JPH0116901B2 - - Google Patents

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Publication number
JPH0116901B2
JPH0116901B2 JP59042972A JP4297284A JPH0116901B2 JP H0116901 B2 JPH0116901 B2 JP H0116901B2 JP 59042972 A JP59042972 A JP 59042972A JP 4297284 A JP4297284 A JP 4297284A JP H0116901 B2 JPH0116901 B2 JP H0116901B2
Authority
JP
Japan
Prior art keywords
point
magnetic tape
alloy
less
corrosion 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
Application number
JP59042972A
Other languages
Japanese (ja)
Other versions
JPS60187654A (en
Inventor
Shigeru Yanagimoto
Akira Niitsuma
Takayuki Kato
Katsumi Yokoi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Resonac Holdings Corp
Original Assignee
Showa Denko KK
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Showa Denko KK filed Critical Showa Denko KK
Priority to JP4297284A priority Critical patent/JPS60187654A/en
Publication of JPS60187654A publication Critical patent/JPS60187654A/en
Publication of JPH0116901B2 publication Critical patent/JPH0116901B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は、磁気テープの接触部品である、たと
えばVTR(ビデオテープレコーダー)のシリンダ
ー即ち、テープ案内用固定または回転ドラム等、
磁気テープに直接接触する磁気記録装置用部品に
適した耐食性に優れたアルミニウム合金に関する
ものである。 VTRは磁気テープに映像信号を磁気記録・再
生する回転磁気ヘツド部と、磁気テープを安定に
走行させるための静止または回転するテープ案内
ドラム等から構成されている。これらの回転磁気
ヘツド部あるいはテープ案内ドラムの如く磁気テ
ープと直接接触する部品は磁粉を付着したテープ
面を損うことなく安定したテープの走行を保持す
るうえで極めて重要な機能を果すことが知られて
おり、再生映像の精度(映像の鮮明度、色むら
等)を向上するため、磁気テープ接触部品材料の
改善が強く要望されている。 従来、VTRのテープ接触部品としては、例え
ば表面にCrハードメツキを施した銅合金、オー
ステナイト系SUS材等が使用されていた。しか
し、最近は、アルミニウム合金のもつ軽量性や加
工性が優れていること、非磁性であることなどの
長所を生かして、アルミニウム合金鋳物又は鋳塊
を切削又は塑性加工(特に鍛造加工)して、
VTRのドラム等磁気テープ接触部品が製造され
るようになつた。 磁気テープ接触部品用材料に求められるアルミ
ニウム合金の性質としては、主として、次の項目
が挙げられる。 (1) テープに対する耐摩耗性がよいこと。 (2) テープとの動摩擦係数が小さく、テープ
走行性がよいこと。 (3) 機械的強度が優れていること。 (4) 被削性に優れ、切削仕上面の平滑性がよ
いこと。 (5) 塑性加工性、特に冷間鍛造性に優れるこ
と。 (6) 高温多湿雰囲気中での磁気テープ接触部
品の耐食性が良好なこと。 従来、塑性加工用合金として、JIS2000番系の
Al―Cu系合金がよく知られており磁気テープ接
触部品用アルミニウム合金としても、広く使用さ
れているが、この合金は、前記1)〜5)の性質
においては優れているが、6)の高温多湿雰囲気
中での耐食性において、次のような問題点があ
る。 VTRのシリンダー等、磁気テープ接触部品に
磁気テープを巻きつけたまま、高温多湿の雰囲気
中に長時間放置すると、磁気テープとシリンダー
間に露結した水分によりシリンダー等磁気テープ
接触部品が腐蝕を受けて発錆し、シリンダー等の
必要な表面の平滑性を失うのみならず、この錆が
磁気テープの磁性塗膜にくいこんで、テープを引
き剥す際に磁性塗膜が剥離される現象が起ること
がわかつて来た。 この対策として、特開昭58−19472号公報に、
金属又は合金の表面に化学処理皮膜を施し、該皮
膜をクロム又はステンレススチールのスパツター
膜で被覆する技術か公開されている。しかしこの
方法は、通常の工程に表面処理およびスパツター
膜被覆という工程が追加されるのでコトカ高にな
るという欠点をもつ。 本発明者らは、このような現状に鑑み磁気テー
プ接触部品用として、機械的性質に優れ、かつ高
温多湿の雰囲気中での磁気テープ接触部位の耐食
性に優れたアルミニウム合金を開発することを技
術的課題として種々研究の結果、これまで広く使
用されている展伸材用のJIS2000番系のAl―Cu系
合金において、特にSi及びMgの含有量が腐蝕に
大きな影響を与えていることを見出し、本発明を
完成した。即ち本発明の目的は、耐摩耗性、動摩
擦係数、機械的強度、被削性、塑性加工性、鍛造
性などの性質を損うことなく磁気テープ接触部品
の耐食性を改善した磁気テープ接触部品用アルミ
ニウム合金を提供することであり、このような技
術的課題は、以下の構成により解決される。 即ち本願の第一発明の要旨は、 重量でCu1〜6%と、SiおよびMgを、第1図
の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未満、
Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、点D
(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8%)、
点F(Si0.15%、Mg1.8%)で囲まれた範囲の量
と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、残
部は通常の不純物を含むAlよりなる耐食性に優
れた磁気テープ接触部品用アルミニウム合金を提
供するものであり、第二発明の要旨は、 重量でCu1〜6%と、SiおよびMgを、第1図
の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未満、
Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、点D
(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8%)、
点F(Si0.15%、Mg1.8%)で囲まれた範囲の量
と、 Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、さら
にMn0.2〜1.2%、Cr0.2〜1.2%のうち1種以上の
元素とを含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合金
を提供するものであり、第三発明の要旨は、 重量でCu1〜6%と、SiおよびMgを、第1図
の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未満、
Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、点D
(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8%)、
点F(Si0.15%、Mg1.8%)で囲まれた範囲の量
と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、さ
らにPb、Bi、Sn、Sbのうち1種以上の元素を総
量で0.5〜2%を含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合金
を提供するものであり、さらに第四発明の要旨
は、 重量でCu1〜6%と、SiおよびMgを、第1図
の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未満、
Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、点D
(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8%)、
点F(Si0.15%、Mg1.8%)で囲まれた範囲の量
と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、さ
らにMn0.2〜1.2%、Cu0.2〜1.2%のうち1種以上
の元素、およびPb、Bi、Sn、Sbのうち1種以上
の元素を総量で0.5〜2%を含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合金
を提供するものである。 以下本発明の合金の組成範囲限定の理由につい
て説明する。本明細書の記載において含有元素の
含有量は、いずれも重量%で示されている。 まず、第一発明について説明する。 Cu:Cuは合金素地の強度を高め、かつ被削性
を向上させる。1%より少ないと効果は不十分で
あり、6%を越えると、鋳造性・鍛造性・耐食性
が低下する。このためCuは、1〜6%の範囲と
する。 SiおよびMg:SiとMgはMg2Si系析出物を形成
して合金の強度を高める。またMgは合金の機械
的強度、特に耐力を向上させると共に、Cuとの
相乗効果により、被削性を一層確実にする。
Si0.15%、Mg0.2%未満では、これらの効果は十
分ではない。 またSiが0.5%を越え、またMgが1.8%を越え
ると、磁気テープ接触部品に切削加工する際、仕
上面の粗さの点で満足なものが得られない。 SiおよびMgの含有量は、高温多湿雰囲気中で
の耐食性に著しく影響する。Si含有量が0.4%を
越え、かつMg含有量が0.8%を越える領域で耐食
性が著しく悪くなる。このため、SiおよびMgの
量は、第1図の点A,B,C,D,E,Fで囲ま
れた範囲の量とする。 Fe:Feは、耐摩耗性および切削性の向上に有
効である。0.1%未満では、その効果が認められ
ず、1.0%を越えると鍛造加工性が低下する。従
つて、Feは、0.1〜1.0%の範囲とする。 Ti:Tiは組織の微細化に有効であり、これに
よつて磁気テープ接触部品の加工仕上り寸法精度
(μmオーダー)を実現することができるので重
要な元素である。Tiが0.005%未満ではこの効果
が認められず、0.2%を越えると効果が飽和する
ばかりか、鍛造加工性が低下する。従つてTiは、
0.005〜0.2%の範囲とする。 本発明の実施にあたつては、上記の添加元素の
ほかに、B0.0004〜0.002%を添加含有せしめても
よい。このように、TiとBを共存させることに
より、結晶の微細化効果を一層高め、部品の仕上
り寸法精度を向上させる。 この出願の第2発明は、第1発明の合金に、
Mn0.2〜1.2%、Cr0.2〜1.2%のうち1種以上の元
素を添加含有せしめて、さらに耐摩耗性を改善し
たものである。 Mn、Crとも、0.2%未満では、耐摩耗性に寄与
する晶出物が十分でなく、1.2%を越えると、晶
出物が粗大化して被削性を害する。従つて、
Mn、Crは0.2〜1.2%の範囲とする。 この出願の第3発明は、第1発明の合金に、
Pb、Bi、Sn、Sbのうち1種以上の元素を総量で
0.5〜2%添加含有せしめ、合金の被削性を、さ
らに向上させたものである。 被削性の向上とは、切削抵抗の減少、切粉の分
断微細化と切削仕上面の精度向上を意味し、単独
より、2種類以上の方が効果的である。0.5%未
満では、上記特性に対して効果はなく、2.0%を
越えると塑性加工性および靭性が極端に低下する
ため得策でない。 これらの元素の含有量(2種類以上の場合は合
計量)が0.5%未満では上記特性に対して効果が
少なく、2.0%を越えると塑性加工性および機械
的強度、特に靭性が極端に低下する。好ましい含
有量は、0.8〜1.4%である。 この出願の第4発明は、第2発明の合金に、さ
らにPb、Bi、Sn及びSbのうち1種以上の元素を
総量で、0.5〜2%添加含有せしめて合金の被削
性をさらに向上させたものである。 本発明合金からなるテープ接触部品を製造する
場合、その出発素材は砂型、金型の鋳物よりはむ
しろ、冷却速度の大きい直冷連続鋳造法によつて
製造される長尺鋳塊を鍛造手段により塑性加工
し、ついで機械的切削手段により成形仕上げされ
ることが最も望ましい。この場合特開昭56−
69348号公報記載の鍛造用アルミニウム合金の製
造法を適用して、冷却速度(連続鋳造時の固液界
面の冷却速度)を25℃/秒以上に保持(特に直径
100mm以下の細径ピレツトがこの条件にふさわし
い)すれば、鋳造性は極めて向上し、長尺鋳塊を
押出し加工することなく直径鍛造加工しうるよう
になり生産性を向上しうるほか、合金塊の組織が
著しく微細化し、かつ金属間化合物からなる第二
相粒子が細かく均一に分散している。このため高
強度で耐摩耗性に富み、加うるにVTRテープ接
触部品として要求される緻密平滑な面いわゆる鏡
面仕上げ加工後の表面粗度は極めて優れたものと
なる。 一般にダイヤモンド切削刃を有する切削工具等
による金属の鏡面仕上げ加工のような精密仕上げ
面が要求される場合、合金塊の組織まで調整する
必要があることが知見されており、上記したよう
な本発明合金の細径長尺鋳塊はかかる要請に適合
する。まさに理想的な合金材料である。 しかし本願発明の合金材は上記したような連続
鋳造塊に限定されるものではなく、金型、砂型、
ダイカスト等の鋳造法によつて成形造塊し、これ
をそのまま又は熱、冷鍛造加工を加えた後、切削
成形加工してVTRテープ接触部品を製造しても
従来の合金材に比し本発明の特徴的効果は充分発
揮されるものである。 以下実施例にもとづいて本発明を説明するが、
その要旨の範囲内で以下の実施例に限定されるも
のではない。 実施例および比較例 第1表に実施例合金No.1〜10、および比較例合
金No.11〜15の合金組成を示す。この表に示した合
金鋳塊の分類において合金鋳塊Aは、垂直半連続
鋳造法によるものである。冷却速度は28℃/秒に
保持され、直径73mmの円柱状長尺鋳塊に製造した
もので、得られた鋳塊の内部組織中のデンドライ
トアーム間隔は、狭く、かつ第2相粒子は微細か
つ均一に分散されていることが認められた。 合金鋳塊Bは、垂直半連続鋳造法によつて得た
直径200mmの円柱状鋳塊を押出して、直径70mmの
丸棒としたものである。 合金鋳塊Cは金型鋳造によつて第2図に示す形
状に造形した。 機械的性質の試験片は、合金材A、Bでは鋳塊
を、又、合金材Cでは、舟底金型鋳塊を各々T6
熱処理(500℃×4時間、水冷焼き入れ、ついで
180℃×8時間の人工時効処理)した後、JIS4号
試験片に加工した。 冷間鍛造性評価用の試験片は、合金材A、Bと
もに、鋳塊を焼鈍熱処理(370℃×4時間、炉冷)
したのちに第3図aに示すウエツジ試験片(L=
150mm、t0=3mm、t1=15mm、W=20mm)に加工
した。 硬さ、切削性、表面粗さ、動摩擦係数、耐食性
の各試験片は、合金材A、Bでは冷間鍛造により
合金材Cでは金型鋳造によつて各々第2図の形状
に造形した。これらの合金材を粗削りした後に上
記と同一条件のT6熱処理を施こし、ついで、ダ
イヤモンド切削刃を有する切削工具によつて鏡面
仕上げ加工を行い、第2図における寸法諸元がD
=63mm、d1=40mm、d2=20mm、H1=16mm、H2
7mmより成るVTR回転ドラムとした。テープが
摺動するドラム外周面の切削条件は切削速度150
m/min、切込み量0.05mm、切削工具送り量0.05
mm/回転であつた。比摩耗量試験片は上記VRT
回転ドラムの一部から切出して判した。 第2表にこれらの試片の特性値を示す。
The present invention applies to magnetic tape contact parts such as VTR (video tape recorder) cylinders, fixed or rotating drums for guiding the tape, etc.
The present invention relates to an aluminum alloy with excellent corrosion resistance suitable for parts of magnetic recording devices that come into direct contact with magnetic tape. A VTR consists of a rotating magnetic head for magnetically recording and reproducing video signals on a magnetic tape, and a stationary or rotating tape guide drum for stably running the magnetic tape. It is known that parts that come into direct contact with the magnetic tape, such as the rotating magnetic head or the tape guide drum, play an extremely important function in maintaining stable tape running without damaging the tape surface that has magnetic particles attached. Therefore, in order to improve the precision of reproduced images (image clarity, color unevenness, etc.), there is a strong demand for improvements in materials for magnetic tape contact parts. Conventionally, VTR tape contact parts have been made of, for example, a copper alloy with Cr hard plating on the surface, an austenitic SUS material, or the like. However, recently, aluminum alloy castings or ingots have been cut or plastic processed (particularly forged) by taking advantage of the advantages of aluminum alloys, such as their light weight, excellent workability, and non-magnetic properties. ,
Magnetic tape contact parts such as VTR drums began to be manufactured. The properties of the aluminum alloy required for the material for magnetic tape contact parts include the following items. (1) Good abrasion resistance against tape. (2) The coefficient of dynamic friction with the tape is small and the tape runs well. (3) Excellent mechanical strength. (4) Excellent machinability and smooth finished surface. (5) Excellent plastic workability, especially cold forgeability. (6) Good corrosion resistance of magnetic tape contact parts in a high temperature and humid atmosphere. Conventionally, JIS2000 series alloys were used as alloys for plastic working.
Al--Cu alloys are well known and widely used as aluminum alloys for magnetic tape contact parts.Although this alloy is excellent in properties 1) to 5) above, There are the following problems with corrosion resistance in a high temperature and humid atmosphere. If magnetic tape is left wrapped around parts that come into contact with the magnetic tape, such as a VTR cylinder, and left in a hot and humid atmosphere for a long time, the parts that come in contact with the magnetic tape, such as the cylinder, will be corroded by moisture that has condensed between the magnetic tape and the cylinder. Not only does this rust occur and the necessary surface smoothness of cylinders etc. is lost, but this rust also embeds the magnetic coating on the magnetic tape, causing the magnetic coating to peel off when the tape is removed. I have come to understand this. As a countermeasure to this problem, Japanese Patent Application Laid-Open No. 1984-19472 describes
A technique has been disclosed in which a chemically treated film is applied to the surface of a metal or alloy, and the film is covered with a sputtered film of chromium or stainless steel. However, this method has the disadvantage of being expensive because the steps of surface treatment and sputter film coating are added to the normal steps. In view of the current situation, the present inventors have developed an aluminum alloy for magnetic tape contact parts that has excellent mechanical properties and excellent corrosion resistance at the magnetic tape contact area in a high temperature and humid atmosphere. As a result of various studies, we found that the content of Si and Mg in particular has a large effect on corrosion in JIS 2000 series Al-Cu alloys for wrought materials, which have been widely used until now. , completed the invention. That is, an object of the present invention is to provide a magnetic tape contacting part that has improved corrosion resistance without impairing properties such as wear resistance, coefficient of dynamic friction, mechanical strength, machinability, plastic workability, and forgeability. The purpose of the present invention is to provide an aluminum alloy, and this technical problem is solved by the following configuration. That is, the gist of the first invention of the present application is as follows: Cu 1 to 6% by weight, Si and Mg, point A (0.15% Si, 0.2% Mg), point B (less than 0.5% Si,
Mg0.2%), point C (Si less than 0.5%, Mg0.8%), point D
(Si0.4%, Mg0.8%), point E (Si0.4%, Mg1.8%),
Corrosion resistance consisting of the amount in the range surrounded by point F (0.15% Si, 1.8% Mg), 0.1 to 1.0% Fe, 0.005 to 0.2% Ti, and the remainder is Al containing normal impurities. The gist of the second invention is to provide an aluminum alloy for magnetic tape contact parts that is excellent in terms of weight. .2%), point B (Si less than 0.5%,
Mg0.2%), point C (Si less than 0.5%, Mg0.8%), point D
(Si0.4%, Mg0.8%), point E (Si0.4%, Mg1.8%),
The amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%, and further includes Mn0.2~1.2%, Cr0.2 The purpose of the third invention is to provide an aluminum alloy for magnetic tape contact parts with excellent corrosion resistance, which contains at least one element among ~1.2%, and the remainder is Al containing ordinary impurities. In Fig. 1, Cu1~6%, Si and Mg were added to point A (Si0.15%, Mg0.2%) and point B (Si less than 0.5%,
Mg0.2%), point C (Si less than 0.5%, Mg0.8%), point D
(Si0.4%, Mg0.8%), point E (Si0.4%, Mg1.8%),
It contains the amount in the range surrounded by point F (0.15% Si, 1.8% Mg), 0.1 to 1.0% Fe, 0.005 to 0.2% Ti, and one of Pb, Bi, Sn, and Sb. The present invention provides an aluminum alloy for magnetic tape contact parts having excellent corrosion resistance, which contains 0.5 to 2% of the total amount of elements of 0.5 to 2%, and the remainder is Al containing ordinary impurities. Cu 1 to 6% by weight, Si and Mg, point A (Si 0.15%, Mg 0.2%), point B (Si less than 0.5%,
Mg0.2%), point C (Si less than 0.5%, Mg0.8%), point D
(Si0.4%, Mg0.8%), point E (Si0.4%, Mg1.8%),
The amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%, and further includes Mn0.2~1.2%, Cu0.2 Contains a total of 0.5 to 2% of one or more elements among ~1.2% and one or more elements of Pb, Bi, Sn, and Sb, and the remainder is Al containing normal impurities. Excellent corrosion resistance. The present invention provides an aluminum alloy for magnetic tape contact parts. The reason for limiting the composition range of the alloy of the present invention will be explained below. In the description of this specification, the contents of all included elements are expressed in weight %. First, the first invention will be explained. Cu: Cu increases the strength of the alloy base and improves machinability. If it is less than 1%, the effect will be insufficient, and if it exceeds 6%, castability, forgeability, and corrosion resistance will deteriorate. Therefore, Cu is in the range of 1 to 6%. Si and Mg: Si and Mg form Mg 2 Si-based precipitates to increase the strength of the alloy. In addition, Mg improves the mechanical strength of the alloy, especially its yield strength, and its synergistic effect with Cu further ensures machinability.
These effects are not sufficient if Si is less than 0.15% and Mg is less than 0.2%. Furthermore, if Si exceeds 0.5% and Mg exceeds 1.8%, a satisfactory finished surface roughness cannot be obtained when cutting magnetic tape contact parts. The content of Si and Mg significantly affects corrosion resistance in a high temperature and humid atmosphere. Corrosion resistance deteriorates significantly in the region where the Si content exceeds 0.4% and the Mg content exceeds 0.8%. Therefore, the amounts of Si and Mg are set within the range surrounded by points A, B, C, D, E, and F in FIG. Fe: Fe is effective in improving wear resistance and machinability. If it is less than 0.1%, no effect will be observed, and if it exceeds 1.0%, forging workability will decrease. Therefore, Fe is in the range of 0.1 to 1.0%. Ti: Ti is an important element because it is effective in making the structure finer and thereby allows achieving finished dimensional accuracy (on the order of μm) of magnetic tape contact parts. If Ti is less than 0.005%, this effect is not recognized, and if it exceeds 0.2%, not only the effect is saturated, but also the forging workability decreases. Therefore, Ti is
It should be in the range of 0.005-0.2%. In carrying out the present invention, 0.0004 to 0.002% of B may be added in addition to the above-mentioned additional elements. In this way, the coexistence of Ti and B further enhances the crystal refinement effect and improves the finished dimensional accuracy of parts. The second invention of this application is based on the alloy of the first invention,
The wear resistance is further improved by adding one or more elements among 0.2 to 1.2% of Mn and 0.2 to 1.2% of Cr. If both Mn and Cr are less than 0.2%, there will be insufficient crystallized substances contributing to wear resistance, and if they exceed 1.2%, the crystallized substances will become coarse and impair machinability. Therefore,
Mn and Cr are in the range of 0.2 to 1.2%. The third invention of this application is based on the alloy of the first invention,
Total amount of one or more elements among Pb, Bi, Sn, and Sb
By adding 0.5 to 2%, the machinability of the alloy is further improved. Improving machinability means reducing cutting resistance, fragmenting chips into fine particles, and improving the accuracy of the cut surface, and two or more types are more effective than using them alone. If it is less than 0.5%, it has no effect on the above properties, and if it exceeds 2.0%, it is not a good idea because the plastic workability and toughness will be extremely reduced. If the content of these elements (total amount if two or more types) is less than 0.5%, there will be little effect on the above properties, and if it exceeds 2.0%, plastic workability and mechanical strength, especially toughness, will be extremely reduced. . The preferred content is 0.8-1.4%. The fourth invention of this application further improves the machinability of the alloy by adding a total amount of 0.5 to 2% of one or more elements among Pb, Bi, Sn, and Sb to the alloy of the second invention. This is what I did. When manufacturing a tape contact part made of the alloy of the present invention, the starting material is not a sand mold or metal mold casting, but rather a long ingot produced by a direct cooling continuous casting method with a high cooling rate, and then forged by a long ingot. Most preferably, it is plastically worked and then shaped and finished by mechanical cutting means. In this case, JP-A-56-
Applying the manufacturing method of aluminum alloy for forging described in Publication No. 69348, the cooling rate (cooling rate of the solid-liquid interface during continuous casting) is maintained at 25°C/second or more (especially when the diameter
If a narrow diameter pillaret of 100 mm or less is suitable for this condition), castability will be greatly improved, and long ingots can be forged in diameter without extrusion, which will improve productivity. The structure has become significantly finer, and the second phase particles made of intermetallic compounds are finely and uniformly dispersed. For this reason, it has high strength and wear resistance, and in addition, it has an extremely excellent surface roughness after being processed to a precise, smooth surface, so-called mirror finishing, which is required for VTR tape contact parts. In general, when a precision finishing surface is required, such as mirror finishing of metal using a cutting tool having a diamond cutting edge, it is known that it is necessary to adjust the structure of the alloy ingot. A long, narrow-diameter ingot of the alloy satisfies these requirements. It is truly an ideal alloy material. However, the alloy material of the present invention is not limited to the above-mentioned continuous casting ingots, but also metal molds, sand molds,
Compared to conventional alloy materials, the present invention can be made by molding ingots using a casting method such as die casting, and then manufacturing VTR tape contact parts by cutting or forming the ingots as they are or by applying heat or cold forging. The characteristic effects of are fully exhibited. The present invention will be explained below based on Examples.
Within the scope of the gist, the present invention is not limited to the following examples. Examples and Comparative Examples Table 1 shows the alloy compositions of Example Alloys No. 1 to 10 and Comparative Example Alloys No. 11 to 15. In the classification of alloy ingots shown in this table, alloy ingot A is produced by the vertical semi-continuous casting method. The cooling rate was maintained at 28°C/sec, and the ingot was manufactured into a long cylindrical ingot with a diameter of 73 mm. The distance between dendrite arms in the internal structure of the obtained ingot was narrow, and the second phase particles were fine. It was also observed that the particles were uniformly dispersed. Alloy ingot B was obtained by extruding a cylindrical ingot with a diameter of 200 mm obtained by a vertical semi-continuous casting method into a round bar with a diameter of 70 mm. The alloy ingot C was formed into the shape shown in FIG. 2 by die casting. The test pieces for mechanical properties were T6 ingots for alloy materials A and B, and boat bottom mold ingots for alloy C.
Heat treatment (500℃ x 4 hours, water cooling quenching, then
After undergoing artificial aging treatment at 180°C for 8 hours, it was processed into JIS No. 4 test pieces. For the test pieces for cold forgeability evaluation, the ingots of both alloy materials A and B were subjected to annealing heat treatment (370°C x 4 hours, furnace cooling).
After that, the wedge test piece shown in Figure 3a (L=
150 mm, t 0 = 3 mm, t 1 = 15 mm, W = 20 mm). Test pieces for hardness, machinability, surface roughness, coefficient of dynamic friction, and corrosion resistance were formed into the shapes shown in FIG. 2 by cold forging for alloy materials A and B, and by die casting for alloy C. After rough-machining these alloy materials, they were subjected to T6 heat treatment under the same conditions as above, and then mirror-finished using a cutting tool with a diamond cutting blade, so that the dimensions in Fig. 2 were D.
= 63mm, d 1 = 40mm, d 2 = 20mm, H 1 = 16mm, H 2 =
The VTR rotating drum is made of 7mm. The cutting conditions for the outer peripheral surface of the drum where the tape slides is a cutting speed of 150.
m/min, depth of cut 0.05mm, cutting tool feed rate 0.05
mm/rotation. The specific wear test piece is the VRT above.
It was cut out from a part of the rotating drum and examined. Table 2 shows the characteristic values of these specimens.

【表】【table】

【表】【table】

【表】 各試験法の概要は次のとおりである。 イ) 引張強さおよび ロ) 伸び オルゼン式50トン万能試験機を用いてJIS4号
試験片によるテストを行つた。 ハ) 冷間鍛造性 第3図aに示すウエツジ試験片1を第3図b
に示す金敷2上に置き、1/2トンハンマー3に
よつて鍛伸し、鍛伸後の試片4の割れ発生位置
を比較することで評価した。評価結果は、◎:
良好、○ふつう、△:やや不良と表示する。 ニ) 硬 さ ビツカース硬度計によつてテープ摺動面直下
の硬さを測定した。 ホ) 切屑処理性 人造焼結ダイヤモンドの切削工具で、切削速
度150m/min、切込み量0.15mmの条件で切削
し、切削屑の形状で比較、評価した。評価結果
は、◎:良好、○:ふつう、△:やや劣ると表
示する。 ヘ) 表面粗さ ドラムの軸方向の表面粗さを、触針式粗さ試
験機にて測定した。 ト) 耐摩耗性 大越式摩耗試験機により、相手をFC30とし、
摩擦速度3m/sec、荷重2.1Kg、摩擦距離600
m、無潤滑の状態で試験し、単位面積のKg当り
の比摩擦量を測定した。 チ) 動摩擦係数 VTRと同様の走行方法で磁気テープの片方
には50grの逆張力(Wp)を負荷し、18.0cm/
秒の相対速度で供試材を回転させ磁気テープの
負荷と相対する片側で作用荷重(WT)を測定
して動摩擦係数を算出した。 リ) 磁気テープ接触部位の耐食性 VTRドラムに、60grの荷重をかけた磁気テ
ープを巻きつけ温度40℃、湿度85%の雰囲気に
1週間保持した後、ドラムと磁気テープについ
て各々が接触し合つていた部分の状態を観察し
た。評価は4段階とした。即ち、 ◎:ドラム、磁気テープに変化なし。 ○:ドラムに小さな腐蝕発生、磁気テープに異
常なし。 △:ドラムに腐蝕発生、磁気テープの所々に磁
性粉のはくりあり。 ×:ドラムが激しく腐蝕、磁気テープの磁性粉
のはくり顕著。 以上の評価で、◎および○は、実用上差し支
えない程度のものである。 上記の耐食性試験によつて得たドラム表面のス
ケツチ図を第4図に、それに対応する磁気テープ
のスケツチ図を第5図に示す。第4図、第5図と
も、aは合金No.2、bは合金No.12に対応する。第
4図bでドラム表面に存在する黒い点が腐蝕部分
であり第5図bでテープ表面の黒い点がドラムの
腐蝕によつて磁性粉がはくりした部分である。 第4図bの腐蝕部の断面を組織観察したとこ
ろ、腐蝕は結晶粒界に伝播して起る粒界腐蝕であ
ることが明らかとなつた。第4図bのドラムの腐
蝕部の断面の顕微鏡組織写真を第6図に示す。 従つて、VTRドラムと磁気テープとを接触さ
せたまま高温、高湿下で静的に放置した場合の耐
食性は、SiおよびMg含有量を管理することによ
つて達成することができる。 第2表の特性値にみられるように、本発明の合
金は、磁気テープ接触部品に要求される機械的性
質に優れ、かつ部品表面にコーテイングなどの特
殊な処理を施さなくとも耐食性に優れており、磁
気テープ接触部品用材料として甚だ好適である。
[Table] A summary of each test method is as follows. A) Tensile strength and B) Elongation Tests were conducted using JIS No. 4 test pieces using an Olsen 50-ton universal testing machine. c) Cold forgeability The wedge test piece 1 shown in Fig. 3a is shown in Fig. 3b.
The specimen was placed on an anvil 2 shown in Figure 1, and forged and stretched using a 1/2 ton hammer 3, and evaluated by comparing the crack occurrence positions in the specimen 4 after forging. The evaluation results are ◎:
Good, ○fair, △: Displayed as slightly poor. d) Hardness The hardness directly below the tape sliding surface was measured using a Bitkers hardness meter. e) Chip disposal property Cutting was performed using an artificial sintered diamond cutting tool at a cutting speed of 150 m/min and a depth of cut of 0.15 mm, and the shape of the chips was compared and evaluated. The evaluation results are indicated as ◎: Good, ○: Fair, and △: Slightly poor. f) Surface roughness The surface roughness of the drum in the axial direction was measured using a stylus roughness tester. g) Abrasion resistance Using an Okoshi type abrasion tester, the test material was FC30.
Friction speed 3m/sec, load 2.1Kg, friction distance 600
The test was conducted without lubrication, and the amount of specific friction per kg of unit area was measured. H) Coefficient of Dynamic Friction A reverse tension (Wp) of 50gr was applied to one side of the magnetic tape using the same running method as a VTR.
The coefficient of dynamic friction was calculated by rotating the test material at a relative speed of seconds and measuring the acting load (WT) on one side facing the magnetic tape load. li) Corrosion resistance of magnetic tape contact parts After wrapping magnetic tape with a load of 60 gr around a VTR drum and keeping it in an atmosphere of 40°C and 85% humidity for one week, the drum and magnetic tape were in contact with each other. I observed the condition of the parts that were in use. The evaluation was in four stages. That is, ◎: No change in drum or magnetic tape. ○: Small corrosion occurred on the drum, no abnormality on the magnetic tape. △: Corrosion occurred on the drum, and magnetic powder was peeled off in some places on the magnetic tape. ×: The drum was severely corroded, and the magnetic powder on the magnetic tape was noticeably peeled off. In the above evaluation, ◎ and ○ indicate that there is no problem in practical use. A sketch of the drum surface obtained from the above corrosion resistance test is shown in FIG. 4, and a corresponding sketch of the magnetic tape is shown in FIG. In both FIGS. 4 and 5, a corresponds to alloy No. 2 and b corresponds to alloy No. 12. The black dots on the drum surface in FIG. 4b are corroded areas, and the black dots on the tape surface in FIG. 5b are areas where magnetic powder has peeled off due to drum corrosion. When the structure of the cross section of the corroded area shown in FIG. 4b was observed, it became clear that the corrosion was intergranular corrosion that propagated to the grain boundaries. FIG. 6 shows a micrograph of the cross section of the corroded portion of the drum shown in FIG. 4b. Therefore, corrosion resistance when the VTR drum and magnetic tape are statically left in contact with each other under high temperature and high humidity can be achieved by controlling the Si and Mg contents. As seen in the characteristic values in Table 2, the alloy of the present invention has excellent mechanical properties required for magnetic tape contact parts, and also has excellent corrosion resistance without special treatment such as coating on the part surface. Therefore, it is extremely suitable as a material for magnetic tape contact parts.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は、SiおよびMgの成分範囲を示す図、
第2図はVTR用回転ドラム形状試験片の断面図、
第3図aは、鍛造性評価のためウエツジ試験片の
形状、第3図bは、鍛造性試験方法の説明図、第
4図および第5図は、高温高湿雰囲気下での耐食
性試験によつて得られたドラム表面(第4図)と
それに対応する磁気テープ(第5図)のスケツチ
図で、それぞれaは、合金No.2、bは合金No.12に
対応する。第6図は、第4図bのドラムの腐蝕部
の断面の顕微鏡組織写真である。
Figure 1 is a diagram showing the component range of Si and Mg;
Figure 2 is a cross-sectional view of a rotating drum-shaped specimen for VTR.
Figure 3a shows the shape of a wedge test piece for forgeability evaluation, Figure 3b is an explanatory diagram of the forgeability test method, and Figures 4 and 5 show the shape of a wedge test piece for forgeability testing. These are sketches of the thus obtained drum surface (FIG. 4) and the corresponding magnetic tape (FIG. 5), in which a corresponds to alloy No. 2 and b corresponds to alloy No. 12, respectively. FIG. 6 is a micrograph of a cross-section of the corroded portion of the drum of FIG. 4b.

Claims (1)

【特許請求の範囲】 1 重量でCu1〜6%と、SiおよびMgを、第1
図の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未
満、Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、
点D(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8
%)、点F(Si0.15%、Mg1.8%)で囲まれた範囲
の量と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、
残部は通常の不純物を含むAlよりなる耐食性に
優れた磁気テープ接触部品用アルミニウム合金。 2 重量でCu1〜6%と、SiおよびMgを、第1
図の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未
満、Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、
点D(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8
%)、点F(Si0.15%、Mg1.8%)で囲まれた範囲
の量と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、
さらにMn0.2〜1.2%、Cr0.2〜1.2%のうち1種以
上の元素とを含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合
金。 3 重量でCu1〜6%と、SiおよびMgを、第1
図の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未
満、Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、
点D(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8
%)、点F(Si0.15%、Mg1.8%)で囲まれた範囲
の量と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、
さらにPb、Bi、Sn、Sbのうち1種以上の元素を
総量で0.5〜2%を含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合
金。 4 重量でCu1〜6%と、SiおよびMgを、第1
図の点A(Si0.15%、Mg0.2%)、点B(Si0.5%未
満、Mg0.2%)、点C(Si0.5%未満、Mg0.8%)、
点D(Si0.4%、Mg0.8%)、点E(Si0.4%、Mg1.8
%)、点F(Si0.15%、Mg1.8%)で囲まれた範囲
の量と、Fe0.1〜1.0%と、Ti0.005〜0.2%を含み、
さらにMn0.2〜1.2%、Cr0.2〜1.2%のうち1種以
上の元素、およびPb、Bi、Sn、Sbのうち1種以
上の元素を総量で0.5〜2%を含み、 残部は通常の不純物を含むAlよりなる耐食性
に優れた磁気テープ接触部品用アルミニウム合
金。
[Claims] 1. 1 to 6% Cu by weight, Si and Mg,
Point A (Si0.15%, Mg0.2%), point B (less than Si0.5%, Mg0.2%), point C (less than Si0.5%, Mg0.8%),
Point D (Si0.4%, Mg0.8%), Point E (Si0.4%, Mg1.8
%), the amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%,
An aluminum alloy for magnetic tape contact parts with excellent corrosion resistance, the remainder of which is Al containing normal impurities. 2 Cu 1 to 6% by weight, Si and Mg in the first
Point A (Si0.15%, Mg0.2%), point B (less than Si0.5%, Mg0.2%), point C (less than Si0.5%, Mg0.8%),
Point D (Si0.4%, Mg0.8%), Point E (Si0.4%, Mg1.8
%), the amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%,
An aluminum alloy for magnetic tape contact parts that further contains 0.2 to 1.2% Mn and 0.2 to 1.2% Cr, and the remainder is Al containing ordinary impurities, and has excellent corrosion resistance. 3 Cu 1-6% by weight, Si and Mg in the first
Point A (Si0.15%, Mg0.2%), point B (less than Si0.5%, Mg0.2%), point C (less than Si0.5%, Mg0.8%),
Point D (Si0.4%, Mg0.8%), Point E (Si0.4%, Mg1.8
%), the amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%,
Furthermore, this aluminum alloy for magnetic tape contact parts has excellent corrosion resistance and contains a total of 0.5 to 2% of one or more elements among Pb, Bi, Sn, and Sb, with the remainder being Al containing ordinary impurities. 4 Cu 1-6% by weight, Si and Mg in the first
Point A (Si0.15%, Mg0.2%), point B (less than Si0.5%, Mg0.2%), point C (less than Si0.5%, Mg0.8%),
Point D (Si0.4%, Mg0.8%), Point E (Si0.4%, Mg1.8
%), the amount in the range surrounded by point F (Si0.15%, Mg1.8%), Fe0.1~1.0%, Ti0.005~0.2%,
Furthermore, it contains one or more elements among 0.2 to 1.2% Mn, 0.2 to 1.2% Cr, and 0.5 to 2% in total of one or more elements among Pb, Bi, Sn, and Sb, with the balance being normal. An aluminum alloy for magnetic tape contact parts that has excellent corrosion resistance and is made of Al containing impurities.
JP4297284A 1984-03-08 1984-03-08 Aluminum alloy for parts to contact with magnetic tape having excellent corrosion resistance Granted JPS60187654A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4297284A JPS60187654A (en) 1984-03-08 1984-03-08 Aluminum alloy for parts to contact with magnetic tape having excellent corrosion resistance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4297284A JPS60187654A (en) 1984-03-08 1984-03-08 Aluminum alloy for parts to contact with magnetic tape having excellent corrosion resistance

Publications (2)

Publication Number Publication Date
JPS60187654A JPS60187654A (en) 1985-09-25
JPH0116901B2 true JPH0116901B2 (en) 1989-03-28

Family

ID=12650949

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4297284A Granted JPS60187654A (en) 1984-03-08 1984-03-08 Aluminum alloy for parts to contact with magnetic tape having excellent corrosion resistance

Country Status (1)

Country Link
JP (1) JPS60187654A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62222040A (en) * 1986-03-24 1987-09-30 Mitsubishi Alum Co Ltd Aluminum alloy excellent in wear resistance and cold forgeability
JPH07113136B2 (en) * 1986-12-02 1995-12-06 古河電気工業株式会社 Free-Cutting Aluminum Alloy Cast Material and Manufacturing Method Thereof
JPH0254736A (en) * 1988-08-17 1990-02-23 Furukawa Alum Co Ltd Wear-resistant aluminum alloy having excellent machinability
JPH0339441A (en) * 1989-07-06 1991-02-20 Sumitomo Light Metal Ind Ltd Aluminum alloy for vtr cylinder
US5980657A (en) * 1998-03-10 1999-11-09 Micron Technology, Inc. Alloy for enhanced filling of high aspect ratio dual damascene structures
US6316356B1 (en) 1998-03-10 2001-11-13 Micron Technology, Inc. Thermal processing of metal alloys for an improved CMP process in integrated circuit fabrication
JP5049481B2 (en) 2005-09-30 2012-10-17 古河スカイ株式会社 Free-cutting aluminum alloy with excellent high-temperature embrittlement resistance
CN105018808B (en) * 2015-08-13 2016-09-28 东北轻合金有限责任公司 A kind of big specification heat treatment can the manufacture method of reinforced aluminium alloy slab ingot

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JPS54153715A (en) * 1978-05-26 1979-12-04 Mitsubishi Keikinzoku Kogyo Aluminum alloy to be used for magnetic tape contact parts
JPS5511118A (en) * 1978-07-07 1980-01-25 Sumitomo Light Metal Ind Ltd Aluminum alloy material for vtr tape rotary member

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