JPS5945744B2 - Manufacturing method for fiber-reinforced composite materials - Google Patents
Manufacturing method for fiber-reinforced composite materialsInfo
- Publication number
- JPS5945744B2 JPS5945744B2 JP51068339A JP6833976A JPS5945744B2 JP S5945744 B2 JPS5945744 B2 JP S5945744B2 JP 51068339 A JP51068339 A JP 51068339A JP 6833976 A JP6833976 A JP 6833976A JP S5945744 B2 JPS5945744 B2 JP S5945744B2
- Authority
- JP
- Japan
- Prior art keywords
- fiber
- reinforced composite
- manufacturing
- container
- 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
Links
- 239000000463 material Substances 0.000 title claims description 13
- 238000004519 manufacturing process Methods 0.000 title claims description 10
- 239000003733 fiber-reinforced composite Substances 0.000 title claims 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 15
- 239000007789 gas Substances 0.000 claims description 12
- 239000010949 copper Substances 0.000 claims description 10
- 239000002657 fibrous material Substances 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 7
- 239000011159 matrix material Substances 0.000 claims description 6
- 238000000465 moulding Methods 0.000 claims description 4
- 229910000640 Fe alloy Inorganic materials 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 238000000748 compression moulding Methods 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- 238000002844 melting Methods 0.000 claims description 2
- 230000008018 melting Effects 0.000 claims description 2
- 230000008595 infiltration Effects 0.000 claims 3
- 238000001764 infiltration Methods 0.000 claims 3
- 230000000903 blocking effect Effects 0.000 claims 1
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 239000000470 constituent Substances 0.000 claims 1
- 239000011261 inert gas Substances 0.000 claims 1
- 230000035699 permeability Effects 0.000 claims 1
- 239000000835 fiber Substances 0.000 description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 9
- 229910002804 graphite Inorganic materials 0.000 description 9
- 239000010439 graphite Substances 0.000 description 9
- 239000002131 composite material Substances 0.000 description 8
- 238000000034 method Methods 0.000 description 8
- 238000007872 degassing Methods 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- 229910001080 W alloy Inorganic materials 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000004868 gas analysis Methods 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical compound CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 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
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 238000004049 embossing Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 150000004679 hydroxides Chemical class 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000005297 pyrex Substances 0.000 description 1
- 229910052903 pyrophyllite Inorganic materials 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
【発明の詳細な説明】
黒鉛繊維やWの細線のような長繊維やウィスカーのごと
き短繊維と金属やセラミックあるいは樹脂との組合せの
複合材料は、近年種々話題となっているが、樹脂をマト
リックスとするもの以外は殆んど工業化されていない。[Detailed Description of the Invention] Composite materials in which long fibers such as graphite fibers and fine wires of W or short fibers such as whiskers are combined with metals, ceramics, or resins have become a hot topic in recent years. Almost nothing other than that has been industrialized.
この理由はその製造が難かしいことによる。The reason for this is that it is difficult to manufacture.
例えば黒鉛繊維と金属との複合材料を作る為には、黒鉛
繊維に溶融した金属を含侵せしめる訳であるが、この時
この両者間に濡れ性がないと溶融した金属は黒鉛繊維間
に含侵しない。For example, in order to make a composite material of graphite fibers and metal, the graphite fibers are impregnated with molten metal, but at this time, if there is no wettability between the two, the molten metal will be impregnated between the graphite fibers. Do not infringe.
この為黒鉛繊維表面に例えばNiを被覆したりしている
。For this purpose, the surface of the graphite fiber is coated with, for example, Ni.
このNiを被覆すること自体も容易でないが、このNi
の存在のために複合材料全体の特徴が損なわれる。It is not easy to coat this Ni, but this Ni
The overall characteristics of the composite material are impaired due to the presence of .
このような事情はSiCと金属の組合せでも、セラミッ
ク繊維とガラスの組合せても全く同様である。This situation is exactly the same for the combination of SiC and metal and for the combination of ceramic fiber and glass.
本発明はこのような複合材料構成要素、すなわち繊維ま
たはウィスカ(以下繊維状物という)とマトリックス(
以下マトリックス母材という)間の濡れ性問題と関係な
く複合材料を製造するという工程的に極めて有用な方法
を提供するものである。The present invention utilizes such composite material components, namely fibers or whiskers (hereinafter referred to as fibrous materials) and matrix (
The present invention provides an extremely useful process for manufacturing composite materials regardless of the wettability problem between the matrix and the matrix.
勿論両者間に濡れ性があることは害とはならない。Of course, it is not harmful that there is wettability between the two.
本発明はマトリックスとなる材料を溶融状態で繊維状物
間に圧入する方法である。The present invention is a method of press-fitting a molten matrix material between fibrous materials.
この考え自体は別に新らしいものではない。This idea itself is not new.
本発明の特徴はこの前処理にある。The feature of the present invention lies in this pretreatment.
圧入ぜんとする時繊維状物間に空気が残っていれば当然
圧入されない部分が残る。If air remains between the fibrous materials when press-fitting, naturally some parts will remain that will not be press-fitted.
また多くの場合繊維状物そのものはガス成分を有してい
る。Further, in many cases, the fibrous material itself contains a gas component.
高温時このガス成分がガス化すれば、これによっても圧
入されない部分が発生する。If this gas component gasifies at high temperatures, this will also result in portions that cannot be press-fitted.
ここでいうガス成分とは物理吸着しているもの、化学吸
着しているものから水酸化物または酸化物の形で繊維の
凹所あるいは表面に存在するものを意味する。The gas component here refers to physically adsorbed components, chemically adsorbed components, and those present in the recesses or surfaces of the fibers in the form of hydroxides or oxides.
加熱によりこれらが温度と時間の関数として発生して来
た。Heating has produced these as a function of temperature and time.
現在ガス分析は、まず試料を常温で高真空にさらしてか
ら真空中で溶融し、発生するガスを定量しているが、こ
こで云うガス成分とはこのガス分析で求められるガス量
に近い。Currently, gas analysis involves first exposing a sample to a high vacuum at room temperature, then melting it in vacuum, and then quantifying the gas generated, but the gas components referred to here are close to the amount of gas determined by this gas analysis.
以上述べたような脱気および脱ガスする方法として今ま
でに公知の方法は、繊維状物を装入した容器に細長い吸
引管をつげておき、この吸収管から真空引きをしながら
全体を加熱し、脱ガス后この吸引管を溶接し封印する方
法である。The previously known method for degassing and degassing as described above involves attaching a long and thin suction tube to a container filled with fibrous material, and heating the entire body while drawing a vacuum from this absorption tube. After degassing, the suction pipe is welded and sealed.
この方法は大きな物品を作る時には何とかなるが、小さ
な物を作る時には面倒でコスト高となり、工業的な実施
は不可能に近い。This method works well when making large items, but when making small items it becomes troublesome and expensive, making it nearly impossible to implement industrially.
本発明は、特に小物を安く作ることに一つの特徴をもつ
方法である。The present invention is a method that is particularly characterized in that it makes small items inexpensively.
すなわち脱ガス終了時の封印を自動的に行なわせる方法
である。In other words, this is a method that automatically seals the gas at the end of degassing.
この方法として通気性のある物質、例えば多孔性焼結体
に他物質を溶浸して通気孔をふさいでしまおうというも
のである。This method involves infiltrating a breathable material, such as a porous sintered body, with another material to block the ventilation holes.
通気性物質と溶浸材の組合せは種々考えられる。Various combinations of breathable substances and infiltrants are possible.
FeまたはFe合金とCu・またはCu合金、COとC
u合金、CrとCu合金WとCu合金、WとNi合金、
Al2O3とガラスなどである。Fe or Fe alloy and Cu/or Cu alloy, CO and C
u alloy, Cr and Cu alloy W and Cu alloy, W and Ni alloy,
These include Al2O3 and glass.
これらは繊維の脱ガス終了温度、繊維との反応性などの
観点から選択される。These are selected from the viewpoints of fiber degassing completion temperature, reactivity with fibers, etc.
これらの組合せの中、安価でしかも最も技術的操作も簡
単なのはFeまたはFe合金とCuまたはCu合金であ
る。Among these combinations, Fe or Fe alloy and Cu or Cu alloy are the cheapest and the easiest to operate technically.
繊維に含侵せしめる物質は容器内に装入してもよく、ま
た容器の一部であっても良い。The substance for impregnating the fibers may be placed within the container or may be part of the container.
例えばNi容器とし、このNiの一部がWウィスカーの
中へ含侵し、残部Niは容器の役割を果すということが
可能であり、真空封印時の溶浸材例えばCuを繊維間の
含浸材として用いることも可能である。For example, if a Ni container is used, a part of this Ni will be impregnated into the W whiskers, and the remaining Ni will serve as the container. It is also possible to use
熱間圧縮成型の方法として最も好ましいのはArガスな
どを用いたいわゆる熱間静圧成型である。The most preferred hot compression molding method is so-called hot static pressure molding using Ar gas or the like.
この外パイロフィライトなどの固体圧力媒体を用いる方
法や、油などの液体圧力媒体を用いることも出来る。It is also possible to use a solid pressure medium such as external pyrophyllite or a liquid pressure medium such as oil.
これらは必要とする温度、圧力によって決められる。These are determined by the required temperature and pressure.
以下実施例を述べる。Examples will be described below.
実施例 1
線径15μミクロンの長い黒鉛繊維の束に厚み0.1.
mmの銅テープを5層に巻いて外径約101mの物を作
った。Example 1 A bundle of long graphite fibers with a wire diameter of 15 microns and a thickness of 0.1.
A piece with an outer diameter of about 101 m was made by winding 5 layers of copper tape with a diameter of about 101 m.
これを容器として内径10.57n7IL、外径13.
5mmの極軟鋼製パイプに充填した。Using this as a container, the inner diameter is 10.57n7IL and the outer diameter is 13.
It was filled into a 5 mm extremely mild steel pipe.
この極軟鋼製パイプの両端に100メツシュ以下150
メツシユ以上の鉄粉を軽く型押后900℃で1時間、水
素雰囲気下で焼結した比重4、■の厚み3m11Lの多
孔性鉄焼結体をはめ込み、10%Mnを含むCu合金の
小片をその上につめたのち同じ多孔性鉄焼結体をその上
にはめ込んで固定した。150 meshes of less than 100 on both ends of this extremely mild steel pipe
After lightly stamping iron powder with a mesh size or larger, a porous iron sintered body with a specific gravity of 4 and a thickness of 3 m and 11 L, which was sintered at 900°C for 1 hour in a hydrogen atmosphere, was inserted, and a small piece of a Cu alloy containing 10% Mn was inserted. After it was packed on top of that, the same porous iron sintered body was fitted onto it and fixed.
この全体を真空炉中に入れ、1030℃まで加熱したの
ち、冷却した。The whole was placed in a vacuum furnace, heated to 1030°C, and then cooled.
取り出してみると栓として用いた多孔質鉄焼結体の外側
のものが赤くなってCuが溶浸したことが明らかに認め
られ、またそれは鉄パイプに完全に接合していた。When it was taken out, the outside of the porous iron sintered body used as the plug turned red and was clearly seen to have been infiltrated with Cu, and it was also completely bonded to the iron pipe.
これをアルゴンガスな使用する熱間静圧成型機中に入れ
、まず温度を1150℃にあげたのち、ガスの圧力を2
000気圧に上昇した。This was put into a hot isostatic pressure molding machine that uses argon gas, and the temperature was first raised to 1150°C, and then the gas pressure was increased to 2.
The pressure rose to 000 atmospheres.
10分間保持したのち冷却降圧した。After holding for 10 minutes, the pressure was lowered by cooling.
取り出してのち表面の鉄パイプを切削加工で除去した。After taking it out, the iron pipe on the surface was removed by cutting.
黒鉛繊維が縦方向にきれいに配列した黒鉛−Cu複合体
が得られた。A graphite-Cu composite in which graphite fibers were neatly arranged in the longitudinal direction was obtained.
このものを切断加工して作ったチップは接点材料として
有用なものであった。Chips made by cutting this material were useful as contact materials.
実施例 2 実施例1と同様にしてAIを黒鉛繊維中に含侵した。Example 2 AI was impregnated into graphite fibers in the same manner as in Example 1.
ただし含浸温度は700℃であった。矢張黒鉛繊維が長
手方向にきれいに配列した黒鉛−AI複合体を得た。However, the impregnation temperature was 700°C. A graphite-AI composite in which Yabari graphite fibers were neatly arranged in the longitudinal direction was obtained.
ただしこの場合、実施例1のCu合金の替わりに溶浸材
として4%Mgを含むA1合金を使用した。However, in this case, instead of the Cu alloy of Example 1, an A1 alloy containing 4% Mg was used as an infiltrant.
実施例 3
Cuの外径151m内径10mm/深さ20mmの容器
の中にWのウィスカーをつめた。Example 3 W whiskers were packed in a Cu container with an outer diameter of 151 m, an inner diameter of 10 mm, and a depth of 20 mm.
この上に数10ミクロンのW粉末型押体をおき、さらに
その上にCuの小片をおいた。A W powder embossing body of several tens of microns was placed on top of this, and a small piece of Cu was further placed on top of this.
この全体をパイレックス製の容器に入れ、それを真空炉
に入れて1150℃まで加熱した。The whole was placed in a Pyrex container, which was then placed in a vacuum furnace and heated to 1150°C.
これを取り出してのち、熱間静圧成型機中に装入し、ま
ず1150℃に加熱したのちガス圧を1000気圧にあ
げ10分間保持した。After taking it out, it was charged into a hot isostatic pressure molding machine, first heated to 1150°C, and then the gas pressure was increased to 1000 atm and held for 10 minutes.
表面にCuが残っていたが、内部はW−Cu複合体で気
孔は全く認められなかった。Although Cu remained on the surface, the inside was a W-Cu composite and no pores were observed.
Claims (1)
を有する変形しうる容器内に繊維状物及びマトリックス
金属を装入し、該容器0通気性を有する部分に通気部を
ふさぐ形で容浸材となる金属焼結体または成形体を載せ
これを真空下におくか、あるいは、容器内を真空に吸引
しながら加熱し、容器内の空気及び繊維状物のもってい
るガス成分の大部分を除去し、該通気性部分を真空加熱
時マトリックス母材及び金属焼結体又は成型体の溶融に
よる溶浸によって密閉し、これを更に高温高圧下で熱間
圧縮成型することを特徴とする繊維強化型複合材の製造
法。 2、特許請求の範囲第1項記載の製造法において、高温
高圧下での熱間圧縮成型を、不活性ガスを用いる熱間静
圧成型法で行うことを特徴とする繊維強化型複合材の製
造法。 3 特許請求の範囲第1項、第2項記載の製造法におい
て、通気性を有する部分を鉄又は鉄合金とし、これへの
溶浸材を銅または銅合金もしくはAIまたはA1合金と
することを特徴とする繊維強化複合材の製造法。 4 特許請求の範囲第1項記載の製造法において、熱間
圧縮成型する時に容器の構成要素の一部を繊維状物間に
含浸することを特徴とする繊維強化複合材の製造法。[Scope of Claims] 1. In a method for producing a fiber-reinforced composite material, a fibrous material and a matrix metal are charged into a deformable container that partially has air permeability; Place a metal sintered body or molded body as an infiltration material in the form of blocking the vent and place it under vacuum, or heat it while vacuuming the inside of the container to remove the air and fibrous material inside the container. Most of the gas components present are removed, and the air-permeable part is sealed by infiltration by melting the matrix base material and the metal sintered body or molded body during vacuum heating, and this is further hot compression molded under high temperature and high pressure. A method for producing a fiber-reinforced composite material characterized by: 2. In the manufacturing method according to claim 1, the fiber-reinforced composite material is characterized in that the hot compression molding under high temperature and high pressure is performed by hot isostatic molding using an inert gas. Manufacturing method. 3 In the manufacturing method described in claims 1 and 2, the air permeable part is made of iron or an iron alloy, and the infiltration material therein is made of copper or a copper alloy, or an AI or A1 alloy. Characteristic manufacturing method for fiber-reinforced composite materials. 4. A method for producing a fiber-reinforced composite material according to claim 1, characterized in that a portion of the constituent elements of the container are impregnated between the fibrous materials during hot compression molding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP51068339A JPS5945744B2 (en) | 1976-06-10 | 1976-06-10 | Manufacturing method for fiber-reinforced composite materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP51068339A JPS5945744B2 (en) | 1976-06-10 | 1976-06-10 | Manufacturing method for fiber-reinforced composite materials |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS52150773A JPS52150773A (en) | 1977-12-14 |
| JPS5945744B2 true JPS5945744B2 (en) | 1984-11-08 |
Family
ID=13370974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP51068339A Expired JPS5945744B2 (en) | 1976-06-10 | 1976-06-10 | Manufacturing method for fiber-reinforced composite materials |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5945744B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1074335A (en) * | 1997-07-16 | 1998-03-17 | Pioneer Electron Corp | Disk player |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6029407A (en) * | 1983-07-27 | 1985-02-14 | Tohoku Metal Ind Ltd | Manufacture of alloy |
-
1976
- 1976-06-10 JP JP51068339A patent/JPS5945744B2/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1074335A (en) * | 1997-07-16 | 1998-03-17 | Pioneer Electron Corp | Disk player |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS52150773A (en) | 1977-12-14 |
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