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JPH0685996B2 - Manufacturing method of metal matrix composite material - Google Patents
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JPH0685996B2 - Manufacturing method of metal matrix composite material - Google Patents

Manufacturing method of metal matrix composite material

Info

Publication number
JPH0685996B2
JPH0685996B2 JP62073150A JP7315087A JPH0685996B2 JP H0685996 B2 JPH0685996 B2 JP H0685996B2 JP 62073150 A JP62073150 A JP 62073150A JP 7315087 A JP7315087 A JP 7315087A JP H0685996 B2 JPH0685996 B2 JP H0685996B2
Authority
JP
Japan
Prior art keywords
preform
sic
composite material
alloy
mold
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
JP62073150A
Other languages
Japanese (ja)
Other versions
JPS63238968A (en
Inventor
晃則 永田
裕 石渡
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.)
Toshiba Corp
Original Assignee
Toshiba 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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP62073150A priority Critical patent/JPH0685996B2/en
Publication of JPS63238968A publication Critical patent/JPS63238968A/en
Publication of JPH0685996B2 publication Critical patent/JPH0685996B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/08Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
    • C22C47/12Infiltration or casting under mechanical pressure

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Description

【発明の詳細な説明】 〔発明の目的〕 (産業上の利用分野) 本発明は繊維強化金属基複合材料の製造方法に係り、特
に加圧鋳造法により、SiC繊維等を強化材料とするMg含
有Al合金の複合材料を製造する方法において、Mg偏析異
常の発生防止が有効的に図れる金属基複合材料の製造方
法に関する。
The present invention relates to a method for producing a fiber-reinforced metal matrix composite material, and in particular to a Mg material containing a SiC fiber or the like as a reinforcing material by a pressure casting method. The present invention relates to a method for producing a metal-based composite material, which can effectively prevent the occurrence of Mg segregation anomaly in the method for producing a composite material containing Al alloy.

(従来の技術) 一般に、繊維強化金属基複合材料に用いられる繊維原料
として、SiC系、Al2O3系、C系、B系等が知られてい
る。特に、Al合金系材料の強化用としては、Alとの濡れ
性に優れているSiCウィスカの短繊維、粒子またはウィ
スカが多用されている。
(Prior Art) Generally, SiC-based, Al 2 O 3 -based, C-based, B-based, etc. are known as fiber raw materials used for fiber-reinforced metal matrix composite materials. In particular, short fibers, particles or whiskers of SiC whiskers, which have excellent wettability with Al, are often used for strengthening Al alloy materials.

また、繊維強化金属基複合材料の製造方法として、従
来、高圧鋳造法(溶浸法)、粉末冶金法、拡散接合法な
どが知られているが、特に高圧鋳造法が大量生産に適
し、軽量強化材料の製造分野などで多く適用されてい
る。
Further, as a method for producing a fiber-reinforced metal matrix composite material, conventionally, a high pressure casting method (infiltration method), a powder metallurgy method, a diffusion bonding method and the like are known, but the high pressure casting method is particularly suitable for mass production and is lightweight. It is widely applied in the field of manufacturing reinforcing materials.

ところで、高圧鋳造法により、Mg含有のAl合金をマトリ
ックスとして、例えばSiCウィスカで強化した複合材料
を製造した場合、マトリックスとSiCウィスカとの複合
化部に著しいMg偏析が起り、均一な組成の複合組織が形
成されず、このため複合材としての十分な強度特性が得
られないというMg含有Al合金系複合材料独特の現象が認
められている。この原因は、SiCウィスカの表層部に介
在するSiO2成分がMg成分と選択的に反応し、Mg2Siを形
成するからである。そこで、このMg偏析の対策として表
層部からSiO2を除去したSiCウィスカを用いることが提
案されている。
By the way, by a high pressure casting method, when a Mg-containing Al alloy is used as a matrix, for example, when a composite material reinforced with SiC whiskers is produced, significant Mg segregation occurs in the composite portion of the matrix and SiC whiskers, and a composite with a uniform composition is formed. A phenomenon peculiar to the Mg-containing Al alloy-based composite material is recognized in that the structure is not formed, and therefore, sufficient strength characteristics as the composite material cannot be obtained. This is because the SiO 2 component present in the surface layer of the SiC whisker selectively reacts with the Mg component to form Mg 2 Si. Therefore, as a countermeasure against this Mg segregation, it has been proposed to use a SiC whisker with SiO 2 removed from the surface layer.

このことから、発明者において、SiO2量が0.2〜0.35%w
t%と極めて少ないSiCウィスカを用い、高圧鋳造法によ
ってSiCウィスカ強化6061Al合金複合材料を試作した。
この場合の製造方法を第5図(A)〜(D)に示す。
From this, the inventors have found that the amount of SiO 2 is 0.2 to 0.35% w
A SiC whisker reinforced 6061Al alloy composite material was prototyped by a high pressure casting method using an extremely small amount of SiC whiskers.
The manufacturing method in this case is shown in FIGS.

まず、SiCウィスカをプレス法によって円筒形状に固め
たプリフォーム1を作成し、これを加熱炉2に挿入し、
プリフォーム1全体の温度が500℃〜700℃になるようヒ
ータ3の加熱により20分〜60分間大気中にて予熱する
(第5図(A))。次に、予めヒータ4で350℃〜650℃
に予熱されている金型5内にプリフォーム1を設置する
(同図(B))。その後、溶湯マトリックス金属6を金
型5内に注湯し(同図(C))、ピストン7で加圧して
プリフォーム2内に溶湯マトリックス金属6を充填し、
SiCウィスカ強化6061Al合金材料8を作成する(同図
(D))。
First, a preform 1 obtained by solidifying a SiC whisker into a cylindrical shape by a pressing method is prepared and inserted into a heating furnace 2.
The preform 1 is preheated in the atmosphere for 20 to 60 minutes by heating the heater 3 so that the temperature of the entire preform 1 becomes 500 to 700 ° C (Fig. 5 (A)). Next, use the heater 4 in advance at 350 ℃ -650 ℃
The preform 1 is set in the mold 5 that has been preheated (FIG. 2B). Then, the molten matrix metal 6 is poured into the mold 5 (FIG. 2C), and is pressurized by the piston 7 to fill the preform 2 with the molten matrix metal 6.
A SiC whisker reinforced 6061 Al alloy material 8 is created (Fig. (D)).

このようにして作成したSiCウィスカ強化6061Al合金材
料8を半割りにし、熱処理した後の断面を示したのが第
6図である。6061Al合金マトリックス部9が金属色、複
合化部8′の斜線部8aが暗緑色、複合化部8′下部の霜
降模様部8bが金属色を呈していた。
FIG. 6 shows a cross section after the SiC whisker reinforced 6061 Al alloy material 8 thus created is halved and heat treated. The 6061 Al alloy matrix portion 9 had a metallic color, the shaded portion 8a of the composite portion 8'had a dark green color, and the frost pattern portion 8b below the composite portion 8'had a metallic color.

このような複合化部8′の異色発生原因を調査するため
に、第6図に示すそれぞれの代表部u1〜x1について化学
分析と機械的引張試験を行なった。その結果、化学分析
については、Mg以外の元素はそれぞれの代表部で殆ど同
一量であったが、Mgの濃度は下記の第1表に示すよう
に、u1〜w1に比べてx1で著しく低下していることが認め
られた。このようなMg濃度の低い領域x1の引張強さはマ
トリックス材である6061Al合金とほぼ同一であった。
To investigate the unique cause of such a composite unit 8 ', it was performed chemical analysis and mechanical tensile test for each of the representative unit u 1 ~x 1 shown in Figure 6. As a result, regarding the chemical analysis, the elements other than Mg were almost the same in each representative part, but the concentration of Mg was x 1 compared to u 1 to w 1 as shown in Table 1 below. It was confirmed that the value was remarkably decreased in. The tensile strength of the low Mg concentration region x 1 was almost the same as that of the 6061 Al alloy as the matrix material.

第1表から、マトリックス部9のMg濃度は1.01%でJIS
規格値(0.8〜1.2%)を満足しているが、暗緑色の複合
化部8aのMg濃度は1.4〜1.62%とJIS規格値を上回り、一
方、金属色を呈している複合化部8bのMg濃度は、0.01%
と極めて小さく、純Alに近い値になっていることが認め
られる。また、引張強さについては、暗緑色の複合化部
8bでは44〜46Kgf/mm2と大きいのに対し、金属色の複合
化部8bでは、31Kgf/mm2と小さく、SiCウィスカ強化純Al
材の強度程度しか得られないことが判る。
From Table 1, the Mg concentration of the matrix part 9 is 1.01% and JIS
Although the standard value (0.8 to 1.2%) is satisfied, the Mg concentration of the dark green composite part 8a is 1.4 to 1.62%, which exceeds the JIS standard value, while the composite color of the composite part 8b exhibiting a metallic color is Mg concentration is 0.01%
It is recognized that the value is extremely small and is close to that of pure Al. Regarding the tensile strength, the dark green composite part
8b is as large as 44-46Kgf / mm 2 , whereas the metal-colored composite part 8b is as small as 31Kgf / mm 2 and SiC whisker reinforced pure Al
It can be seen that only the strength of the material can be obtained.

この現象は、溶湯アルミニウム合金が予熱後のプリフォ
ーム内に含浸する過程で、活性作用の強いMgがSiCウィ
スカ表層部のSiO2と反応し、Mgがトラップされてしまう
ために、複合化部8bのMg濃度が低下したものと思われ
る。
This phenomenon is because in the process of impregnation of the molten aluminum alloy into the preform after preheating, Mg having a strong activating action reacts with SiO 2 in the surface layer of the SiC whiskers, and Mg is trapped. It is considered that the Mg concentration of the is decreased.

すなわち、微量のSiO2を含有したSiCウィスカを用いて
も、そのSiO2量からでは予想することもできない程に大
きな割合でMg偏析が生じ、このため、表層部のSiO2を除
去したSiCウィスカを用いただけでは、Mgを含有するAl
合金のMg偏析を防止することは不可能であることが明ら
かになった。
That is, even if a SiC whisker containing a small amount of SiO 2 was used, Mg segregation occurred at a rate that was unpredictable from the SiO 2 amount, and therefore, the SiC whisker from which SiO 2 in the surface layer portion was removed was generated. Just using, Al containing Mg
It became clear that it was impossible to prevent Mg segregation of the alloy.

このようなMg偏析が生じると、所定の強度を有する複合
材として利用できる部分が限定され、材料の歩留りが悪
くなる。また、複合材のビレットを圧延あるいは押出し
加工によって塑性加工すると、Mg偏析の位置、状況によ
っては加工材の全面にMg濃度の低い部分が生じ、加工材
の特性が著しく損なわれる。
When such Mg segregation occurs, the portion that can be used as a composite material having a predetermined strength is limited, and the yield of the material deteriorates. Further, when the billet of the composite material is subjected to plastic working by rolling or extrusion, depending on the position of Mg segregation and the situation, a portion with a low Mg concentration is formed on the entire surface of the worked material, and the characteristics of the worked material are significantly impaired.

(発明が解決しようとする問題点) Mgを含有するAl合金マトリックスをSiCの短繊維、粒子
またはウィスカで強化した金属基複合材を高圧鋳造法に
よって作成する場合、強化材料であるSiCウィスカとAl
合金との複合化部に著しいMg元素の偏析が起り、複合材
としての十分な特性が得られず、また材料の歩留りが悪
くなるという問題がある。
(Problems to be solved by the invention) When a metal matrix composite material in which an Al alloy matrix containing Mg is reinforced with SiC short fibers, particles or whiskers is prepared by a high pressure casting method, SiC whiskers and Al which are reinforcement materials are used.
There is a problem that significant segregation of Mg element occurs in the composite portion with the alloy, sufficient characteristics as a composite material cannot be obtained, and the yield of the material deteriorates.

本発明はこのような事情に鑑みてなされたもので、Mgを
含有するAl合金をマトリックスとして、SiCの短繊維、
粒子またはウィスカとの複合化部を成形する場合にMg偏
析異常がなく、性状の均一化、品質および歩留りの向上
が図れる金属基複合材料の製造方法を提供することを目
的とする。
The present invention has been made in view of such circumstances, as an Al alloy containing Mg as a matrix, SiC short fibers,
An object of the present invention is to provide a method for producing a metal-based composite material, which is free from anomalous Mg segregation when forming a composite portion with particles or whiskers, and which is capable of achieving uniform properties and improved quality and yield.

(発明の構成) (問題点を解決するための手段と作用) SiCの短繊維、粒子またはウィスカの表層部のSiO2を除
去し、これを強化材として用いることがMg偏析量の減少
に有効であることは既に述べたとおりである。
(Structure of Invention) (Means and Actions for Solving Problems) It is effective to reduce the amount of Mg segregation by removing SiO 2 from the SiC short fibers, particles or the surface layer of whiskers and using it as a reinforcing material. Is as described above.

ところで、高圧鋳造法による製造方法では、Al合金溶湯
がプリフォーム内へ容易に含浸できるようにするため、
予めプリフォームを高温状態に予熱する必要がある。発
明者等は、この予熱温度およびその雰囲気に関する数多
くの基礎実験と調査分析を行なった。その結果、たとえ
微量のSiO2しか含まれていないSiC強化材を用いても、
プリフォームの予熱を高温大気中で長時間実施すること
によって、SiC強化材の表層部に存在する遊離Siが大気
中の酸素と反応してSiO2が形成され、このため、複合部
のMg偏析量が増加することを見出した。
By the way, in the manufacturing method by the high pressure casting method, in order to allow the molten Al alloy to be easily impregnated into the preform,
It is necessary to preheat the preform to a high temperature state in advance. The inventors have conducted a number of basic experiments and research analyzes on this preheating temperature and its atmosphere. As a result, even if a SiC reinforcement containing only a trace amount of SiO 2 is used,
By preheating the preform for a long time in a high-temperature atmosphere, free Si existing in the surface layer of the SiC reinforcement reacts with oxygen in the atmosphere to form SiO 2, which results in Mg segregation of the composite part. It was found that the amount increases.

また、Al合金溶湯をプリフォーム内に高圧で充填する際
に、プリフォームの空孔内に活性ガスが存在すると、Si
O2量の少ないプリフォームを用いても、結果的にはMg偏
析量が増加するということが実験的に明らかになった。
この理由はSiC強化材の表層部の遊離Siが高温において
極めて短時間内で酸素等の活性ガスを反応し、この反応
が高圧下ではさらに加速されるためによるものと推察さ
れる。
Further, when the molten Al alloy is filled into the preform at high pressure, if active gas exists in the pores of the preform, Si
It was experimentally clarified that even if a preform having a small amount of O 2 is used, the amount of Mg segregation increases as a result.
It is speculated that the reason for this is that free Si in the surface layer of the SiC reinforcement reacts with an active gas such as oxygen at a high temperature within an extremely short time, and this reaction is further accelerated under high pressure.

本発明は、このような知見に基づき、SiCの短繊維、粒
子またはウィスカを集積したプリフォームに、Mg含有の
Al合金溶湯をマトリックスとして加圧含浸させて金属基
複合材料を製造する方法であって、前記プリフォームは
表層部のSiO2を除去したSiCの短繊維、粒子またはウィ
スカを用いて作成する金属基複合材料の製造方法におい
て、まず前記プリフォームを金型内に入れ、その金型内
を密閉して真空ポンプで真空状態として500℃〜700℃の
温度まで加熱し、プリフォーム内の水分が完全に消失し
た後、不活性ガスタンクからArその他の高純度不活性ガ
スを前記金型内に充満してプリフォーム内の空孔への活
性ガスの侵入を阻止しつつMg含有のAl合金マトリックス
溶湯を注湯し、加圧含浸させることを特徴とする。
The present invention is based on such findings, in the preform in which SiC short fibers, particles or whiskers are accumulated, Mg-containing
A method for producing a metal-based composite material by pressure-impregnating a molten Al alloy as a matrix, wherein the preform is a metal base formed by using SiC short fibers, particles or whiskers of which SiO 2 in the surface layer portion is removed. In the method of manufacturing a composite material, first, the preform is put into a mold, the mold is hermetically sealed, and a vacuum pump is used to heat it to a temperature of 500 ° C to 700 ° C in a vacuum state so that the moisture in the preform is completely removed. After disappearing, the Mg-containing Al alloy matrix molten metal was filled from the inert gas tank with Ar and other high-purity inert gas to prevent the active gas from entering the pores in the preform by filling the mold. It is characterized by pouring molten metal and impregnating it under pressure.

本発明によれば、プリフォーム内のSiC強化材表層部にS
iO2成分が形成されず、かつ溶浸過程においても活性ガ
スのプリフォーム内への侵入を防止しているため、Mg2S
iの析出を完全に防ぐことができる。これにより、Mg含
有Al合金をマトリックスとする複合材の製造において、
複合化部にMgの偏析という組成の異常が起る不具合を解
消することが可能となる。
According to the present invention, S is added to the surface layer of the SiC reinforcement in the preform.
Since no iO 2 component is formed and active gas is prevented from entering the preform during the infiltration process, Mg 2 S
The precipitation of i can be completely prevented. As a result, in the production of a composite material using a Mg-containing Al alloy as a matrix,
It becomes possible to solve the problem that the composition abnormality such as segregation of Mg occurs in the composite part.

(実施例) 以下、本発明の一実施例を第1図〜第4図を参照して説
明する。この実施例では、マトリックスとしてのAl合金
にMg元素が1.01%含有された6061Alを用い、強化繊維と
しては、SiCウィスカを用いた。このSiCウィスカは、表
層部のSiO2や遊離Siを弗酸、硝酸等の酸液で除去するこ
とにより、SiO2量を0.025%とした。
(Embodiment) An embodiment of the present invention will be described below with reference to FIGS. 1 to 4. In this example, 6061 Al containing 1.01% of Mg element was used as the Al alloy as the matrix, and SiC whiskers were used as the reinforcing fibers. The SiC whiskers, hydrofluoric acid and SiO 2 and the free Si surface layer portion, is removed by acid solution such as nitric acid, and the amount of SiO 2 and 0.025%.

第1図(A)〜(C)に製造工程を示す。The manufacturing process is shown in FIGS. 1 (A) to (C).

まず、SiCウィスカに少量の水を均一に混合し、プリフ
ォーム成形型内に挿入して圧縮成形する。このようにし
て作成したプリフォーム12を金型13に設置し、Al合金湯
口14と金型上部15とを密閉状態にしてから、真空ポンプ
16で金型内を真空状態にする。その後、金型13の外周部
のヒータ17によって所定の温度(500℃〜700℃)まで加
熱し、プリフォーム内の水分が完全に消失してから、Ar
タンク18から高純度Arガスを金型13内に充満して、プリ
フォーム12の予熱を20分〜60分間行なう(第1図
(A))。次に、プリフォーム12内のArガスが消失しな
い状態で、湯口14からAl合金溶湯19が金型13内に注入す
る(同図(B))。その後、金型上部15を取外して上部
から加圧ピストン20を挿入し、高圧状態でAl合金溶湯19
をプリフォーム12内に含浸する(同図(C))。凝固
後、金型内より複合材のビレットを取り出す。
First, a small amount of water is uniformly mixed with SiC whiskers, which are inserted into a preform mold and compression molded. The preform 12 thus created is installed in the mold 13, and the Al alloy sprue 14 and the upper part 15 of the mold are hermetically sealed, and then the vacuum pump
Vacuum the inside of the mold with 16. After that, the heater 17 on the outer periphery of the mold 13 is heated to a predetermined temperature (500 ° C to 700 ° C) to completely remove the moisture in the preform, and then Ar
The mold 13 is filled with high-purity Ar gas from the tank 18, and the preform 12 is preheated for 20 to 60 minutes (FIG. 1 (A)). Next, the molten Al alloy 19 is injected into the die 13 from the sprue 14 in a state where Ar gas in the preform 12 is not lost (FIG. 2B). After that, the upper part 15 of the mold is removed and the pressure piston 20 is inserted from the upper part.
Is impregnated into the preform 12 (FIG. 2C). After the solidification, the composite billet is taken out of the mold.

第2図はこのようにして製造したSiCウィスカ強化6061A
l複合材のビレット21を半割りにして熱処理した縦断面
形状を示す。
Figure 2 shows SiC whisker reinforced 6061A manufactured in this way.
1 shows a vertical cross-sectional shape obtained by heat-treating a composite billet 21 in half.

6061Al合金マトリックス部22は金属色、複合化部21′の
大半部分21aは暗緑色を呈し、下部に若干の金属色部分2
1bが認められる。下記の第2表はそれぞれの部位の代表
部u2〜y2についてのMg濃度分析と引張試験した結果を示
す。
The 6061 Al alloy matrix part 22 has a metallic color, the majority part 21a of the composite part 21 'has a dark green color, and a slight metallic color part 2 at the bottom.
1b is recognized. Table 2 below shows the results of the Mg concentration analysis and the tensile test for the representative parts u 2 to y 2 of each part.

v2〜x2に該当する複合化部21aではほぼ均一にMg元素が
含有され、その引張強さも45〜46Kgf/mm2で十分な複合
結果が得られている。
In the composite portion 21a corresponding to v 2 to x 2 , the Mg element is contained almost uniformly, and the tensile strength thereof is 45 to 46 Kgf / mm 2, which is a sufficient composite result.

しかしながら、金属色の複合化部21bのMg濃度は0.02%
と少なく、Mg偏析が生じている。これは受入れたSiCウ
ィスカ中に含まれていた微量のSiO2(0.25%wt%)に起
因しているものと思われる。したがって、よりSiO2量の
少ないSiCウィスカを用いることによって、この僅かなM
g偏析は完全に防止することができると推測される。
However, the Mg concentration of the metallic color composite part 21b is 0.02%.
And the segregation of Mg occurs. This is probably due to the trace amount of SiO 2 (0.25% wt%) contained in the received SiC whiskers. Therefore, by using SiC whiskers with a smaller amount of SiO 2,
It is speculated that g segregation can be completely prevented.

次に、前記実施例の溶浸工程によるプリフォーム構成用
のSiCウィスカの表層部に存在するSiO2量の減少度合を
従来の方法と比較して調査した結果を第3図および第4
図によって考察する。
Next, the reduction degree of the amount of SiO 2 existing in the surface layer portion of the SiC whisker for forming a preform by the infiltration process of the above-mentioned example was investigated by comparing with the conventional method, and the results are shown in FIGS. 3 and 4.
Consider the figure.

第3図は、第1図の工程により、初期のSiO2量が0.2〜
0.35%であるSiCウィスカから成るプリフォームを、500
℃〜900℃の大気中および高純度Arガス雰囲気中でそれ
ぞれ60分間加熱し、その後のSiO2量を測定した結果を示
している。
FIG. 3 shows that the initial amount of SiO 2 is 0.2 to
Preform consisting of 0.35% SiC whiskers
Shown are the results of measuring the amount of SiO 2 after heating for 60 minutes each in the atmosphere of ℃ to 900 ℃ and in the high-purity Ar gas atmosphere.

大気中の加熱では、加熱温度の上昇と共に、SiO2量が著
しく増加し、初期のSiO2量の10倍以上にも達することが
判る。
It can be seen that with heating in the atmosphere, the amount of SiO 2 increases remarkably as the heating temperature rises, reaching more than 10 times the initial amount of SiO 2 .

これに対し、Ar雰囲気中の加熱の場合には、その増加量
は微量であり、60分間の加熱によっても初期のSiO2量に
殆ど等しいことが認められる。
On the other hand, in the case of heating in the Ar atmosphere, the amount of increase is very small, and it is recognized that even after heating for 60 minutes, it is almost equal to the initial amount of SiO 2 .

また、第4図は、加熱温度を一定として、大気中の加熱
時間を変えたときのSiO2量の生成挙動を調べた結果であ
る。プリフォームの予熱時間はその大きさにも依存する
が、小さなプリフォームでも10〜20分以上を必要とす
る。このような短時間の大気中加熱によってもSiO2量は
急速に増加することが判る。
Further, FIG. 4 shows the results of examining the behavior of generation of the amount of SiO 2 when the heating temperature in air is changed while the heating temperature is kept constant. The preheating time of the preform depends on its size, but even a small preform requires 10 to 20 minutes or more. It can be seen that the amount of SiO 2 rapidly increases even by heating in the atmosphere for such a short time.

このように、SiCウィスカ表層部のSiO2量が初期の時点
で微量であっても、ウィスカ表層部に遊離したSiと大気
中の酸素とが高温雰囲気で反応し、このためプリフォー
ムを形成するSiCウィスカ表層部にSiO2が増加するので
ある。
Thus, even if the amount of SiO 2 on the surface of the SiC whisker is very small at the initial stage, Si released to the surface of the whisker reacts with oxygen in the atmosphere in a high-temperature atmosphere, thus forming a preform. SiO 2 increases on the surface of the SiC whiskers.

なお、本発明を適用するMg含有のAl合金としては、AC8
A,AC4C,AC4Dなどの鋳造用、あるいは展伸材用Al合金と
して代表される2024,5052,6061,7075等が好適である。
即ち、これらのAl合金のMg含有量は0.2〜3.0%の範囲内
にあり、本発明が最も有効に適用できるMg含有領域であ
る。但し、Mgの含有量が3.0%以上のMg含有Al合金につ
いても、Mg量の濃淡による偏析現象が生じるものである
から、本発明が有効に適用できるのは勿論である。
Incidentally, as the Mg-containing Al alloy to which the present invention is applied, AC8
2024,5052,6061,7075 and the like, which are represented by Al alloys for casting of A, AC4C, AC4D, etc., or for wrought materials, are suitable.
That is, the Mg content of these Al alloys is in the range of 0.2 to 3.0%, which is the Mg-containing region to which the present invention can be most effectively applied. However, even in a Mg-containing Al alloy having a Mg content of 3.0% or more, the segregation phenomenon occurs due to the lightness and darkness of the Mg content, and thus the present invention can be effectively applied.

なお、前記実施例ではSiCウィスカでプリフォームを形
成した場合について述べたが、本発明はSiC短繊維ある
いは粒子を用いてプリフォームを形成する場合について
も前記実施例と同様の効果を得ることができる。
In addition, in the above-mentioned embodiment, the case where the preform is formed by the SiC whiskers is described, but the present invention can obtain the same effect as the above-mentioned embodiment also in the case where the preform is formed by using the SiC short fibers or particles. it can.

(発明の効果) 以上のように、本発明によれば、表層部のSiO2を除去し
たSiCの短繊維、粒子またはウィスカを用いて作成した
プリフォームを、金型内で真空状態にて500℃〜700℃の
温度で加熱することによりプリフォーム内の水分を完全
に消失させ、その後、高純度不活性ガスを前記金型内に
充満してプリフォーム内の空孔への活性ガスの侵入を阻
止しつつMg含有のAl合金マトリックス溶湯を注湯する工
程を採用することで、同一の金型を利用して容易に作業
が行えるとともに、まず真空加熱を行い、その後に不活
性ガス雰囲気中で溶湯注を行うという一連の工程によっ
てMg偏析がなく材料歩留りがよい品質の安定した製品が
確実に得られる。
(Effects of the Invention) As described above, according to the present invention, a preform prepared by using SiC short fibers, particles or whiskers of which SiO 2 in the surface layer portion is removed is vacuum-molded in a mold under a vacuum condition of 500 By heating at a temperature of ℃ ~ 700 ℃ to completely eliminate the moisture in the preform, then fill the mold with high-purity inert gas, the invasion of the active gas into the pores in the preform By adopting the process of pouring the Mg-containing Al alloy matrix melt while blocking the above, it is possible to easily perform the work using the same mold, and at the same time perform vacuum heating first and then in an inert gas atmosphere. By a series of steps of pouring the molten metal in the above, it is possible to surely obtain a stable product with a good material yield and no Mg segregation.

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

第1図(A),(B),(C)は本発明の一実施例を説
明するための工程図、第2図は前記実施例によって得ら
れるSiCウィスカ強化6061Al複合材料の断面状態を示す
模式図、第3図および第4図はSiCウィスカから成るプ
リフォームを大気中およびArガス雰囲気で加熱し、SiO2
量の変化を調べた結果を示すグラフ、第5図(A),
(B),(C),(D)は従来の製造方法を説明するた
めの工程図、第6図は従来の方法によって得られるSiC
ウィスカ強化6061Al複合材料の断面形状を示す模式図で
ある。 12……プリフォーム、13……金型、19……溶湯。
1 (A), (B), and (C) are process drawings for explaining one embodiment of the present invention, and FIG. 2 shows a cross-sectional state of a SiC whisker reinforced 6061Al composite material obtained by the above embodiment. Schematic diagrams, Fig. 3 and Fig. 4 show SiO 2 preforms made of SiC whiskers in the atmosphere and Ar gas atmosphere
A graph showing the results of examining the change in the amount, FIG. 5 (A),
(B), (C) and (D) are process drawings for explaining a conventional manufacturing method, and FIG. 6 is a SiC obtained by the conventional method.
FIG. 3 is a schematic view showing a cross-sectional shape of a whisker-reinforced 6061Al composite material. 12 …… Preform, 13 …… Mold, 19 …… Molten metal.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】SiCの短繊維、粒子またはウィスカを集積
したプリフォームに、Mg含有のAl合金溶湯をマトリック
スとして加圧含浸させて金属基複合材料を製造する方法
であって、前記プリフォームは表層部のSiO2を除去した
SiCの短繊維、粒子またはウィスカを用いて作成する金
属基複合材料の製造方法において、まず前記プリフォー
ムを金型内に入れ、その金型内を密閉して真空ポンプで
真空状態として500℃〜700℃の温度まで加熱し、プリフ
ォーム内の水分が完全に消失した後、不活性ガスタンク
からArその他の高純度不活性ガスを前記金型内に充満し
てプリフォーム内の空孔への活性ガスの侵入を阻止しつ
つMg含有のAl合金マトリックス溶湯を注湯し、加圧含浸
させることを特徴とする金属基複合材料の製造方法。
1. A method for producing a metal matrix composite material by impregnating a preform in which SiC short fibers, particles or whiskers are accumulated with a molten Mg-containing Al alloy as a matrix to produce a metal-based composite material. Removed SiO 2 from the surface layer
In a method for producing a metal-based composite material using short fibers of SiC, particles or whiskers, first, the preform is placed in a mold, the mold is hermetically sealed, and a vacuum pump is used to produce a vacuum state at 500 ° C. After heating to a temperature of 700 ° C to completely eliminate the water content in the preform, fill the mold with Ar or other high-purity inert gas from the inert gas tank to activate the pores in the preform. A method for producing a metal-based composite material, which comprises pouring a molten Mg-containing Al alloy matrix and impregnating it under pressure while preventing gas from entering.
JP62073150A 1987-03-27 1987-03-27 Manufacturing method of metal matrix composite material Expired - Lifetime JPH0685996B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62073150A JPH0685996B2 (en) 1987-03-27 1987-03-27 Manufacturing method of metal matrix composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62073150A JPH0685996B2 (en) 1987-03-27 1987-03-27 Manufacturing method of metal matrix composite material

Publications (2)

Publication Number Publication Date
JPS63238968A JPS63238968A (en) 1988-10-05
JPH0685996B2 true JPH0685996B2 (en) 1994-11-02

Family

ID=13509867

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62073150A Expired - Lifetime JPH0685996B2 (en) 1987-03-27 1987-03-27 Manufacturing method of metal matrix composite material

Country Status (1)

Country Link
JP (1) JPH0685996B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010024621A3 (en) * 2008-08-29 2010-06-24 경상대학교산학협력단 Low-pressure impregnation apparatus

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01266958A (en) * 1988-04-15 1989-10-24 Mitsubishi Alum Co Ltd Production of fiber reinforced composite material
JP7050978B1 (en) * 2021-02-26 2022-04-08 デンカ株式会社 Molded body and its manufacturing method

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61538A (en) * 1984-06-13 1986-01-06 Tokai Carbon Co Ltd Manufacture of sic whisker reinforced al alloy material
JPS61284542A (en) * 1985-06-10 1986-12-15 Kobe Steel Ltd Production of fiber reinforced composite metallic material

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010024621A3 (en) * 2008-08-29 2010-06-24 경상대학교산학협력단 Low-pressure impregnation apparatus

Also Published As

Publication number Publication date
JPS63238968A (en) 1988-10-05

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