)C4=C4C3=CC=C(C=C3)C4=C2C3=C1 VPUGDVKSAQVFFS-UHFFFAOYSA-N 0.000 claims description 4
- YNPNZTXNASCQKK-UHFFFAOYSA-N phenanthrene Chemical class C1=CC=C2C3=CC=CC=C3C=CC2=C1 YNPNZTXNASCQKK-UHFFFAOYSA-N 0.000 claims description 4
- BBEAQIROQSPTKN-UHFFFAOYSA-N pyrene Chemical class C1=CC=C2C=CC3=CC=CC4=CC=C1C2=C43 BBEAQIROQSPTKN-UHFFFAOYSA-N 0.000 claims description 4
- 239000004593 Epoxy Chemical group 0.000 claims description 3
- 125000004018 acid anhydride group Chemical group 0.000 claims description 3
- 125000003172 aldehyde group Chemical group 0.000 claims description 3
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 claims description 3
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 claims description 3
- 125000001033 ether group Chemical group 0.000 claims description 3
- 229910052739 hydrogen Inorganic materials 0.000 claims description 3
- 239000001257 hydrogen Substances 0.000 claims description 3
- 150000002431 hydrogen Chemical group 0.000 claims description 3
- 125000002887 hydroxy group Chemical group [H]O* 0.000 claims description 3
- UFWIBTONFRDIAS-UHFFFAOYSA-N naphthalene-acid Natural products C1=CC=CC2=CC=CC=C21 UFWIBTONFRDIAS-UHFFFAOYSA-N 0.000 claims description 3
- 239000003208 petroleum Substances 0.000 claims description 3
- 229920001059 synthetic polymer Polymers 0.000 claims description 3
- XNKFCDGEFCOQOM-UHFFFAOYSA-N 1,2-dinitronaphthalene Chemical compound C1=CC=CC2=C([N+]([O-])=O)C([N+](=O)[O-])=CC=C21 XNKFCDGEFCOQOM-UHFFFAOYSA-N 0.000 claims description 2
- 229910015900 BF3 Inorganic materials 0.000 claims description 2
- 125000004054 acenaphthylenyl group Chemical class C1(=CC2=CC=CC3=CC=CC1=C23)* 0.000 claims description 2
- HXGDTGSAIMULJN-UHFFFAOYSA-N acetnaphthylene Chemical class C1=CC(C=C2)=C3C2=CC=CC3=C1 HXGDTGSAIMULJN-UHFFFAOYSA-N 0.000 claims description 2
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 2
- WTEOIRVLGSZEPR-UHFFFAOYSA-N boron trifluoride Chemical compound FB(F)F WTEOIRVLGSZEPR-UHFFFAOYSA-N 0.000 claims description 2
- GVEPBJHOBDJJJI-UHFFFAOYSA-N fluoranthrene Chemical class C1=CC(C2=CC=CC=C22)=C3C2=CC=CC3=C1 GVEPBJHOBDJJJI-UHFFFAOYSA-N 0.000 claims description 2
- 125000000686 lactone group Chemical group 0.000 claims description 2
- 125000002080 perylenyl group Chemical class C1(=CC=C2C=CC=C3C4=CC=CC5=CC=CC(C1=C23)=C45)* 0.000 claims description 2
- CSHWQDPOILHKBI-UHFFFAOYSA-N peryrene Chemical class C1=CC(C2=CC=CC=3C2=C2C=CC=3)=C3C2=CC=CC3=C1 CSHWQDPOILHKBI-UHFFFAOYSA-N 0.000 claims description 2
- 238000002294 plasma sputter deposition Methods 0.000 claims description 2
- IFLREYGFSNHWGE-UHFFFAOYSA-N tetracene Chemical class C1=CC=CC2=CC3=CC4=CC=CC=C4C=C3C=C21 IFLREYGFSNHWGE-UHFFFAOYSA-N 0.000 claims description 2
- 150000001875 compounds Chemical class 0.000 claims 2
- 238000010304 firing Methods 0.000 claims 2
- LSNNMFCWUKXFEE-UHFFFAOYSA-M Bisulfite Chemical compound OS([O-])=O LSNNMFCWUKXFEE-UHFFFAOYSA-M 0.000 claims 1
- 239000013040 bath agent Substances 0.000 claims 1
- 150000001732 carboxylic acid derivatives Chemical class 0.000 claims 1
- 150000002790 naphthalenes Chemical class 0.000 claims 1
- 230000007935 neutral effect Effects 0.000 claims 1
- 238000003763 carbonization Methods 0.000 description 24
- 230000035939 shock Effects 0.000 description 14
- JOXIMZWYDAKGHI-UHFFFAOYSA-N toluene-4-sulfonic acid Chemical compound CC1=CC=C(S(O)(=O)=O)C=C1 JOXIMZWYDAKGHI-UHFFFAOYSA-N 0.000 description 12
- 238000005087 graphitization Methods 0.000 description 10
- 230000000694 effects Effects 0.000 description 9
- 239000011295 pitch Substances 0.000 description 8
- 238000003754 machining Methods 0.000 description 5
- 239000000047 product Substances 0.000 description 5
- 239000011342 resin composition Substances 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 4
- BWVAOONFBYYRHY-UHFFFAOYSA-N [4-(hydroxymethyl)phenyl]methanol Chemical compound OCC1=CC=C(CO)C=C1 BWVAOONFBYYRHY-UHFFFAOYSA-N 0.000 description 4
- 239000000571 coke Substances 0.000 description 4
- 229910001882 dioxygen Inorganic materials 0.000 description 4
- QGJOPFRUJISHPQ-UHFFFAOYSA-N Carbon disulfide Chemical compound S=C=S QGJOPFRUJISHPQ-UHFFFAOYSA-N 0.000 description 3
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 3
- 239000000654 additive Substances 0.000 description 3
- 238000001723 curing Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 239000007770 graphite material Substances 0.000 description 3
- 238000009832 plasma treatment Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- QPUYECUOLPXSFR-UHFFFAOYSA-N 1-methylnaphthalene Chemical compound C1=CC=C2C(C)=CC=CC2=C1 QPUYECUOLPXSFR-UHFFFAOYSA-N 0.000 description 2
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- ZZHIDJWUJRKHGX-UHFFFAOYSA-N 1,4-bis(chloromethyl)benzene Chemical compound ClCC1=CC=C(CCl)C=C1 ZZHIDJWUJRKHGX-UHFFFAOYSA-N 0.000 description 1
- 229920002633 Kraton (polymer) Polymers 0.000 description 1
- 239000002841 Lewis acid Substances 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 1
- 235000010724 Wisteria floribunda Nutrition 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 238000010306 acid treatment Methods 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 150000001491 aromatic compounds Chemical class 0.000 description 1
- 229910021383 artificial graphite Inorganic materials 0.000 description 1
- 239000011449 brick Substances 0.000 description 1
- 239000007833 carbon precursor Substances 0.000 description 1
- 238000010000 carbonizing Methods 0.000 description 1
- 150000001735 carboxylic acids Chemical class 0.000 description 1
- 239000011300 coal pitch Substances 0.000 description 1
- 238000006356 dehydrogenation reaction Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000007849 furan resin Substances 0.000 description 1
- 150000004820 halides Chemical class 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 150000007517 lewis acids Chemical class 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 125000000325 methylidene group Chemical group [H]C([H])=* 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 150000004763 sulfides Chemical class 0.000 description 1
- 150000003460 sulfonic acids Chemical class 0.000 description 1
- 239000011269 tar Substances 0.000 description 1
- 238000001029 thermal curing Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
- Adhesives Or Adhesive Processes (AREA)
Description
(産業上の利用分野)
本発明は炭素、黒鉛あるいはこれらの前駆体か
ら選ばれるいずれか少なくとも1種の被着材と、
熱硬化性組成物から主として成る接着剤の炭化物
若しくは黒鉛化合物からなる接着剤層とから構成
されて成る接着構造物であつて、前記接着剤層と
被着材の熱膨張係数が同等である耐熱構造物に適
した炭素、黒鉛質接着構造物及びその製造方法に
関するものである。
(従来の技術)
従来、炭素、黒鉛の接着剤としては、数種のも
のが知られており、市販されているが、詳細につ
いては何ら発表されていないのが現状である。
これらの接着剤は、大別すると以下のようであ
ると考えられる。
(1) 炭素、黒鉛質若しくはこれらの前駆体を骨材
とし、フエノール樹脂、エポキシ樹脂、フラン
樹脂等の熱硬化性樹脂をBステージ樹脂として
混合したもの。
(2) 炭素、黒鉛質若しくはこれらの前駆体を骨材
とし、石油系若しくは石炭系のタール、ピツチ
と(1)と同様の熱硬化性樹脂のBステージ樹脂と
の混合物と混合したもの。
これらの内、(1)については、商品名V58a(西ド
イツSIGRI社製)が市販されており(2)について
は、商品名ニユーコートGC(アメリカDYLON
INDUSTRY INC.)が市販されており、また特
開昭54−114543号公報に「タール含有耐火煉瓦用
接着剤」が開示されている。
(発明が解決しようとする問題点)
まず、前記(1)の炭素、黒鉛の接着剤において
は、硬化した樹脂の炭素化収率が低い欠点を有
し、被着材に対し接着剤の炭素化収縮が著しく大
きいため骨材を添加しない場合には炭素化後の接
着強度が著しく低い、このため接着厚みは骨材粒
度に依存し、高い寸法精度が得られなかつた。ま
た、炭素化、黒鉛化後の接着剤層の熱膨張係数を
変化させうるものではなかつた。このため、得ら
れた接着構造物は熱衝撃に弱いという欠点を有し
ていた。
次に(2)の炭素、黒鉛の接着剤においては、熱硬
化性樹脂の炭素化収率が低いため炭素化収率の高
いタール、ピツチを添加し、この欠点を解決しよ
うとしたものと思慮される。しかし本来ピツチが
熱可塑性を有するため添加量に制限があり、多量
に添加すると接着剤層が炭素化過程で発泡したり
軟化するため根本的な解決に到らず、接着強度が
低く、また炭素化、黒鉛化後の接着剤層の熱膨張
係数の制御ができないため接着部の耐熱衝撃性は
著しく低い欠点を有していた。
また、(1)、(2)いずれも被着材と接着剤との結合
が物理的接着(アンカー効果)に依存しており積
極的に化学的結合を導入したものではなく、得ら
れた接着構造物の耐熱衝撃性、寸法安定性、強
度、弾性率、靭性等の性質を充分に引き出してい
るとは言い難い。
(問題点を解決するための手段及び作用)
本発明は、硬化時の収縮が小さく、炭素化収率
が高く炭素化時の収縮の小さい熱硬化性組成物を
接着剤として使用するものであつて、接着剤層と
被着材が強固に結合しており、基本的に骨材なし
で炭素化、黒鉛化後に高い接着強度が得られる。
このため接着精度は精密機械加工と同様の数μm
オーダーが確保できる。また、熱硬化性組成物の
組成、骨材の種類、添加量を変化させることによ
つて、得られる接着構造物の接着剤層の熱膨張係
数を制御し被着材のそれと一致させることによつ
て、接着構造物の耐熱衝撃性を向上させることを
特徴とする、治具、坩堝、ヒーター等の耐熱用部
材、複雑な加工を要する化学反応装置用部材、熱
交換器用部材等に適した炭素、黒鉛質接着構造物
を提供することを目的とするものであり、特許請
求の範囲の炭素、黒鉛質接着構造物及びその製造
方法を提供することによつて前記目的を達成する
ことができる。
次に本発明を詳細に説明する。
即ち、本発明は炭素、黒鉛あるいはこれらの前
駆体からなる被着材が、主として二環以上の縮合
多環芳香族化合物とヒドロキシメチル基、ハロメ
チル基のいずれか少なくとも一種の基を二個以上
有する一環又は二環以上の芳香環から成る芳香族
架橋剤と酸触媒との混合物が反応して成る熱硬化
性組成物(以下、COPNA樹脂組成物と略記す
る)の炭化物あるいは黒鉛化物を主成分とする接
着剤層とから構成されて成る接着構造物であつ
て、前記接着剤層と被着材の熱膨張係数が同等で
あることを特徴とする炭素、黒鉛質接着構造物及
びその製造方法に関するものであり、炭化物ある
いは黒鉛化物を主成分とする接着剤層の熱膨張係
数は以下の4種の方法の組み合わせによつて被着
材の熱膨張係数に応じて制御しうる。
(1) 分子内に酸素若しくは硫黄若しくはハロゲン
のいずれか少なくとも一種の元素を含有する縮
合多環芳香族化合物を使用するかあるいは、接
着剤に硫黄を添加して使用する。
(2) 骨材として、炭素前駆体を使用する。
(3) 骨材として、炭素、黒鉛、膨張黒鉛を使用す
る。
(4) 接着構造物の熱処理温度を変化させる。
これらのうち(1)、(2)は炭化物若しくは黒鉛化物
を主成分とする接着剤層の熱膨張係数を上げる作
用があり、(3)、(4)は下げる作用がある。これらの
添加物の有無、種類、量、さらには熱処理温度を
適宜変化させることによつて、例えば2800℃の温
度で黒鉛化を施した後の接着剤層の熱膨張係数を
2.0〜8.0×10-6/℃(50〜400℃)と広い範囲にわ
たり制御することができる。
また、添加物若しくは黒鉛化物を主成分とする
接着剤層の接着強度は接着前の被着材の被着面に
表面官能基が存在すると飛躍的に向上する。耐熱
衝撃性は主に強度、熱伝導率、弾性率、熱膨張係
数によつて支配される。接着構造物の場合は被着
材と接着剤層の熱膨張係数が同等であることが最
も重要であり、次に接着強度が大きいことが耐熱
衝撃性を向上させる。
接着剤としては、熱硬化性中間反応生成物の生
成反応条件を変えることにより、所謂Bステージ
樹脂の軟化点や溶融粘度を広い範囲にわたつて制
御することができる。また特に、重質油、ピツチ
系の縮合多環芳香族化合物を用いることにより、
飛躍的に炭素化収率が向上する。この場合、重質
油、ピツチを構成する縮合多環芳香族分子が直接
芳香族架橋剤と反応して熱硬化性樹脂となるた
め、炭素化収率の向上のみならず炭素化時の収縮
が小さい特徴を有する。これらの作用により耐熱
衝撃性、寸法安定性、強度、靭性を有し、かつ、
優れた接着寸法精度を有する、サイズ、形状の限
定のない、従来の機械加工では得られなかつた炭
素、黒鉛質接着構造物を得ることができる。
以下、本発明の熱硬化性組成物の原料であると
ころの縮合多環芳香族化合物、芳香族架橋剤及び
酸触媒について説明する。
本発明の二環以上の縮合多環芳香族化合物は、
ナフタレン、アントラセン、フエナントレン、ピ
レン、クリセン、ナフタセン、アセナフチレン、
ペリレン、コロネンを主骨格とする誘導体の中か
ら選ばれる一種又は二種以上の混合物、あるいは
石炭系若しくは石油系の重質油、タール、ピツチ
若しくは上記物質の酸化物あるいは硫化物あるい
はハロゲン化物等を使用できる。
また、含まれる酸素、硫黄あるいはハロゲンは
単独で存在しても、官能基としてあるいは環内に
存在してもよく、その数も限定されるものではな
い。これらの酸素、硫黄あるいはハロゲンは、
COPNA樹脂を構成するメチレン架橋のほかにこ
れらの元素が脱水素することによつて接着剤層中
に三次元架橋結合を形成するため、炭素化、黒鉛
化後の接着剤層の熱膨張係数を大きくする作用が
ある。
次に本発明の架橋剤には、ヒドロキシメチル
基、ハロメチル基のいずれか少なくとも一種の基
を二個以上有する一環又は二環以上の芳香環から
成る芳香族化合物、例えばp−キシリレンジクロ
ライド、1,4−ベンゼンジメタノール(p−キ
シリレングリコール)あるいはこれらの誘導体を
使用できる。
また、本発明の酸触媒には塩化アルミニウム、
弗化ホウ素等のルイス酸、硫酸、りん酸、有機ス
ルホン酸、カルボン酸等のプロトン酸、あるいは
これらの誘導体の中から選ばれる一種又は二種以
上の混合物を使用できる。
前記縮合多環芳香族化合物、架橋剤、酸触媒を
COPNA樹脂組成物とするための混合比率につい
ては、架橋剤/縮合多環芳香族化合物=0.5〜4.0
(モル比)の範囲;酸触媒添加量については、架
橋剤/縮合多環芳香族化合物の混合物に対して
0.5〜10wt%が好適な範囲である。
また、COPNA樹脂組成物を加熱反応させてB
ステージの接着剤を得るための反応温度範囲につ
いては、60〜300℃が好適な範囲である。以上の
ようにして、COPNA樹脂組成物を加熱反応させ
ることにより所謂Bステージ樹脂の接着剤が得ら
れる。さらに、このBステージ樹脂の接着剤に硫
黄あるいは、ジニトロナフタレンを添加する場合
の添加量は0.5〜10wt%が好適な範囲である。添
加の方法は粉末で混合してもよいが、二硫化炭素
等の溶媒を使用するのが好ましい。
本発明の接着剤層は、骨材として炭素、黒鉛、
膨張黒鉛、天然又は合成高分子あるいはこれらの
前駆体を使用することができる。また、骨材の表
面官能基については、水素、ハロゲン、ヒドロキ
シル基、カルボニル基、カルボキシル基、アルデ
ヒド基、エポキシ構造、クラトン構造、エーテル
構造、酸無水物構造等が挙げられ、これらは
COPNA樹脂と骨材との結合を強固にする効果が
ある。一方、同一量の骨材を添加した場合の接着
剤層の熱膨張係数はこれらの表面官能基が少ない
程または骨材の熱履歴温度が高い程小さくなる傾
向を示す、即ち炭素前駆体>炭素>黒鉛>膨張黒
鉛の順に熱膨張係数は小さくなる。
また、骨材の粒度は接着剤精度から10μm以下
が好ましく、添加量は特に限定されるものではな
いが、Bステージ樹脂に対し1〜50wt%が好適
な範囲である。添加の方法としては、加熱反応前
にCOPNA樹脂組成物に混合する方法あるいは反
応後のBステージ樹脂に混合する方法が使用でき
る。
本発明の被着材(第1図の1)としては炭素、
黒鉛あるいはこれらの前駆体を使用することがで
きる。被着材についても、水素、ハロゲン、ヒド
ロキシル基、カルボニル基、カルボキシル基、ア
ルデヒド基、エポキシ構造、ラクトン構造、エー
テル構造、酸無水物構造等の表面官能基が被着面
に存在すると、炭素化、黒鉛化後の接着強度は著
しく向上する。このため硝酸処理等の化学的導入
あるいは酸素ガスプラズマ(第1図の2)処理に
よる導入が好適である。このように表面官能基が
被着面に存在する場合には、接着前にCOPNA樹
脂組成物を構成する芳香族架橋剤と酸触媒の混合
物のアルコール等の溶液を被着面に塗布しておく
とさらに接着強度は向上する。
接着操作は接着剤であるBステージCOPNA樹
脂組成物(第1図の3)が常温で液状の場合は常
温で、軟化点を有する場合には軟化点より20〜60
℃高い温度で被着面に塗布した後、被着面どうし
を接着(第1図の3d)し、接着剤を熱硬化させ
て行う。この際、高い接着精度を得るためには、
接着部を治具で固定するのが好ましい。
熱硬化温度範囲は、100〜400℃、好ましくは
150〜250℃が好適である。
硬化後の炭素化(第1図の4)は非酸化性雰囲
気中で400℃/hr以下、好ましくは100℃/hr以下
の昇温速度で600〜1500℃まで昇温して行う。黒
鉛化(第1図の5)についても非酸化性雰囲気中
で600℃/hr以下、好ましくは200℃/hr以下の昇
温速度で2000〜3000℃まで昇温して行う。
以上の様にして耐熱衝撃性、寸法安定性、強
度、靭性を有し、かつ、優れた接着寸法精度を有
する、サイズや形状に限定されることなく治具、
坩堝、ヒーター等の耐熱用部材、複雑な加工を要
する化学反応装置用部材、熱交換器用部材等ある
いは従来全く機械加工では得られなかつた形状の
炭素、黒鉛質接着構造物を提供することができ
る。
(実施例)
次に、本発明を実施例について更に詳細に説明
する。
実施例 1
軟化点85℃の石炭系ピツチ(平均分子量約400)
を縮合多環芳香族化合物とし、架橋剤としてp−
キシレングリコール(PXG)をモル比で1:2
の割合で添加し、ここにp−トルエンスルホン酸
(PTS)を5wt%添加した混合物を140℃で40分間
反応させ、BステージのCOPNA樹脂接着剤を得
た。被着材として商品名T−6(イビデン(株)製黒
鉛材)を用い(第1図a)、2cm2の被着面を研磨
仕上げしアセトン中で超音波洗浄した試験片を使
用した。被着材の被着面を徳田製作所(株)製CFS−
8EP−55のプラズマスパツタ装置で圧力
0.3mbar、出力500W、3時間、酸素ガスプラズ
マ処理を行つた(第1図b)。処理後の被着面に
p−キシリレングリコール及びp−トルエンスル
ホン酸のエタノール溶液(濃度:各々0、2.5、
5.0、7.5wt%)をスプレーで塗布し150℃に加熱
した。加熱した被着面に前記接着剤を塗布(第1
図c)後、接着(第1図d)し、接着部を黒鉛製
治具で固定し、180℃で40分間加熱し、接着剤を
硬化させた。炭素化は接着部を黒鉛製治具で固定
したまま、非酸化性雰囲気中で50℃/hrの昇温速
度で100℃まで加熱し行い(第1図e)、黒鉛化は
同様にして3000℃まで加熱し行つた(第1図f)。
また、酸素ガスプラズマ処理を行なわない試料
についても同様の操作を行つた。炭素化後及び黒
鉛化後の試料は引つ張り強度を測定した。これら
の結果は第1表に示した。
(Industrial Application Field) The present invention provides at least one adherend material selected from carbon, graphite, or their precursors;
A heat-resistant adhesive structure comprising an adhesive layer mainly made of a carbide or graphite compound of an adhesive made of a thermosetting composition, wherein the adhesive layer and the adherend have the same coefficient of thermal expansion. The present invention relates to a carbon and graphite bonded structure suitable for structures and a method for manufacturing the same. (Prior Art) Several types of carbon and graphite adhesives have been known and are commercially available, but at present no details have been published. These adhesives can be roughly classified as follows. (1) Carbon, graphite, or their precursors are used as aggregates, and thermosetting resins such as phenolic resins, epoxy resins, and furan resins are mixed as B-stage resins. (2) Aggregates made of carbon, graphite, or their precursors, mixed with a mixture of petroleum-based or coal-based tar, pitch, and B-stage thermosetting resin similar to (1). Among these, for (1), the product name V58a (manufactured by SIGRI in West Germany) is commercially available, and for (2), the product name Newcoat GC (American DYLON) is commercially available.
INDUSTRY INC.) is commercially available, and ``Tar-containing adhesive for refractory bricks'' is disclosed in Japanese Patent Application Laid-Open No. 114543/1983. (Problems to be Solved by the Invention) First, the carbon and graphite adhesive described in (1) above has the drawback that the carbonization yield of the cured resin is low, and the carbon of the adhesive Since the carbonization shrinkage is extremely large, the adhesive strength after carbonization is extremely low when no aggregate is added.For this reason, the adhesive thickness depends on the aggregate particle size, and high dimensional accuracy cannot be obtained. Furthermore, it was not possible to change the coefficient of thermal expansion of the adhesive layer after carbonization or graphitization. Therefore, the obtained bonded structure had the disadvantage of being susceptible to thermal shock. Next, in the carbon and graphite adhesive mentioned in (2), since the carbonization yield of the thermosetting resin is low, tar and pitch, which have a high carbonization yield, are added in an attempt to solve this drawback. be done. However, since pitch is inherently thermoplastic, there is a limit to the amount that can be added, and if too much is added, the adhesive layer will foam or soften during the carbonization process, so a fundamental solution cannot be reached, resulting in low adhesive strength and Since the thermal expansion coefficient of the adhesive layer after carbonization and graphitization cannot be controlled, the thermal shock resistance of the bonded portion is extremely low. In addition, in both (1) and (2), the bond between the adherend and the adhesive relies on physical adhesion (anchor effect), and is not based on actively introducing chemical bonding. It cannot be said that properties such as thermal shock resistance, dimensional stability, strength, elastic modulus, and toughness of the structure are fully brought out. (Means and effects for solving the problems) The present invention uses, as an adhesive, a thermosetting composition that exhibits low shrinkage during curing, a high carbonization yield, and low shrinkage during carbonization. Therefore, the adhesive layer and the adherend are strongly bonded, and basically high adhesive strength can be obtained after carbonization and graphitization without any aggregate.
Therefore, the adhesion accuracy is several μm, which is the same as precision machining.
Orders can be secured. In addition, by changing the composition of the thermosetting composition, the type of aggregate, and the amount added, it is possible to control the coefficient of thermal expansion of the adhesive layer of the resulting adhesive structure and make it match that of the adherend. Therefore, it is suitable for heat-resistant parts such as jigs, crucibles, heaters, etc., parts for chemical reaction devices that require complicated processing, parts for heat exchangers, etc., which are characterized by improving the thermal shock resistance of bonded structures. The object of the present invention is to provide a bonded structure made of carbon and graphite, and the above object can be achieved by providing the bonded structure made of carbon and graphite and the manufacturing method thereof according to the claims. . Next, the present invention will be explained in detail. That is, the present invention provides that an adherend made of carbon, graphite, or a precursor thereof mainly has two or more fused polycyclic aromatic compounds having two or more rings and at least one of a hydroxymethyl group and a halomethyl group. A thermosetting composition (hereinafter abbreviated as COPNA resin composition) formed by reacting a mixture of an aromatic crosslinking agent consisting of one or two or more aromatic rings with an acid catalyst, whose main component is a carbide or graphitized product. The present invention relates to a carbon or graphite adhesive structure comprising an adhesive layer, the adhesive layer and an adherend having the same coefficient of thermal expansion, and a method for manufacturing the same. The coefficient of thermal expansion of the adhesive layer containing carbide or graphitized material as a main component can be controlled according to the coefficient of thermal expansion of the adherend by a combination of the following four methods. (1) Use a condensed polycyclic aromatic compound containing at least one element of oxygen, sulfur, or halogen in the molecule, or add sulfur to the adhesive. (2) Use carbon precursor as aggregate. (3) Carbon, graphite, and expanded graphite are used as aggregates. (4) Change the heat treatment temperature of the bonded structure. Among these, (1) and (2) have the effect of increasing the thermal expansion coefficient of the adhesive layer containing carbide or graphitized material as a main component, and (3) and (4) have the effect of lowering it. By appropriately changing the presence, type, and amount of these additives, as well as the heat treatment temperature, it is possible to change the thermal expansion coefficient of the adhesive layer after graphitization at a temperature of, for example, 2800°C.
It can be controlled over a wide range of 2.0 to 8.0×10 -6 /°C (50 to 400°C). Further, the adhesive strength of an adhesive layer containing an additive or a graphitized material as a main component is dramatically improved when a surface functional group is present on the surface of the adherend before adhesion. Thermal shock resistance is mainly controlled by strength, thermal conductivity, modulus of elasticity, and coefficient of thermal expansion. In the case of adhesive structures, it is most important that the adherend and the adhesive layer have the same coefficient of thermal expansion, and secondly, high adhesive strength improves thermal shock resistance. As an adhesive, the softening point and melt viscosity of the so-called B-stage resin can be controlled over a wide range by changing the reaction conditions for producing the thermosetting intermediate reaction product. In particular, by using heavy oil and pitch-based condensed polycyclic aromatic compounds,
Carbonization yield is dramatically improved. In this case, the condensed polycyclic aromatic molecules that make up the heavy oil and pitch react directly with the aromatic crosslinking agent to form a thermosetting resin, which not only improves the carbonization yield but also reduces shrinkage during carbonization. It has small characteristics. Due to these effects, it has thermal shock resistance, dimensional stability, strength, and toughness, and
It is possible to obtain a bonded structure made of carbon or graphite, which has excellent bonding dimensional accuracy, is not limited in size or shape, and cannot be obtained by conventional machining. Hereinafter, the fused polycyclic aromatic compound, aromatic crosslinking agent, and acid catalyst, which are raw materials for the thermosetting composition of the present invention, will be explained. The fused polycyclic aromatic compound of the present invention has two or more rings,
Naphthalene, anthracene, phenanthrene, pyrene, chrysene, naphthacene, acenaphthylene,
One or a mixture of two or more selected from derivatives with main skeletons of perylene and coronene, coal-based or petroleum-based heavy oil, tar, pitch, or oxides, sulfides, or halides of the above substances. Can be used. Furthermore, the oxygen, sulfur, or halogen contained therein may be present alone, as a functional group, or within a ring, and the number thereof is not limited. These oxygen, sulfur or halogens are
In addition to the methylene crosslinks that make up COPNA resin, these elements form three-dimensional crosslinks in the adhesive layer by dehydrogenation, so the coefficient of thermal expansion of the adhesive layer after carbonization and graphitization is It has the effect of enlarging it. Next, the crosslinking agent of the present invention includes an aromatic compound consisting of one or more aromatic rings having two or more of at least one of hydroxymethyl group and halomethyl group, such as p-xylylene dichloride, , 4-benzenedimethanol (p-xylylene glycol) or derivatives thereof can be used. In addition, the acid catalyst of the present invention includes aluminum chloride,
One or a mixture of two or more selected from Lewis acids such as boron fluoride, protonic acids such as sulfuric acid, phosphoric acid, organic sulfonic acids, and carboxylic acids, and derivatives thereof can be used. The fused polycyclic aromatic compound, crosslinking agent, and acid catalyst are
Regarding the mixing ratio for forming a COPNA resin composition, crosslinking agent/condensed polycyclic aromatic compound = 0.5 to 4.0
(molar ratio) range; the amount of acid catalyst added is based on the mixture of crosslinking agent/fused polycyclic aromatic compound.
A suitable range is 0.5 to 10 wt%. In addition, B
The reaction temperature range for obtaining the stage adhesive is preferably 60 to 300°C. In the manner described above, a so-called B-stage resin adhesive can be obtained by subjecting the COPNA resin composition to a heat reaction. Further, when sulfur or dinitronaphthalene is added to this B-stage resin adhesive, the amount added is preferably in the range of 0.5 to 10 wt%. Although the addition method may be by mixing powder, it is preferable to use a solvent such as carbon disulfide. The adhesive layer of the present invention uses carbon, graphite,
Expanded graphite, natural or synthetic polymers or precursors thereof can be used. In addition, the surface functional groups of the aggregate include hydrogen, halogen, hydroxyl group, carbonyl group, carboxyl group, aldehyde group, epoxy structure, kraton structure, ether structure, acid anhydride structure, etc.
It has the effect of strengthening the bond between COPNA resin and aggregate. On the other hand, when the same amount of aggregate is added, the coefficient of thermal expansion of the adhesive layer tends to decrease as the number of these surface functional groups decreases or as the thermal history temperature of the aggregate increases. The coefficient of thermal expansion decreases in the order of > graphite > expanded graphite. Further, the particle size of the aggregate is preferably 10 μm or less from the viewpoint of adhesive accuracy, and the amount added is not particularly limited, but is preferably in the range of 1 to 50 wt% based on the B-stage resin. As a method of addition, a method of mixing it into the COPNA resin composition before the heating reaction or a method of mixing it into the B-stage resin after the reaction can be used. The adherend of the present invention (1 in Fig. 1) is carbon,
Graphite or a precursor thereof can be used. Regarding adherends, if surface functional groups such as hydrogen, halogen, hydroxyl group, carbonyl group, carboxyl group, aldehyde group, epoxy structure, lactone structure, ether structure, acid anhydride structure, etc. are present on the adherend surface, carbonization may occur. , the adhesive strength after graphitization is significantly improved. For this reason, chemical introduction such as nitric acid treatment or introduction by oxygen gas plasma treatment (2 in FIG. 1) is suitable. If surface functional groups exist on the surface to be adhered in this way, apply a solution of a mixture of an aromatic crosslinking agent and an acid catalyst, such as alcohol, to the surface before adhesion. This further improves the adhesive strength. The adhesive operation is performed at room temperature if the B-stage COPNA resin composition (3 in Figure 1) is liquid at room temperature, or at 20 to 60 degrees below the softening point if it has a softening point.
After applying the adhesive to the surfaces to be adhered to at a high temperature of .degree. C., the surfaces to be adhered to each other are bonded together (3d in FIG. 1), and the adhesive is thermally cured. At this time, in order to obtain high adhesion accuracy,
It is preferable to fix the adhesive part with a jig. Thermal curing temperature range is 100-400℃, preferably
150-250°C is suitable. Carbonization after curing (4 in Figure 1) is carried out in a non-oxidizing atmosphere by raising the temperature from 600 to 1500°C at a temperature increase rate of 400°C/hr or less, preferably 100°C/hr or less. Graphitization (5 in Figure 1) is also carried out in a non-oxidizing atmosphere by raising the temperature to 2000-3000°C at a rate of 600°C/hr or less, preferably 200°C/hr or less. As described above, the jig has thermal shock resistance, dimensional stability, strength, and toughness, and has excellent adhesion dimensional accuracy, regardless of size or shape.
It is possible to provide heat-resistant parts such as crucibles and heaters, parts for chemical reaction equipment that require complicated processing, parts for heat exchangers, etc., and carbon and graphite bonded structures in shapes that could not previously be obtained by machining. . (Example) Next, the present invention will be described in more detail with reference to Examples. Example 1 Coal-based pitcher with a softening point of 85°C (average molecular weight approximately 400)
is a fused polycyclic aromatic compound, and p- is used as a crosslinking agent.
Xylene glycol (PXG) in a molar ratio of 1:2
A mixture of p-toluenesulfonic acid (PTS) and 5 wt% of p-toluenesulfonic acid (PTS) was reacted at 140° C. for 40 minutes to obtain a B-stage COPNA resin adhesive. As the adherend material, trade name T-6 (graphite material manufactured by IBIDEN Co., Ltd.) was used (Fig. 1a), and a 2 cm 2 adherend surface was polished and a test piece was used which was ultrasonically cleaned in acetone. The adhering surface of the adherend material is CFS- manufactured by Tokuda Seisakusho Co., Ltd.
Pressure with 8EP-55 plasma sputtering device
Oxygen gas plasma treatment was performed at 0.3 mbar and an output of 500 W for 3 hours (Fig. 1b). Ethanol solutions of p-xylylene glycol and p-toluenesulfonic acid (concentrations: 0, 2.5,
5.0, 7.5wt%) was applied by spray and heated to 150℃. Applying the adhesive to the heated adhering surface (first
After Figure c), the adhesive was bonded (Figure 1D), the adhesive part was fixed with a graphite jig, and heated at 180°C for 40 minutes to harden the adhesive. Carbonization was carried out by heating the bonded part with a graphite jig in a non-oxidizing atmosphere at a temperature increase rate of 50 °C/hr to 100 °C (Fig. 1e), and graphitization was performed in the same manner for 3000 °C. ℃ (Fig. 1f). Further, the same operation was performed on a sample that was not subjected to oxygen gas plasma treatment. The tensile strength of the samples after carbonization and graphitization was measured. These results are shown in Table 1.
【表】
実施例 2
軟化点235℃の石炭系ピツチと精製メチルナフ
タレンを1:2の重量比で混合し縮合多環芳香族
化合物とし、架橋剤としてp−キシリレングリコ
ールを混合物に対し重量比で1:0.8の割合で添
加し、この混合物にp−トルエンスルホン酸を
10wt%、硫黄を5wt%、骨材として5μm以下に粉
砕した石炭系生コークスを30wt%それぞれ添加
し、120℃で15分間反応させBステージの
COPNA樹脂接着剤を得た。被着材として商品名
T−4及びET10(イビデン(株)製黒鉛材:引つ張り
強度、両者共約200Kg/cm2)を用い、2cm2の被着
面を研磨仕上げしアセトン中で超音波洗浄した試
験片を使用した。
被着材の被着面に常温で前記接着剤を塗布し、
接着後金属製治具で固定し、180℃で60分間加熱
し、接着剤を硬化させた。硬化後治具を外し、非
酸化性雰囲気中で30℃/hrの昇温速度で1000℃ま
で昇温し、接着部を炭素化した。
また、骨材を添加しない接着剤を用い、同様の
操作に従つて試験片を作成した。
炭素化後の試料は接着剤層の厚みを光学顕微鏡
で測定した後、接着部の引つ張り強度を測定し
た。この結果を第2表に示した。[Table] Example 2 Coal-based pitch with a softening point of 235°C and purified methylnaphthalene were mixed at a weight ratio of 1:2 to form a condensed polycyclic aromatic compound, and p-xylylene glycol was added as a crosslinking agent to the mixture by weight ratio. p-toluenesulfonic acid was added to this mixture at a ratio of 1:0.8.
10 wt%, 5 wt% sulfur, and 30 wt% of coal-based raw coke crushed to 5 μm or less as aggregate were added, and reacted at 120°C for 15 minutes to produce the B-stage.
COPNA resin adhesive was obtained. Using trade name T-4 and ET10 (graphite material made by IBIDEN Co., Ltd.; tensile strength of both approximately 200 Kg/cm 2 ) as adherend materials, the 2 cm 2 adhering surface was polished and then super-absorbed in acetone. A test piece that had been sonicated was used. Applying the adhesive at room temperature to the adherend surface of the adherend,
After adhesion, it was fixed with a metal jig and heated at 180°C for 60 minutes to harden the adhesive. After curing, the jig was removed and the temperature was raised to 1000°C at a rate of 30°C/hr in a non-oxidizing atmosphere to carbonize the bonded portion. In addition, test pieces were prepared in the same manner using an adhesive that did not contain aggregate. After carbonizing the sample, the thickness of the adhesive layer was measured using an optical microscope, and then the tensile strength of the bonded portion was measured. The results are shown in Table 2.
【表】
実施例 3
実施例1で使用した接着剤a及びaに5wt%硫
黄を添加した接着剤bを用い、骨材として10μm
以下に粉砕した(1)石炭系生コークス、(2)石炭系か
焼コークス、(3)人造黒鉛の3種をそれぞれ接着剤
に対して30wt%添加した。被着材として商品名
T−4、T−6及びET10(イビデン(株)製黒鉛材:
熱膨張係数(50〜400℃)それぞれ(3.8、4.8、
6.3×10-6/℃)を用い、50mmφ、4mm厚みで中
心に8φの穴があいた円板を半割にした形状に加
工し、接着後に前記円板状になるよう、実施例1
と同様の条件で接着後炭素化した。炭素化後の試
料は非酸化性雰囲気中で400℃/hrの昇温速度で
2000℃まで昇温し、接着部を黒鉛化した。黒鉛化
後の試料は耐熱衝撃性を調べる目的で、富士電波
(株)製高周波誘導加熱装置で外周部を急速加熱し、
破壊までの時間を測定した。耐熱衝撃性の評価は
次式に示した耐熱衝撃指標FIを算出して行つた。
FI=5.46+4.43ln(t/n)
t:破壊に要した電力負荷時間
n:出力係数
20KW 3.14
30KW 2.34
40KW 1.44
50KW 1.00
(FI値が大きい程耐熱衝撃性は大きい。)
この結果を第3表に示した。[Table] Example 3 Using adhesive a used in Example 1 and adhesive b in which 5 wt% sulfur was added to a, 10 μm of aggregate was used.
Three types of crushed coke (1) raw coal-based coke, (2) calcined coal-based coke, and (3) artificial graphite were each added at 30 wt% to the adhesive. Product names T-4, T-6 and ET10 (graphite material manufactured by IBIDEN Co., Ltd.) are used as adherends.
Thermal expansion coefficient (50~400℃) respectively (3.8, 4.8,
6.3×10 -6 /℃), a disk of 50 mmφ and 4 mm thickness with a hole of 8φ in the center was cut in half, and after bonding, the disk shape was prepared as shown in Example 1.
Carbonization was carried out after adhesion under the same conditions as above. After carbonization, the sample was heated at a heating rate of 400℃/hr in a non-oxidizing atmosphere.
The temperature was raised to 2000°C to graphitize the bonded area. After graphitization, the sample was sent to Fuji Denpai for the purpose of examining thermal shock resistance.
The outer periphery is rapidly heated using a high-frequency induction heating device manufactured by Co., Ltd.
The time until destruction was measured. The thermal shock resistance was evaluated by calculating the thermal shock resistance index FI shown in the following formula. FI=5.46+4.43ln (t/n) t: Power load time required for destruction n: Output coefficient 20KW 3.14 30KW 2.34 40KW 1.44 50KW 1.00 (The larger the FI value, the greater the thermal shock resistance.) This result is shown in the third section. Shown in the table.
【表】
(発明の効果)
以上説明した如く本発明の炭素、黒鉛質接着構
造物は炭素、黒鉛あるいはこれらの前駆体からな
る被着材が、主として二環以上の縮合多環芳香族
化合物とヒドロキシメチル基、ハロメチル基のい
ずれ少なくとも一種の基を二個以上有する一環又
は二環以上の芳香環から成る前記芳香族架橋剤と
酸触媒との混合物が反応して成る熱硬化性組成物
の炭化物あるいは黒鉛化物を主成分とする接着剤
層とから構成されて成る接着構造物であつて、前
記接着剤層と被着材の熱膨張係数で同等であるこ
とを特徴とするものであり、炭化物あるいは黒鉛
化物を主成分とする接着剤層の熱膨張係数は製造
時における骨材や硫黄等の添加物の種類、量、さ
らには熱処理温度を適宜変化させることによつて
広い範囲にわたり制御することができる。
さらに、接着強度は被着材の被着面に表面官能
基が存在すると飛躍的に向上する。被着材と接着
剤層の熱膨張係数が同等であること及び接着強度
が大きいことで本発明の接着構造物の耐熱衝撃性
は著しく良好である。
また、重質油、ピツチ系の縮合多環芳香族化合
物を用いることにより、飛躍的に炭素化収率を向
上させることができる。この場合、重質油、ピツ
チを構成する縮合多環芳香族分子が直接芳香族架
橋剤と反応して熱硬化性樹脂となるため、炭素化
収率の向上のみならず炭素化時の収縮が小さい特
徴を有し、骨材なしでも充分な接着強度が得られ
る。このため精密機械加工精度に匹敵する接着精
度が得られる。これらの特徴から本発明の接着構
造物は従来に例をみない耐熱衝撃性、寸法安定
性、強度、靭性を有し、かつ、優れた接着寸法精
度を有するものであり、サイズや形状に限定され
ることなく治具、坩堝、ヒーター等の耐熱用部
材、複雑な形状の化学反応装置用部材、熱交換器
用部材等さらには従来全く機械加工で得られなか
つた形状の炭素、黒鉛質構造物を供給することが
でるばかりでなく、従来簡略化することが困難で
あつた加工工程を簡略化することができる。これ
らの利点により大幅なコスト削減が可能であり、
産業上寄与する効果は極めて大きい。[Table] (Effects of the Invention) As explained above, the carbon and graphite adhesive structure of the present invention has an adherend consisting of carbon, graphite, or a precursor thereof, which is mainly composed of a condensed polycyclic aromatic compound having two or more rings. A carbonized product of a thermosetting composition obtained by reacting a mixture of the aromatic crosslinking agent and an acid catalyst, which is composed of one or two or more aromatic rings having two or more of at least one of hydroxymethyl groups and halomethyl groups. Alternatively, it is an adhesive structure composed of an adhesive layer mainly composed of graphitized material, and is characterized in that the adhesive layer and the adherend have the same coefficient of thermal expansion. Alternatively, the coefficient of thermal expansion of the adhesive layer whose main component is graphitized material can be controlled over a wide range by appropriately changing the type and amount of additives such as aggregate and sulfur during manufacturing, as well as the heat treatment temperature. I can do it. Furthermore, the adhesive strength is dramatically improved when surface functional groups are present on the adhering surface of the adherend. The thermal shock resistance of the bonded structure of the present invention is extremely good because the adherend and the adhesive layer have the same coefficient of thermal expansion and high adhesive strength. Furthermore, by using heavy oil or a pitch-based condensed polycyclic aromatic compound, the carbonization yield can be dramatically improved. In this case, the condensed polycyclic aromatic molecules that make up the heavy oil and pitch react directly with the aromatic crosslinking agent to form a thermosetting resin, which not only improves the carbonization yield but also reduces shrinkage during carbonization. It has small characteristics and sufficient adhesive strength can be obtained even without aggregate. Therefore, adhesion accuracy comparable to precision machining accuracy can be obtained. Due to these characteristics, the bonded structure of the present invention has unprecedented thermal shock resistance, dimensional stability, strength, and toughness, as well as excellent bonding dimensional accuracy, and is not limited to size or shape. Heat-resistant parts such as jigs, crucibles, and heaters, parts for chemical reaction equipment with complex shapes, parts for heat exchangers, etc., as well as carbon and graphite structures with shapes that could not previously be obtained by machining. In addition to being able to supply the following, it is also possible to simplify processing steps that have been difficult to simplify in the past. These advantages enable significant cost savings;
The industrial effects are extremely large.
第1図のa〜fは、本願発明の炭素、黒鉛質接
着構造物の製造工程である。
1……黒鉛被着材、2……酸素ガスプラズマ、
3……接着剤、4……接着剤の炭化物、5……接
着剤の黒鉛化物。
1A to 1F are steps for manufacturing the carbon and graphite bonded structure of the present invention. 1...Graphite adherend material, 2...Oxygen gas plasma,
3...Adhesive, 4...Carbide of adhesive, 5...Graphitized adhesive.
Claims (1)
れるいずれか少なくとも1種の被着材と、下記(イ)
(ロ)(ハ)の混合物が反応して成る熱硬化性組成物を焼
成することにより得られる、炭化物あるいは黒鉛
化物を主成分とする接着剤層とから構成されて成
る接着構造物であつて、前記の接着剤層と被着材
の熱膨張係数が同等であることを特徴とする炭
素、黒鉛質接着構造物。 (イ) 主として二環以上の縮合多環芳香族化合物 (ロ) ヒドロキシメチル基、ハロメチル基のいずれ
か少なくとも一種の基を二個以上有する一環又
は二環以上の芳香環から成る芳香族架橋剤 (ハ) 酸触媒。 2 前記接着剤層と被着材の熱膨張係数の差が30
%以内であることを特徴とする特許請求の範囲第
1項記載の炭素、黒鉛質接着構造物。 3 前記主として二環以上の縮合多環芳香族化合
物は、ナフタレン、アントラセン、フエナントレ
ン、ピレン、クリセン、ナフタセン、アセナフチ
レン、ペリレン、コロネンを主骨格とする誘導体
の中から選ばれる一種又は二種以上の混合物、あ
るいは石炭又は石油系の重質油、タール、ピツチ
である特許請求の範囲第1項記載の炭素、黒鉛質
接着構造物。 4 前記主として二環以上の縮合多環芳香族化合
物は分子内に酸素、硫黄あるいはハロゲンのいず
れか少なくとも一種の元素を含有する特許請求の
範囲第1項記載の炭素、黒鉛質接着構造物。 5 前記酸触媒は、塩化アルミニウム、弗化ホウ
素、りん酸、有機スルホン酸、カルボン酸あるい
はこれらの誘導体の中から選ばれる一種又は二種
以上の混合物である特許請求の範囲第1項記載の
炭素、黒鉛質接着構造物。 6 前記接着剤は、炭素、黒鉛、膨張黒鉛、天然
又は合成高分子あるいはこれらの前駆体の中から
選ばれる一種又は二種以上の化合物若しくは混合
物を骨材として含む特許請求の範囲第1項記載の
炭素、黒鉛質接着構造物。 7 少なくとも下記の(a)〜(c)工程のシーケンスか
ら成ることを特徴とする炭素、黒鉛接着構造物の
製造方法。 (a) 主として二環以上の縮合多環芳香族化合物
と、ヒドロキシメチル基、ハロメチル基のいず
れか少なくとも一種の基を二個以上有する一環
又は二環以上の芳香環から成る芳香族架橋剤
と、酸触媒を組み合わせて成る熱硬化性組成物
を酸化性あるいは非酸化性雰囲気中60〜300℃
の温度範囲に加熱し、軟化点が150℃以下の中
間反応生成物(Bステージ樹脂)とする工程。 (b) 前記(a)工程により得られた中間反応生成物
(Bステージ樹脂)を接着剤として、被着材の
被着面に塗布し、被着面同志を接着後、酸化性
あるいは非酸化性雰囲気中100〜400℃の温度範
囲に加熱し、接着剤を熱硬化させる工程。 (c) 前記(b)工程により得られた接着構造物を非酸
化性雰囲気中で、炭素化あるいは黒鉛化する焼
成工程。 8 前記接着剤は接着を行う前に、炭素、黒鉛、
膨張黒鉛、天然又は合成高分子あるいはこれらの
前駆体の中から選ばれる一種又は二種以上の化合
物若しくは混合物を骨材として混合されてなる特
許請求の範囲第7項記載の製造方法。 9 接着前の前記被着材の被着面は水素、ハロゲ
ン、ヒドロキシル基、カルボニル基、カルボキシ
ル基、アルデヒド基、エポキシ構造、ラクトン構
造、エーテル構造、酸無水物構造のなかから選ば
れる少なくとも1種の表面官能基を有する特許請
求の範囲第7項記載の製造方法。 10 接着前の前記被着材の被着面に表面官能基
を化学反応若しくはプラズマスパツタ処理によつ
て導入する特許請求の範囲第7項記載の製造方
法。 11 前記中間反応生成物(Bステージ樹脂)を
浴剤に溶解させた溶液状で使用する特許請求の範
囲第7項記載の製造方法。 12 前記縮合多環芳香族化合物は、分子内に酸
素、硫黄あるいはハロゲンのいずれか少なくとも
一種の元素を有する特許請求の範囲第7項記載の
製造方法。 13 前記接着剤は接着前に硫黄あるいはジニト
ロナフタレンから選ばれるいずれか少なくとも1
種が添加されて成る特許請求の範囲第7項記載の
製造方法。[Scope of Claims] 1. At least one adherend material selected from carbon, graphite, or their precursors, and the following (a):
(b) An adhesive structure comprising an adhesive layer mainly composed of carbide or graphitized material obtained by firing a thermosetting composition formed by reacting the mixture of (b) and (c). . A carbon/graphite bonded structure, wherein the adhesive layer and the adherend have the same coefficient of thermal expansion. (a) A fused polycyclic aromatic compound mainly having two or more rings (b) An aromatic crosslinking agent consisting of one or two or more aromatic rings having two or more of at least one type of hydroxymethyl group or halomethyl group ( c) Acid catalyst. 2 The difference in thermal expansion coefficient between the adhesive layer and the adherend is 30
% or less, the carbon-graphite bonded structure according to claim 1. 3. The fused polycyclic aromatic compound having mainly two or more rings is one or a mixture of two or more selected from derivatives having a main skeleton of naphthalene, anthracene, phenanthrene, pyrene, chrysene, naphthacene, acenaphthylene, perylene, and coronene. 2. The carbon or graphite adhesive structure according to claim 1, which is coal or petroleum-based heavy oil, tar, or pitch. 4. The carbon-graphite adhesive structure according to claim 1, wherein the fused polycyclic aromatic compound having mainly two or more rings contains at least one element selected from oxygen, sulfur, and halogen in the molecule. 5. The carbonaceous acid catalyst according to claim 1, wherein the acid catalyst is one or a mixture of two or more selected from aluminum chloride, boron fluoride, phosphoric acid, organic sulfonic acid, carboxylic acid, or derivatives thereof. , graphitic bonded structures. 6. The adhesive contains as an aggregate one or more compounds or mixtures selected from carbon, graphite, expanded graphite, natural or synthetic polymers, or their precursors. carbon, graphite bonded structure. 7. A method for producing a carbon-graphite bonded structure, comprising at least the following sequence of steps (a) to (c). (a) An aromatic crosslinking agent consisting mainly of a fused polycyclic aromatic compound having two or more rings and one or more aromatic rings having two or more of at least one type of hydroxymethyl group or halomethyl group; A thermosetting composition comprising an acid catalyst is heated at 60 to 300°C in an oxidizing or non-oxidizing atmosphere.
The process of heating to a temperature range of 150°C or less to produce an intermediate reaction product (B-stage resin) with a softening point of 150°C or less. (b) The intermediate reaction product (B-stage resin) obtained in step (a) above is applied as an adhesive to the adherend surfaces of the adherends, and after adhering the adherend surfaces together, oxidizing or non-oxidizing A process in which the adhesive is thermally cured by heating to a temperature range of 100 to 400°C in a neutral atmosphere. (c) A firing step in which the bonded structure obtained in step (b) is carbonized or graphitized in a non-oxidizing atmosphere. 8 The adhesive may contain carbon, graphite,
8. The manufacturing method according to claim 7, wherein one or more compounds or mixtures selected from expanded graphite, natural or synthetic polymers, or their precursors are mixed as an aggregate. 9 The adhering surface of the adherend before adhesion has at least one type selected from hydrogen, halogen, hydroxyl group, carbonyl group, carboxyl group, aldehyde group, epoxy structure, lactone structure, ether structure, and acid anhydride structure. The manufacturing method according to claim 7, which has a surface functional group. 10. The manufacturing method according to claim 7, wherein a surface functional group is introduced to the adhering surface of the adherend material by chemical reaction or plasma sputtering treatment before adhesion. 11. The manufacturing method according to claim 7, wherein the intermediate reaction product (B-stage resin) is used in the form of a solution dissolved in a bath agent. 12. The manufacturing method according to claim 7, wherein the fused polycyclic aromatic compound has at least one element selected from oxygen, sulfur, and halogen in the molecule. 13 The adhesive contains at least one selected from sulfur and dinitronaphthalene before adhesion.
The manufacturing method according to claim 7, wherein a seed is added.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25771586A JPS63112147A (en) | 1986-10-30 | 1986-10-30 | Carbon and graphite bonding structure and manufacture thereof |
| US06/938,253 US4911983A (en) | 1985-12-10 | 1986-12-05 | Adhesion structures and method of producing the same |
| EP19860309562 EP0225802B1 (en) | 1985-12-10 | 1986-12-09 | Adhesion structures and method of producing the same |
| DE8686309562T DE3686561T2 (en) | 1985-12-10 | 1986-12-09 | ADHESIVE STRUCTURES AND METHOD FOR THE PRODUCTION THEREOF. |
| US07/460,620 US5017431A (en) | 1985-12-10 | 1990-01-03 | Adhesion structures and method of producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25771586A JPS63112147A (en) | 1986-10-30 | 1986-10-30 | Carbon and graphite bonding structure and manufacture thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63112147A JPS63112147A (en) | 1988-05-17 |
| JPH0531469B2 true JPH0531469B2 (en) | 1993-05-12 |
Family
ID=17310099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP25771586A Granted JPS63112147A (en) | 1985-12-10 | 1986-10-30 | Carbon and graphite bonding structure and manufacture thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63112147A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5322093B2 (en) * | 2007-03-29 | 2013-10-23 | 日立化成株式会社 | Plasma facing material and manufacturing method thereof |
| JP5011556B2 (en) | 2007-11-09 | 2012-08-29 | イビデン株式会社 | Carbon composite material |
| JP2013093447A (en) * | 2011-10-26 | 2013-05-16 | Toyo Tanso Kk | Heat radiation structure |
| JP6700068B2 (en) * | 2016-02-29 | 2020-05-27 | 株式会社アカネ | Bonding method of carbon sheet in multi-axis electrification sintering device |
-
1986
- 1986-10-30 JP JP25771586A patent/JPS63112147A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63112147A (en) | 1988-05-17 |
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