JPH04341537A - Aluminum alloy having high strength and wear resistance and excellent in cold forgeability - Google Patents

Aluminum alloy having high strength and wear resistance and excellent in cold forgeability

Info

Publication number
JPH04341537A
JPH04341537A JP11213891A JP11213891A JPH04341537A JP H04341537 A JPH04341537 A JP H04341537A JP 11213891 A JP11213891 A JP 11213891A JP 11213891 A JP11213891 A JP 11213891A JP H04341537 A JPH04341537 A JP H04341537A
Authority
JP
Japan
Prior art keywords
alloy
wear resistance
cold forgeability
aluminum alloy
strength
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.)
Granted
Application number
JP11213891A
Other languages
Japanese (ja)
Other versions
JP2776645B2 (en
Inventor
Yoshimasa Okubo
喜正 大久保
Hideo Sano
秀男 佐野
Shuntaro Sudo
俊太郎 須藤
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.)
Sumitomo Light Metal Industries Ltd
Toyota Motor Corp
Original Assignee
Sumitomo Light Metal Industries Ltd
Toyota Motor Corp
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 Sumitomo Light Metal Industries Ltd, Toyota Motor Corp filed Critical Sumitomo Light Metal Industries Ltd
Priority to JP11213891A priority Critical patent/JP2776645B2/en
Publication of JPH04341537A publication Critical patent/JPH04341537A/en
Application granted granted Critical
Publication of JP2776645B2 publication Critical patent/JP2776645B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To obtain the alloy by incorporating Mn and Cr and specifying a composition in an alloy where hard grains of SiC, etc., are dispersed into an Al-Cu-Mg-Si series. CONSTITUTION:This Al alloy has a composition consisting of, by weight, 2.5-5.5% Cu, 0.3-2.5% Mg, 0.1-0.19% Si, 0.3-1.0% Mn and/or Cr, and the balance Al and further containing, if necessary, 0.02-0.7% Ti and/or Zr. The Al alloy can be prepared by dispersing one or more kinds among ceramic grains of Si, Si3N4, etc., metal grains of ferromolybdenum, Co-Cr-W-C alloy, Co-Cr-Mo-Si alloy, etc., and grains harder than the matrix alloy, e.g., intermetallic compound, such as TiAl and FeAl, by 0.2-5vol.% into the Al alloy matrix. This Al alloy combines superior strength and wear resistance with excellent cold forgeability and can be suitably used for producing engine parts, such as valve lifter and valve spring retainer.

Description

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

【0001】0001

【産業上の利用分野】本発明は、すぐれた高力アルミニ
ウム合金の耐摩耗性を改善し、バルブリフター、バルブ
スプリングリテーナー、オイルポンプギア、スプロケッ
ト、プ−リ−その他エンジン部品に応用し得る冷間鍛造
性にすぐれた高強度耐摩耗性アルミニウム合金に関する
ものである。
[Industrial Application Field] The present invention improves the wear resistance of an excellent high-strength aluminum alloy, and is applicable to valve lifters, valve spring retainers, oil pump gears, sprockets, pulleys, and other engine parts. This invention relates to a high-strength, wear-resistant aluminum alloy with excellent forgeability.

【0002】0002

【従来の技術】最近、エンジンを従来の鋼材に代えてア
ルミニウム合金を用いて作製し、軽量化して省エネルギ
ーを図ることが行われている。しかし、特にバルブリフ
ター、バルブスプリングリテーナー、プーリーその他エ
ンジン部品は高温強度、耐摩耗性が必要とされるため、
現在まで鉄系材料が主として使われてきた。
2. Description of the Related Art Recently, engines have been manufactured using aluminum alloys instead of conventional steel materials to reduce weight and save energy. However, valve lifters, valve spring retainers, pulleys, and other engine parts in particular require high-temperature strength and wear resistance.
Until now, iron-based materials have been mainly used.

【0003】これらの部品を軽量化するため、Al合金
を使用すると、通常のAl合金では耐摩耗性が不足する
。そこで耐摩耗性不足を補うため、Al中にセラミック
粒子を複合した材料が開発されている(例えば特開昭6
4−56844号参照)。これらの部品を量産化するに
は、冷間鍛造によって成形することが望ましいが、上記
の材料では冷間鍛造が困難である。
[0003] When Al alloys are used to reduce the weight of these parts, ordinary Al alloys lack wear resistance. Therefore, in order to compensate for the lack of wear resistance, materials have been developed that are composites of ceramic particles in Al (for example, JP-A No. 6
4-56844). In order to mass produce these parts, it is desirable to form them by cold forging, but cold forging is difficult with the above materials.

【0004】0004

【発明が解決しようとする課題】そこで先にこの問題を
解決するため、Al−Cu−Mg−Si系にSiCその
他の硬質粒子を分散させてなる合金を開発している。 (特願平2−96487号)この合金は、すぐれた冷間
鍛造性を有しているが、複雑形状の部品を量産するため
には、さらにすぐれた冷間鍛造性を有する合金が必要と
されている。
[Problem to be Solved by the Invention] In order to solve this problem first, an alloy made of Al--Cu--Mg--Si with SiC and other hard particles dispersed therein has been developed. (Patent Application No. 2-96487) This alloy has excellent cold forgeability, but in order to mass produce parts with complex shapes, an alloy with even better cold forgeability is required. has been done.

【0005】本発明はかかる点に鑑み、高強度と耐摩耗
性とを兼ね備え、しかも十分な冷間鍛造性をもったアル
ミニウム合金を提供せんとするものである。
[0005] In view of these points, the present invention aims to provide an aluminum alloy that has both high strength and wear resistance, and also has sufficient cold forgeability.

【0006】[0006]

【課題を解決するための手段】本発明は、Cu:2.5
〜5.5%、Mg:0.3〜2.5%、Si:0.1〜
0.19%と更に、MnとCrの1種または2種:0.
3〜1.0%を含み、あるいはさらにこれらにTiとZ
rの1種または2種:0.02〜0.7%を含み、残部
が不可避的不純物を含むAlからなるアルミニウム合金
マトリックスの中に、SiC、Si3N4、ZrO2、
Al2O3、ZrSiO4、ムライトの如きセラミック
粒子あるいはフェロモリブデン、Co−Cr−W−C合
金、Co−Cr−Mo−Si合金、タングステンの如き
金属粒子あるいはTiAl、FeAl、Ni3Alの如
き金属間化合物のようなマトリックス合金よりも硬質な
粒子の1種又は2種以上を0.2〜5vol%を分散さ
せてなる冷間鍛造性にすぐれた高強度耐摩耗性アルミニ
ウム合金である。
[Means for Solving the Problems] The present invention provides Cu: 2.5
~5.5%, Mg: 0.3~2.5%, Si: 0.1~
0.19%, and one or both of Mn and Cr: 0.19%.
3 to 1.0%, or further contains Ti and Z.
SiC, Si3N4, ZrO2,
Ceramic particles such as Al2O3, ZrSiO4, mullite or metal particles such as ferromolybdenum, Co-Cr-W-C alloy, Co-Cr-Mo-Si alloy, tungsten or intermetallic compounds such as TiAl, FeAl, Ni3Al. This is a high-strength, wear-resistant aluminum alloy with excellent cold forgeability, which is made by dispersing 0.2 to 5 vol% of one or more types of particles harder than the matrix alloy.

【0007】上記において合金成分、硬質粒子の限定理
由は下記のとおりである。
The reasons for limiting the alloy components and hard particles in the above are as follows.

【0008】Cu:常温及び高温強度を向上する。2.
5%未満ではその効果が小さく、5.5%を超えると冷
間鍛造性が低下する。
[0008] Cu: Improves strength at room temperature and high temperature. 2.
If it is less than 5%, the effect will be small, and if it exceeds 5.5%, cold forgeability will deteriorate.

【0009】Mg:Cuと共存して時効硬化して常温及
び高温強度を高める。0.3%未満では効果が十分でな
く、2.5%を越えると冷間鍛造性が低下する。
[0009] Mg: Coexists with Cu and ages hardens to increase strength at room temperature and high temperature. If it is less than 0.3%, the effect is not sufficient, and if it exceeds 2.5%, cold forgeability deteriorates.

【0010】Si:Siの添加によりAl−Cu−Mg
系析出中間相(S´)が微細に形成され、時効硬化量が
大きくなる。更に後述のMnあるいはCrが共存してい
るとAl−Mn−Si系析出相あるいはAl−Cr−S
i系析出相が生じ、これが、転位のピンニング効果を高
め、サブグレイン組織ないし微細な再結晶組織となる。 0.1%未満ではその効果が認められず、0.19%を
越えると一部のSiが粒界上に析出するため冷間鍛造性
を低下させる。
[0010]Si: By adding Si, Al-Cu-Mg
The system precipitated intermediate phase (S') is formed finely, and the amount of age hardening increases. Furthermore, if Mn or Cr (described later) coexists, an Al-Mn-Si precipitate phase or Al-Cr-S
An i-based precipitate phase is generated, which enhances the pinning effect of dislocations and becomes a subgrain structure or a fine recrystallized structure. If it is less than 0.1%, no effect will be observed, and if it exceeds 0.19%, some Si will precipitate on the grain boundaries, reducing cold forgeability.

【0011】Mn、Cr:前述したように、Siと共存
して再結晶組織が微細になる。この結果、T4あるいは
T6処理材における常温および高温強度を向上させ、同
時に延性、靭性も向上する。延性および靭性向上の効果
は0.5〜0.6%のとき最も強く現れ、0.3%未満
でも1.0%を超えても、その効果は不十分である。さ
らに0.3%未満のときは強度の向上が認められない。
Mn, Cr: As mentioned above, they coexist with Si and the recrystallized structure becomes fine. As a result, the room temperature and high temperature strength of the T4 or T6 treated material is improved, and at the same time, the ductility and toughness are also improved. The effect of improving ductility and toughness appears most strongly when the content is 0.5 to 0.6%, and the effect is insufficient when the content is less than 0.3% or more than 1.0%. Furthermore, when the content is less than 0.3%, no improvement in strength is observed.

【0012】Ti、Zr:凝固時の結晶粒を微細化する
とともに、溶体化処理中に発生する再結晶を抑制し、繊
維状組織あるいは微細な再結晶を有する組織をつくり、
強度を向上させる。合計量が0.02%未満ではその効
果が小さく、0.7%を越えると効果が飽和する。
Ti, Zr: refines crystal grains during solidification, suppresses recrystallization that occurs during solution treatment, creates a fibrous structure or a structure with fine recrystallization,
Improve strength. If the total amount is less than 0.02%, the effect will be small, and if it exceeds 0.7%, the effect will be saturated.

【0013】硬質粒子:SiC、Si3N4、ZrO2
、Al2O3、ZrSiO4、ムライト等のセラミック
粒子、フェロモリブデン、Co−Cr−W−C合金、C
o−Cr−Mo−Si合金、タングステン等の金属粒子
あるいはTiAl、FeAl、Ni3Alの如き金属間
化合物の如き硬質粒子を添加することによって耐摩耗性
が大幅に向上する。0.2vol%未満では耐摩耗性が
十分でなく、5vol%超えると冷間鍛造性および切削
性が低下する。
Hard particles: SiC, Si3N4, ZrO2
, Al2O3, ZrSiO4, ceramic particles such as mullite, ferromolybdenum, Co-Cr-W-C alloy, C
By adding hard particles such as o-Cr-Mo-Si alloys, metal particles such as tungsten, or intermetallic compounds such as TiAl, FeAl, Ni3Al, the wear resistance is greatly improved. If it is less than 0.2 vol%, wear resistance will not be sufficient, and if it exceeds 5 vol%, cold forgeability and machinability will deteriorate.

【0014】[0014]

【実施例】表1に示す成分の硬質粒子を含むアルミニウ
ム合金を製造した。製造方法は次のとおりである。
EXAMPLE An aluminum alloy containing hard particles having the components shown in Table 1 was produced. The manufacturing method is as follows.

【0015】エアアトマイズ法によって各種Al合金粉
末を製造後149μm以下に分級し、これに所定の粒度
および量の硬質粒子を加えボ−ルミルによって混合した
。 この混合粉末を外径2.5インチのアルミニウム缶に装
入した後、缶内の空気及び粉末表面に吸着している水分
を取除くため480℃にて1時間の真空脱ガス処理をし
て、これを押出用ビレットとした。これを400℃で直
径18mmに押出した(押出比15)。そして、冷間鍛
造性を評価するため軟化処理(300℃×5h保持→空
冷)を施し、据込み試験を実施して限界据込率を測定し
た。又、T6処理(495℃×1h保持→水焼入れ→1
85℃×6h保持)を施し、引張試験及びピン・ディス
ク式摩耗試験を行った。 結果を表1に併記する。ここで摩耗量とは、摩擦摩耗試
験(120℃のマシン油の中でピンを供試合金、ディス
クをFC20として、50kgf/cm2(4.9MP
a)の面圧、速度0.5m/secで摩擦を1時間行う
)におけるピンの長さ減量である。
After producing various Al alloy powders by air atomization, they were classified to 149 μm or less, and hard particles of a predetermined particle size and amount were added thereto and mixed using a ball mill. After charging this mixed powder into an aluminum can with an outer diameter of 2.5 inches, vacuum degassing treatment was performed at 480°C for 1 hour to remove the air inside the can and moisture adsorbed on the powder surface. This was made into a billet for extrusion. This was extruded at 400°C to a diameter of 18 mm (extrusion ratio 15). Then, in order to evaluate cold forgeability, a softening treatment (holding at 300° C. for 5 hours → air cooling) was performed, and an upsetting test was conducted to measure the limit upsetting rate. In addition, T6 treatment (495°C x 1h holding → water quenching → 1
A tensile test and a pin-disk abrasion test were conducted. The results are also listed in Table 1. Here, the amount of wear is 50 kgf/cm2 (4.9 MP
This is the reduction in the length of the pin under a) friction is performed for 1 hour at a surface pressure of 0.5 m/sec and a speed of 0.5 m/sec.

【0016】[0016]

【表1】[Table 1]

【0017】上記表1から明らかなとおり、本発明合金
No.1〜14は高い強度、伸びおよび限界据込率を示
し、更にピンの摩耗量も小さい。これに対し、比較合金
No.15は硬質粒子を含んでいないためピンの摩耗量
が大きい。No.16はCuが少ないため強度が十分で
なく、No.17はCuが多いため限界据込率が低い。 No.18はMgが少ないために強度が十分でなく、N
o.19はMgが多いために限界据込率が低い。No.
20はSiが多いために限界据込率が低い。
[0017] As is clear from Table 1 above, the present invention alloy No. Nos. 1 to 14 exhibit high strength, elongation, and limit upsetting rate, and furthermore, pin wear is small. In contrast, comparative alloy No. Since No. 15 does not contain hard particles, the amount of pin wear is large. No. No. 16 does not have sufficient strength due to a small amount of Cu. No. 17 has a low marginal upsetting rate because it contains a lot of Cu. No. 18 does not have sufficient strength due to low Mg content, and N
o. No. 19 has a low marginal upsetting rate due to its high Mg content. No.
No. 20 has a low marginal upsetting rate because it has a large amount of Si.

【0018】[0018]

【発明の効果】本発明によれば強度と耐摩耗性にすぐれ
、しかもすぐれた冷間鍛造性を兼ね備えたアルミニウム
合金を得ることができる。したがって、本発明合金はバ
ルブリフター、バルブスプリングリテーナーをはじめ、
エンジン部品等に適し、従来の鋼製品と置き換え得る材
料である。
[Effects of the Invention] According to the present invention, an aluminum alloy having excellent strength and wear resistance as well as excellent cold forgeability can be obtained. Therefore, the alloy of the present invention can be used in valve lifters, valve spring retainers, etc.
This material is suitable for engine parts and can replace conventional steel products.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】  Cu:2.5〜5.5%(重量%:以
下同じ)、Mg:0.3〜2.5%、Si:0.1〜0
.19%と更に、MnとCrの1種または2種:0.3
〜1.0%を含み、残部が不可避的不純物を含むAlか
らなるアルミニウム合金マトリックスの中に、SiC、
Si3N4、ZrO2、Al2O3、ZrSiO4、ム
ライトの如きセラミック粒子あるいはフェロモリブデン
、Co−Cr−W−C合金、Co−Cr−Mo−Si合
金、タングステンの如き金属粒子あるいはTiAl、F
eAl、Ni3Alの如き金属間化合物のようなマトリ
ックス合金よりも硬質な粒子の1種又は2種以上を0.
2〜5vol%分散させてなる冷間鍛造性にすぐれた高
強度耐摩耗性アルミニウム合金。
[Claim 1] Cu: 2.5 to 5.5% (weight %: same below), Mg: 0.3 to 2.5%, Si: 0.1 to 0
.. 19% and one or two of Mn and Cr: 0.3
SiC,
Ceramic particles such as Si3N4, ZrO2, Al2O3, ZrSiO4, mullite or metal particles such as ferromolybdenum, Co-Cr-W-C alloy, Co-Cr-Mo-Si alloy, tungsten or TiAl, F
One or more types of particles harder than the matrix alloy such as intermetallic compounds such as eAl and Ni3Al are mixed with 0.
A high-strength, wear-resistant aluminum alloy with excellent cold forgeability made by dispersing 2 to 5 vol%.
【請求項2】  Cu:2.5〜5.5%、Mg:0.
3〜2.5%、Si:0.1〜0.19%と更にMnと
Crの1種又は2種:0.3〜1.0%、TiとZrの
1種又は2種:0.02〜0.7%を含み、残部が不可
避的不純物を含むAlからなるアルミニウム合金マトリ
ックスの中に、SiC、Si3N4、ZrO2、Al2
O3、ZrSiO4、ムライトの如きセラミック粒子あ
るいはフェロモリブデン、Co−Cr−W−C合金、C
o−Cr−Mo−Si合金、タングステンの如き金属粒
子あるいはTiAl、FeAl、Ni3Alの如き金属
間化合物のようなマトリックス合金よりも硬質な粒子の
1種又は2種以上を0.2〜5vol%分散させてなる
冷間鍛造性にすぐれた高強度耐摩耗性アルミニウム合金
[Claim 2] Cu: 2.5 to 5.5%, Mg: 0.
3 to 2.5%, Si: 0.1 to 0.19%, and further one or two of Mn and Cr: 0.3 to 1.0%, one or two of Ti and Zr: 0. SiC, Si3N4, ZrO2, Al2
O3, ZrSiO4, ceramic particles such as mullite or ferromolybdenum, Co-Cr-W-C alloy, C
Dispersion of 0.2 to 5 vol% of one or more particles harder than the matrix alloy, such as o-Cr-Mo-Si alloy, metal particles such as tungsten, or intermetallic compounds such as TiAl, FeAl, and Ni3Al. A high-strength, wear-resistant aluminum alloy with excellent cold forging properties.
JP11213891A 1991-04-18 1991-04-18 High-strength wear-resistant aluminum alloy with excellent cold forgeability Expired - Fee Related JP2776645B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11213891A JP2776645B2 (en) 1991-04-18 1991-04-18 High-strength wear-resistant aluminum alloy with excellent cold forgeability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11213891A JP2776645B2 (en) 1991-04-18 1991-04-18 High-strength wear-resistant aluminum alloy with excellent cold forgeability

Publications (2)

Publication Number Publication Date
JPH04341537A true JPH04341537A (en) 1992-11-27
JP2776645B2 JP2776645B2 (en) 1998-07-16

Family

ID=14579165

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11213891A Expired - Fee Related JP2776645B2 (en) 1991-04-18 1991-04-18 High-strength wear-resistant aluminum alloy with excellent cold forgeability

Country Status (1)

Country Link
JP (1) JP2776645B2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08120378A (en) * 1994-08-25 1996-05-14 Honda Motor Co Ltd Heat resistant and wear resistant aluminum alloy, aluminum alloy retainer and aluminum alloy valve lifter
US5616192A (en) * 1994-07-21 1997-04-01 Fuji Oozx Inc. Coil retainer for engine valve and preparation of the same
GB2334966A (en) * 1998-03-05 1999-09-08 Aeromet International Plc An aluminium-copper alloy
JP2001032033A (en) * 1999-07-23 2001-02-06 Toshiba Tungaloy Co Ltd Friction material
KR20030065018A (en) * 2002-01-29 2003-08-06 (주) 우리산업기계 Check valve made of aluminum alloy
CN108411172A (en) * 2018-04-11 2018-08-17 安徽建国电力有限公司 A kind of high intensity and high abrasion composite aluminum base material and preparation method thereof
CN111118358A (en) * 2020-01-07 2020-05-08 北京工业大学 Er-containing castable wrought Al-Cu alloy

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5616192A (en) * 1994-07-21 1997-04-01 Fuji Oozx Inc. Coil retainer for engine valve and preparation of the same
JPH08120378A (en) * 1994-08-25 1996-05-14 Honda Motor Co Ltd Heat resistant and wear resistant aluminum alloy, aluminum alloy retainer and aluminum alloy valve lifter
GB2334966A (en) * 1998-03-05 1999-09-08 Aeromet International Plc An aluminium-copper alloy
US6126898A (en) * 1998-03-05 2000-10-03 Aeromet International Plc Cast aluminium-copper alloy
GB2334966B (en) * 1998-03-05 2003-03-05 Aeromet Internat Plc Cast aluminium-copper alloy
JP2001032033A (en) * 1999-07-23 2001-02-06 Toshiba Tungaloy Co Ltd Friction material
KR20030065018A (en) * 2002-01-29 2003-08-06 (주) 우리산업기계 Check valve made of aluminum alloy
CN108411172A (en) * 2018-04-11 2018-08-17 安徽建国电力有限公司 A kind of high intensity and high abrasion composite aluminum base material and preparation method thereof
CN111118358A (en) * 2020-01-07 2020-05-08 北京工业大学 Er-containing castable wrought Al-Cu alloy
CN111118358B (en) * 2020-01-07 2021-02-02 北京工业大学 Er-containing castable wrought Al-Cu alloy

Also Published As

Publication number Publication date
JP2776645B2 (en) 1998-07-16

Similar Documents

Publication Publication Date Title
US7811395B2 (en) High strength L12 aluminum alloys
US20130240095A1 (en) Heat treatable l12 aluminum alloys
US20100252148A1 (en) Heat treatable l12 aluminum alloys
WO2012026354A1 (en) Co-based alloy
JPS63157831A (en) Heat-resisting aluminum alloy
JPH04341537A (en) Aluminum alloy having high strength and wear resistance and excellent in cold forgeability
JPS63312901A (en) Heat resistant high tensile al alloy powder and composite ceramics reinforced heat resistant al alloy material using said powder
JP3504917B2 (en) Aluminum-beryllium-silicon alloy for automotive engine moving parts and casing members
CN1320713A (en) High-Al Zn-base alloy
JP3920656B2 (en) High rigidity aluminum alloy containing boron
JP2711296B2 (en) Heat resistant aluminum alloy
JPS6244547A (en) Composite aluminum alloy material
JPH01316442A (en) Hot processing aluminum base alloy
JPH03294446A (en) Heat-resistant and wear-resistant aluminum alloy
US5370752A (en) Cast steel suitable for machining
JP2007527951A (en) Cast iron material
JPH08144002A (en) High strenght aluminum alloy excellent in heat resistance
JPH1017975A (en) Aluminum alloy for casting
JPH01177340A (en) Thermo-mechanical treatment of high-strength and wear-resistant al powder alloy
JPH036344A (en) Aluminum alloy having heat resistance and wear resistance
JPS63183148A (en) Wear resistant al-si-mn sintered alloy
JPH01290738A (en) Aluminum alloy having excellent heat resistance
JP2787703B2 (en) A-l-Si alloy powder forged member with extremely low coefficient of thermal expansion
JP3179095B2 (en) Valve train members for internal combustion engines
JPS62149840A (en) High strength, heat and wear resistant al alloy

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees