JPH0327618B2 - - Google Patents
Info
- Publication number
- JPH0327618B2 JPH0327618B2 JP579983A JP579983A JPH0327618B2 JP H0327618 B2 JPH0327618 B2 JP H0327618B2 JP 579983 A JP579983 A JP 579983A JP 579983 A JP579983 A JP 579983A JP H0327618 B2 JPH0327618 B2 JP H0327618B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- resistance
- corrosion resistance
- corrosion
- wear resistance
- 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
Landscapes
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Description
この発明は、耐摩耗性ならびに耐食性に優れた
合金に関し、とくに耐摩耗性ならびに耐食性が要
求される部分のライニング材として適する耐摩耗
耐食合金に関するものである。
耐摩耗性ならびに耐食性が要求される部材とし
ては、例えば、樹脂成形機、スラリーポンプ、コ
ンプレツサ等に使用されるシリンダがある。
一方、樹脂成形体中に、ガラス繊維、炭素繊
維、金属繊維等の補強材を混入させ(FRP、
FRM等)て、樹脂成形体の強度、難燃性、耐摩
耗性等の諸特性を向上させようとすることが近年
多くなつてきている。したがつて、樹脂成形機の
シリンダ部分においては、樹脂に加えた補強材や
添加剤による摩耗が少ないこと、および樹脂や添
加剤等から出るガスによる腐食が少ないことな
ど、従来以上の厳しい特性が要求される。
ところで、従来の樹脂成形機におけるシリンダ
には、窒化鋼を使用してその表面に窒化処理を施
し、耐摩耗性を向上させることも行われていた
が、硬化層の薄さから耐摩耗性および耐食性が十
分でないという欠点を有していた。
この発明は、上記した従来の欠点を解消するた
めになされたもので、耐摩耗性ならびに耐食性に
すぐれ、特にライニング材としての使用に適する
耐摩耗耐食合金を提供することを目的としてい
る。
この発明による耐摩耗耐食合金は、耐食性を有
する金属をマトリツクスとし、このマトリツクス
を高硬度化することにより耐摩耗性を向上させた
ことを特徴とし、その組成範囲は、重量%で、
Ni:35%以下、Cr:3〜15%、Mo:1〜10%、
B:1〜4%、Si:1〜4%、Mn:0.2〜2%、
残部実質的にCoよりなることを特徴としている。
次に、この発明による耐摩耗耐食合金の組成範
囲(重量%)の限定理由について説明する。
Ni:35%以下
Niは合金の耐食性を向上させるのに有効な元
素であるが、多すぎると合金の硬さを低下して耐
摩耗性を劣化させるので、35%以下、より望まし
くは耐食性および硬さのバランスから5〜15%の
範囲とするのが良い。
Cr:3〜15%
Crはマトリツクス中に固溶して当該マトリツ
クスの硬さを増大し、合金の耐摩耗性を向上させ
るのに有効な元素であるが、3%未満では上記し
た硬化が小さく、15%を越えると靭性が劣化する
ので、3〜15%、より望ましくは5〜15%の範囲
とするのが良い。
Mo:1〜10%
Moはマトリツクス中に固溶して合金の耐食性
を向上させるのに有効な元素であるが、1%未満
では上記した効果が小さく、10%を超えても耐食
性の向上は顕著に得られず、かえつて加工性が劣
化して仕上げ加工を困難にするので、1〜10%、
より望ましくは1〜5%の範囲とするのが良い。
B:1〜4%
BはCo、Ni、Crと化合して硼化物を作り、合
金の硬さを増大させて耐摩耗性を向上させるのに
有効な元素であるが、1%未満ではこのような効
果が小さく、4%超過ではCoと金属間化合物を
作つて脆化し、合金の靭性を劣化させるので、1
〜4%の範囲とする。
Si:1〜4%
Siは合金の湯流れ性を向上させる元素であり、
特にライニング鋳造によつて形成する場合に必要
な湯流れ性を確保するのに有効な元素であるが、
1%未満ではそのような効果が小さく、4%超過
ではCoと金属間化合物を作つて脆化し、合金の
靭性を劣化させるので、1〜4%の範囲とする。
Mn:0.2〜2%
Mnは脱酸剤として作用する元素であり、十分
な脱酸作用を得るためには0.2%以上とする必要
がある。しかし、2%を超過しても脱酸作用の向
上は得られず、かえつて靭性を劣化するので、2
%以下とする。
Co:残部
CoはCrおよびBと化合して合金の耐摩耗性を
向上させると共に十分な耐食性を得るのに必要な
元素であり、合金の残部とした。
この発明による合金は、上記各成分の相互作用
により、優れた耐摩耗性ならびに耐食性を有し、
耐摩耗性ならびに耐食性が要求される部材の表面
にコーテイングあるいはライニングして当該部材
の耐摩耗性ならびに耐食性を高めるのに有効であ
り、合金の湯流れ性が良いため上記コーテイング
あるいはライニングに際して鋳造法を利用するこ
とができるものである。
以下、この発明の実施例を比較例と共に説明す
る。
まず、マグネシアるつぼ中で本発明合金成分を
6種類混合し、電気炉にて1450〜1500℃に加熱溶
解した後板状試験片を作成し、各試験片の成分組
成を分析したところ、第1表(No.1〜6)に示す
結果であつた。また、比較例として、同じく第1
表(No.7)に示す窒化鋼(SACM645)を用いて
窒化処理を行つた。
次いで、各試験片(No.1〜7)の硬さ、耐摩耗
性、耐食性を調べたところ、第2表に示す結果と
なつた。なお、硬さ試験は、この発明の実施例に
おいてはロツクウエル、比較例においてはビツカ
ースで行つた。また、耐摩耗性試験は、大越式摩
耗試験機を用い、標準ロール;直径30mm×3mm、
荷重;12.6Kg、距離;200mの条件で比摩耗量の
測定を行つた。さらに、耐食性試験は、試験片の
大きさを2×10×25mmとし、20℃、24Hrの条件
で行つた。
The present invention relates to an alloy with excellent wear resistance and corrosion resistance, and in particular to an abrasion and corrosion resistant alloy suitable as a lining material for parts where wear resistance and corrosion resistance are required. Examples of members that require wear resistance and corrosion resistance include cylinders used in resin molding machines, slurry pumps, compressors, and the like. On the other hand, reinforcing materials such as glass fiber, carbon fiber, and metal fiber are mixed into the resin molding (FRP,
In recent years, there have been many attempts to improve the strength, flame retardance, abrasion resistance, and other properties of resin molded products (FRM, etc.). Therefore, the cylinder part of a resin molding machine has stricter characteristics than before, such as less wear due to reinforcing materials and additives added to the resin, and less corrosion due to gases emitted from the resin and additives. required. By the way, the cylinders in conventional resin molding machines have been made of nitrided steel and have their surfaces nitrided to improve their wear resistance, but due to the thinness of the hardened layer, the wear resistance and It had the disadvantage of insufficient corrosion resistance. The present invention was made in order to eliminate the above-mentioned conventional drawbacks, and an object of the present invention is to provide a wear-resistant and corrosion-resistant alloy that has excellent wear resistance and corrosion resistance, and is particularly suitable for use as a lining material. The wear-resistant and corrosion-resistant alloy according to the present invention is characterized in that the matrix is made of a metal having corrosion resistance, and the wear resistance is improved by increasing the hardness of this matrix, and the composition range is as follows:
Ni: 35% or less, Cr: 3-15%, Mo: 1-10%,
B: 1-4%, Si: 1-4%, Mn: 0.2-2%,
It is characterized in that the remainder essentially consists of Co. Next, the reason for limiting the composition range (wt%) of the wear-resistant and corrosion-resistant alloy according to the present invention will be explained. Ni: 35% or less Ni is an effective element for improving the corrosion resistance of alloys, but too much Ni reduces the hardness of the alloy and deteriorates wear resistance. From the viewpoint of hardness balance, it is preferable to set it within the range of 5 to 15%. Cr: 3-15% Cr is an effective element for increasing the hardness of the matrix by solid solution in the matrix and improving the wear resistance of the alloy, but if it is less than 3%, the above-mentioned hardening will be small. If it exceeds 15%, the toughness deteriorates, so it is preferably in the range of 3 to 15%, more preferably 5 to 15%. Mo: 1 to 10% Mo is an element that is effective in improving the corrosion resistance of alloys by solid solution in the matrix, but if it is less than 1%, the above effect is small, and if it exceeds 10%, the corrosion resistance will not be improved. 1 to 10%, as it will not be noticeable and will actually deteriorate the workability and make finishing difficult.
More preferably, it is in the range of 1 to 5%. B: 1-4% B is an effective element for combining with Co, Ni, and Cr to form boride, increasing the hardness of the alloy and improving wear resistance, but if it is less than 1%, this element This effect is small, and if it exceeds 4%, it will form an intermetallic compound with Co, causing embrittlement and deteriorating the toughness of the alloy.
-4% range. Si: 1-4% Si is an element that improves the flowability of the alloy.
It is an effective element to ensure the necessary fluidity, especially when forming by lining casting.
If it is less than 1%, such an effect will be small, and if it exceeds 4%, it will form an intermetallic compound with Co, causing embrittlement and deteriorating the toughness of the alloy, so it should be in the range of 1 to 4%. Mn: 0.2-2% Mn is an element that acts as a deoxidizing agent, and in order to obtain a sufficient deoxidizing effect, it needs to be 0.2% or more. However, even if it exceeds 2%, the deoxidizing effect cannot be improved and the toughness will deteriorate on the contrary.
% or less. Co: Remainder Co is an element necessary to combine with Cr and B to improve the wear resistance of the alloy and to obtain sufficient corrosion resistance, and was used as the remainder of the alloy. The alloy according to the present invention has excellent wear resistance and corrosion resistance due to the interaction of the above components,
It is effective for coating or lining the surface of parts that require wear resistance and corrosion resistance to increase the wear resistance and corrosion resistance of the parts.Since the alloy has good flowability, casting methods are often used for the above coating or lining. It is something that can be used. Examples of the present invention will be described below along with comparative examples. First, six types of alloy components of the present invention were mixed in a magnesia crucible, heated and melted at 1450 to 1500°C in an electric furnace, and plate-shaped test pieces were created.The component composition of each test piece was analyzed. The results are shown in the table (Nos. 1 to 6). Also, as a comparative example, the first
Nitriding treatment was performed using the nitriding steel (SACM645) shown in Table (No. 7). Next, the hardness, abrasion resistance, and corrosion resistance of each test piece (Nos. 1 to 7) were examined, and the results are shown in Table 2. The hardness test was conducted using Rockwell in the examples of the present invention and with Vickers in the comparative examples. In addition, the abrasion resistance test was carried out using an Okoshi type abrasion tester, using a standard roll; diameter 30 mm x 3 mm;
The specific wear amount was measured under the conditions of load: 12.6 kg and distance: 200 m. Furthermore, the corrosion resistance test was conducted using a test piece with a size of 2 x 10 x 25 mm at 20°C and 24 hours.
【表】【table】
【表】
第1表および第2表に示すように、この発明に
よる合金(No.1〜6)は、従来の窒化鋼(No.7)
に比べて、いずれも比摩耗量が小さく耐摩耗性に
優れていると同時に、腐食量が少なく耐食性にも
優れていることが明らかである。
次に、第1表に示す合金の中から3種(No.1、
3、5)を選定し、外径100mm、内径32mm、長さ
1000mmの炭素鋼(SC)製シリンダの中に、当該
シリンダの内壁面に片肉厚3mmのライニングを行
うのに必要な量の上記合金の割片を入れたのち、
前記シリンダの両端を封じ、その後約1200℃の炉
内に装入して加熱し、加熱後にシリンダを炉内か
ら取り出し、前記シリンダを遠心機に装着して回
転しつつ800℃まで冷却し、その後室温まで徐冷
し、次いでシリンダを所定長さの寸法に切削およ
び研削仕上げした。この結果、シリンダ内面に高
硬度の耐摩耗耐食性層が形成されており、とくに
樹脂成形機、モルタルポンプ、スラリーポンプ、
コンプレツサ等の耐摩耗性、耐食性が要求される
シリンダに適したものが得られた。そして、シリ
ンダ内面のライニング厚さは著しく均一なもので
あり、湯流れ性が良好であつてこのような遠心鋳
造によるライニング用合金として著しく優れたも
のであり、加えて、ライニング後のシリンダ内面
の切削は、表面が高硬度化したにもかかわらず非
常に容易に行うことができ、被削性が良好である
ことも確認された。
以上説明してきたように、この発明による合金
は耐摩耗性ならびに耐食性に著しく優れたもので
あり、耐摩耗性ならびに耐食性が要求される部材
そのものとして、あるいはライニング材やコーテ
イング材として適したものであり、湯流れ性が良
好であるため鋳造による成形あるいは積層が容易
に可能であり、切削も可能であるため成形あるい
は積層後の仕上げ加工が容易であるなどの数々の
すぐれた効果を有する。[Table] As shown in Tables 1 and 2, the alloys according to the present invention (No. 1 to 6) are different from the conventional nitrided steel (No. 7).
It is clear that both have a small specific wear amount and excellent wear resistance, as well as a small amount of corrosion and excellent corrosion resistance. Next, three types (No. 1,
3, 5), outer diameter 100mm, inner diameter 32mm, length
After putting the necessary amount of split pieces of the above alloy into a 1000 mm carbon steel (SC) cylinder to line the inner wall of the cylinder with a wall thickness of 3 mm,
Both ends of the cylinder were sealed, and then placed in a furnace at about 1200°C and heated. After heating, the cylinder was taken out of the furnace, and the cylinder was attached to a centrifuge and cooled to 800°C while rotating, and then The cylinder was slowly cooled to room temperature, and then cut and ground to a predetermined length. As a result, a highly hard wear-resistant and corrosion-resistant layer is formed on the inner surface of the cylinder, which is especially useful for resin molding machines, mortar pumps, slurry pumps, etc.
A product suitable for cylinders that require wear resistance and corrosion resistance, such as compressors, was obtained. The lining thickness on the inner surface of the cylinder is extremely uniform, and the melt flowability is good, making it an extremely excellent alloy for linings made by centrifugal casting. It was also confirmed that cutting could be performed very easily despite the high hardness of the surface, and that the material had good machinability. As explained above, the alloy according to the present invention has extremely excellent wear resistance and corrosion resistance, and is suitable as a member itself that requires wear resistance and corrosion resistance, or as a lining material or coating material. Since it has good flowability, it can be easily formed by casting or laminated, and it can also be cut, so it has many excellent effects such as easy finishing after molding or lamination.
Claims (1)
Mo:1〜10%、B:1〜4%、Si:1〜4%、
Mn:0.2〜2%、残部実質的にCoよりなること
を特徴とする耐摩耗耐食合金。1% by weight, Ni: 35% or less, Cr: 3-15%,
Mo: 1-10%, B: 1-4%, Si: 1-4%,
A wear-resistant and corrosion-resistant alloy characterized by consisting of Mn: 0.2 to 2%, and the remainder substantially consisting of Co.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP579983A JPS59133343A (en) | 1983-01-19 | 1983-01-19 | Wear-resistant and corrosion-resistant alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP579983A JPS59133343A (en) | 1983-01-19 | 1983-01-19 | Wear-resistant and corrosion-resistant alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59133343A JPS59133343A (en) | 1984-07-31 |
| JPH0327618B2 true JPH0327618B2 (en) | 1991-04-16 |
Family
ID=11621123
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP579983A Granted JPS59133343A (en) | 1983-01-19 | 1983-01-19 | Wear-resistant and corrosion-resistant alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59133343A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6013042A (en) * | 1983-07-05 | 1985-01-23 | Daido Steel Co Ltd | Wear- and corrosion-resistant alloy |
| US11155904B2 (en) | 2019-07-11 | 2021-10-26 | L.E. Jones Company | Cobalt-rich wear resistant alloy and method of making and use thereof |
-
1983
- 1983-01-19 JP JP579983A patent/JPS59133343A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59133343A (en) | 1984-07-31 |
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