JPS6232152B2 - - Google Patents
Info
- Publication number
- JPS6232152B2 JPS6232152B2 JP57176215A JP17621582A JPS6232152B2 JP S6232152 B2 JPS6232152 B2 JP S6232152B2 JP 57176215 A JP57176215 A JP 57176215A JP 17621582 A JP17621582 A JP 17621582A JP S6232152 B2 JPS6232152 B2 JP S6232152B2
- Authority
- JP
- Japan
- Prior art keywords
- weight
- silicon nitride
- graphite
- refractory material
- high alumina
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 43
- 229910052751 metal Inorganic materials 0.000 claims description 43
- 239000002184 metal Substances 0.000 claims description 43
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 43
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 39
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 38
- 239000010439 graphite Substances 0.000 claims description 38
- 229910002804 graphite Inorganic materials 0.000 claims description 38
- 239000002245 particle Substances 0.000 claims description 38
- 239000000203 mixture Substances 0.000 claims description 31
- 238000002844 melting Methods 0.000 claims description 30
- 230000008018 melting Effects 0.000 claims description 30
- 239000011230 binding agent Substances 0.000 claims description 17
- 239000010419 fine particle Substances 0.000 claims description 15
- 239000000843 powder Substances 0.000 claims description 13
- 239000011362 coarse particle Substances 0.000 claims description 12
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims description 12
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 claims 2
- 239000011819 refractory material Substances 0.000 description 62
- 239000002893 slag Substances 0.000 description 22
- 230000003628 erosive effect Effects 0.000 description 21
- 230000035939 shock Effects 0.000 description 18
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 16
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 12
- 239000004927 clay Substances 0.000 description 10
- 229910052570 clay Inorganic materials 0.000 description 10
- 230000035515 penetration Effects 0.000 description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 7
- 229910001093 Zr alloy Inorganic materials 0.000 description 7
- 239000010949 copper Substances 0.000 description 7
- 229910052802 copper Inorganic materials 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 229910001096 P alloy Inorganic materials 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 238000002156 mixing Methods 0.000 description 6
- 239000000377 silicon dioxide Substances 0.000 description 6
- 235000012239 silicon dioxide Nutrition 0.000 description 6
- 229910000881 Cu alloy Inorganic materials 0.000 description 5
- XTYUEDCPRIMJNG-UHFFFAOYSA-N copper zirconium Chemical compound [Cu].[Zr] XTYUEDCPRIMJNG-UHFFFAOYSA-N 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000010304 firing Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- ILRRQNADMUWWFW-UHFFFAOYSA-K aluminium phosphate Chemical compound O1[Al]2OP1(=O)O2 ILRRQNADMUWWFW-UHFFFAOYSA-K 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 230000035699 permeability Effects 0.000 description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 229910052593 corundum Inorganic materials 0.000 description 3
- 239000010431 corundum Substances 0.000 description 3
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 3
- 229910052863 mullite Inorganic materials 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 239000012466 permeate Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 239000000376 reactant Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 229910052726 zirconium Inorganic materials 0.000 description 3
- 229910001369 Brass Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000004115 Sodium Silicate Substances 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- IDDKUWZJZGIPGE-UHFFFAOYSA-N [Cu].[P].[Zr] Chemical compound [Cu].[P].[Zr] IDDKUWZJZGIPGE-UHFFFAOYSA-N 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 239000007795 chemical reaction product Substances 0.000 description 2
- -1 ferrous metals Chemical class 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 2
- 229910052911 sodium silicate Inorganic materials 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 239000005751 Copper oxide Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910000431 copper oxide Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 229910021652 non-ferrous alloy Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Landscapes
- Ceramic Products (AREA)
- Compositions Of Oxide Ceramics (AREA)
Description
〔発明の利用分野〕
本発明は、1200℃以下の融点を有する非鉄金属
の溶解炉のライニングに使用する高アルミナ質不
焼成粉末組成物に係り、特に銅合金の溶解炉に用
いるのに好適な不焼成粉末組成物に関する。
〔従来技術〕
銅、黄銅、亜鉛、アルミニウムなどの非鉄金属
の溶解炉の炉材たとえば内張り材には、高アルミ
ナ質耐火材が用いられる。高アルミナ質耐火材
は、高アルミナ質骨材の粒子と結合剤とからな
る。高アルミナ質骨材は、酸化アルミニウムが60
重量%以上を占め、残りが主に二酸化珪素からな
る。
しかし、前記高アルミナ質耐火材は熱衝撃に弱
くしかもアルミニウム溶湯に接触した場合に反応
物を生成するという欠点がある。前記耐火材は熱
衝撃に弱いため銅或は銅合金の溶解炉に使用する
と、炉の冷却時に炉内面に亀裂が生じ、つぎの溶
解時にそこから炉内部へ溶湯が浸透する。炉内部
への溶湯の浸透によつて、浸透部と未浸透部との
間に熱膨張係数の差が生じ、炉の冷却時に浸透部
が剥離してしまう。誘導溶解炉においては、銅溶
湯の浸透によつてコイル短絡事故を生じることも
ある。
アルミニウム或はアルミニウム合金の溶解の場
合には、溶湯と耐火材とが反応し、反応生成物が
炉壁に付着して炉内面積を減少させる。更にアル
ミニウム合金溶湯の成分によつては、反応生成物
の一部が炉内部へ浸透し、炉壁の剥離をもたら
す。
本発明者は、先に前述の高アルミナ質耐火材中
へ窒化珪素を含有させることによつて、耐火材の
耐熱衝撃性を高め得ること及びアルミニウム溶湯
との反応を阻止できることを見出した。例えば特
開昭56−22675号公報参照。
〔発明の目的〕
本発明の目的は、前述の窒化珪素含有高アルミ
ナ質耐火材よりも、銅合金溶解時のスラグによる
侵食に強い非鉄金属溶解炉のライニング用高アル
ミナ質不焼成粉末組成物を提供するにある。
〔発明の概要〕
本発明は、高アルミナ質骨材の粒子と窒化珪素
粒子との混合物或は更に結合剤を含む混合物から
なる不焼成粉末組成物中に黒鉛の粒子を含有する
ものである。
本発明の高アルミナ質不焼成粉末組成物は、酸
化アルミニウムを60重量%以上含有する高アルミ
ナ質骨材と窒化珪素と黒鉛とからなり、且つ粒径
が1.2mm以上の粗粒と粒径が0.15〜1.2mm未満の中
間粒と粒径が0.15mm未満の微粒との混合物よりな
る粉末組成物であつて、窒化珪素を5〜25重量
%、黒鉛を3〜12重量%含有する。
アルミナ質骨材は粗粒が40〜70重量%と中間粒
が10〜30重量%と微粒が10〜40重量%とからな
る。
窒化珪素及び黒鉛は、中間粒と微粒からなる。
本発明の高アルミナ質不焼成粉末組成物は、
1200℃以下の融点を有する非鉄金属の溶解炉のラ
イニングすなわち内張り用耐火材として使用され
る。
本発明の耐火材は、銅―ジルコニウム合金或は
銅―ジルコニウム―リン合金などの銅―ジルコニ
ウム系合金の溶解炉に使用した場合に、先に開発
した耐火材よりも著しく高寿命を示現する。
本発明の耐火材は、先に開発した窒化珪素含有
耐火材と同じように熱衝撃にも強い。しかもアル
ミニウム合金の溶解に使用した場合に、溶湯と反
応物を生成しない。
本発明者は、高アルミナ質骨材粒子と窒化珪素
粒子との混合物からなる耐火材によつて作られた
溶解炉を用いて、数種類の銅合金を溶解している
うちに、次のことを発見した。銅―ジルコニウム
合金或は銅―ジルコニウム―リン合金などの銅―
ジルコニウム系合金を溶解すると、溶湯表面のス
ラグによつて炉壁が侵食されスラグ近傍の耐火材
が溶け落ちる。かかる侵食は銅―ジルコニウム系
合金の溶解においてCuOを主成分とするスラグ
が生成し、このスラグと耐火材中の主に二酸化珪
素とが反応して低融点の反応物を生成してスラグ
中に溶け込むことによつて起こることがわかつ
た。
従つて、窒化珪素含有高アルミナ質耐火材が
CuOを主成分とするスラグによつて侵食されな
いようにすることが必要になり、本発明の耐火材
を見出すに至つた。
高アルミナ質骨材と窒化珪素とを含む耐火材中
に、非鉄金属溶湯と反応して一酸化炭素を発生す
る固体物質たとえば黒鉛を含有することによつ
て、次の現象が生じる。この結果スラグ中の
CuOの量が減少してスラグによる耐火材の侵食
が抑制される。
(i) 耐火材中の黒鉛によつて、スラグ及び溶湯中
のCuOの一部が(1)式のように還元される。
CuO+C→Cu+CO ……(1)
(ii) 耐火材中の黒鉛が酸化して生じたCOが、(2)
式のようにスラグ及び溶湯中の残りのCuOの
一部を還元する。
CuO+CO→Cu+CO2 ……(2)
(iii) 黒鉛が酸化して生じたCOは、炉壁表面にCO
又はCO2からなるガス膜を形成し、溶湯と耐火
材とのぬれを妨げる。
本発明の各構成要件について説明する。
(イ) アルミナ質骨材
骨材には、酸化アルミニウムを60重量%以上含
むものを使用すべきである。骨材中の酸化アルミ
ニウム含有量が多くなると、それに伴つて二酸化
珪素の量が少なくなるために、CuOを主成分と
するスラグと耐火材との反応による生成物の量が
低減する。このため、耐火材の侵食作用が弱ま
る。
第1図は、高アルミナ質骨材中の酸化アルミニ
ウム量を変えたときに、CuOを主成分とするス
ラグによる耐火材の侵食率がどのように変化する
かをグラフで示したものである。骨材中の酸化ア
ルミニウムの量が多くなるほど侵食率が少なくな
ることが明らかである。骨材中の酸化アルミニウ
ムの量は、特に70重量%以上が望ましいことが明
らかである。実験は、耐火材に窒化珪素12重量
%、黒鉛5重量%、粘土10重量%、残り高アルミ
ナ質骨材からなるものを用いて行つた。高アルミ
ナ質骨材は、4.7〜1.2mmの粗粒と1.2mm未満〜0.15
mmの中間粒及び0.15mm未満の微粒からなり、粗粒
が骨材全体のおよび60重量%を占め、中間粒がお
よそ25重量%を占めている。
かかる耐火材によつて、外径50mmφ、高さ50mm
の円柱状を有し、中央に直径20mmφ、高さ30mmの
穴を有するるつぼを成型し、このるつぼを黒鉛る
つぼ中に入れ、大気の影響を受けないように周囲
を密閉して1200℃で焼成した。1200℃で焼成した
のは、溶解炉ライニング材として長時間使用後の
状態を模擬するためである。
この耐火材るつぼを用いて、銅―0.01重量%ジ
ルコニウム―0.01重量%リン合金を溶解し、2時
間保持したのち溶湯を除去して、るつぼを縦に真
二つに切り、スラグによる侵食率を次式によつて
求めた。なお、後述する侵食率の測定は、すべて
このようにして行つた。
侵食率(%)=(侵食によつて増大した穴の断面積)―(元の穴の断面積)/(元の穴の断面積)×100
高アルミナ質骨材は、電融法或は焼成法等によ
つて得ることができる。焼成法によつて得られた
骨材は、電融法によつて得られた骨材にくらべて
耐熱衝撃性及び焼結性がすぐれる。電融法によつ
て得られた骨材は、焼成法によつて得られた骨材
にくらべてCuOを主成分とするスラグによる耐
侵食性がすぐれる。従つて、両方を混合して用い
ることが望ましい。
酸化アルミニウムを70重量%以上含む骨材とし
ては、ムライト或はコランダムがある。酸化アル
ミニウム量が少ないシヤモツトを用いる場合に
は、コランダム或はムライトと混合して酸化アル
ミニウム量を60重量%以上とすることが望まし
い。
高アルミナ質骨材の粒度構成によつて、耐火材
の耐熱衝撃性、強度、溶湯による浸透性、侵食性
などが影響を受ける。高アルミナ質骨材は、粒径
1.2mm以上の粗粒と、1.2mm未満〜0.15mmの中間粒
及び粒径0.15mm未満の微粒からなることが望まし
い。耐火材の強度たとえば圧縮強度を高めるには
粗粒を用いる必要がある。耐熱衝撃性を高めるう
えでも粗粒は必要である。しかし、粗粒だけでは
空隙が多くなり緻密なものが得られないので強度
も小さく溶湯が浸透しやすく、溶湯により物理的
に溶損する傾向が大きい。微粒を混ぜることによ
つて、耐火材の組織を強化し、強度を増し、溶湯
の浸透、侵食を防止することができる。しかし、
粗粒と微粒だけでは耐熱衝撃性が不十分で、耐侵
食性も十分ではない。中間粒を混入することによ
つて、これらの欠点を補うことができる。高アル
ミナ質骨材に占める粗粒、中間粒及び微粒の量
は、夫々粗粒40〜70重量%、中間粒10〜30重量
%、微粒10〜40重量%が望ましい。粗粒の大きさ
は4.7mm以下が望ましい。
(ロ) 窒化珪素
窒化珪素を含むことによつて、耐火材の耐熱衝
撃性が高まり、炉の冷却時にクラツクが入りにく
くなる。更にアルミニウム或はアルミニウム合金
溶湯と耐火材とが反応しにくくなる。
窒化珪素としては、Si3N4を用いることが望ま
しい。
窒化珪素の粒子の大きさは、空隙の少ない緻密
な耐火材が得られるようにするために、なるべく
小さくすることが望ましい。粒径0.15mm未満の微
粒とすることが望ましい。窒化珪素の粒径は、最
大でも1.2mm未満とすることが望ましく、粒径
0.15mm未満の粒子が窒化珪素全量の80重量%以上
を占めるようにすることが望ましい。
第2〜7図のグラフは、耐火材中の窒化珪素の
量によつて、溶湯の浸透率、スラグによる耐火材
の侵食率、耐火材の圧縮強度及び耐熱衝撃性がど
のように変わるかを示したものである。
耐火材の構成は、高アルミナ質骨材、窒化珪
素、黒鉛及び粘土からなる。粘土の量は10重量%
一定とし、黒鉛の量は3,5,10重量%と変化さ
せた。高アルミナ質骨材の粗粒と中間粒と微粒の
比率は、粗粒がおよそ60重量%、中間粒がおよそ
25重量%、残りが微粒である。窒化珪素には
Si3N4からなる粒径0.15mm未満の微粒を用いた。
黒鉛にも粒径0.15mm未満の微粒を用いた。溶湯成
分は、銅―0.01重量%ジルコニウム―0.01重量%
リン合金である。
溶湯の浸透率は、るつぼの穴のまわりに溶湯お
よびスラグが浸透した層ができるので、るつぼを
縦断したときに浸透層の断面積を測り、これをる
つぼの元の穴の断面積で割つて求める。浸透率の
測定は以後すべてこのようにして行つた。
第2図は、黒鉛を5重量%含有する耐火材の溶
湯浸透率を示している。窒化珪素量が5〜20重量
%のときに浸透率が最も少なく、20重量%を超え
ると浸透率が増加する傾向にある。窒化珪素量
は、最大でも25重量%とすることが望ましい。
第3図は、黒鉛量を3,5,10重量%とし、窒
化珪素の量を変えたときに溶湯浸透率がどのよう
に変化するかを示している。いずれの黒鉛量のと
きも、窒化珪素の量が5〜20重量%であれば、溶
湯の浸透防止に対し顕著な効果を発揮することが
確認された。
第4図は、黒鉛量を5重量%とした耐火材につ
いて、窒化珪素量とスラグによる侵食率との関係
を示している。第5図は黒鉛量を3,5,10重量
%と変えた耐火材について、窒化珪素量とスラグ
による侵食率との関係を示している。CuOを主
成分とするスラグによる侵食を防止するには、窒
化珪素の量を10重量%前後、具体的には7〜12重
量%にすることが好適である。
第6図は、黒鉛量を5重量%とした耐火材の焼
成後の圧縮強さと窒化珪素量との関係を示し、第
7図はかかる耐火材を熱衝撃試験したときのクラ
ツク発生に至る衝撃回数と窒化珪素量との関係を
示している。試験片の形状は、いずれも直径50mm
φ、長さ50mmの丸棒である。溶解炉ライニングが
溶湯にさらされることを想定して予め焼成し、焼
成温度は1000℃、1200℃及び1400℃とした。熱衝
撃試験は、1200℃で焼成した丸棒について行つ
た。熱衝撃試験は、丸棒を加熱炉に入れて1200℃
の温度に15分間加熱保持したのち炉から取り出し
て水中に投入する操作をくり返すことによつて行
つた。圧縮強さ及び耐熱衝撃性の点からは、窒化
珪素量は7〜15重量%が望ましいことが明らかに
なつた。
(ハ) 黒鉛
炉の内張り耐火材に黒鉛を含有させることによ
つて、銅―ジルコニウム系合金溶湯中のCuOの
量が少なくなり、CuOを主成分とするスラグの
生成量が少なくなつて耐火材の侵食が抑えられ
る。黒鉛は、耐火材と溶湯との間にガス膜を形成
するので、耐火材が溶湯にぬれにくくなる。
黒鉛の量は、第8図から明らかなように3〜12
重量%が望ましく、特に5〜10重量%が適当であ
る。
第8図は、窒化珪素の量を10重量%、粘結剤と
しての粘土の量を10重量%とし、黒鉛の量を変化
させた耐火材製るつぼを用いて銅―0.01重量%ジ
ルコニウム―0.01重量%リン合金を溶解したとき
のスラグによる侵食率を示したものである。黒鉛
量が少なすぎても又多すぎても侵食率が増大する
ことが明らかである。
黒鉛には、粒径1.2mm未満の粒子を用いること
が望ましく、特に粒径1.2未満〜0.15mmの粒子と
粒径0.15mm未満の粒子との混合物を用いることが
望ましい。混合の割合は、0.15mm未満の粒子を40
〜80重量%とするのがよい。黒鉛は、溶湯と反応
し酸化して消失する。この結果、黒鉛粒子が存在
したところは、のちに空隙として残る。したがつ
て空隙の大きさが大きいと、耐火材の強度が低下
する。更に溶湯との接触面積が増加するので、溶
湯が浸透しやすくなる。
他方、黒鉛の大きさが小さすぎると、溶湯と反
応する前に大気中の酸素と反応して消失しやす
い。従つて、粒径1.2mm未満の中間粒及び微粒を
用い且つ中間粒と微粒を混ぜて用いることが望ま
しい。
黒鉛としては、土状黒鉛及び鱗片状黒鉛がある
が、どちらも使用できる。
(ニ) 粘結剤
高アルミナ質耐火材は、骨材の微粒が一種の粘
結剤として作用するので、粘結剤を含まなくても
成形できる。しかし、粘結剤を入れた方が成形し
やすく成形後の強度も大きい。
粘結剤には、無機質の粘土、珪酸ナトリウム、
モノリン酸アルミニウムなどあるいはパルプ廃液
などの有機質のものを用いることができる。粘土
が最も望ましい。粘結剤の量は、0.05〜15重量%
が望ましく、粘土を用いるときには7〜12重量%
が特に望ましい。珪酸ナトリウム、モノリン酸ア
ルミニウム、パルプ廃液などの粘結剤を用いると
きには0.05〜5重量%が望ましい。粘土粒径は、
十分な粘結力を発揮させるために、0.15mm未満の
微粒を用いることが望ましい。
(ホ) 耐火材の使用方法
本発明の耐火材は、焼成せずに用いる。
焼成しないで用いる方法としては、たとえば耐
火材の各粒子の混合物に粘結性を高めるために若
干の水を加え、溶解炉の所定の箇所に装填してエ
アーランマー等でつき固める方法がある。混合物
を予め所定の形状に成形し、乾燥させてから溶解
炉の所定の箇所にはめ込むようにしてもよい。
本発明の耐火材は、1200℃以下の融点を有する
非鉄金属の溶解炉に適用される。本発明の耐火材
で作られた溶解炉を1200℃以上の温度で使用する
と、耐火材中の窒化珪素が急速に酸化して、二酸
化珪素SiO2に変換する。変換した二酸化珪素は
溶湯と反応し、かえつて炉壁の剥離及び溶湯の浸
透をもたらす原因となる。1200℃以下の温度で使
用すれば、窒化珪素の酸化に基づく炉壁の剥離等
は生ぜず、窒化珪素による耐熱衝撃性の改善及び
アルミニウム溶湯との反応防止の効果が有効に発
揮される。
本発明の耐火材によつて作られた溶解炉で溶解
される非鉄合金中には、合金成分として鉄が含ま
れていてもかまわない。
耐火材全体に占める粗粒、中間粒及び微粒の量
は、それぞれ粗粒40〜50重量%、中間粒15〜25重
量%、微粒30〜45重量%が望ましい。
〔発明の実施例〕
第1表に示すように、10種類の耐火材によつて
るつぼ及び丸棒を作つた。高アルミナ質骨材には
電融ムライトと電融コランダムを混合して用い
た。アルミナ質骨材、窒化珪素及び粘土の化学組
成は、第2表の通りである。高アルミナ質骨材の
粗粒の大きさは4.7〜1.2mmとした。
本発明の実施例は試料No.1〜9である。これら
のうち試料No.1〜6は粘結剤として粘土を含む。
No.7とNo.8は粘結剤としてモノリン酸アルミニウ
ムを含む。No.9は粘結剤を含まない。No.10は、従
来例であり、黒鉛を含まない。
[Field of Application of the Invention] The present invention relates to a high alumina unfired powder composition used for lining a melting furnace for non-ferrous metals having a melting point of 1200°C or less, and particularly suitable for use in a melting furnace for copper alloys. The present invention relates to an unfired powder composition. [Prior Art] High alumina refractory materials are used for furnace materials, such as lining materials, in furnaces for melting nonferrous metals such as copper, brass, zinc, and aluminum. High alumina refractories consist of particles of high alumina aggregate and a binder. High alumina aggregate has aluminum oxide of 60%
% by weight or more, and the remainder mainly consists of silicon dioxide. However, the high alumina refractory material has drawbacks in that it is weak against thermal shock and generates reactants when it comes into contact with molten aluminum. Since the refractory material is susceptible to thermal shock, when used in a furnace for melting copper or copper alloys, cracks occur on the inner surface of the furnace when the furnace is cooled, and molten metal permeates into the interior of the furnace from there during the next melting process. As the molten metal permeates into the furnace, a difference in coefficient of thermal expansion occurs between the permeated part and the unpermeated part, and the permeated part peels off when the furnace is cooled. In induction melting furnaces, coil short circuit accidents may occur due to penetration of molten copper. In the case of melting aluminum or an aluminum alloy, the molten metal and the refractory material react, and reaction products adhere to the furnace wall, reducing the area inside the furnace. Furthermore, depending on the composition of the molten aluminum alloy, some of the reaction products may penetrate into the interior of the furnace, resulting in peeling of the furnace wall. The present inventors have previously discovered that by incorporating silicon nitride into the above-mentioned high alumina refractory material, the thermal shock resistance of the refractory material can be improved and the reaction with molten aluminum can be prevented. For example, see Japanese Patent Application Laid-Open No. 56-22675. [Object of the Invention] The object of the present invention is to provide a high alumina unfired powder composition for lining a nonferrous metal melting furnace that is more resistant to erosion by slag during copper alloy melting than the silicon nitride-containing high alumina refractory material described above. It is on offer. [Summary of the Invention] The present invention contains graphite particles in an unfired powder composition consisting of a mixture of high alumina aggregate particles and silicon nitride particles, or a mixture further containing a binder. The high alumina unfired powder composition of the present invention is composed of high alumina aggregate containing 60% by weight or more of aluminum oxide, silicon nitride, and graphite, and coarse particles with a particle size of 1.2 mm or more and coarse particles with a particle size of 1.2 mm or more. A powder composition consisting of a mixture of intermediate grains with a diameter of 0.15 to less than 1.2 mm and fine grains with a grain size of less than 0.15 mm, and contains 5 to 25% by weight of silicon nitride and 3 to 12% by weight of graphite. The alumina aggregate consists of 40 to 70% by weight of coarse particles, 10 to 30% by weight of medium particles, and 10 to 40% by weight of fine particles. Silicon nitride and graphite consist of intermediate grains and fine grains. The high alumina unfired powder composition of the present invention is
Used as a refractory material for the lining of melting furnaces for nonferrous metals with a melting point of 1200°C or less. The refractory material of the present invention exhibits a significantly longer service life than previously developed refractory materials when used in a melting furnace for copper-zirconium alloys such as copper-zirconium alloys or copper-zirconium-phosphorus alloys. The refractory material of the present invention is resistant to thermal shock, similar to the previously developed silicon nitride-containing refractory material. Moreover, when used for melting aluminum alloy, it does not generate any reactants with the molten metal. The present inventor discovered the following while melting several types of copper alloys using a melting furnace made of a refractory material made of a mixture of high alumina aggregate particles and silicon nitride particles. discovered. Copper such as copper-zirconium alloy or copper-zirconium-phosphorus alloy
When a zirconium alloy is melted, the furnace wall is eroded by the slag on the surface of the molten metal, and the refractory material near the slag melts away. This corrosion is caused by the formation of slag containing CuO as the main component when copper-zirconium alloys are melted, and this slag reacts with silicon dioxide, which is mainly present in the refractory material, to produce low-melting-point reactants. I found out that this happens by blending in. Therefore, high alumina refractory materials containing silicon nitride are
It became necessary to prevent corrosion by slag whose main component is CuO, and this led to the discovery of the refractory material of the present invention. The following phenomenon occurs when a refractory material containing high alumina aggregate and silicon nitride contains a solid substance, such as graphite, which reacts with molten nonferrous metal to generate carbon monoxide. This results in
The amount of CuO is reduced and the erosion of the refractory material by slag is suppressed. (i) A portion of CuO in the slag and molten metal is reduced by the graphite in the refractory material as shown in equation (1). CuO+C→Cu+CO ……(1) (ii) CO generated by oxidation of graphite in the refractory material is (2)
Part of the remaining CuO in the slag and molten metal is reduced as shown in the formula. CuO+CO→Cu+CO 2 ……(2) (iii) CO generated by oxidation of graphite is deposited on the furnace wall surface.
Alternatively, a gas film consisting of CO 2 is formed, which prevents wetting of the molten metal and the refractory material. Each component of the present invention will be explained. (b) Alumina aggregate Aggregates containing at least 60% by weight of aluminum oxide should be used. As the aluminum oxide content in the aggregate increases, the amount of silicon dioxide decreases, and therefore the amount of products from the reaction between CuO-based slag and refractory material decreases. Therefore, the erosion effect of the refractory material is weakened. Figure 1 is a graph showing how the rate of erosion of refractory materials by slag containing CuO as the main component changes when the amount of aluminum oxide in high alumina aggregate is changed. It is clear that the higher the amount of aluminum oxide in the aggregate, the lower the erosion rate. It is clear that the amount of aluminum oxide in the aggregate is preferably 70% by weight or more. The experiment was conducted using a refractory material consisting of 12% by weight silicon nitride, 5% by weight graphite, 10% by weight clay, and the remainder high alumina aggregate. High alumina aggregate has coarse grains from 4.7 to 1.2 mm and less than 1.2 mm to 0.15
It consists of medium grains of mm and fine grains of less than 0.15 mm, with coarse grains accounting for 60% by weight of the total aggregate, and medium grains accounting for approximately 25% by weight. Due to the fireproof material, the outer diameter is 50mmφ and the height is 50mm.
A crucible with a cylindrical shape and a hole with a diameter of 20 mmφ and a height of 30 mm in the center is molded, this crucible is placed in a graphite crucible, the surrounding area is sealed to prevent it from being affected by the atmosphere, and the crucible is fired at 1200℃. did. The reason for firing at 1200℃ was to simulate the condition after long-term use as a melting furnace lining material. Using this refractory crucible, a copper-0.01% by weight zirconium-0.01% by weight phosphorus alloy was melted, held for 2 hours, the molten metal was removed, and the crucible was cut lengthwise into two to reduce the corrosion rate due to slag. It was calculated using the following formula. Note that all measurements of the erosion rate described below were performed in this manner. Erosion rate (%) = (Cross-sectional area of the hole increased by erosion) - (Cross-sectional area of the original hole) / (Cross-sectional area of the original hole) x 100 High alumina aggregate is It can be obtained by a calcination method or the like. Aggregates obtained by the firing method have better thermal shock resistance and sinterability than aggregates obtained by the electrofusion method. Aggregates obtained by the electrofusion method have superior erosion resistance due to slag containing CuO as a main component, compared to aggregates obtained by the sintering method. Therefore, it is desirable to use a mixture of both. Examples of aggregates containing 70% by weight or more of aluminum oxide include mullite and corundum. When using chamotu with a small amount of aluminum oxide, it is desirable to mix it with corundum or mullite to make the amount of aluminum oxide 60% by weight or more. The particle size structure of high alumina aggregate affects the thermal shock resistance, strength, permeability by molten metal, erosion resistance, etc. of the refractory material. High alumina aggregate has a particle size of
It is desirable to consist of coarse particles of 1.2 mm or more, intermediate particles of less than 1.2 mm to 0.15 mm, and fine particles of less than 0.15 mm in diameter. In order to increase the strength of the refractory material, such as compressive strength, it is necessary to use coarse particles. Coarse particles are also necessary to improve thermal shock resistance. However, if only coarse particles are used, there will be many voids and a dense product cannot be obtained, so the strength is low and the molten metal easily penetrates, and there is a strong tendency to be physically eroded by the molten metal. By mixing fine particles, it is possible to strengthen the structure of the refractory material, increase its strength, and prevent penetration and erosion of molten metal. but,
Coarse particles and fine particles alone do not provide sufficient thermal shock resistance or corrosion resistance. These drawbacks can be compensated for by mixing intermediate grains. The amounts of coarse grains, medium grains, and fine grains in the high alumina aggregate are preferably 40 to 70% by weight of coarse grains, 10 to 30% by weight of medium grains, and 10 to 40% by weight of fine grains, respectively. The size of coarse particles is preferably 4.7 mm or less. (b) Silicon nitride By containing silicon nitride, the thermal shock resistance of the refractory material increases, making it difficult for cracks to occur during cooling of the furnace. Furthermore, it becomes difficult for aluminum or molten aluminum alloy to react with the refractory material. As silicon nitride, it is desirable to use Si 3 N 4 . It is desirable that the size of the silicon nitride particles be as small as possible in order to obtain a dense refractory material with few voids. It is desirable to use fine particles with a particle size of less than 0.15 mm. It is desirable that the particle size of silicon nitride is less than 1.2 mm at most;
It is desirable that particles smaller than 0.15 mm account for 80% by weight or more of the total amount of silicon nitride. The graphs in Figures 2 to 7 show how the penetration rate of molten metal, the rate of erosion of the refractory material by slag, the compressive strength and thermal shock resistance of the refractory material change depending on the amount of silicon nitride in the refractory material. This is what is shown. The composition of the refractory material consists of high alumina aggregate, silicon nitride, graphite and clay. The amount of clay is 10% by weight
The amount of graphite was kept constant and varied to 3, 5, and 10% by weight. The ratio of coarse grains, medium grains, and fine grains in high alumina aggregate is approximately 60% by weight for coarse grains and approximately 60% by weight for medium grains.
25% by weight, the rest being fine particles. For silicon nitride
Fine particles made of Si 3 N 4 and having a particle size of less than 0.15 mm were used.
Fine particles with a particle size of less than 0.15 mm were also used for graphite. Molten metal components: Copper - 0.01% by weight Zirconium - 0.01% by weight
It is a phosphorus alloy. The permeation rate of molten metal is determined by measuring the cross-sectional area of the permeated layer when the crucible is cut lengthwise, and dividing this by the cross-sectional area of the original hole in the crucible, since a layer of molten metal and slag permeates around the hole in the crucible. demand. All subsequent measurements of permeability were performed in this manner. FIG. 2 shows the molten metal penetration rate of a refractory material containing 5% by weight of graphite. When the amount of silicon nitride is 5 to 20% by weight, the permeability is the lowest, and when it exceeds 20% by weight, the permeability tends to increase. The amount of silicon nitride is desirably 25% by weight at most. Figure 3 shows how the molten metal penetration rate changes when the amount of graphite is 3, 5, and 10% by weight and the amount of silicon nitride is changed. It has been confirmed that for any amount of graphite, if the amount of silicon nitride is 5 to 20% by weight, a remarkable effect is exhibited in preventing penetration of molten metal. FIG. 4 shows the relationship between the amount of silicon nitride and the rate of erosion by slag for a refractory material containing 5% by weight of graphite. Figure 5 shows the relationship between the amount of silicon nitride and the rate of erosion by slag for refractory materials with varying amounts of graphite of 3, 5, and 10% by weight. In order to prevent erosion by slag containing CuO as a main component, it is preferable that the amount of silicon nitride be around 10% by weight, specifically 7 to 12% by weight. Figure 6 shows the relationship between the compressive strength after firing and the amount of silicon nitride of a refractory material with a graphite content of 5% by weight, and Figure 7 shows the impact that leads to cracking when such a refractory material is subjected to a thermal shock test. The relationship between the number of times and the amount of silicon nitride is shown. The shape of the test piece is 50mm in diameter.
It is a round bar with a diameter of 50 mm and a length of 50 mm. The melting furnace lining was fired in advance assuming that it would be exposed to the molten metal, and the firing temperatures were set at 1000°C, 1200°C, and 1400°C. Thermal shock tests were conducted on round bars fired at 1200°C. In the thermal shock test, a round bar is placed in a heating furnace and heated to 1200℃.
This was carried out by repeatedly heating and maintaining the temperature for 15 minutes, then taking it out of the furnace and putting it into water. From the viewpoint of compressive strength and thermal shock resistance, it has become clear that the amount of silicon nitride is desirably 7 to 15% by weight. (c) Graphite By including graphite in the refractory lining of the furnace, the amount of CuO in the molten copper-zirconium alloy decreases, and the amount of slag that is mainly composed of CuO is reduced, resulting in a refractory material. erosion is suppressed. Graphite forms a gas film between the refractory material and the molten metal, making it difficult for the refractory material to wet the molten metal. As is clear from Figure 8, the amount of graphite is 3 to 12
% by weight is preferred, particularly 5 to 10% by weight. Figure 8 shows that using a refractory crucible in which the amount of silicon nitride was 10% by weight, the amount of clay as a binder was 10% by weight, and the amount of graphite was varied, copper - 0.01% by weight, zirconium - 0.01%. This figure shows the corrosion rate due to slag when a weight percent phosphorus alloy is melted. It is clear that if the amount of graphite is too small or too large, the erosion rate will increase. For graphite, it is desirable to use particles with a particle size of less than 1.2 mm, and it is particularly desirable to use a mixture of particles with a particle size of less than 1.2 to 0.15 mm and particles with a particle size of less than 0.15 mm. The mixing ratio is 40 to 40 particles less than 0.15mm
It is preferable to set it to 80% by weight. Graphite reacts with the molten metal, oxidizes, and disappears. As a result, the areas where graphite particles were present remain as voids. Therefore, when the size of the voids is large, the strength of the refractory material decreases. Furthermore, since the contact area with the molten metal increases, the molten metal can more easily penetrate. On the other hand, if the graphite is too small, it is likely to react with oxygen in the atmosphere and disappear before reacting with the molten metal. Therefore, it is desirable to use intermediate particles and fine particles with a particle size of less than 1.2 mm, and to use a mixture of intermediate particles and fine particles. Graphite includes earthy graphite and flaky graphite, both of which can be used. (d) Binder High alumina refractory materials can be molded without the use of a binder, as fine aggregate particles act as a kind of binder. However, adding a binder makes it easier to mold and provides greater strength after molding. Binding agents include inorganic clay, sodium silicate,
Organic substances such as aluminum monophosphate or pulp waste liquid can be used. Clay is most preferred. The amount of binder is 0.05-15% by weight
is desirable, and when using clay, it is 7 to 12% by weight.
is particularly desirable. When using a binder such as sodium silicate, aluminum monophosphate, or pulp waste liquid, the amount is preferably 0.05 to 5% by weight. The clay particle size is
In order to exhibit sufficient caking power, it is desirable to use fine particles less than 0.15 mm. (e) How to use the refractory material The refractory material of the present invention is used without being fired. As a method for using the material without firing, for example, there is a method in which a small amount of water is added to a mixture of particles of the refractory material in order to increase the caking property, and the mixture is loaded into a predetermined place in a melting furnace and compacted with an air rammer or the like. The mixture may be formed into a predetermined shape in advance, dried, and then fitted into a predetermined position in the melting furnace. The refractory material of the present invention is applied to a melting furnace for non-ferrous metals having a melting point of 1200°C or lower. When a melting furnace made of the refractory material of the present invention is used at a temperature of 1200°C or higher, the silicon nitride in the refractory material is rapidly oxidized and converted to silicon dioxide SiO2 . The converted silicon dioxide reacts with the molten metal, causing peeling of the furnace wall and penetration of the molten metal. If used at a temperature of 1200° C. or lower, peeling of the furnace wall due to oxidation of silicon nitride will not occur, and the effect of improving thermal shock resistance and preventing reaction with molten aluminum by silicon nitride will be effectively exhibited. The non-ferrous alloy melted in the melting furnace made of the refractory material of the present invention may contain iron as an alloy component. The amounts of coarse particles, intermediate particles, and fine particles in the entire refractory material are preferably 40 to 50% by weight of coarse particles, 15 to 25% by weight of intermediate particles, and 30 to 45% by weight of fine particles, respectively. [Embodiments of the Invention] As shown in Table 1, crucibles and round bars were made from 10 types of refractory materials. A mixture of fused mullite and fused corundum was used as the high alumina aggregate. The chemical compositions of the alumina aggregate, silicon nitride, and clay are shown in Table 2. The coarse grain size of the high alumina aggregate was 4.7 to 1.2 mm. Examples of the present invention are samples Nos. 1-9. Among these, Samples Nos. 1 to 6 contain clay as a binder.
Nos. 7 and 8 contain aluminum monophosphate as a binder. No. 9 does not contain a binder. No. 10 is a conventional example and does not contain graphite.
【表】【table】
【表】
No.7とNo.8の耐火材は、粘結剤を除く原料を所
定量配合し、モノリン酸アルミニウム溶液を添
加、混合し成型して作つた。このため粘結剤を混
合しないときの組成を100%として表してある。
耐火材の圧縮強さ及び熱衝撃試験結果を第3表
に示す。試験は、成形した丸棒が溶湯にさらされ
た状態を想定して予め焼成したものについて実施
した。第3表中、20回剥落0は熱衝撃を20回くり
返したが、耐火材が剥落しなかつたことを示して
いる。[Table] Refractory materials No. 7 and No. 8 were made by blending specified amounts of raw materials excluding a binder, adding an aluminum monophosphate solution, mixing, and molding. Therefore, the composition without a binder is expressed as 100%. Table 3 shows the compressive strength and thermal shock test results of the refractory materials. The test was conducted on a molded round bar that had been fired in advance, assuming that it would be exposed to molten metal. In Table 3, 0 flaking after 20 times indicates that the refractory material did not flake off even though the thermal shock was repeated 20 times.
【表】【table】
【表】
粘結剤を含むものは、含まないものにくらべて
圧縮強さが高い。圧縮強さは、黒鉛の有無による
影響を殆ど受けない。
試料No.1〜10の耐火材で作つたるつぼを用い
て、酸化銅、銅―0.01重量%ジルコニウム合金、
銅―0.01重量%ジルコニウム―0.01重量%リン合
金及び黄銅(亜鉛量28重量%)の溶解を行い、ス
ラグによる侵食率及び溶湯の浸透率を求めた。結
果を第4表に示す。酸化銅(CuO)の溶解を行
つたのは、耐火材がCuOによつてどのくらい侵
食されるかを調べるためである。[Table] Products containing a binder have higher compressive strength than those without. Compressive strength is hardly affected by the presence or absence of graphite. Using crucibles made of refractory materials of samples No. 1 to 10, copper oxide, copper-0.01% by weight zirconium alloy,
Copper - 0.01% by weight zirconium - 0.01% by weight phosphorus alloy and brass (zinc content: 28% by weight) were melted, and the erosion rate by slag and the penetration rate of the molten metal were determined. The results are shown in Table 4. The purpose of dissolving copper oxide (CuO) was to examine the extent to which refractory materials are eroded by CuO.
【表】【table】
以上の説明から明らかなように、本発明の耐火
材は銅合金溶解時のスラグによつて侵食されにく
いという効果を有する。
As is clear from the above description, the refractory material of the present invention has the effect of being less likely to be corroded by slag during melting of the copper alloy.
第1図は高アルミナ質骨材中の酸化アルミニウ
ム量と侵食率との関係を示すグラフ、第2図及び
第3図は窒化珪素量と溶湯浸透率との関係を示す
グラフ、第4図及び第5図は、窒化珪素量と侵食
率との関係を示すグラフ、第6図は、窒化珪素量
と圧縮強さとの関係を示すグラフ、第7図は、熱
衝撃試験におけるクラツク発生までの衝撃回数と
窒化珪素量との関係を示すグラフ、第8図は、黒
鉛量と侵食率との関係を示すグラフである。
Figure 1 is a graph showing the relationship between the amount of aluminum oxide in high alumina aggregate and the erosion rate, Figures 2 and 3 are graphs showing the relationship between the amount of silicon nitride and the molten metal penetration rate, and Figures 4 and Figure 5 is a graph showing the relationship between the amount of silicon nitride and the erosion rate, Figure 6 is a graph showing the relationship between the amount of silicon nitride and compressive strength, and Figure 7 is the impact required to generate a crack in a thermal shock test. A graph showing the relationship between the number of times and the amount of silicon nitride, and FIG. 8 is a graph showing the relationship between the amount of graphite and the erosion rate.
Claims (1)
アルミナ質骨材と窒化珪素と黒鉛とからなり、且
つ粒径が1.2mm以上の粗粒と粒径が0.15〜1.2mm未
満の中間粒と粒径が0.15mm未満の微粒との混合物
よりなる粉末組成物であつて、アルミナ質骨材は
粗粒が40〜70重量%と中間粒が10〜30重量%と微
粒が10〜40重量%からなり、窒化珪素及び黒鉛は
中間粒と微粒からなり、窒化珪素を混合物全体の
5〜25重量%、黒鉛を混合物全体の3〜12重量%
含み、1200℃以下の融点を有する非鉄金属の溶解
炉のライニングに用いられることを特徴とする非
鉄金属溶解炉のライニング用高アルミナ質不焼成
粉末組成物。 2 特許請求の範囲第1項において、前記窒化珪
素は、微粒を80重量%以上含むことを特徴とする
非鉄金属溶解炉のライニング用高アルミナ質不焼
成粉末組成物。 3 特許請求の範囲第1項において、前記黒鉛
は、微粒を40〜80重量%含むことを特徴とする非
鉄金属溶解炉のライニング用高アルミナ質不焼成
粉末組成物。 4 特許請求の範囲第1項において、前記粉末組
成物が結合剤を0.05〜15重量%含むことを特徴と
する非鉄金属溶解炉のライニング用高アルミナ質
不焼成粉末組成物。[Claims] 1. Consisting of high alumina aggregate containing 60% by weight or more of aluminum oxide, silicon nitride, and graphite, coarse particles with a particle size of 1.2 mm or more and particles with a particle size of 0.15 to less than 1.2 mm. It is a powder composition consisting of a mixture of medium grains and fine grains with a particle size of less than 0.15 mm, and the alumina aggregate contains 40 to 70% by weight of coarse grains, 10 to 30% by weight of medium grains, and 10 to 10% by weight of fine grains. Silicon nitride and graphite consist of intermediate grains and fine grains, silicon nitride is 5-25% by weight of the entire mixture, and graphite is 3-12% by weight of the entire mixture.
A high alumina unfired powder composition for lining a non-ferrous metal melting furnace, characterized in that it is used for lining a non-ferrous metal melting furnace having a melting point of 1200° C. or lower. 2. The high alumina unfired powder composition for lining a nonferrous metal melting furnace according to claim 1, wherein the silicon nitride contains 80% by weight or more of fine particles. 3. The high alumina unfired powder composition for lining a nonferrous metal melting furnace according to claim 1, wherein the graphite contains 40 to 80% by weight of fine particles. 4. The high alumina unfired powder composition for lining a nonferrous metal melting furnace according to claim 1, wherein the powder composition contains 0.05 to 15% by weight of a binder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57176215A JPS5969469A (en) | 1982-10-08 | 1982-10-08 | High alumina unfired powder composition for lining nonferrous metal melting furnaces |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57176215A JPS5969469A (en) | 1982-10-08 | 1982-10-08 | High alumina unfired powder composition for lining nonferrous metal melting furnaces |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5969469A JPS5969469A (en) | 1984-04-19 |
| JPS6232152B2 true JPS6232152B2 (en) | 1987-07-13 |
Family
ID=16009628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57176215A Granted JPS5969469A (en) | 1982-10-08 | 1982-10-08 | High alumina unfired powder composition for lining nonferrous metal melting furnaces |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5969469A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02120466A (en) * | 1988-10-26 | 1990-05-08 | Iwataro Moriyama | Multilevel parking apparatus |
-
1982
- 1982-10-08 JP JP57176215A patent/JPS5969469A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02120466A (en) * | 1988-10-26 | 1990-05-08 | Iwataro Moriyama | Multilevel parking apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5969469A (en) | 1984-04-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS62207771A (en) | Heat insulative composition and manufacture of formed body therefrom | |
| US5856251A (en) | Castable refractory for slide gate | |
| JP2986785B1 (en) | Castable refractory and refractory brick using the same | |
| US4608353A (en) | High-alumina refractory for use in non-ferrous metal melting furnace | |
| JPS6232152B2 (en) | ||
| CN116867753B (en) | Castable refractory | |
| JP2000103684A (en) | Castable refractory and firebrick using the same | |
| JP2556416B2 (en) | Casting material for blast furnace gutter | |
| KR910002576B1 (en) | High alumina refractories for non-ferric metal melting furnace | |
| JPH02221164A (en) | Castable refractory containing silicon carbide | |
| JPS6152099B2 (en) | ||
| KR910005026B1 (en) | Graphitic refractories and preparation method thereof | |
| KR830001463B1 (en) | Manufacturing method of fire brick | |
| JP2000191364A (en) | Magnesia chrome refractories | |
| JPH05117043A (en) | Dry ramming refractory for induction furnace | |
| US3410930A (en) | Method of improving the operation of a cupola | |
| JP2024070352A (en) | Unshaped refractories for molten aluminum | |
| JP3238592B2 (en) | Irregular cast refractory moldings | |
| GB1564927A (en) | Bonds for refractory materials | |
| JP2872670B2 (en) | Irregular refractories for lining of molten metal containers | |
| KR100473111B1 (en) | Amorphous refractory materials for casting and molten steel containers | |
| JPH0244069A (en) | Basic cast refractories | |
| JP2552980B2 (en) | Alumina-magnesia cast refractory | |
| JPH07291710A (en) | Graphite-containing refractory brick | |
| JPS6024072B2 (en) | Blast furnace gutter material |