JPH0321618B2 - - Google Patents

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Publication number
JPH0321618B2
JPH0321618B2 JP58100185A JP10018583A JPH0321618B2 JP H0321618 B2 JPH0321618 B2 JP H0321618B2 JP 58100185 A JP58100185 A JP 58100185A JP 10018583 A JP10018583 A JP 10018583A JP H0321618 B2 JPH0321618 B2 JP H0321618B2
Authority
JP
Japan
Prior art keywords
aluminum
alloy
molybdenum
weight
master alloy
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 - Lifetime
Application number
JP58100185A
Other languages
Japanese (ja)
Other versions
JPS59226147A (en
Inventor
Yoshi Kitai
Tamotsu Akeno
Masao Tomita
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.)
Shinko Chemical Co Ltd
Original Assignee
Shinko Chemical Co Ltd
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 Shinko Chemical Co Ltd filed Critical Shinko Chemical Co Ltd
Priority to JP10018583A priority Critical patent/JPS59226147A/en
Publication of JPS59226147A publication Critical patent/JPS59226147A/en
Publication of JPH0321618B2 publication Critical patent/JPH0321618B2/ja
Granted legal-status Critical Current

Links

Description

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

〔産業分野〕 この発明は軽くて、耐蝕性、耐熱性に優れたチ
タン(Ti)合金、例えばTi−6Al−2Sn−4zr−
6Mo合金、Ti−6Al−2Sn−4zr−2Mo合金等の
溶製に適するチタニウム合金製造用のアルミニウ
ム(Al)、モリブデン(Mo)母合金に係るもの
である。 従来Ti合金溶製に供される母合金としては、
Al−V(バナジウム)母合金が特公昭53−7368又
は特公昭53−8642の特許公報において知られてい
るが、本件発明前において、発明者はTi合金溶
製のための実用性のあるAl−Mo母合金の存在を
知らない。 純金属Al−Moの基本状態図としては、出願人
会社において実験したところ図に示す通りであ
り、図中、曲線CDE、FEは液相線を示すもので
あり、Mo57重量%以下においては包晶系である
ために液相状態から冷却させた場合に曲線DCに
おいて初晶としてAl8Mo3を折出し、以後1130℃
までAl8Mo3を折出し続けるがこゝで凝固が完了
せずさらに735℃まで溶接状態が続くため、生成
される合金は放出ガスによる巣や、収縮孔の発生
及び成分偏析を起こし、Al−Mo母合金に要求さ
れる清浄性、及び均質性にかける。また結晶の粗
大化した合金の為、Ti合金用母合金として要求
される粒度に調整する場合、微粉が発生する等加
工上の歩留が著しく低下し、実用に供し得るもの
ではない。 そこで、発明者は前記状態図の曲線DE間の
Mo57乃至67重量%の共晶系部に着目し、その共
晶反応線GEHより低温固相部において凝固が共
晶組織よりなる母合金が得られることを知見し
た。 Al−Moの溶製法としては、誘導溶製、真空ア
ーク炉内の溶接、アルミノテルミツト溶製の三つ
が考えられるが、誘導溶製法は術式が極めて複雑
で装置も高価であり、AlとMoの比重差による合
金内部の偏析も大きい。また真空アーク炉内での
溶製法においてもアーク電柱の溶解によつて、母
合金が汚染されるし、また均質な母合金ができ難
い。アルミノテルミツト溶製法は、その装置が簡
単なことゝ、反応時間が短かい特質を有するが、
その特質故に、従来Mo50重量%、残部Alの組成
においては反応が激しく、爆発に近い反応とな
り、その組成物のるつぼ外への噴出及び揮散が激
しく、収率が著しく低下(約50%)し、Al−Mo
のアルミノテルミツト法において溶製できる組成
比は従来Mo50重量%以下とされていたが、この
組成比では前述の通り包晶系の域であつて、実用
に供し得ない。 そこで発明者は、従来極めて困難とされていた
前記共晶系部分におけるアルミノテルミツト法の
実用的方法を開発した。 〔目的〕 この発明の目的とするところは、 組成の共晶組織Al−Mo母合金の新規物質を得
るための方法を開発することであり、反応が激し
くなくて、Alの蒸発や、MoO3の揮散による損失
が少なく、周率が著しく高く、清浄なAl−Mo母
合金を得るためのものである。 また他の目的とするところは、この新規物質は
Tiの融点に比較的近く、破砕した場合に微粉化
せず、粒度調整が容易な母合金たる新規物質を得
ることを目的とする。 〔構成〕 この発明はアルミニウム・モリブデン合金にお
いて、これらの合金組成がアルミニウム33乃至43
重量%、モリブデン57乃至67重量%の共晶組織よ
りなることを特徴とするチタニウム合金製造用の
アルミニウム・モリブデン母合金である。 また他の発明はアルミニウム粉末と酸化モリブ
デン粉末を混合し、テルミツト法を用いて反応さ
せる場合において、母合金組織をアルミニウム33
乃至43重量%、モリブデン57乃至67重量%となる
ように、前記酸化モリブデン粉末とアルミニウム
粉末を混合し、これらの混合物の重量に対し、重
量比で約30乃至50%、好ましくは42乃至43%、の
造滓剤を入れることを特徴とするアルミニウム・
モリブデン母合金の製造法である。 〔効果〕 上述のような方法を採用することによつて、ア
ルミノテルミツト法を用いたとしても、造滓剤を
上述の比で用いることによつてるつぼ中における
反応によつて、内部の組成物が散逸する程の激し
い反応を起さず、かつこれら造滓剤によるスラグ
は液湯の表面を覆い、Alの揮散や、MoO3の状態
での揮発を防ぎ、かつAl−Moの重量比が上述の
範囲内においては、共晶域であるから、溶製され
た合金は共晶組織となる。またMoの重量%の上
限が67重量%としたために次のような欠点がな
い。即ち共晶点Eに余りにも近ずくとAlsMo3
晶の析出後、共晶析出までの凝固温度範囲が余り
にも狭く、比金属介在物の巻き込みが起り、また
ガスの放出が不完全となり、母合金の必要条件で
ある清浄な合金と気孔のない物が得がたくなる。
又従来テルミツト法では、溶湯を抜き出し、脱ガ
ス処理を行ない、鋳型に鋳込むという複雑な処理
が行なわれているが、この発明では単に反応炉
で、若くは鋳型に注き込んで冷却凝固させる簡単
な方法で極めて良好な合金を得る。 またこの方法により得られた母合金は粉砕した
場合の粒度調整が簡便である。 今この発明を以下の実験例に従つて具体的に説
明する。
[Industrial field] This invention is a lightweight titanium (Ti) alloy with excellent corrosion resistance and heat resistance, such as Ti-6Al-2Sn-4zr-
The present invention relates to aluminum (Al) and molybdenum (Mo) master alloys for producing titanium alloys suitable for melting 6Mo alloys, Ti-6Al-2Sn-4zr-2Mo alloys, etc. The master alloys conventionally used for Ti alloy melting are:
Al-V (vanadium) master alloy is known from Japanese Patent Publication No. 53-7368 or Japanese Patent Publication No. 53-8642. -I don't know about the existence of Mo master alloy. The basic phase diagram of pure metal Al-Mo is as shown in the figure, based on experiments carried out by the applicant's company. In the figure, curves CDE and FE indicate liquidus lines, and when Mo is 57% by weight or less, it is an envelope. Because it is a crystalline system, when it is cooled from a liquid phase state, Al 8 Mo 3 is precipitated as a primary crystal in the curve DC, and after that, Al 8 Mo 3 is precipitated as a primary crystal at 1130℃.
Although Al 8 Mo 3 continues to precipitate until the temperature reaches 735°C, solidification is not completed and the welding state continues up to 735°C, resulting in the formation of voids and shrinkage pores due to released gas and segregation of ingredients, resulting in Al -Applies to the cleanliness and homogeneity required of the Mo master alloy. In addition, since the alloy has coarse crystals, when adjusting the grain size to the required grain size as a master alloy for Ti alloys, the processing yield is significantly reduced due to the generation of fine powder, making it impossible to put it to practical use. Therefore, the inventor decided to
Focusing on the eutectic part containing 57 to 67% by weight of Mo, we found that a master alloy can be obtained from the eutectic reaction line GEH in which the solidification in the low-temperature solid part has a eutectic structure. There are three possible melting methods for Al-Mo: induction melting, welding in a vacuum arc furnace, and aluminothermite melting, but the induction melting method is extremely complicated and the equipment is expensive. Segregation inside the alloy due to the difference in specific gravity of Mo is also large. Also, in the melting method in a vacuum arc furnace, the master alloy is contaminated by the melting of the arc pole, and it is difficult to produce a homogeneous master alloy. The aluminothermite melting method has the characteristics of simple equipment and short reaction time;
Due to its characteristics, conventional compositions of 50% by weight Mo and the balance Al caused a violent reaction, almost explosive, and the composition was violently blown out and volatilized outside the crucible, resulting in a significant decrease in yield (approximately 50%). , Al−Mo
Conventionally, the composition ratio that can be melted using the aluminothermite method was set to be less than 50% by weight of Mo, but as described above, this composition ratio is in the peritectic range and cannot be put to practical use. Therefore, the inventors developed a practical method for the aluminothermite method in the eutectic region, which had been considered extremely difficult in the past. [Purpose] The purpose of this invention is to develop a method for obtaining a new material of Al-Mo master alloy with a eutectic structure, which does not cause intense reaction and does not cause evaporation of Al or MoO 3 The objective is to obtain a clean Al--Mo mother alloy with little loss due to volatilization, a significantly high circumferential ratio, and a clean Al--Mo mother alloy. Another objective is that this new substance
The purpose is to obtain a new material that is a master alloy that is relatively close to the melting point of Ti, does not become pulverized when crushed, and whose particle size can be easily adjusted. [Structure] The present invention relates to an aluminum-molybdenum alloy whose alloy composition is aluminum 33 to 43.
This is an aluminum-molybdenum master alloy for producing titanium alloys, which is characterized by having a eutectic structure containing 57 to 67% by weight of molybdenum. In another invention, when aluminum powder and molybdenum oxide powder are mixed and reacted using the thermite method, the mother alloy structure is changed to aluminum 33.
The molybdenum oxide powder and aluminum powder are mixed so that the molybdenum is 57 to 67% by weight, and the weight ratio is about 30 to 50%, preferably 42 to 43% based on the weight of the mixture. Aluminum, which is characterized by containing a slag-forming agent.
This is a method for producing molybdenum master alloy. [Effect] By adopting the above method, even if the aluminothermite method is used, the internal composition can be changed by the reaction in the crucible by using the slag forming agent in the above ratio. The slag caused by these slag-forming agents covers the surface of the liquid water, prevents volatilization of Al, and volatilization in the MoO 3 state, and reduces the Al-Mo weight ratio. is in the eutectic region within the above range, so the melted alloy has a eutectic structure. Furthermore, since the upper limit of the weight percentage of Mo is 67 weight percent, the following drawbacks are not present. That is, if the temperature is too close to the eutectic point E, the solidification temperature range from the precipitation of AlsMo 3 primary crystals to the eutectic precipitation will be too narrow, entrainment of specific metal inclusions will occur, and gas release will be incomplete. It becomes difficult to obtain a clean alloy and a material without pores, which are necessary conditions for the master alloy.
In addition, in the conventional thermite method, a complicated process is performed in which the molten metal is extracted, degassed, and then cast into a mold, but in this invention, the molten metal is simply poured into a mold in a reactor, and then cooled and solidified. A very good alloy is obtained by a simple method. Furthermore, the particle size of the master alloy obtained by this method can be easily adjusted when it is crushed. This invention will now be explained in detail with reference to the following experimental examples.

【表】 上記のような配合の原料を混合し、底部内径
200mm上部内径400mm、深さ300mmのマグネシアラ
イニング炉(るつぼ)中で、テルミツト反応さ
せ、放置、スラグ層と合金層を比重差により分離
させる。充分冷却させた後、凝固した合金を炉よ
り取り出し、スラグ、引け巣等を除去して、成品
たるAl−Mo合金を得る。
[Table] Mix the raw materials with the above composition, and
Thermite is reacted in a magnesia-lined furnace (crucible) with a 200mm top, an inner diameter of 400mm, and a depth of 300mm, and the slag layer and alloy layer are separated by the difference in specific gravity. After cooling sufficiently, the solidified alloy is taken out of the furnace and slag, shrinkage cavities, etc. are removed to obtain a finished Al--Mo alloy.

【表】 上記のような配合の原料を混合し、実験例1と
同様の方法で合金を回収した。
[Table] The raw materials having the above composition were mixed and an alloy was recovered in the same manner as in Experimental Example 1.

【表】 上記のような配合の原料を混合し、実験例1と
同様の方法で合金を回収した。
[Table] The raw materials having the above composition were mixed and an alloy was recovered in the same manner as in Experimental Example 1.

【表】 上記のような配合の原料を混合し、実験例1と
同様の方法で溶融し、溶湯を塩素ガスにより脱ガ
スした後、底部内径150mm、上部内径300mm、深さ
300mmの銅製の鋳型の鋳込み、冷却凝固させた。
[Table] The raw materials with the above composition were mixed, melted in the same manner as in Experimental Example 1, and after degassing the molten metal with chlorine gas, the bottom inner diameter was 150 mm, the upper inner diameter was 300 mm, and the depth was
It was poured into a 300mm copper mold and allowed to cool and solidify.

【表】 上記のような配合の原料を他の実験例と同方法
で合金を回収した。 これらの実験結果は次に示す表の通りである。
[Table] Alloys were recovered using the same method as in other experimental examples using raw materials with the above-mentioned composition. The results of these experiments are shown in the table below.

【表】【table】

【表】 上記の結果表よりも明らかなように、この発明
の方法で得られた合金はTi母合金として優れた
要件を有しており、殊に収率の高さ、清浄度に優
れ、介在物の含有率が従来例に比較して約1/10に
なり、特にTi合金のようにその不純物の介在率
によつて大きく特性が変化するものにおいては、
この母合金の清浄度は注目すべき効果である。 またこれら実験例1、2、3及び4の合金を破
砕した場合において、微粉末にならず粒度調整が
容易である。 このAl−Mo母合金の融点は1760℃であり、Ti
の融点1665℃と比較的近傍で、三元合金の溶製が
容易である。 実験例1乃至3に示した態様の方法において
は、テルミツト反応をさせるるつぼ中において、
溶湯を冷却凝固させる方法であるから鋳型も不要
で、操作が簡便となる。 実験例4に示す態様の方法においては、テルミ
ツト反応により、るつぼ内で溶湯となつた金属を
鋳型に注ぎ込む方法であるから、この過程でのガ
ス抜ができ気孔の発生率を更に低くすることが可
能であり、空にしたるつぼは次の反応のために利
用できるからるつぼの使用効率が高まる。
[Table] As is clear from the above result table, the alloy obtained by the method of the present invention has excellent requirements as a Ti master alloy, especially in high yield and cleanliness. The content of inclusions is about 1/10 of that of conventional examples, especially for materials such as Ti alloys whose properties change greatly depending on the inclusion rate of impurities.
The cleanliness of this master alloy is a noteworthy effect. Furthermore, when the alloys of Experimental Examples 1, 2, 3, and 4 are crushed, they do not become fine powders and the particle size can be easily adjusted. The melting point of this Al-Mo master alloy is 1760℃, and the Ti
Its melting point is relatively close to 1665℃, making it easy to melt into a ternary alloy. In the methods shown in Experimental Examples 1 to 3, in a crucible for carrying out a thermite reaction,
Since the method involves cooling and solidifying the molten metal, no mold is required, making the operation simple. In the method shown in Experimental Example 4, the metal that has become molten in the crucible is poured into the mold by thermite reaction, so gas can be removed during this process and the rate of porosity can be further reduced. This increases crucible usage efficiency since the empty crucible can be used for the next reaction.

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

図はAl−Mo合金の状態図である。 The figure is a phase diagram of an Al-Mo alloy.

Claims (1)

【特許請求の範囲】 1 アルミニウム・モリブデン合金において、こ
れらの合金組成がアルミニウム33乃至43重量%、
モリブデン57乃至67重量%の共晶組織よりなるこ
とを特徴とするチタニウム合金製造用のアルミニ
ウム・モリブデン母合金。 2 アルミニウム粉末と酸化モリブデン粉末を混
合し、テルミツト法を用いて反応させる場合にお
いて、母合金組織をアルミニウム33乃至43重量
%、モリブデン57乃至67重量%となるように、前
記酸化モリブデン粉末とアルミニウム粉末を混合
し、これらの混合物の重量に対し、重量比で約30
乃至50%、好ましくは42乃至43%の造滓剤を入れ
ることを特徴とするアルミニウム・モリブデン母
合金の製造法。 3 前記造滓剤は酸化カルシウム、弗化カルシ
ウ、及びこれらの混合物のうちの一種であること
を特徴とする特許請求の範囲第2項記載のアルミ
ニウム・モリブデン母合金の製造法。
[Claims] 1. In aluminum-molybdenum alloys, these alloy compositions include 33 to 43% by weight of aluminum;
An aluminum-molybdenum master alloy for producing titanium alloys, characterized by having a eutectic structure containing 57 to 67% by weight of molybdenum. 2. When aluminum powder and molybdenum oxide powder are mixed and reacted using the thermite method, the molybdenum oxide powder and aluminum powder are mixed so that the mother alloy structure is 33 to 43% by weight of aluminum and 57 to 67% by weight of molybdenum. and the weight ratio of about 30 to the weight of these mixtures.
A method for producing an aluminum-molybdenum master alloy, which comprises adding a sludge forming agent of 50% to 50%, preferably 42 to 43%. 3. The method for producing an aluminum-molybdenum master alloy according to claim 2, wherein the slag-forming agent is one of calcium oxide, calcium fluoride, and a mixture thereof.
JP10018583A 1983-06-07 1983-06-07 Aluminum-molybdenum mother alloy used in manufacture of titanium alloy and its manufacture Granted JPS59226147A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10018583A JPS59226147A (en) 1983-06-07 1983-06-07 Aluminum-molybdenum mother alloy used in manufacture of titanium alloy and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10018583A JPS59226147A (en) 1983-06-07 1983-06-07 Aluminum-molybdenum mother alloy used in manufacture of titanium alloy and its manufacture

Publications (2)

Publication Number Publication Date
JPS59226147A JPS59226147A (en) 1984-12-19
JPH0321618B2 true JPH0321618B2 (en) 1991-03-25

Family

ID=14267244

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10018583A Granted JPS59226147A (en) 1983-06-07 1983-06-07 Aluminum-molybdenum mother alloy used in manufacture of titanium alloy and its manufacture

Country Status (1)

Country Link
JP (1) JPS59226147A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108149082B (en) * 2018-01-08 2019-08-27 东北大学 A kind of Al-Mo master alloy and preparation method thereof
CN111945049B (en) * 2020-08-29 2021-07-30 承德天大钒业有限责任公司 A kind of aluminum molybdenum master alloy and preparation method thereof

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5523895B2 (en) * 1972-12-19 1980-06-25

Also Published As

Publication number Publication date
JPS59226147A (en) 1984-12-19

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