JPS6043454A - Aluminum alloy for vtr cylinder - Google Patents
Aluminum alloy for vtr cylinderInfo
- Publication number
- JPS6043454A JPS6043454A JP15205583A JP15205583A JPS6043454A JP S6043454 A JPS6043454 A JP S6043454A JP 15205583 A JP15205583 A JP 15205583A JP 15205583 A JP15205583 A JP 15205583A JP S6043454 A JPS6043454 A JP S6043454A
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- less
- machinability
- aluminum alloy
- content
- 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
- 229910000838 Al alloy Inorganic materials 0.000 title claims description 15
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 6
- 238000005520 cutting process Methods 0.000 claims abstract description 6
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 6
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 5
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 5
- 229910052797 bismuth Inorganic materials 0.000 claims abstract description 4
- 229910052796 boron Inorganic materials 0.000 claims abstract 3
- 239000000956 alloy Substances 0.000 abstract description 18
- 229910045601 alloy Inorganic materials 0.000 abstract description 17
- 229910052742 iron Inorganic materials 0.000 abstract description 3
- 229910052745 lead Inorganic materials 0.000 abstract description 3
- 229910052759 nickel Inorganic materials 0.000 abstract description 3
- 229910052718 tin Inorganic materials 0.000 abstract description 3
- 229910052802 copper Inorganic materials 0.000 abstract 2
- 229910052719 titanium Inorganic materials 0.000 abstract 2
- 229910052725 zinc Inorganic materials 0.000 abstract 2
- 230000000694 effects Effects 0.000 description 12
- 150000001875 compounds Chemical class 0.000 description 11
- 230000001771 impaired effect Effects 0.000 description 4
- 239000013078 crystal Substances 0.000 description 3
- 238000005553 drilling Methods 0.000 description 3
- 229910000765 intermetallic Inorganic materials 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 229910002482 Cu–Ni Inorganic materials 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910018580 Al—Zr Inorganic materials 0.000 description 1
- 229910018563 CuAl2 Inorganic materials 0.000 description 1
- 229910002555 FeNi Inorganic materials 0.000 description 1
- 229910005347 FeSi Inorganic materials 0.000 description 1
- 229910019743 Mg2Sn Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- QQHSIRTYSFLSRM-UHFFFAOYSA-N alumanylidynechromium Chemical compound [Al].[Cr] QQHSIRTYSFLSRM-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 229940096118 ella Drugs 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- OOLLAFOLCSJHRE-ZHAKMVSLSA-N ulipristal acetate Chemical compound C1=CC(N(C)C)=CC=C1[C@@H]1C2=C3CCC(=O)C=C3CC[C@H]2[C@H](CC[C@]2(OC(C)=O)C(C)=O)[C@]2(C)C1 OOLLAFOLCSJHRE-ZHAKMVSLSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Abstract
Description
【発明の詳細な説明】
本発明はV T Rシリジグ−用アルミニウム合金に関
し、さらに詳しくは、切削性および耐摩耗性に優れたV
TRシリンダ用アルミニウム合金に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an aluminum alloy for VTR series jig, and more specifically, to an aluminum alloy for V
This invention relates to an aluminum alloy for TR cylinders.
現在、\lTRシリンダー用アルミニウム合金として使
用されているものに、A HS合金(A1−10.81
11t%5i−2,1+ut%Cu O,4wL%Mg
)および2218合金(AI−4u+L%Cu−1,5
u+t%Mg−2,0IIIL%Ni)等がある。Currently, AHS alloy (A1-10.81
11t%5i-2,1+ut%CuO,4wL%Mg
) and 2218 alloy (AI-4u+L%Cu-1,5
u+t%Mg-2,0III%Ni), etc.
しかして、AH3合金は耐摩耗性には優れているけれど
も鍛造性に劣り、特に、穴あけ等の機械加工の際にSi
等の硬い金属間化合物や酸化物等のためドリルが折れる
という問題があって槻(威加工性が劣っている。However, although the AH3 alloy has excellent wear resistance, it has poor forgeability, and in particular, when machining such as drilling, Si
There is a problem that the drill will break due to hard intermetallic compounds and oxides, etc., and the machinability is poor.
このようにA I−I S合金には問題点があるため、
適度の耐)I/:耗性と優れた鍛造性を有する2218
系統の合金が多く使用される傾向にある。しかしながら
、2218合金は熱処理後最終\I T Rシリンダ一
部品として、外周の旋盤による切削加]二を行なう際に
切屑処理性の問題があり、さらに、その後の多数の穴あ
けを行なう際に切削性が劣っているので穴あけ時にパ□
すが発生する。そして、このバリ除去のために多数の人
手および時間がかかり生産能率を著しく悪くする。As mentioned above, there are problems with AI-IS alloy, so
Moderate resistance) I/: 2218 with wear resistance and excellent forgeability
There is a tendency for many alloys of this type to be used. However, after heat treatment, the 2218 alloy has problems with chip disposal when the outer circumference is machined with a lathe as a part of the final ITR cylinder. is inferior, so pa□
This occurs. Removal of this burr requires a large amount of manpower and time, which significantly impairs production efficiency.
本発明は上記に説明した現在使用されているVTRシリ
ンダー用アルミニウム合金のA )l S合金および2
218合金の種々の問題点に鑑みなされたものであり、
即ち、2218合金と同程度の強度および鍛造性を有し
ながら2218合金より優れた耐摩耗性を有し、かつ、
切削時の切屑処理性が良好で、さらに、穴あけ加工時に
パリの発生がなく、極めて切削性の優れたNi i’
Rシリンダー用アルミニウム合金を提供するものである
。The present invention is based on the A)lS alloy and 2 of the currently used aluminum alloys for VTR cylinders as described above.
It was created in view of the various problems of 218 alloy,
That is, it has strength and forgeability comparable to that of 2218 alloy, but has superior wear resistance than 2218 alloy, and
Ni i' has excellent chip disposal properties during cutting, and also has no burrs during drilling, and has extremely excellent machinability.
This invention provides an aluminum alloy for R cylinders.
本発明に係るVTRシリンダーアルミニウム合金の特徴
とするところは、Cu’4〜101IIL%、Mn0.
3−1.7u+L%、Fe O’、2−’1.5u+L
%、Ni O,5−3,Ou+t%、PlyO,1〜]
、5+ut%、Sho、1〜2.0田t%を含有し、M
gを0.7wt%以下に抑制し、Z+13.0wt%以
下、Si 3.Ou+L%以゛下、Cr 0.3wL%
以下、ZrO,3IIIL%以下、Bi 1.O+uL
%以下のうちから選んだ1種または2種以上を含有し、
さらに、Ti0.3ψt%以下、B O,ht%以下の
1種または2種を含有し、残部が実質的にA1からなる
ことにある。The VTR cylinder aluminum alloy according to the present invention is characterized by Cu'4-101IIL%, Mn0.
3-1.7u+L%, Fe O', 2-'1.5u+L
%, NiO, 5-3, Ou+t%, PlyO, 1~]
, 5+ut%, Sho, 1-2.0t%, M
g to 0.7 wt% or less, Z+13.0 wt% or less, Si 3. Ou+L% or less, Cr 0.3wL%
Below, ZrO, 3III% or less, Bi 1. O+uL
Contains one or more selected from below %,
Furthermore, it contains one or two of Ti 0.3 ψt % or less and B 2 O, ht % or less, and the remainder consists essentially of A1.
本発明に係るVTRシリンダー用アルミニウム合金はこ
のような構成であるから、主として、CuAl2、Al
−Cu−Ni系化合物の析出硬化、さらに、Mn、Fe
の固溶により充分な強度を保持させ、かつ、MIIAI
6、Mn(Fe)A16、Al−Cu−N1系化合物に
より充分な耐摩耗性を保持させ、切削性は上記化合物の
他にPb−3n或いはPl)−3n−Bi系化合物か含
有されるので驚くへた改善効果を発揮するものである。Since the aluminum alloy for VTR cylinders according to the present invention has such a structure, it mainly contains CuAl2, Al
-Precipitation hardening of Cu-Ni based compounds, furthermore, Mn, Fe
Maintains sufficient strength by solid solution of MIIAI
6. Sufficient wear resistance is maintained by Mn(Fe)A16, Al-Cu-N1 type compounds, and machinability is improved by containing Pb-3n or Pl)-3n-Bi type compounds in addition to the above compounds. It has a surprising effect on improving fatigue.
本発明に係るVTRシリンダー用アルミニウム合金につ
いて前用に説明する。The aluminum alloy for VTR cylinders according to the present invention will be explained first.
先ず、含有成分および成分割合について説明する。First, the contained components and component ratios will be explained.
Cuは強度を高める元素であり、含有量が4+llL%
未′T8もでは効果か充分でなく、また、H)u+t%
を越える含有量では鍛造性が低下する。よって、Cu含
有量は4〜10田L%とする。Cu is an element that increases strength, and the content is 4+llL%
The effect is not sufficient even if T8 is not used, and H) u+t%
If the content exceeds 100%, forgeability deteriorates. Therefore, the Cu content is set to 4 to 10 L%.
Mnは固溶することにより若干強度を高めるが、大部分
はMnAl6、Mn(Fe)A16の金属間化合物を作
って、面l摩耗性および切削性をf」与腰含有量が0.
3u+L%未満ではこれらの効果はなく、また、]、7
vIt%を越える含有量では巨大な初晶化合物を作りV
TRシリンダーとしての性能に欠陥を生じる。よって、
Mn含有量は0.3〜1.7u+t%とする。Mn slightly increases strength by solid solution, but mostly forms intermetallic compounds of MnAl6 and Mn(Fe)A16, which improves surface abrasion resistance and machinability.
There are no these effects below 3u+L%, and ], 7
If the content exceeds vIt%, a huge primary crystal compound is formed and V
This causes defects in the performance of the TR cylinder. Therefore,
Mn content shall be 0.3-1.7u+t%.
Fe1.tMn或いはSiと結合してMn(Fe)A1
.。Fe1. Combined with tMn or Si, Mn(Fe)A1
.. .
ノ\1−FeNi系化合物、ノ\1−FeSi系化合物
を作り、Mn同様に切削性および耐摩耗性を付与し、含
有量が0.2u+t%未満ではこれらの効果が充分でな
く、1.51%を越える含有量ではMn同様にMn(F
ellA 1.の巨大初晶化合物を晶出する。よって
、Fe含有量は0,2〜1.51%とする。No\1-FeNi-based compounds and no\1-FeSi-based compounds are made to provide machinability and wear resistance similar to Mn, but if the content is less than 0.2u+t%, these effects are not sufficient.1. At a content exceeding 51%, Mn (F
ellA 1. crystallizes a gigantic primary crystal compound. Therefore, the Fe content is set to 0.2 to 1.51%.
N1はAl−Cu−Ni系化合物を作り、耐摩耗性、強
度、切削性を改善する元素であり、含有量が0.5u+
L%未満ではこのような効果は充分でなく、3.0u1
1%を越える含有量では粗大な化合物を作り鍛造性を害
する。よって、N1含有量は0.5〜3.OwL%とす
る。N1 is an element that creates Al-Cu-Ni-based compounds and improves wear resistance, strength, and machinability, and the content is 0.5u+
If it is less than L%, such an effect is not sufficient, and 3.0u1
If the content exceeds 1%, a coarse compound is formed and the forgeability is impaired. Therefore, the N1 content is between 0.5 and 3. Let it be OwL%.
円)、SLlの低融点金属は夫々マトリックスに固溶せ
ず微細に分散して存在し、そして、Ply、Snは同時
に含有されることにより極めて大きな切削性改善の効果
を発揮腰夫々単独の含有ではこの効果は小さく、Pb、
Snの含有量か0.1u+L%未7μJでは切削性改善
の効果は充分でなく、円r ]、、5+uL%、511
2、O…t%を越えて含有されると鍛造性、表面仕上り
性を害する。よって、円〕含有量は0.11111%−
1,5wL%とし、Sn含有量は0.1−2.Ou+t
%とする。The low melting point metals of SL1 and SL1 do not form a solid solution in the matrix but exist as finely dispersed particles, and Ply and Sn exhibit an extremely large effect of improving machinability when contained simultaneously. This effect is small in Pb,
If the Sn content is less than 0.1u+L% or 7μJ, the effect of improving machinability is not sufficient;
2. If the content exceeds O...t%, it will impair forgeability and surface finish. Therefore, the content is 0.11111%-
1.5wL%, and the Sn content is 0.1-2. Ou+t
%.
M、は切削性に効果を有する円〕、S11と結合してM
g2Pb、 Mg2Sn化合物を作り切削性を害するの
で、h話合有量は0,7u+L%以下に規制しなければ
ならない。M is a circle that has an effect on machinability], combined with S11, M
Since g2Pb and Mg2Sn compounds are formed and machinability is impaired, the amount of h-carbon must be regulated to 0.7u+L% or less.
Znは切削性を改善する効果を有するが、表面性」二〇
性を害するので含有量は3,0…t%以下とする。Although Zn has the effect of improving machinability, it impairs surface properties, so the content is limited to 3.0...t% or less.
Siは耐摩耗性および切削性を伺与する効果をもつが、
耐蝕性、鍛造性を害するので耐摩耗性および鍛造性の兼
合いを考慮して含有させるのがよいが、含有量が3.0
…1%を越えると鍛造性、表面仕上り性を害する。よっ
て、Si含有量は3.Ou+L%以下とする。Si has the effect of improving wear resistance and machinability, but
Since it impairs corrosion resistance and forgeability, it is better to include it in consideration of the balance between wear resistance and forgeability, but the content is 3.0
...If it exceeds 1%, forgeability and surface finish will be impaired. Therefore, the Si content is 3. Ou+L% or less.
Cr、Zrは夫々Al−Cr系、Al−Zr系の晶出物
を作って耐摩耗性および切削性を向上させるが、0.3
IIIL%を越える含有量では鍛造性、表面仕上り性を
害する。よって、Cr、Zrの含有量は夫々0.3wL
%以下とする。Cr and Zr form Al-Cr-based and Al-Zr-based crystallized products, respectively, to improve wear resistance and machinability, but 0.3
If the content exceeds IIIL%, forgeability and surface finish will be impaired. Therefore, the content of Cr and Zr is 0.3wL each.
% or less.
B1は切削性をさらに改善するためPb、Snに加えて
含有させることができるが、含有量は1.Ou+t%以
下とする。B1 can be included in addition to Pb and Sn to further improve machinability, but the content is 1. Ou+t% or less.
T1、Bは鋳塊の結晶粒を微細化して晶出物或いは低融
点金属を均一分散させ、かつ、表面仕上り性を改善する
効果があり、含有量がTi O,3u+1%およびB
、0.11111%を夫々越えるとA1との間に巨大な
金属間化合物を晶出して、鍛造性、表面仕上I)性を害
する。よって、Ti含有量は0.3u+t%以下、B含
有量は0.11%以下とする。T1 and B have the effect of refining the crystal grains of the ingot, uniformly dispersing crystallized substances or low melting point metals, and improving the surface finish.
, 0.11111%, respectively, a huge intermetallic compound will crystallize between A1 and impair forgeability and surface finish. Therefore, the Ti content is 0.3u+t% or less, and the B content is 0.11% or less.
次に、本発明に係るVTRシリング−用アルミニウム合
金の実施例を説明する。Next, examples of the aluminum alloy for VTR cartridges according to the present invention will be described.
実施例
第1表に示す含有成分および成分割合のアルミニウム合
金を常法に従って)8解鋳造して195φのビレットに
鋳造した後、475°CX8Hrの均熱処理を行なった
後に押出温度400℃で63φの丸棒に押出し、ロール
矯正後450℃X 2 HrのO材処理して切断してV
TRシリング−形状に冷間鍛造した。熱処理は520℃
X60分溶体化後水焼入れしてから焼戻し、180 ’
C’X 8’ HrのT6処理を施した。Example An aluminum alloy having the components and proportions shown in Table 1 was cast into a 195φ billet according to a conventional method, and after soaking at 475°C and 8 hours, it was extruded at a temperature of 400°C and a 63φ billet was cast. Extruded into a round bar, after roll straightening, treated with O material at 450℃ x 2 hours and cut into V
Cold forged to TR Schilling shape. Heat treatment is 520℃
After solution treatment for x60 minutes, water quenching and then tempering, 180'
C'X 8' Hr T6 treatment was performed.
外周切削により切削テストを行ない、l]v硬度を41
11定した。A cutting test was performed by cutting the outer periphery, and the hardness was 41.
It was fixed at 11.
\+゛rRシリンダ一部品については鋭面切削加工後穴
あけを行ないパリの発生状況をみた。\+゛rFor one part of the R cylinder, holes were drilled after machining the sharp surface, and the occurrence of cracks was observed.
また、V T Rシリンダ一部品として従来の2218
合金材と耐摩耗性のテープ走行テストを実施した。In addition, the conventional 2218 is used as a part of the VTR cylinder.
We conducted tape running tests on alloy materials and wear resistance.
これらの調査結果を第2表に示す。The results of these investigations are shown in Table 2.
第2表(2)
硬度:120以上合格
この第2表(1)<2)よりわかるよう1こ、本発明に
係るVTRシリンダ用アルミニウム合金によれば、従来
の2218合金に比較して切削性が著しく改善され、穴
あけ後のパリの発生もみられず、耐摩耗性も良好であっ
た。なお、テープ走行性ら良好であった。Table 2 (2) Hardness: Passed 120 or above As can be seen from Table 2 (1) < 2), the aluminum alloy for VTR cylinders according to the present invention has better machinability than the conventional 2218 alloy. was significantly improved, no flaking was observed after drilling, and wear resistance was also good. Note that the tape running properties were good.
以上説明したように、本発明に係るV T Rシリンダ
ー用アルミニウム合金は上記の構成を有しているもので
あるから、切削性に優れ、かつ、耐摩耗性にも優れてい
るVTRシリンダー用アルミニウム合金として好適なも
のである。As explained above, since the aluminum alloy for VTR cylinders according to the present invention has the above structure, it is an aluminum alloy for VTR cylinders that has excellent machinability and wear resistance. It is suitable as an alloy.
Claims (1)
、FeO,2〜1.5Illt%、Ni0.5〜3,0
iut%、Pb0.1〜1.5+ut%、Sn0.1〜
2.01llL%を含有し、Mgを0.7u+L%以下
に抑制し、Zn3.O切t%以下、Si 3.0ult
%以下、Cr O,3wL%以下、Zr 0.3u+t
%以下、Bi 1.0LllL%以下 のうちから選んだ1種または2種以上を含有し、さらに
、 ′l’i 0.3+uL%以下、B O,ht%以下の
1種または2種を含有し、残部が実質的にA1からなる
ことを特徴とする切削性と耐摩耗性に優れたVTRシリ
ンダー用アルミニウム合金。[Claims] Cu 4-4-1O%, Mn 0.3-1,7u+t%
, FeO, 2-1.5Illt%, Ni0.5-3.0
iut%, Pb0.1-1.5+ut%, Sn0.1-
2.01llL%, suppresses Mg to 0.7u+L% or less, and contains Zn3. O cutting t% or less, Si 3.0ult
% or less, Cr O, 3wL% or less, Zr 0.3u+t
% or less, Bi 1.0LllL% or less, and further contains one or two selected from 'l'i 0.3+uL% or less, B O,ht% or less An aluminum alloy for VTR cylinders having excellent machinability and wear resistance, characterized in that the remainder consists essentially of A1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15205583A JPS6043454A (en) | 1983-08-20 | 1983-08-20 | Aluminum alloy for vtr cylinder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15205583A JPS6043454A (en) | 1983-08-20 | 1983-08-20 | Aluminum alloy for vtr cylinder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6043454A true JPS6043454A (en) | 1985-03-08 |
Family
ID=15532057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15205583A Pending JPS6043454A (en) | 1983-08-20 | 1983-08-20 | Aluminum alloy for vtr cylinder |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6043454A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01272741A (en) * | 1988-04-25 | 1989-10-31 | Showa Alum Corp | Aluminum alloy having excellent wear resistance and machinability |
-
1983
- 1983-08-20 JP JP15205583A patent/JPS6043454A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01272741A (en) * | 1988-04-25 | 1989-10-31 | Showa Alum Corp | Aluminum alloy having excellent wear resistance and machinability |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3485049B1 (en) | Copper-nickel-tin alloy, method for the production and use thereof | |
| DE102016008753B4 (en) | Copper-nickel-tin alloy, process for their production and their use | |
| JPS60215750A (en) | Low temperature ageing of lithium-containing aluminum alloy | |
| US5637160A (en) | Corrosion-resistant bismuth brass | |
| EP3485051B1 (en) | Copper-nickel-tin alloy, method for the production and use thereof | |
| EP3485048B1 (en) | Copper-nickel-tin-alloy, method for the production and use thereof | |
| CN101158000A (en) | Leadless easy-cutting aluminum alloy | |
| US3031299A (en) | Aluminum base alloy | |
| JPH0557348B2 (en) | ||
| US3663213A (en) | Nickel-chromium-iron alloy | |
| JPS58167757A (en) | Preparation of al-mg-si alloy for processing excellent in corrosion resistance, weldability and hardenability | |
| JPS62211351A (en) | Tool steel having superior machinability | |
| JPS60138038A (en) | Aluminum alloy having superior wear resistance and machinability | |
| JPS61183439A (en) | Wear resistant sintered hard alloy having superior oxidation resistance | |
| JPH083701A (en) | Production of wear resistant aluminum alloy extruded material excellent in strength and machinability | |
| US5370752A (en) | Cast steel suitable for machining | |
| JPH0925533A (en) | Aluminum alloy for cutting excellent in cold forgeability and method for manufacturing cold forged aluminum alloy | |
| JPS59193236A (en) | Free cutting aluminum alloy and preparation thereof | |
| JP3225604B2 (en) | Method for producing intermetallic compound precipitation-strengthened Ni-Cr-Mo-based alloy cast member having excellent corrosion resistance | |
| JPS60211034A (en) | Alminium-lithium alloy | |
| JPS6210290B2 (en) | ||
| US3144326A (en) | Casting steel alloy having great tenacity and wear resistance | |
| JPS6039141A (en) | Wear resistant aluminum bronze with high hardness | |
| JPH0797653A (en) | Free-cutting aluminum alloy casting rod | |
| JPH07173567A (en) | Aluminum alloy for forging with excellent machinability |