JPS6310059A - Manufacture of fiber reinforced metal composition material - Google Patents
Manufacture of fiber reinforced metal composition materialInfo
- Publication number
- JPS6310059A JPS6310059A JP15267786A JP15267786A JPS6310059A JP S6310059 A JPS6310059 A JP S6310059A JP 15267786 A JP15267786 A JP 15267786A JP 15267786 A JP15267786 A JP 15267786A JP S6310059 A JPS6310059 A JP S6310059A
- Authority
- JP
- Japan
- Prior art keywords
- preform
- molten metal
- metal
- plunger
- composite material
- 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
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 29
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 27
- 239000002184 metal Substances 0.000 title claims abstract description 27
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 239000000835 fiber Substances 0.000 title abstract description 17
- 238000002844 melting Methods 0.000 claims abstract description 5
- 230000008018 melting Effects 0.000 claims abstract description 5
- 239000011159 matrix material Substances 0.000 claims abstract description 4
- 239000002905 metal composite material Substances 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 8
- 238000000859 sublimation Methods 0.000 claims description 2
- 230000008022 sublimation Effects 0.000 claims description 2
- 239000002657 fibrous material Substances 0.000 claims 1
- 239000011156 metal matrix composite Substances 0.000 claims 1
- 238000007711 solidification Methods 0.000 abstract description 8
- 230000008023 solidification Effects 0.000 abstract description 8
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 4
- 238000003825 pressing Methods 0.000 abstract description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 abstract description 4
- 229910010271 silicon carbide Inorganic materials 0.000 abstract description 3
- 239000000126 substance Substances 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 238000005470 impregnation Methods 0.000 description 4
- 238000007796 conventional method Methods 0.000 description 3
- 239000007791 liquid phase Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 238000001192 hot extrusion Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 239000012466 permeate Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000208125 Nicotiana Species 0.000 description 1
- 235000002637 Nicotiana tabacum Nutrition 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000011208 reinforced composite material Substances 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
Landscapes
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は酸化物、炭化物、窒化物々どセラさックスのウ
ィスカまたは炭tA繊維、炭化珪素繊維あるいはアルミ
ナ繊mカどの連続繊維を短くチョップした短繊維によっ
て強化された金属基複合材料、特に高圧溶湯含浸法によ
る複合材料の製造法に関する。[Detailed Description of the Invention] [Industrial Field of Application] The present invention is directed to chopping continuous fibers such as oxide, carbide, and nitride ceramics whiskers or carbon tA fibers, silicon carbide fibers, and alumina fibers into short pieces. The present invention relates to a metal-based composite material reinforced with short fibers, particularly a method for producing the composite material by high-pressure molten metal impregnation.
セツンツクスのウィスカや各種のセラミック系のチ盲ツ
プドファイバなどの耐熱性、引張強さ、弾性率の優れた
短繊維を各埋金W4に複合させれば引張強さ、弾性率な
どの特性が優れた複合材料が得られることが知られてい
る。If short fibers with excellent heat resistance, tensile strength, and modulus of elasticity, such as whiskers of C. setunthus and various types of ceramic-based twisted fibers, are combined with each filler metal W4, properties such as tensile strength and modulus of elasticity will be excellent. It is known that composite materials can be obtained.
従来のこのような複合材料の製造方法の一例を、第4図
、第5図によって説明する。An example of a conventional method for manufacturing such a composite material will be explained with reference to FIGS. 4 and 5.
先ず、ウィスカ等の短繊維を水、有機樹脂溶液あるいは
無機質の塩類等を添加した水溶液と混合してスラリ状と
して、これを金型等に充填圧縮してプリフォームを成形
する。次いでこのプリフォームを予熱して第4図に示す
ような鋳型に装入する。第4図において1はプリフォー
ム、2は鋳型、3は上型プラテン、5は下型プラテンで
ある。次いで第5図に示すように下型プラテン5の溶湯
コンテナ部に金属の溶湯4を注入した後、加圧プランジ
ャ6にて金属溶gJ4を短繊維のプリフォーム1中に含
浸させて複合材料を得る。First, short fibers such as whiskers are mixed with water, an organic resin solution, or an aqueous solution to which inorganic salts are added to form a slurry, and this is filled and compressed into a mold or the like to form a preform. This preform is then preheated and placed in a mold as shown in FIG. In FIG. 4, 1 is a preform, 2 is a mold, 3 is an upper mold platen, and 5 is a lower mold platen. Next, as shown in FIG. 5, after pouring the molten metal 4 into the molten metal container of the lower mold platen 5, the pressurized plunger 6 impregnates the short fiber preform 1 with the molten metal GJ4 to form a composite material. obtain.
この方法によシ炭化珪素ウィスカとアルミニウム合金の
組合せの複合材料を製造する場合の条件の一例としては
、プリフォームの予熱温度650℃、アルミニウム合金
溶湯温度75otl:、溶湯加圧力800 kl/cm
”であプ、これKよシクイスカの含有体積率50幅程度
までの複合材料の製造が可能である。複合材料はこのま
\の状態で使用されることもあるが、熱間押出、鍛造、
圧縮等の辺性加工を硅て、型材、鍜造品、板、棒等くし
て使用されることが多い。An example of the conditions for producing a composite material combining silicon carbide whiskers and aluminum alloy by this method is as follows: preform preheating temperature 650°C, aluminum alloy molten metal temperature 75 otl, molten metal pressing force 800 kl/cm.
It is possible to manufacture composite materials with a content volume ratio of up to about 50.Composite materials may be used in their current state, but they can also be processed by hot extrusion, forging,
After undergoing edge processing such as compression, it is often used to make shapes, carved products, plates, rods, etc.
〔発明が解決しようとする問題点]
前述の方法により、短繊維と金属の複合化はお\むね満
足すべきものとなるが、複合材料の内部、特に中心部く
微細なポロシティが残存することが多い。通常の金属材
料においては、鋳造インゴットに生じたポロシティはそ
の後の圧延、押出等の塑性加工によってほとんどの場合
消滅する。しかし、と\で問題とする複合材料の場合は
七2ずツクの短繊維が相当量含有しているので、塑性加
工によってポロシティは押しつぶされみかけ上は消滅す
るが、完全には圧着接合していないため、材料の機械的
性fft−低下させ、複合材料の信頼性を乏しいものに
する大きな原因となっている。特に疲労強度に対する悪
影響は大きく、複合材料の広範表実用化を図る上でこの
マイクロポロシティの発生し表い複合材料の製造法の開
発が強く要舅されている。[Problems to be solved by the invention] Although the above-described method results in a generally satisfactory composite of short fibers and metal, fine porosity often remains inside the composite material, especially in the center. . In ordinary metal materials, porosity that occurs in cast ingots is almost always eliminated by subsequent plastic working such as rolling and extrusion. However, in the case of the composite material in question, it contains a considerable amount of short fibers, so the porosity is crushed by plastic processing and appears to disappear, but it is not completely crimped and bonded. This decreases the mechanical properties of the material and is a major cause of poor reliability of the composite material. In particular, the negative impact on fatigue strength is significant, and in order to put composite materials into practical use over a wide range of areas, there is a strong need to develop a manufacturing method for composite materials due to the generation of microporosity.
本発明ばこの要望に答えた覆合材料の製造法を提供しよ
うとするものである。It is an object of the present invention to provide a method for producing a covering material that meets the needs of tobacco smokers.
〔問題点を解決するための手段]
本発明は、全4マトリツクス複合材料の製造において、
マトリックス金属の融点より高い融点ご念は昇華温度を
もつm、錐状物質のプリフォームを金型中く装入し、こ
れに金属の溶湯を加圧しプリフォーム中へ含浸させ、含
浸が達成され死時点で、形成された当該複合体を更に部
分的に加圧することを特徴とする繊維強化金属複合材料
の製造方法である。[Means for solving the problems] The present invention provides the following features in the production of a total 4-matrix composite material:
If the melting point is higher than the melting point of the matrix metal, a preform of a conical material with a sublimation temperature is placed in a mold, and the molten metal is pressurized to impregnate the preform, and impregnation is achieved. This method of manufacturing a fiber-reinforced metal composite material is characterized in that the formed composite is further partially pressurized at the point of death.
そして本発明の上記構成において、部分的に加圧する部
分にあらかじめ断熱層を設けておき、その近傍の凝固完
了時点を遅延させるようくすることを好まし−実施島様
とするものである。In the above structure of the present invention, it is preferable to provide a heat insulating layer in advance in the part to be partially pressurized so as to delay the completion of solidification in the vicinity thereof.
マイクロポロシティの成因としては、短amの高密度の
集積体であるプリフォーム中へ高圧含浸させ九金属溶湯
の凝固時のマイクロシュリンケージであシ、繊維の高密
度集積体を通じての溶湯の補給が不十分と々る結果、こ
れが残存すると考えられる。そこで本発明は浴湯を高圧
含浸後の凝固開始さら完了までの中間の時点で更に部分
的に加圧することによ)シュリンケージ中に金属の液相
を浸透させ、これを消滅させるのである。The causes of microporosity include micro-shrinkage during solidification of nine metal molten metal by high-pressure impregnation into the preform, which is a high-density aggregate of short am, and replenishment of the molten metal through a high-density aggregate of fibers. It is thought that this remains as a result of insufficient performance. Therefore, in the present invention, the liquid phase of the metal permeates into the shrinkage by partially pressurizing the bath water at an intermediate point between the start of solidification and the completion of solidification after high-pressure impregnation), thereby causing the metal liquid phase to permeate into the shrinkage and disappear.
前述のようく、凝固完了前の部分的に液相が残っている
時点で加圧するので、シュリンケージ中はシティの消滅
は容易に起る。As mentioned above, since pressurization is applied before the solidification is completed and the liquid phase remains partially, the city easily disappears during shrinkage.
本発明の一実yl!!態様を第1図及び第2図によって
説明する。:′a1図、f¥2図において、第4図、第
5図と同一符号F!第4図、第5図と同一部を示す。7
は複動グランジャー、8はその内側プランジャーである
。A fruit of this invention! ! The embodiment will be explained with reference to FIGS. 1 and 2. :' In figures a1 and f¥2, the same symbol F as in figures 4 and 5! The same part as FIGS. 4 and 5 is shown. 7
is a double-acting granger, and 8 is its inner plunger.
テンの溶鉛コンテナ部に7501:の70751合金の
溶湯4を注入し、複動機mを有するプランジャー7にて
溶@4を加圧(700kg/α8)、シ、ウィスカプリ
フォーム1中へ含浸させた。Pour molten metal 4 of 7501: 70751 alloy into the molten lead container of the ten, pressurize the molten metal 4 with a plunger 7 having a compound mechanism (700 kg/α8), and impregnate it into the whisker preform 1. I let it happen.
ムを合金溶湯4がウィスカプリフォーム1中へ含浸、充
”満し注入が限界に達した時点で、第2図に示すように
複動プランジャー7の内側プランジャー8にて更(加圧
(プランジャー上面での面圧(s o o o k2/
eWl” ) ) L、複合材料全体の凝固が完了する
まで保持した。When the molten alloy 4 impregnates and fills the whisker preform 1 and the injection reaches its limit, the inner plunger 8 of the double-acting plunger 7 is used to pressurize (Surface pressure on the top surface of the plunger (so o o k2/
eWl”) L, held until solidification of the entire composite material was completed.
この方法によ抄製造し九複合材料の軸方向断面を研磨仕
上げ(す40ロエメ!J −fi ) 、酸溶液(@成
:硝a10Q Q: / 4 、クロム酸sat/ t
s弗酸1o a: / L b 残り水) K ’C
S 分子s”l xッチングし之のち、蛍光浸透探傷検
査を行ったが、欠陥は検出されなかった。The axial cross section of the nine composite materials manufactured by this method was polished and finished with an acid solution (@Nitrica10Q Q: /4, chromic acid sat/t).
s Hydrofluoric acid 1o a: / L b remaining water) K 'C
After etching, fluorescent penetrant inspection was performed, but no defects were detected.
これに対して複動プランジャによる2段加圧を行わない
従来法で製造した複合材料についての上記の検査では、
断面の中央部の下側(プランジャ側)K許状にマイク胃
ポロシティが検出された。On the other hand, in the above inspection of composite materials manufactured by the conventional method that does not perform two-stage pressurization with a double-acting plunger,
Microgastric porosity was detected on the lower side (plunger side) of the central part of the cross section.
)う;なか、本発明の複動プランジャーによろ2段■
維あるいは炭化珪素繊維などで作った布、フエパルト等
を置くか、ちるいはジル;ニアが−のセ1j】
−’)tツクスをコーティングして断熱効果をもた;
゛ぜてプランジャー上部の凝固を部分的に遅延させて加
圧することくよシ欠陥消滅の効果は吏に火車くすること
ができた。) Inside the double-acting plunger of the present invention, place a cloth or fabric made of fiber or silicon carbide fiber, etc. By coating the plunger with Tux to provide a heat insulating effect; by partially retarding the solidification of the upper part of the plunger and pressurizing it, the effect of eliminating defects could be greatly improved.
なお本発明方法で得られた複合材料は、熱間押出などの
後工at経九後でも、本発明の効果を失うことなく保有
している。すなわち、本発明方法で製造した複合材料を
ビレットとして熱間押出(押出比10:1)した押出材
(e1aウィスカ/7075ムを複合材料押出材、ウィ
スカ含有体積″X30%)の疲労強度を、従来法で製造
し九同種複合材の同一条件での熱間押出材との疲労強度
を比較したところ、第5図に示すような結果となり、本
発明方法で得られ九複合材料の効果が優れていることが
明らかとなった。The composite material obtained by the method of the present invention retains the effects of the present invention even after post-processing such as hot extrusion without losing the effects of the present invention. That is, the fatigue strength of an extruded material (e1a whisker/7075 μm composite material extruded material, whisker content volume ''X30%) obtained by hot extruding (extrusion ratio 10:1) the composite material produced by the method of the present invention as a billet is A comparison of the fatigue strength of a homogeneous composite material produced by the conventional method with a hot extruded material under the same conditions resulted in the results shown in Figure 5, indicating that the composite material produced by the method of the present invention has superior effects. It became clear that
なお第3図は破断までの繰返し数と応力のN係を示す図
表で、図中、1は本発明方法で製造した複合材料の熱間
押出材、2#ii来法で)遺し念複合材料の熱間押出材
の物性を示す。Furthermore, Figure 3 is a chart showing the number of repetitions until breakage and the N coefficient of stress. The physical properties of the hot extruded material are shown below.
得られ九ff1J1強化複合材料がその後の機械的加工
においても優れた効果を保有していることを複合材料の
製造方法を説明するための図である。FIG. 9 is a diagram for explaining the method for manufacturing the composite material, showing that the obtained 9ff1J1 reinforced composite material has excellent effects even in subsequent mechanical processing.
Claims (1)
ス金属の融点より高い融点または昇華温度をもつ繊維状
物質のプリフオームを金型中に装入し、これに金属の溶
湯を加圧し、プリフオーム中へ含浸させ、含浸が達成さ
れた時点で、形成された当該複合体を更に部分的に加圧
することを特徴とする繊維強化金属複合材料の製造方法
。In the production of metal matrix composite materials, a preform of a fibrous material with a melting point or sublimation temperature higher than the melting point of the matrix metal is charged into a mold, and molten metal is pressurized to impregnate the preform. A method for producing a fiber-reinforced metal composite material, which comprises further partially pressurizing the formed composite when the above is achieved.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15267786A JPS6310059A (en) | 1986-07-01 | 1986-07-01 | Manufacture of fiber reinforced metal composition material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15267786A JPS6310059A (en) | 1986-07-01 | 1986-07-01 | Manufacture of fiber reinforced metal composition material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6310059A true JPS6310059A (en) | 1988-01-16 |
| JPH028823B2 JPH028823B2 (en) | 1990-02-27 |
Family
ID=15545695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15267786A Granted JPS6310059A (en) | 1986-07-01 | 1986-07-01 | Manufacture of fiber reinforced metal composition material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6310059A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108527155A (en) * | 2016-03-03 | 2018-09-14 | P.R.霍夫曼机械制品有限公司 | Wafer holder of polishing machine |
| CN109080076A (en) * | 2018-06-26 | 2018-12-25 | 安徽昊方机电股份有限公司 | A kind of injection moulding apparatus of novel B MC material |
-
1986
- 1986-07-01 JP JP15267786A patent/JPS6310059A/en active Granted
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108527155A (en) * | 2016-03-03 | 2018-09-14 | P.R.霍夫曼机械制品有限公司 | Wafer holder of polishing machine |
| US10556317B2 (en) | 2016-03-03 | 2020-02-11 | P.R. Hoffman Machine Products Inc. | Polishing machine wafer holder |
| CN109080076A (en) * | 2018-06-26 | 2018-12-25 | 安徽昊方机电股份有限公司 | A kind of injection moulding apparatus of novel B MC material |
| CN109080076B (en) * | 2018-06-26 | 2023-09-15 | 安徽昊方机电股份有限公司 | Novel BMC material injection molding device |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH028823B2 (en) | 1990-02-27 |
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