JP2644093B2 - Composite wire manufacturing equipment and plate using composite wire - Google Patents
Composite wire manufacturing equipment and plate using composite wireInfo
- Publication number
- JP2644093B2 JP2644093B2 JP3011348A JP1134891A JP2644093B2 JP 2644093 B2 JP2644093 B2 JP 2644093B2 JP 3011348 A JP3011348 A JP 3011348A JP 1134891 A JP1134891 A JP 1134891A JP 2644093 B2 JP2644093 B2 JP 2644093B2
- Authority
- JP
- Japan
- Prior art keywords
- composite wire
- passage
- base material
- permeation
- hollow
- 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
Links
- 239000002131 composite material Substances 0.000 title claims description 50
- 238000004519 manufacturing process Methods 0.000 title claims description 19
- 239000012783 reinforcing fiber Substances 0.000 claims description 37
- 239000000463 material Substances 0.000 claims description 14
- 239000000835 fiber Substances 0.000 claims description 13
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- 238000001816 cooling Methods 0.000 claims description 7
- 238000004891 communication Methods 0.000 claims description 5
- 238000003825 pressing Methods 0.000 claims description 5
- 238000001125 extrusion Methods 0.000 claims description 4
- 239000011261 inert gas Substances 0.000 claims description 4
- 230000035515 penetration Effects 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 12
- 239000004917 carbon fiber Substances 0.000 description 12
- 229910052782 aluminium Inorganic materials 0.000 description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 11
- 238000000034 method Methods 0.000 description 9
- 239000011159 matrix material Substances 0.000 description 7
- 238000013329 compounding Methods 0.000 description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 230000008595 infiltration Effects 0.000 description 4
- 238000001764 infiltration Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 239000011888 foil Substances 0.000 description 3
- 239000002952 polymeric resin Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 229920001169 thermoplastic Polymers 0.000 description 2
- 101100493712 Caenorhabditis elegans bath-42 gene Proteins 0.000 description 1
- 241000219122 Cucurbita Species 0.000 description 1
- 235000009852 Cucurbita pepo Nutrition 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000003204 osmotic effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000004634 thermosetting polymer Substances 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Description
【０００１】[0001]
【産業上の利用分野】本発明は、例えば、炭素繊維やア
ルミナ繊維などの長い強化繊維を連続的に複合化して複
合線材を製造するための装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an apparatus for manufacturing a composite wire by continuously compounding long reinforcing fibers such as carbon fibers and alumina fibers.
【０００２】また、複合線材の製造装置によって製造さ
れた複合線材を積層状に積み重ねた複合線材を用いた板
材に関する。[0002] Further, the present invention relates to a sheet material using a composite wire rod in which composite wire rods manufactured by a composite wire rod manufacturing apparatus are stacked.
【０００３】[0003]
【従来の技術】従来、炭素繊維やアルミナ繊維をアルミ
ニウム（Ａｌ）などの母地によって複合化する方法とし
て種々の装置があるが、そのうち代表的なものとして以
下のようなものがある。2. Description of the Related Art Conventionally, there have been various apparatuses for combining carbon fibers or alumina fibers with a matrix such as aluminum (Al). Among them, the following are typical ones.
【０００４】図８は、高圧鋳造法の装置を示す概略図で
あって、20はＬ字形の空洞部21を有するＬ字形の金型で
ある。この金型20の垂直部22に加圧部23が嵌入し、この
加圧部23が上下動するようになっている。Ｌ字形空洞部
21の水平部24には強化繊維の配列体25が詰め込まれて、
このＬ字形の空洞部21に母地となる金属26が溶融状態で
入れられている。そして、加圧部23が下方に移動するこ
とによって金属26を加圧し、強化繊維内に母地が浸透す
るように構成されている。FIG. 8 is a schematic view showing an apparatus for a high-pressure casting method. Reference numeral 20 denotes an L-shaped mold having an L-shaped cavity 21. A pressing portion 23 is fitted into the vertical portion 22 of the mold 20, and the pressing portion 23 moves up and down. L-shaped cavity
An array 25 of reinforcing fibers is packed in the horizontal part 24 of 21,
In the L-shaped hollow portion 21, a metal 26 serving as a base is put in a molten state. Then, the metal part 26 is pressurized by the downward movement of the pressure part 23, so that the base material penetrates into the reinforcing fibers.
【０００５】図９は、熱間引抜き法の概略図であって、
ダイス30に入口側が大径で出口側が小径の透孔31が形成
され、加熱されたダイス30の透孔31に金属箔が巻き付け
られたワイヤ状の強化繊維32を通過させて引き抜きなが
ら強化繊維32を複合化していく。一定の太さの複合線材
を製作するにはダイス30の透孔31に引き抜いた複合線材
32を再度金属箔を巻き付けて束ね前記手順を繰り返す。FIG. 9 is a schematic view of a hot drawing method.
A through hole 31 having a large diameter on the inlet side and a small diameter on the outlet side is formed in the die 30, and the reinforcing fiber 32 is drawn while passing through a wire-like reinforcing fiber 32 in which a metal foil is wound around the through hole 31 of the heated die 30. Will be compounded. To produce a composite wire of a certain thickness, the composite wire drawn into the through hole 31 of the die 30
32 is wound around with a metal foil again and bound, and the above procedure is repeated.
【０００６】図１０は、炭素繊維を複合化する場合の製
造装置の概略図であって、ロール40に巻き付けられた炭
素繊維41が中央のスラリーバス42に浸漬されノズル43に
よって絞られて巻取機44によって巻き取られている。FIG. 10 is a schematic view of a manufacturing apparatus in which carbon fibers are compounded. A carbon fiber 41 wound around a roll 40 is immersed in a slurry bath 42 at the center, squeezed by a nozzle 43 and wound up. Winded by machine 44.
【０００７】以上のようにして製作された複合線材は、
一般に強化紐や電線などに用いられている。The composite wire manufactured as described above is
Generally used for reinforcing cords and electric wires.
【０００８】[0008]
【発明が解決しようとする課題】しかし、上記実施例の
うち図８の高圧鋳造法は、限られた金型のＬ字形空洞部
内に一定に裁断された強化繊維を詰め込まなければなら
ないため、強化繊維の大きさや形状に制限があり、しか
も、連続的な複合化はできない。However, in the high-pressure casting method shown in FIG. 8 in the above embodiment, the reinforcing fibers cut into a fixed L-shaped cavity must be packed into the L-shaped cavity. There are restrictions on the size and shape of the fibers, and furthermore, continuous compounding is not possible.
【０００９】また、図９の熱間引抜き法の場合は、強化
繊維に母地の金属箔を巻き付けて複合化しただけである
ことから個々の繊維まで複合化でき難く、強化繊維同士
の複合化が十分ではない。しかも、一定の太さの複合線
材を製作するには再度同じ手順を繰り返さなければなら
ないことから手間がかかる。Further, in the case of the hot drawing method shown in FIG. 9, since the reinforcing fiber is simply wound around the base metal foil to form a composite, it is difficult to compound individual fibers. Is not enough. In addition, the same procedure must be repeated to produce a composite wire having a certain thickness, which is troublesome.
【００１０】図１０の炭素繊維をスラリーバスに浸漬す
る装置は繊維の配列が不揃いになって母地内の気泡の除
去や繊維の配列の乱れを防止することができない。この
発明は、上記課題を解決するためになされたもので、強
化繊維の大きさや形状に制限されることがなく連続的に
複合化が可能で、強化繊維同士の複合化の密度も高く、
強化繊維の配列も適性な複合線材を製造するための製造
装置を提供することを目的とする。The apparatus shown in FIG. 10 for dipping carbon fibers in a slurry bath has a non-uniform fiber arrangement, and cannot remove air bubbles in the matrix and prevent the fiber arrangement from being disordered. The present invention has been made in order to solve the above problems, it is possible to continuously compound without being limited by the size and shape of the reinforcing fibers, the density of the compounding of the reinforcing fibers is high,
An object of the present invention is to provide a manufacturing apparatus for manufacturing a composite wire rod having an appropriate arrangement of reinforcing fibers.
【００１１】また、複合線材を積層状に積み重ねた軽く
て丈夫な複合線材の板材を提供することを目的としてい
る。It is another object of the present invention to provide a light and strong composite wire rod in which composite wire rods are stacked.
【００１２】[0012]
【課題を解決するための手段】本発明の複合線材の製造
装置は、母地を溜める中空部を有する金型と、中空部に
内嵌し中空部内の母地を加圧して押し出す押出部と、中
空部から加圧して押し出された母地を強化繊維に加圧浸
透させる浸透通路と、浸透通路の一端側に設けられた強
化繊維が入る入口部と、浸透通路の他端側に設けられ母
地が浸透した強化繊維が出るノズル部とから構成されて
いる。An apparatus for manufacturing a composite wire according to the present invention comprises: a mold having a hollow portion for storing a base;
An extrusion section for extruding a mother locations inner fitting Shi the hollow portion under pressure, and permeate passages to the reinforcing fibers pressurized extruded base fabric from the hollow portion pressure immersion <br/>-tight, one end side of the penetration path And a nozzle portion provided at the other end of the infiltration passage and through which the reinforcing fibers penetrated by the mother ground emerge.
【００１３】また、本発明の複合線材を用いた板材は、
均一な太さの強化繊維に母地が浸透してなる複合線材を
積層状に積み重ねて加圧成型し、隣接する複合線材間に
空隙を無くし、板状に形成している。Further, the plate using the composite wire of the present invention is:
Uniform thickness composite wire mother land on reinforcing fibers formed by penetration of the pressurized and pressure-molded stacked in layers, between adjacent composite wire
It is formed in a plate shape with no voids .
【００１４】[0014]
【作用】本願発明の複合線材の製造装置は前記構成によ
り、中空部内の母地が押出部によって浸透通路に加圧し
て押し出され浸透通路を通過する強化繊維の束に母地が
加圧浸透する。母地が加圧浸透した強化繊維はノズル部
から引き抜かれ高圧加圧され巻き取られる。浸透通路を
通過する強化繊維はテンションがかけられているので繊
維が整列している。By the action apparatus for producing composite wire of the present applied invention is the arrangement, pressurized to osmotic passage mother locations within the hollow portion by the pushing portion
The base of the bundle of reinforcing fibers that is pushed out and passes through the permeation passage
Infiltrate under pressure . The reinforcing fibers whose base material has been pressurized and infiltrated are pulled out from the nozzle portion, are pressurized under high pressure, and are wound. The reinforcing fibers passing through the infiltration passage are under tension so that the fibers are aligned.
【００１５】また、複合線材を用いた板材は、単なる板
材に比べて軽くて丈夫である。A plate made of a composite wire is lighter and stronger than a simple plate.
【００１６】[0016]
【実施例】以下、本発明の一実施例を図面に基づいて説
明する。図１及び図２は、本発明の複合線材の製造装置
の一実施例であつて、この実施例の複合線材の製造装置
１は、母地２を溜める中空部３を有する金型４と、中空
部３内に圧入し中空部３内の母地２を押し出す押出部５
と、中空部３の下端部に設けられた中空部３と浸透通路
６とを連通する連通路７と、連通路７の下端部に設けら
れた浸透通路６と、浸透通路６の一端側に設けられた入
口部８と、浸透通路６の他端側に設けられたノズル部９
とから構成されている。この図１及び図２の構成図は加
圧のためのプレス及び外枠は省略されている。An embodiment of the present invention will be described below with reference to the drawings. 1 and 2 show an embodiment of a composite wire manufacturing apparatus according to an embodiment of the present invention. The composite wire manufacturing apparatus 1 of this embodiment includes a mold 4 having a hollow portion 3 for storing a base 2, Extruding part 5 which presses into hollow part 3 and pushes out base 2 in hollow part 3
A communication passage 7 provided at the lower end of the hollow portion 3 and communicating with the permeation passage 6; a permeation passage 6 provided at the lower end of the communication passage 7; The inlet 8 provided and the nozzle 9 provided on the other end side of the permeation passage 6
It is composed of 1 and 2, the press for pressurization and the outer frame are omitted.
【００１７】金型４の中空部３には、内型11が嵌め込ま
れて、この内型11を取り囲んで加熱ヒータ10ーが設けら
れ、母地２を加熱するよう構成されている。但し、この
加熱ヒータ10ーは、常温の母地２を使用する場合には必
ずしも必要ではない。An inner mold 11 is fitted into the hollow portion 3 of the mold 4, and a heater 10 is provided so as to surround the inner mold 11, so that the base 2 is heated. However, the heater 10- is not always necessary when the base 2 at room temperature is used.
【００１８】この金型４の内型11にはプランジヤなどの
押出部５が内嵌し、この押出部５によって加熱ヒータ10
ーにより溶融した母地２を２本の通路からなる連通路７
へ押し出す。An extruded portion 5 such as a plunger is fitted in the inner die 11 of the mold 4, and the extruded portion 5 allows the heater 10 to be heated.
A communication path 7 composed of two paths through the base 2 melted by
Push out.
【００１９】この連通路７の下端に設けられた浸透通路
６は断面が図２に示すように半円同士を結合して略瓢箪
形の通路であって、強化繊維12A がこの浸透通路６の一
端側から他端側の中央部を通過する。このように浸透通
路６の断面を略瓢箪形に形成することにより強化繊維12
A に母地２を均等に浸透させることができる。但し、浸
透通路６は上記のような形状である必要はなく断面が円
形や楕円形のものであつてもよく、その形状は問わな
い。The permeation passage 6 provided at the lower end of the communication passage 7 is a substantially gourd-shaped passage whose semi-circles are joined together as shown in FIG. It passes through the center from one end to the other end. By forming the cross section of the infiltration passage 6 into a substantially gourd shape in this manner, the reinforcing fibers 12 are formed.
A can evenly penetrate the mother land 2. However, the permeation passage 6 does not need to have the above-mentioned shape, and may have a circular or elliptical cross section, and the shape is not limited.
【００２０】浸透通路６の一端側には入口部８が設けら
れている。この入口部８は金型４の浸透通路６の一端部
に嵌合部13A が形成され、この嵌合部13A に入口部８が
嵌合している。入口部８の通路は一端と他端が細く、中
央部8Aが太くなつており、この中央部8Aの下部から不活
性ガス14（アルゴンガスを使用）が中央部8A内に充填し
炭素繊維などの強化繊維12A が酸化しないようになって
いる。An inlet 8 is provided at one end of the permeation passage 6. The inlet 8 has a fitting portion 13A formed at one end of the permeation passage 6 of the mold 4, and the inlet 8 is fitted into the fitting portion 13A. One end and the other end of the passage of the inlet portion 8 are thin, and the central portion 8A is thick. An inert gas 14 (using argon gas) is filled into the central portion 8A from the lower portion of the central portion 8A, and carbon fiber and the like are filled. Of the reinforcing fiber 12A is not oxidized.
【００２１】金型４の浸透通路６の他端側に嵌合部13B
が形成され、この嵌合部13B にはノズル部９が嵌合し、
このノズル部９は、母地２が浸透した強化繊維12A を高
圧に絞り込んで母地２がたれ落ちないようにダイス（図
示せず）が取り付けられている。A fitting portion 13B is provided at the other end of the permeation passage 6 of the mold 4.
The nozzle portion 9 is fitted into the fitting portion 13B,
The nozzle portion 9 is provided with a die (not shown) so that the reinforcing fibers 12A into which the base 2 has penetrated are squeezed to a high pressure to prevent the base 2 from dripping.
【００２２】このノズル部９から他端方向に筒状の冷却
部15が設けられ、この冷却部15の通路にも不活性ガス14
が通るように構成され、母地２が浸透した強化繊維12A
を冷却しするとともに、強化繊維12A が酸化しないよう
配慮されている。A cylindrical cooling section 15 is provided from the nozzle section 9 toward the other end, and an inert gas 14 is also provided in a passage of the cooling section 15.
Through which the reinforcing fibers 12A impregnated with the base 2
In addition to cooling, the reinforcing fibers 12A are not oxidized.
【００２３】次に、上記実施例の複合線材の製造装置１
によって金属の母地２で炭素繊維やアルミナ繊維などの
強化繊維12A を複合化する場合の使用状態を説明する。
まず、金型４を加熱ヒータ10で加熱し、金型４の中空部
３に入れられたアルミニウム（Ａｌ）を軟化ないしは溶
融状態になるように４５０℃〜７００℃で加熱する。Next, the composite wire manufacturing apparatus 1 of the above embodiment will be described.
The state of use in the case where the reinforcing fiber 12A such as carbon fiber or alumina fiber is compounded in the metal matrix 2 will be described.
First, the mold 4 is heated by the heater 10, and the aluminum (Al) put in the hollow portion 3 of the mold 4 is heated at 450 ° C to 700 ° C so as to be in a softened or molten state.
【００２４】そして、軟化ないしは溶融状態のアルミニ
ウム（Ａｌ）を５０kgf/cm2 から７０００kgf/cm2 で加
圧し、アルミニウム（Ａｌ）を連通路７を通して浸透通
路６側に押し出す。[0024] Then, extrude softened or aluminum in the molten state (Al) pressurized from 50 kgf / cm 2 at 7000kgf / cm 2, the aluminum (Al) through the communicating path 7 to the penetration passage 6 side.
【００２５】浸透通路６の一端側の入口部８から他端側
のノズル部９にかけて強化繊維12A の束がテンシヨンを
かけた状態で通されている。そして、浸透通路６内の強
化繊維12A の束に加圧されたアルミニウム（Ａｌ）が浸
透し、さらに強化繊維12A を引き抜く際にノズル部９の
ダイス（図示せず）によって高圧加圧されアルミニウム
（Ａｌ）と複合化し、冷却部15で不活性ガス14によって
冷却される。冷却部15で冷却された複合線材12B は巻取
機16によって連続的に巻き取られる。A bundle of reinforcing fibers 12A is passed from the inlet 8 at one end of the permeation passage 6 to the nozzle 9 at the other end thereof under tension. Then, the pressurized aluminum (Al) penetrates into the bundle of the reinforcing fibers 12A in the permeation passage 6, and when the reinforcing fibers 12A are pulled out, the aluminum (Al) is pressurized with a high pressure by a die (not shown) of the nozzle portion 9. Al) and cooled by the inert gas 14 in the cooling unit 15. The composite wire 12B cooled by the cooling unit 15 is continuously wound by a winder 16.
【００２６】このようにして強化繊維12A は短時間で母
地２に包みこまれワイヤとして巻き取られるので強化繊
維12A の高温酸化や金属との反応も最小限に抑えること
ができる。In this manner, the reinforcing fiber 12A is wrapped in the matrix 2 in a short time and wound up as a wire, so that the high-temperature oxidation of the reinforcing fiber 12A and the reaction with the metal can be minimized.
【００２７】なお、複合線材12B の径はノズル部９のダ
イス（図示せず）を変えることにより自由な大きさに変
更することができる。上記のようにして製造された複合
線材12B の断面を図３に示しているが、同図のように複
合線材12B は母地２の中心付近にやや密に強化繊維12A
が複合化されている。The diameter of the composite wire 12B can be freely changed by changing a die (not shown) of the nozzle portion 9. A cross section of the composite wire 12B manufactured as described above is shown in FIG. 3, and as shown in FIG.
Is compounded.
【００２８】次に上記の実施例のさらに具体的な実施例
を数値に基づいて説明する。強化繊維12A は炭素繊維を
用い、繊維数は約２０００本を束ねたものである。母地
２は純度が９９．７％のアルミニウム（Ａｌ）を使用し
た。製造条件はアルミニウム（Ａｌ）の加熱温度６３０
℃、金型４の加熱温度（内型11の温度）６７０℃、押圧
部５による加圧力３０００kgf/cm2 、炭素繊維の引張速
度は張力が働く程度の任意速度、入口部８とノズル部９
の径は１．５mmであった。Next, a more specific embodiment of the above embodiment will be described based on numerical values. The reinforcing fibers 12A are made of carbon fibers, and the number of fibers is about 2,000 bundled. Base 2 used aluminum (Al) having a purity of 99.7%. The manufacturing condition is a heating temperature of aluminum (Al) 630.
° C, the heating temperature of the mold 4 (the temperature of the inner mold 11) is 670 ° C, the pressing force by the pressing portion 5 is 3000 kgf / cm 2 , the tension speed of the carbon fiber is an arbitrary speed at which the tension works, the inlet portion 8 and the nozzle portion 9.
Was 1.5 mm in diameter.
【００２９】その結果、炭素繊維がほぼ均一に複合化さ
れて、炭素繊維と母地２のアルミニウムとの境界には空
洞はみられなかつた。なお、上記実施例では母地２とし
てアルミニウム（Ａｌ）を使用した例を説明したが、高
分子系樹脂を母地２として使用することもできる。例え
ば、母地２として熱可塑性高分子系樹脂を使用した場
合、アルミニウム（Ａｌ）を母地２として使用した場合
と同様な押出し方法であるが、加熱温度と加圧圧力が熱
可塑性高分子系樹脂に適した値を用いればよい。As a result, the carbon fibers were almost uniformly compounded, and no cavities were found at the boundary between the carbon fibers and the aluminum of the base 2. In the above embodiment, an example in which aluminum (Al) is used as the base 2 has been described. However, a polymer resin may be used as the base 2. For example, when a thermoplastic polymer resin is used as the matrix 2, the extrusion method is the same as that when aluminum (Al) is used as the matrix 2, but the heating temperature and the pressurizing pressure are different from those of the thermoplastic polymer resin. A value suitable for the resin may be used.
【００３０】また、母地として熱硬化性高分子系樹脂を
使用した場合、金型４を加熱することなく、冷却部15を
ノズル部９として、このノズル部９を加熱し、その他は
アルミニウム（Ａｌ）を母地として使用した場合と同様
にして押し出せばよい。When a thermosetting polymer resin is used as the matrix, the cooling section 15 is used as the nozzle section 9 without heating the mold 4, and the nozzle section 9 is heated. Al) may be extruded in the same manner as when the base is used.
【００３１】上記のようにして製造した複合線材12B は
図４に示すように繊維密度が高く整然と並んでいる。次
に、前記のようにして製作した複合線材12B を板体に製
作する場合を説明する。図５から図７は、板材17の製造
例を示し、図５は、複合線材12B を束ね積層状に積み重
ねた状態を示している。そして、図６のように積層状に
積み重ねた複合線材12B をホットプレス法や熱間圧延な
どの手法により加圧成型を行う。このように加圧成型し
て図７のように最終成型を行って複合線材12B の板材17
が完成する。このようにしてできた複合線材12B の板材
17は、軽くて丈夫であることから飛行機の翼や、飛行機
のフラップさらにはロボットのアームなどに用いること
ができる。The composite wires 12B manufactured as described above have a high fiber density and are arranged neatly as shown in FIG. Next, a case in which the composite wire 12B manufactured as described above is manufactured in a plate body will be described. 5 to 7 show a production example of the plate material 17, and FIG. 5 shows a state in which the composite wires 12B are bundled and stacked in a stacked manner. Then, as shown in FIG. 6, the composite wires 12B stacked in a layered form are subjected to pressure molding by a technique such as hot pressing or hot rolling. Press forming is performed as described above, and final forming is performed as shown in FIG.
Is completed. Plate material of composite wire 12B made in this way
The 17 is light and durable and can be used for airplane wings, airplane flaps, and even robot arms.
【００３２】[0032]
【発明の効果】本発明の複合線材の製造装置は、前記構
成により、強化繊維の大きさや形状に制限されることが
なく連続的に複合化が可能で、強化繊維同士の複合化の
密度も高く、繊維の配列も適性である。According to the apparatus for manufacturing a composite wire of the present invention, the above-described configuration enables continuous compounding without being limited by the size and shape of the reinforcing fiber, and also increases the density of the compounding of the reinforcing fibers. High, the fiber arrangement is also suitable.
【００３３】また、本発明の複合線材を用いた板材は、
複合線材を積層状に積み重ねて加圧したことから軽くて
丈夫である。The plate using the composite wire of the present invention is
Since the composite wires are stacked and pressed, they are light and durable.
【図１】本発明の複合線材の製造装置の正面側の断面図
である。FIG. 1 is a front sectional view of a composite wire manufacturing apparatus according to the present invention.
【図２】本発明の複合線材の製造装置の側面側の断面図
である。FIG. 2 is a side sectional view of the composite wire manufacturing apparatus of the present invention.
【図３】金属を母地とする複合線材を裁断した端部の斜
視図である。FIG. 3 is a perspective view of an end portion obtained by cutting a composite wire having metal as a base.
【図４】高分子系複合材料を母地とする複合線材を裁断
した端部の斜視図である。FIG. 4 is a perspective view of an end portion obtained by cutting a composite wire rod based on a polymer composite material.
【図５】複合線材を積層状に積み重ねた端部の斜視図で
ある。FIG. 5 is a perspective view of an end portion in which composite wires are stacked in a layered manner.
【図６】積層状に積み重ねた複合線材を加圧した端部の
斜視図である。FIG. 6 is a perspective view of an end portion of a composite wire rod that is stacked in a laminated state and is pressed.
【図７】複合線材を板状に最終成型した端部の斜視図で
ある。FIG. 7 is a perspective view of an end portion of the composite wire rod which is finally formed into a plate shape.
【図８】従来の高圧鋳造法の概略図である。FIG. 8 is a schematic view of a conventional high-pressure casting method.
【図９】従来の熱間引抜き法の概略図である。FIG. 9 is a schematic view of a conventional hot drawing method.
【図10】従来の炭素繊維の複合化の概略図である。FIG. 10 is a schematic diagram of a conventional carbon fiber composite.
１ 複合線材の製造装置 ２ 母地 ３ 中空部 ４ 金型 ５ 押出部 ６ 浸透通路 ８ 入口部 ９ ノズル部 12Ａ 強化繊維 17 板材 DESCRIPTION OF SYMBOLS 1 Manufacturing apparatus of composite wire 2 Base 3 Hollow part 4 Mold 5 Extrusion part 6 Infiltration passage 8 Inlet part 9 Nozzle part 12A Reinforcing fiber 17 Board material
───────────────────────────────────────────────────── フロントページの続き (72)発明者 小竹 誠一 大阪府大阪市此花区西九条５丁目３番28 号 日立造船株式会社内 (72)発明者 堀田 隆一 大阪府大阪市此花区西九条５丁目３番28 号 日立造船株式会社内 (72)発明者 堀 徹 大阪府大阪市此花区西九条５丁目３番28 号 日立造船株式会社内 (72)発明者 岸田 坦 大阪府大阪市此花区西九条５丁目３番28 号 日立造船株式会社内 (56)参考文献 特開 昭63−132036（ＪＰ，Ａ) 特開 昭59−95133（ＪＰ，Ａ) 実開 昭58−82242（ＪＰ，Ｕ) ──────────────────────────────────────────────────続 き Continuing on the front page (72) Inventor Seiichi Kotake 5-28 Nishikujo, Konohana-ku, Osaka-shi, Osaka Inside Hitachi Zosen Corporation (72) Inventor Ryuichi Hotta 5-chome, Nishikujo, Konohana-ku, Osaka-shi, Osaka 3-28 No. Hitachi Zosen Corporation (72) Inventor Toru Hori 5-28 Nishikujo, Konohana-ku, Osaka-shi, Osaka Prefecture (72) Inventor Tan Kishida Nishikujo, Konohana-ku, Osaka-shi, Osaka 5-3-28, Hitachi Zosen Corporation (56) References JP-A-63-132036 (JP, A) JP-A-59-95133 (JP, A) Japanese Utility Model 58-82242 (JP, U)
Claims (4)
空部に内嵌し中空部内の母地を加圧して押し出す押出部
と、中空部から加圧して押し出された母地を強化繊維に
加圧浸透させる浸透通路と、浸透通路の一端側に設けら
れた強化繊維が入る入口部と、浸透通路の他端側に設け
られ母地が浸透した強化繊維が出るノズル部とから構成
されていることを特徴とする複合線材の製造装置。1. A mold having a hollow portion for storing a base material, an extruding portion which is fitted into the hollow portion and presses out the base material in the hollow portion and extrudes the base material, and a base material pressed and extruded from the hollow portion to strengthen the base material. Fiber
A permeation passage for pressurized permeation, an inlet portion provided at one end of the permeation passage into which the reinforcing fiber enters, and a nozzle portion provided at the other end side of the permeation passage and through which the reinforcing fiber permeated by the base material comes out. An apparatus for manufacturing a composite wire.
空部に内嵌し中空部内の母地を加圧して押し出す押出部Extrusion part that fits in the hollow part and presses out the base in the hollow part
と、中空部に隣接し中央部が括れた楕円形の断面をし、And an oval cross section with a central part contiguous to the hollow part,
中空部から加圧して押し出された母地を強化繊維に加圧Press the base material extruded by pressing from the hollow part to the reinforcing fiber
浸透させる浸透通路と、前記括れた浸透通路の両側と前The permeation passage to be permeated, and both sides and front of the confined permeation passage
記中空部とを連通する連通路と、浸透通路の一端側に設A communication passage communicating with the hollow portion and one end of the permeation passage are provided.
けられた強化繊維が入る入口部と、浸透通路の他端側にAt the entrance where the reinforced fiber enters and the other end of the penetration passage
設けられ母地が浸透した強化繊維が出るノズル部とからFrom the nozzle part where the reinforcing fiber that was provided and the mother land permeated out
構成されていることを特徴とする複合線材の製造装置。An apparatus for manufacturing a composite wire, comprising:
部が広く両端部が狭く形成され、ノズル部に、不活性ガThe nozzle is wide and the ends are narrow.
スの通路が形成された冷却部が設けられ、強化繊維が炭The cooling section is provided with a water passage, and the reinforcing fibers are
素繊維で、母地が金属であることを特徴とする請求項１The raw fiber is made of a metal, and the base is made of metal.
又は２記載の複合線材の製造装置。Or the manufacturing apparatus of the composite wire according to 2.
なる複合線材を積層状に積み重ねて加圧成型し、隣接すComposite wire rods that are stacked in
る複合線材間に空隙を無くし、板状に形成したことを特The gap between the composite wire rods is eliminated, and
徴とする複合線材を用いた板材。A plate made of composite wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3011348A JP2644093B2 (en) | 1991-02-01 | 1991-02-01 | Composite wire manufacturing equipment and plate using composite wire |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3011348A JP2644093B2 (en) | 1991-02-01 | 1991-02-01 | Composite wire manufacturing equipment and plate using composite wire |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH04253560A JPH04253560A (en) | 1992-09-09 |
| JP2644093B2 true JP2644093B2 (en) | 1997-08-25 |
Family
ID=11775536
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3011348A Expired - Lifetime JP2644093B2 (en) | 1991-02-01 | 1991-02-01 | Composite wire manufacturing equipment and plate using composite wire |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2644093B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ATE431848T1 (en) | 1999-03-05 | 2009-06-15 | Mitsubishi Rayon Co | MICROARRAY WITH A BIOLOGICAL SUBSTANCE |
| CN104339667B (en) * | 2013-07-23 | 2018-06-19 | 科思创聚合物（中国）有限公司 | Fiber impregnation system and the technique using system manufacture fibre reinforced composites |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5882242U (en) * | 1981-11-28 | 1983-06-03 | 日立化成工業株式会社 | reinforced laminate |
| JPS5995133A (en) * | 1982-11-22 | 1984-06-01 | 日本発条株式会社 | Fiber reinforced plastic board |
| JPS63132036A (en) * | 1986-11-22 | 1988-06-04 | Nippon Steel Corp | Manufacture of fiber reinforced composite material |
-
1991
- 1991-02-01 JP JP3011348A patent/JP2644093B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH04253560A (en) | 1992-09-09 |
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