JPH01305849A - Magnesia-carbon brick - Google Patents
Magnesia-carbon brickInfo
- Publication number
- JPH01305849A JPH01305849A JP63135298A JP13529888A JPH01305849A JP H01305849 A JPH01305849 A JP H01305849A JP 63135298 A JP63135298 A JP 63135298A JP 13529888 A JP13529888 A JP 13529888A JP H01305849 A JPH01305849 A JP H01305849A
- Authority
- JP
- Japan
- Prior art keywords
- magnesia
- carbon
- fibers
- starting material
- brick
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000011449 brick Substances 0.000 title claims abstract description 30
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 30
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims abstract description 81
- 239000000395 magnesium oxide Substances 0.000 claims abstract description 43
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 42
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 33
- 239000004917 carbon fiber Substances 0.000 claims abstract description 33
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 24
- 239000002994 raw material Substances 0.000 claims description 9
- 230000035939 shock Effects 0.000 abstract description 13
- 239000000835 fiber Substances 0.000 abstract description 12
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 abstract description 5
- 238000002156 mixing Methods 0.000 abstract description 4
- 230000007797 corrosion Effects 0.000 abstract description 3
- 238000005260 corrosion Methods 0.000 abstract description 3
- 229920002239 polyacrylonitrile Polymers 0.000 abstract description 2
- 229920003002 synthetic resin Polymers 0.000 abstract description 2
- 239000000057 synthetic resin Substances 0.000 abstract description 2
- 239000007858 starting material Substances 0.000 abstract 5
- 230000002542 deteriorative effect Effects 0.000 abstract 1
- 229910002804 graphite Inorganic materials 0.000 description 14
- 239000010439 graphite Substances 0.000 description 14
- 230000000052 comparative effect Effects 0.000 description 8
- 230000000694 effects Effects 0.000 description 8
- 238000005452 bending Methods 0.000 description 6
- 239000000843 powder Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 230000001590 oxidative effect Effects 0.000 description 4
- 239000005011 phenolic resin Substances 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 3
- 239000000654 additive Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- -1 magnesium-aluminum-calcium Chemical compound 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000013001 point bending Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- 229910052580 B4C Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- 230000003064 anti-oxidating effect Effects 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 210000000554 iris Anatomy 0.000 description 1
- 238000004898 kneading Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、マグネシア・カーボンれんかに関し、特に、
耐熱衝撃性を低下させることなく、機械的強度及び耐摩
耗性を高められるようにしたマグネシア・カーボンれん
かに関するものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to magnesia carbon bricks, and in particular,
This invention relates to a magnesia carbon brick that has improved mechanical strength and abrasion resistance without reducing thermal shock resistance.
マグネシア・カーボンれんがは、耐食性及び耐熱衝撃性
に優れていることから製鋼用耐火物として近年広く使用
されるようになった。しかし、マグネシア・カーボンれ
んがは、酸化雰囲気の下ではカーボンが消失してしまう
欠点の他にその主要なカーボン源である黒鉛の性質が原
因となって機械的強度や耐摩耗性を高める上では不利で
あり、例えば転炉の装入側炉壁のようにスクラップや溶
銑の投入によって機械的衝撃を受けたり摩耗が生じ易い
箇所では損傷が大きく、炉体の寿命を短くする一因とな
っている。Magnesia carbon bricks have become widely used as refractories for steelmaking in recent years because of their excellent corrosion resistance and thermal shock resistance. However, magnesia carbon bricks have disadvantages in terms of increasing mechanical strength and wear resistance due to the disadvantage that carbon disappears in an oxidizing atmosphere and the properties of graphite, which is the main carbon source. For example, damage is severe in areas that are subject to mechanical shock and wear due to the input of scrap and hot metal, such as the charging side wall of a converter, which is one of the causes of shortening the life of the furnace body. .
そこで、マグネシア・カーボンれんがの機械的強度や耐
摩耗性を高めるために、アルミニウム、珪素、マグネシ
ウム、カルシウム等の金属粉末を添加することが提案さ
れているが、主カーボン源として黒鉛を使用する限り飛
躍的な強度及び耐摩耗性の向1を図ることはできず、ま
た、加熱後に金属添加物によってれんがが硬直化して耐
熱衝撃性が低下することがある。Therefore, in order to increase the mechanical strength and wear resistance of magnesia carbon bricks, it has been proposed to add metal powders such as aluminum, silicon, magnesium, and calcium, but as long as graphite is used as the main carbon source, It is not possible to achieve dramatic improvements in strength and wear resistance, and the metal additives may harden the bricks after heating, resulting in a decrease in thermal shock resistance.
本発明は、上記の事情を考慮してなされたものであって
、耐熱衝撃性を低下させることなく、機械的強度及び耐
摩耗性を高められるようにしたマグネシア・カーボンれ
んがを提供することを目的とするものである。The present invention has been made in consideration of the above circumstances, and an object of the present invention is to provide a magnesia carbon brick that can improve mechanical strength and abrasion resistance without reducing thermal shock resistance. That is.
本発明者らは、鋭意研究した結果、マグネシア・カーボ
ンれんがの機械的強度や耐摩耗性を不利にしている原因
が主カーボン源として黒鉛を使用することにあると推察
して、黒鉛に代わって機械的強度の高いカーボンファイ
バーをカーボン源として使用することにより上記の目的
を達成できることを発見し、本発明を完成するに至った
。As a result of intensive research, the present inventors deduced that the cause of disadvantageous mechanical strength and wear resistance of magnesia carbon bricks was the use of graphite as the main carbon source. The inventors have discovered that the above objects can be achieved by using carbon fibers with high mechanical strength as a carbon source, and have completed the present invention.
即ち、本発明に係るマグネシア・カーボンれんがは、上
記の目的を達成するために、マグネシア原料にカーボン
ファイバーを内掛けで0.1〜50重量%添加したこと
を特徴としている。That is, in order to achieve the above object, the magnesia-carbon brick according to the present invention is characterized in that 0.1 to 50% by weight of carbon fiber is added to the magnesia raw material.
カーボンファイバーは、機械的強度が鱗状黒鉛等に比べ
て強く、鱗状黒鉛よりも蟲かに少ない使用量で同程度の
耐熱衝撃性を得ることができる。Carbon fiber has higher mechanical strength than flaky graphite and the like, and can obtain the same level of thermal shock resistance with a much smaller amount of use than flaky graphite.
また、カーボンファイバーは繊維の長さ方向に対する引
っ張り強度が大きく、かつ、鱗状黒鉛のような層状構造
を持たないのでカーボンファイバーの添加に伴う強度低
下はほとんど無く、逆に結合材を補強して強度が高めら
れる。In addition, carbon fiber has a high tensile strength in the longitudinal direction of the fiber, and does not have a layered structure like graphite scales, so there is almost no decrease in strength due to the addition of carbon fiber.On the contrary, it can be strengthened by reinforcing the binding material. is enhanced.
本発明において使用するFグネシア原料は、特に限定さ
れず、例えば、焼結マグネシアクリンカ−1電融マグネ
シアクリンカ−1その他のマグネシアクリンカ−等のう
ちの1種または2種以上を使用することができる。しか
しながら、れんがの耐食性を高めることを考慮にいれる
ならば、酸化マグネシウム(MgO)成分が90%以上
のものを使用することが好ましい。The F gnesia raw material used in the present invention is not particularly limited, and for example, one or more of sintered magnesia clinker, fused magnesia clinker, other magnesia clinkers, etc. can be used. . However, if we take into account the improvement of the corrosion resistance of bricks, it is preferable to use a material containing 90% or more of magnesium oxide (MgO).
また、本発明に使用されるカーボンファイバーは、特に
限定されず、例えば、市販のポリアクリルニトリル系に
代表される合成樹脂系の繊維、あるいはピンチ系の繊維
を高温で熱処理した炭素質あるいは黒鉛質のカーボンフ
ァイバーを使用すればよい。カーボンファイバーの繊維
長は0.1〜50+nが好ましく、0.5〜20mとす
ることが更に好ましい。カーボンファイバーの繊維長が
O3l mi未満では剥離防止効果が乏しくなるので好
ましくなく、50mを超えるとマグネシア原料との均一
混合が困難になるので好ましくない。カーボンファイバ
ーの繊維長が0.5〜20鰭では十分な剥離防止効果が
得られるとともに、容易にマグネシア原料と均一混合す
ることができるので特に好ましい。カーボンファイバー
の径は2〜50μmとすることが好ましい。カーボンフ
ァイバーの径が2μm未満では必要とする強度が得られ
ないので好ましくなく、50μmを超えると柔軟性に乏
しくなり、れんがの成形性を損なうので好ましくない。The carbon fibers used in the present invention are not particularly limited, and include, for example, commercially available synthetic resin fibers such as polyacrylonitrile fibers, carbonaceous or graphite fibers obtained by heat-treating pinch fibers at high temperatures. Carbon fiber can be used. The fiber length of the carbon fiber is preferably 0.1 to 50+n, more preferably 0.5 to 20 m. If the fiber length of the carbon fiber is less than O3l mi, it is not preferable because the peeling prevention effect becomes poor, and if it exceeds 50 m, it becomes difficult to mix uniformly with the magnesia raw material, which is not preferable. It is particularly preferable that the carbon fiber has a fiber length of 0.5 to 20 fins, since a sufficient peeling prevention effect can be obtained and it can be easily mixed uniformly with the magnesia raw material. The diameter of the carbon fiber is preferably 2 to 50 μm. If the diameter of the carbon fiber is less than 2 μm, it is not preferable because the required strength cannot be obtained, and if it exceeds 50 μm, the flexibility becomes poor and the moldability of the brick is impaired, so it is not preferable.
尚、この範囲内であれば繊維長や径の異なるカーボンフ
ァイバーを混合使用することは何等妨げがない。カーボ
ンファイバーの添加量は、マグネシア原料に対して内掛
けで0.1〜50重量%とすることが好ましく、0.5
〜10重量%とすることがさらに好ましい。カーボンフ
ァイバーの添加量が0.1重量%未満では添加による強
度及び耐熱衝撃性を向上する効果が不十分になるので好
ましくなく、50重量%を超えるとマグネシア原料との
均一混合が困難になるので好ましくない。カーボンファ
イバーの添加量が0.5〜10重量%ではマグネシア原
料と容易に均一混合でき、しかも、添加による強度及び
耐熱衝撃性を向上する効果が十分に得られるので特に好
ましい。It should be noted that within this range, there is no hindrance to mixing and using carbon fibers having different fiber lengths and diameters. The amount of carbon fiber added is preferably 0.1 to 50% by weight based on the magnesia raw material, and 0.5% by weight.
It is more preferable to set the content to 10% by weight. If the amount of carbon fiber added is less than 0.1% by weight, the effect of adding carbon fiber to improve strength and thermal shock resistance will be insufficient, which is undesirable, and if it exceeds 50% by weight, it will be difficult to mix uniformly with the magnesia raw material. Undesirable. It is particularly preferable that the amount of carbon fiber added is 0.5 to 10% by weight, since it can be easily and uniformly mixed with the magnesia raw material, and the effect of adding carbon fiber to improve strength and thermal shock resistance can be sufficiently obtained.
尚、本発明に係るマグネシア・カーボンれんがを特に酸
化性の強い雰囲気下で使用する場合、カーボンファイバ
ー及び結合部が酸化して著しく損耗が大きくなることが
ある。これを防止するためにはアルミニウム、珪素、マ
グネシウム、カルシウム等の金属粉末、マグネシウム−
アルミニウム、アルミニウムー珪素、マグネシウム−ア
ルミニウムーカルシウム、マグネシウム−アルミニウム
ー珪素等の合金粉末、炭化硼素(84C)粉末、窒化硼
素(BN)粉末等の酸化抑制材の1種あるいは2種以上
を合計量で外掛け0.2〜30重量%の範囲で添加すれ
ばよい。これらの添加物の合計添加量が外掛け0.2重
量%未満では酸化防止効果が十分でないので好ましくな
く、30重量%を超えると添加物の炭化あるいは酸化時
の体積膨張が大きくなり、れんがが多孔質になったり、
亀裂を生じたりすることがあるので好ましくない。In addition, when the magnesia carbon brick according to the present invention is used in a particularly strongly oxidizing atmosphere, the carbon fibers and the bonding parts may be oxidized and wear and tear may be significantly increased. To prevent this, metal powders such as aluminum, silicon, magnesium, and calcium, magnesium
Total amount of one or more oxidation inhibitors such as aluminum, aluminum-silicon, magnesium-aluminum-calcium, magnesium-aluminum-silicon alloy powder, boron carbide (84C) powder, boron nitride (BN) powder, etc. It may be added in an amount of 0.2 to 30% by weight. If the total amount of these additives is less than 0.2% by weight, the anti-oxidation effect will not be sufficient, which is undesirable; if it exceeds 30% by weight, the volumetric expansion during carbonization or oxidation of the additives will increase, and the brick become porous,
This is not preferable as it may cause cracks.
また、本発明のマグネシア・カーボンれんがを製造する
手順は、上記の成分構成でありさえすれば特に限定され
ることはなく、例えば、粒度調整したマグネシア原料に
カーボンファイバーを添加して混合した後、液状あるい
は粉末のピッチ、タール、フェノール樹脂等の各種有機
結合剤のうちの1種あるいは2種以上を選んで添加し、
混練してから成形し、更にこの後、100〜400℃の
低温熱処理により不焼成品としてのマグネシア・カーボ
ンれんがが得られ、あるいは、400℃以上の高温還元
雰囲気下で熱処理して焼成品としてのマグネシア・カー
ボンれんがが得られる。更に、焼成品としてのマグネシ
ア・カーボンれんがは必要に応じてピンチ、フェノール
レジン等を含浸させて用いられることもある。Further, the procedure for manufacturing the magnesia carbon brick of the present invention is not particularly limited as long as it has the above-mentioned composition. For example, after adding and mixing carbon fiber to the magnesia raw material whose particle size has been adjusted, Add one or more selected organic binders such as liquid or powder pitch, tar, phenolic resin, etc.
After kneading and molding, the magnesia carbon brick is then heat-treated at a low temperature of 100 to 400°C to obtain an unfired product, or it is heat-treated at a high temperature of 400°C or higher in a reducing atmosphere to produce a fired product. Magnesia carbon bricks are obtained. Furthermore, the magnesia carbon brick as a fired product may be used after being impregnated with pinch, phenol resin, etc., if necessary.
以下、本発明の実施例について説明する。 Examples of the present invention will be described below.
MgO純度98重量%の焼結マグネシアクリンカ−と、
カーボンファイバーとを第1表の実施例1〜5に示すよ
うに配合し、結合剤としてフェノールレジンを使用して
ロールパンで混練した後、500)ン油圧プレスを用い
て皿形れんが形状に成形し、250℃で12時間熱処理
して不焼成品としてのマグネシア・カーボンれんがを得
た。Sintered magnesia clinker with MgO purity of 98% by weight,
The mixture was mixed with carbon fiber as shown in Examples 1 to 5 in Table 1, kneaded in a roll pan using phenol resin as a binder, and then molded into a dish-shaped brick shape using a 500 mm hydraulic press. A magnesia carbon brick was obtained as an unfired product by heat treatment at 250° C. for 12 hours.
また、比較例として、MgO純度98重量%の焼結マグ
ネシアクリンカ−と鱗状黒鉛とを第1表の比較例1〜4
に示すように配合し、結合剤としてフェノールレジンを
使用してロールパンで混練した後、500トン油圧プレ
スを用いて皿形れんが形状に成形し、250℃で12時
間熱処理して不焼成品としてのマグネシア・カーボンれ
んがを得た。In addition, as a comparative example, sintered magnesia clinker with an MgO purity of 98% by weight and scaly graphite were used in Comparative Examples 1 to 4 in Table 1.
After mixing in a roll pan using phenol resin as a binder, it was formed into a dish-shaped brick shape using a 500-ton hydraulic press, and heat-treated at 250°C for 12 hours to form an unfired product. Obtained Magnesia Carbon Brick.
各実施例及び各比較例について、常温曲げ強さ試験、1
400℃曲げ強さ試験、耐熱衝撃性試験、酸化摩耗試験
を行った。これらの試験条件は、次の通りである。For each example and each comparative example, room temperature bending strength test, 1
A 400°C bending strength test, a thermal shock resistance test, and an oxidative wear test were conducted. These test conditions are as follows.
まず、常温曲げ強さ試験は、スパン100m墓の3点曲
げで測定した。First, the room temperature bending strength test was performed by three-point bending with a span of 100 m.
また、1400℃曲げ強さ試験は、試片をコークスプリ
ーズに埋めたまま1400℃で30分間保持した後、ス
パン127.5mmの3点曲げで測定した。In addition, the 1400° C. bending strength test was performed by holding the specimen buried in coke pleat at 1400° C. for 30 minutes, and then performing three-point bending with a span of 127.5 mm.
耐熱衝撃性試験は、れんがを1700℃の溶鋼中に3分
間浸漬し、取り出した後カーポンプリーズ中で室温まで
放冷する操作を繰り返し、剥離が生じるまでの回数を計
った。In the thermal shock resistance test, a brick was immersed in molten steel at 1,700°C for 3 minutes, taken out, and allowed to cool to room temperature in a carbon pleat.The operation was repeated, and the number of times until peeling occurred was counted.
酸化摩耗試験は、1辺が50臘菖の立方体の試片を12
00℃の回転炉中にて2Or、p、m、で30分間回転
させ、放冷した後の重量減少率を測定した。In the oxidation wear test, 12 cubic specimens with 50 irises on each side were
The sample was rotated for 30 minutes at 2Or, p, m in a rotary furnace at 00°C, and the weight loss rate after cooling was measured.
これらの試験結果は第1表に示す通りである。The results of these tests are shown in Table 1.
第1表から明らかなように、各実施例に係るマグネシア
・カーボンれんがは、従来の鱗状黒鉛を添加するものに
比べて常温曲げ強度及び1400℃曲げ強度が著しく大
きい。As is clear from Table 1, the magnesia carbon bricks according to each example have significantly higher room temperature bending strength and 1400° C. bending strength than those to which conventional scaly graphite is added.
また、耐熱衝撃性も遥かに優れている。即ち、カーボン
ファイバー2重量%添加の実施例2〜4は鱗状黒鉛20
重量%添加の比較例2〜4と同等以上であり、また、カ
ーボンファイバー0.5重量%添加の実施例1は鱗状黒
鉛10重世%添加の比較例1よりも優れている。It also has far superior thermal shock resistance. That is, in Examples 2 to 4 in which 2% by weight of carbon fiber was added, 20% of scale graphite was added.
It is equivalent to or higher than Comparative Examples 2 to 4 in which carbon fiber is added in an amount of 0.5 weight %, and Example 1 in which carbon fiber is added in an amount of 0.5 weight % is superior to Comparative Example 1 in which scaly graphite is added in an amount of 10 weight %.
また、鱗状黒鉛とカーボンファイバー−を併用した比較
例4では、比較例3に対してカーボンファイバーを添加
した効果がみられない。Furthermore, in Comparative Example 4 in which scale graphite and carbon fiber were used in combination, the effect of adding carbon fiber to Comparative Example 3 was not seen.
更に、本発明の各実施例は各比較例に比べてカーボンが
少ないので、耐酸化摩耗性においても著し←優れている
ことが分かる。Furthermore, since each of the examples of the present invention contains less carbon than each of the comparative examples, it can be seen that they are significantly superior in oxidative wear resistance.
更に、実施例4のれんがを250トン転炉の装入側炉壁
に使用し、黒鉛20重量%使用の従来品と比較実用試験
をした結果、従来品の損耗速度が2.4mm/chであ
ったのに対して、実施例4のものでは1.81■/ch
にとどまり、耐用性が向上したことを確認できた。Furthermore, the bricks of Example 4 were used for the charging side wall of a 250-ton converter, and as a result of a practical test comparing them with a conventional product containing 20% graphite, the wear rate of the conventional product was 2.4 mm/ch. In contrast, in Example 4, it was 1.81■/ch.
It was confirmed that the durability was improved.
(以下余白)
〔発明の効果〕
本発明のマグネシア・カーボンれんがは、以上に説明し
たように、鱗状黒鉛等の層状構造を有するカーボン源に
代えて機械的強度の高いカーボンファイバーをカーボン
源として使用することにより、耐熱衝撃性を低下させる
ことなく、機械的強度やI′iit摩耗性を飛躍的に向
上させることができた。(The following is a blank space) [Effects of the Invention] As explained above, the magnesia carbon brick of the present invention uses carbon fiber with high mechanical strength as a carbon source instead of a carbon source having a layered structure such as scaly graphite. By doing so, it was possible to dramatically improve mechanical strength and I'iit abrasion resistance without reducing thermal shock resistance.
Claims (1)
0.1〜50重量%添加したことを特徴とするマグネシ
ア・カーボンれんが。(1) A magnesia carbon brick characterized by adding 0.1 to 50% by weight of carbon fiber to the magnesia raw material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63135298A JPH01305849A (en) | 1988-05-31 | 1988-05-31 | Magnesia-carbon brick |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63135298A JPH01305849A (en) | 1988-05-31 | 1988-05-31 | Magnesia-carbon brick |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01305849A true JPH01305849A (en) | 1989-12-11 |
Family
ID=15148432
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63135298A Pending JPH01305849A (en) | 1988-05-31 | 1988-05-31 | Magnesia-carbon brick |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01305849A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014196229A (en) * | 2013-03-06 | 2014-10-16 | 黒崎播磨株式会社 | Magnesia carbon brick |
JP2016047939A (en) * | 2014-08-27 | 2016-04-07 | Jfeスチール株式会社 | Refractory for converter tuyere |
CN106052396A (en) * | 2016-07-25 | 2016-10-26 | 宜兴市中环耐火材料有限公司 | High-performance steel fiber tough wear-resisting brick |
CN108484130A (en) * | 2018-06-14 | 2018-09-04 | 营口石元耐火材料有限公司 | A kind of low carbon magnesia carbon brick and preparation method thereof of nano-sized carbon enhancing |
CN108863414A (en) * | 2018-08-14 | 2018-11-23 | 上海新泰山高温工程材料有限公司 | A kind of high performance magnesia carbon brick and preparation method thereof |
-
1988
- 1988-05-31 JP JP63135298A patent/JPH01305849A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014196229A (en) * | 2013-03-06 | 2014-10-16 | 黒崎播磨株式会社 | Magnesia carbon brick |
JP2016047939A (en) * | 2014-08-27 | 2016-04-07 | Jfeスチール株式会社 | Refractory for converter tuyere |
CN106052396A (en) * | 2016-07-25 | 2016-10-26 | 宜兴市中环耐火材料有限公司 | High-performance steel fiber tough wear-resisting brick |
CN108484130A (en) * | 2018-06-14 | 2018-09-04 | 营口石元耐火材料有限公司 | A kind of low carbon magnesia carbon brick and preparation method thereof of nano-sized carbon enhancing |
CN108863414A (en) * | 2018-08-14 | 2018-11-23 | 上海新泰山高温工程材料有限公司 | A kind of high performance magnesia carbon brick and preparation method thereof |
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