JPH0232840A - Composite reinforced plastic prepared by laminating air-tight reinforcing material - Google Patents

Composite reinforced plastic prepared by laminating air-tight reinforcing material

Info

Publication number
JPH0232840A
JPH0232840A JP18156888A JP18156888A JPH0232840A JP H0232840 A JPH0232840 A JP H0232840A JP 18156888 A JP18156888 A JP 18156888A JP 18156888 A JP18156888 A JP 18156888A JP H0232840 A JPH0232840 A JP H0232840A
Authority
JP
Japan
Prior art keywords
reinforcing material
sheet
plastic
reinforcing
hole diameter
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.)
Pending
Application number
JP18156888A
Other languages
Japanese (ja)
Inventor
Yasuyuki Sugi
杉 康行
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP18156888A priority Critical patent/JPH0232840A/en
Publication of JPH0232840A publication Critical patent/JPH0232840A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To improve such characteristics as toughness, interlaminar peeling and anisotropic shrinkage at higher temp. of a composite reinforced plastic laminate by using an air-tight metal foil or metal or plastic film- or sheet-like flat sheet wherein a number of small holes are perforated in such a way that rate of opening is in a specified range. CONSTITUTION:As a reinforcing material, an air-tight foil or a thin sheet with a thickness of 0.5mm or thinner of aluminum, iron, stainless steel or copper or a plastic film or sheet is used. An ordinary punching process can be used for perforation, but a process using an electron beam or a laser ray is pref. for the metal foil. As the hole diameter, in case of a commercially available metal sheet with a hole diameter of 0.5mm (the rate of opening is 35% or higher), pressurizing is needed for passing a resin soln. and if the hole diameter is too large, the resin side for reinforcement is too emphasized. As the result, a hole diameter of 3.0mm or smaller is suitable. The rate of opening has a positive correlation with the characteristics of a reinforcing material and it is pref. that the rate of opening is set in the range of 1.0-20%. A plastic for reinforcement thereby penetrates the upper and lower sides of reinforcing material and has a three dimensional structure and a tough composite plastic can be obtd.

Description

【発明の詳細な説明】 イ 産業上の利用分野 本発明は車輛、航空機その他構造用材料及び電子機器用
の電磁遮蔽材料・回路基板その他の部材などに用いられ
るテープ状板状の強化プラスチックス分野に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION A. Field of Industrial Application The present invention relates to the field of tape-like and plate-like reinforced plastics used for vehicles, aircraft and other structural materials, electromagnetic shielding materials for electronic devices, circuit boards, and other members. It is related to.

従って射出成型用材料には不適である。Therefore, it is unsuitable as an injection molding material.

p 従来技術 強化プラスチック材料の強化法としてガラス繊維、カー
ボン線維、セラミック材、金属繊維、金属コーテング繊
維などを補強材として各種プラスチックスな含浸して製
作されているが金属代替材料としては靭性(弾性率及び
衝撃強さ)層間剥離(層間破壊靭性)が劣るとされてお
り、繊維系での強化プラスチックスでは、高温(150
℃以上連続使用温度)での異方性収縮に問題を残してい
てコストが割高となっている。
P Conventional technology Reinforced plastic materials are manufactured by impregnating various plastics with glass fiber, carbon fiber, ceramic materials, metal fibers, metal coated fibers, etc. as reinforcing materials. The delamination (interlaminar fracture toughness) is said to be poor, and fiber-based reinforced plastics have a high temperature (150
However, the cost remains high due to the problem of anisotropic shrinkage at temperatures above ℃ (continuous use).

ハ 発明が解決しようとする問題点 複合強化プラスチックス積層板の欠点である靭性・層間
剥離性・高温時異方収縮性などの特性向上を狙ったもの
で軽量・強靭な複合プラスチックスを成形することにあ
る。特に補強材として高価なカーボンファイバー・金属
繊維・セラミック材料などを安価な材料に代替すること
が要望されている@ 二 問題点を解決する為の手段 本発明は綱状補強材をより合理的に追求したものである
C. Problems to be solved by the invention The invention aims to improve properties such as toughness, delamination, and anisotropic shrinkage at high temperatures, which are disadvantages of composite reinforced plastic laminates, and molds lightweight and strong composite plastics. There is a particular thing. In particular, there is a demand for replacing expensive carbon fibers, metal fibers, ceramic materials, etc. with inexpensive materials as reinforcing materials. This is what I pursued.

通常綱状物は通気性・透過性をもたせるので開孔率が3
0%以上のものであるため綱を構成する素材のもつ引張
り強度・伸び率・曲げ弾性率などの特性が大きく変化し
特性によっては50係以上劣化するのが常識とされてい
る。よってこの綱状物の素材の特性値が加暢以下の劣化
に止まる範囲に小孔を搾孔することにより大きな補強効
果を実現したものである。即ち、補強材に、3.9m以
下の小孔を面積当りの開孔率として20係以下になる如
く搾孔することにより強化用プラスチックスが補強材の
上下を貫通して立体構造をもつこととなり、強靭な複合
プラスチックスを得ることが出来る。
Normally, rope-like materials have air permeability and permeability, so the porosity is 3.
It is common knowledge that the properties of the material that makes up the rope, such as tensile strength, elongation, and flexural modulus, change significantly because it is more than 0%, and that some properties deteriorate by a factor of 50 or more. Therefore, a large reinforcing effect is achieved by forming small holes in a range where the characteristic values of the material of this rope-like material do not deteriorate to a level below that of Kano. That is, by punching small holes of 3.9 m or less in the reinforcing material so that the pore area per area is 20 or less, the reinforcing plastic penetrates the upper and lower parts of the reinforcing material and has a three-dimensional structure. As a result, strong composite plastics can be obtained.

ホ 本発明の効果 補強材の小孔を介し強化用プラスチックスで積層内部構
造が綱状又はラグ状を形成する為積層材料それぞれの伸
縮歪の差が小区画に独立した働きとなるのでトータルと
しての伸縮歪度を最小にすることが出来る。又強化用プ
ラスチックスと補強材の接触が恰もピン止めされた状態
となるので被強化プラスチックスのもつ引張強度が加算
されて接着強度が増加する。更に補強材の特性値の劣化
を極力低く押えるため金属材料を補強材とした場合より
金属性能に近い特性が得られる。且つ高価なカーボン・
金属・セラミック材などの繊維を用いる場合に比し本性
では1/10 以上のコストが合理化される。
E. Effects of the present invention Since the inner structure of the laminate is formed into a rope-like or lug-like structure by reinforcing plastics through the small holes of the reinforcing material, the difference in expansion and contraction strain of each laminate material acts independently on the small sections, so the total The expansion and contraction distortion of can be minimized. Furthermore, since the reinforcing plastic and the reinforcing material are in a pinned state, the tensile strength of the reinforced plastic is added to increase the adhesive strength. Furthermore, since the deterioration of the characteristic values of the reinforcing material is kept as low as possible, properties closer to metal performance can be obtained than when a metallic material is used as the reinforcing material. And expensive carbon
Compared to the case of using fibers made of metal or ceramic materials, the cost is essentially 1/10 or more rationalized.

へ 本発明の説明 補強材としては気密なアルミ・鉄・ステンレス鋼・銅な
どの箔又は0.5−以下の薄板状ノモの或いはプラスチ
ックスのフィルム・シート状のものが用いられるが強化
用プラスチックスとの組合せにより、その応)14形態
は可変となる。即ち500℃以上の耐熱性をもつ金属材
料においては強化用プラスチックスとして熱硬化性会熱
可塑性のいずれの樹脂にも適用される。補強材として耐
熱度が金4類より低いプラスチックス類にあっては補強
用プラスチックスの耐熱度に応じ強化用プラスチックス
の拷類を撰択する必要がある。即ち200℃前後の耐熱
性をもつ補強用プラスチックスにあっては常温乃至10
0℃以下にて含浸可能の熱硬化樹脂又は重縮合性樹脂を
用いるなどである。
Description of the present invention As a reinforcing material, an airtight foil of aluminum, iron, stainless steel, copper, etc., a thin plate with a thickness of 0.5 or less, or a plastic film or sheet is used, and reinforcing plastics are used. Depending on the combination with the base, the corresponding form can be changed. That is, for metal materials having heat resistance of 500° C. or higher, any thermosetting or thermoplastic resins can be used as reinforcing plastics. When using plastics as reinforcing materials whose heat resistance is lower than Class 4 metal, it is necessary to select the type of reinforcing plastic depending on the heat resistance of the reinforcing plastic. In other words, for reinforcing plastics that have a heat resistance of around 200°C, the temperature ranges from room temperature to 10°C.
For example, a thermosetting resin or a polycondensable resin that can be impregnated at 0° C. or lower is used.

従つてプラスチックス系補強材としては強化用プラスチ
ックスの浴融a度に対応したポリアミド・イミド、ポリ
イミド、ポリエーテAI ケ) :/ 、ポリフェニレ
ン0オキサイド、ポリフェニレンサルファイド、ポリア
セタール、ポリカーボネートなどの各111脂が、又強
化用プラスチックスとしてはポリオレフィン系スチレン
系を含めた熱可塑性樹脂及び熱硬化性、重縮合性樹脂を
それぞれ適応した組合せが可能となる。
Therefore, as reinforcing materials for plastics, 111 resins such as polyamide/imide, polyimide, polyether AI, polyphenylene 0 oxide, polyphenylene sulfide, polyacetal, and polycarbonate, which correspond to the bath meltability of reinforcing plastics, are used. Furthermore, as the reinforcing plastics, suitable combinations of thermoplastic resins including polyolefin-based styrene-based resins, thermosetting resins, and polycondensation resins can be used.

搾孔法としては通常の打ち抜きき加工法でよいが金属箔
など無圧状態での搾孔を必要とする場合などでは電子線
又はレーザー光線による方法がすぐれている。孔径につ
いてはパンチ法により0.5m径(開孔率35俤以上)
の金属板が市場に出廻っているがこの孔径ともなれば樹
脂液の通過には加圧が必要となり、又孔径が大きくなる
と強化用樹脂面が強調されすぎることになるので孔径3
.0■以下が適当である。開孔率は強化材の特性と正相
関あり概ね特性値の20%低下は開孔率約2096以下
と推定されるのでこの範囲に設定するのが望ましい。
A conventional punching method may be used as the hole punching method, but methods using electron beams or laser beams are superior in cases where hole punching is required under no pressure, such as in metal foils. The hole diameter is 0.5m by the punch method (open area ratio of 35 or more)
Metal plates with a diameter of 3 are on the market, but with this hole diameter, pressure is required for the resin liquid to pass through, and if the hole diameter becomes large, the reinforcing resin surface will be too emphasized, so the hole diameter of 3 is used.
.. A value of 0■ or less is appropriate. The porosity has a positive correlation with the properties of the reinforcing material, and it is estimated that a 20% decrease in the characteristic value is approximately 2096 or less in the porosity, so it is desirable to set it within this range.

実施例(1) 強化用プラスチックスとして市販の金属接着用の2液型
常温硬化のエポキシ樹脂を用いた。強化材として市販の
アルミ板(0,1m )の10cdのものを切り出し3
枚を用意しこれを重ねてその上に1 ’w方眼紙をおき
5.0+m間隔に打点して搾孔位置を定め2■の小孔を
ドリルにて搾孔した。この場合の開孔率は約12.5チ
であった。エポキシ混合物をアルミ箔の片面に塗付し2
枚目のアルミ箔にもエポキシ樹脂を塗り、2枚を重ねた
。3枚目も同様に繰返し1最後に表裏両面にもエポキシ
樹脂を塗り、テフロン・シート上に置き、上部に4.?
フロンシートを重ねて、軽く押え成形し反応を完了せし
め7層からなる厚み0.9mの積層品を得た。
Example (1) A commercially available two-component room-temperature curing epoxy resin for metal bonding was used as the reinforcing plastic. Cut out a 10 cd piece of commercially available aluminum plate (0.1 m) as a reinforcing material 3
Two pieces of paper were prepared, stacked on top of each other, and a 1'w graph paper was placed on top of the paper, dots were dotted at intervals of 5.0+ m to determine the position for drilling, and 2 small holes were drilled using a drill. The porosity in this case was approximately 12.5 inches. Apply the epoxy mixture to one side of the aluminum foil 2
I also coated the second sheet of aluminum foil with epoxy resin and stacked the two sheets together. Repeat the same process for the third sheet. 1. Finally, apply epoxy resin to both the front and back sides, place it on a Teflon sheet, and apply 4. ?
The fluorocarbon sheets were stacked and lightly pressed to complete the reaction and a 7-layer laminate with a thickness of 0.9 m was obtained.

製品の断面はエポキシ樹脂を柱とする立体構造がルーパ
により確認された。搾孔しない比較品を同様手法で作製
し厚み0.75mのものなは2回目に早くもアルミ板と
の剥離がみられたが本性によるものは4回以上剥離しな
かった更にセラミック鋏で試験片を巾5m位いに切断し
たとき対象品の5■巾のものはアルき板が剥離するに対
し本性品では層間剥離がi!!!あら朴グいことによっ
ても確認出来た。
The cross section of the product was confirmed to have a three-dimensional structure with epoxy resin as pillars using a looper. Comparison products without hole punching were made using the same method, and the one with a thickness of 0.75 m showed peeling from the aluminum plate as early as the second time, but the one due to its nature did not peel more than four times.Furthermore, it was tested with ceramic scissors. When a piece is cut to a width of about 5 m, the aluminum plate of the 5-cm-wide product in question peels off, but with the original product, interlayer peeling occurs. ! ! I was able to confirm this by doing some simple things.

実施例(2) 強化用プラスチックスとして熱可塑性ナイロン6(融点
225℃)の微粉末を用いた。
Example (2) Fine powder of thermoplastic nylon 6 (melting point: 225° C.) was used as the reinforcing plastic.

補強材としてアルミ板(0,1wm )を用イ実施例(
1)に従い2枚を用意したがこの場合5■間隔に1.5
 msの孔径で搾孔した。開孔率は約7係であった。テ
フロン・シート上にナイロン6粉末を薄((約1.0 
m )広げアルミ板を置き、その上にナイロン6粉末を
同様に薄く広げ更にアルミ板を重ね最後にナイロン6を
薄く広げテフロン・シートで軽く押えて成形し約200
1の鉄板をおき加熱炉に入れ炉温220℃まで昇温し、
約2分後、加熱をやめ除冷した。5層からなる厚さ約2
.5謹の積層品を得た。
Example using an aluminum plate (0.1wm) as a reinforcing material (
According to 1), two sheets were prepared, but in this case, 1.5 at 5 ■ intervals.
The holes were drilled with a hole diameter of ms. The open area ratio was approximately 7. Spread a thin layer of nylon 6 powder on a Teflon sheet (approximately 1.0
m) Place a spread aluminum plate, spread nylon 6 powder on top of it in the same way, and then layer the aluminum plate again.Finally, spread nylon 6 thinly and press it lightly with a Teflon sheet to form it.
Place the iron plate No. 1 in the heating furnace and raise the furnace temperature to 220℃.
After about 2 minutes, heating was stopped and the mixture was gradually cooled. Approximately 2 thick, consisting of 5 layers
.. A laminate product of 50% was obtained.

製品の断面はナイロン6樹脂を柱とする立体構造がルー
パにより確認されたが若干気泡が存在していた。工業的
には当然脱泡処理を考慮する必要がある。
In the cross section of the product, a three-dimensional structure with nylon 6 resin as pillars was confirmed using a looper, but there were some air bubbles. Industrially, it is naturally necessary to consider defoaming treatment.

実施例(3) 強化用プラスチックスとして実施例(1)の市販エポキ
シ樹脂を用いた。補強材とし″″c25μmc25μm
ポリイミド用い実施例(1)に従い3枚を孔径2.5−
間隔5.0mに搾孔した。開孔率は約15.7%であっ
た。用意したポリイミド・フィルム上にエポキシ樹脂を
塗付し実施例(1)に従い7層の厚さ約0.7mの積層
品を得た。
Example (3) The commercially available epoxy resin of Example (1) was used as the reinforcing plastic. As a reinforcing material ″″c25μmc25μm
According to Example (1) using polyimide, three sheets were made with a pore size of 2.5-
Holes were drilled at intervals of 5.0 m. The open area ratio was about 15.7%. An epoxy resin was applied onto the prepared polyimide film to obtain a 7-layer laminate with a thickness of about 0.7 m according to Example (1).

製品の断面はエポキシ樹脂を柱とする立体構造がルーパ
により確認された。
The cross section of the product was confirmed to have a three-dimensional structure with epoxy resin as pillars using a looper.

Claims (2)

【特許請求の範囲】[Claims] (1)気密性の金属箔又は金属のフィルム・シート状の
平板を補強材料とし、熱硬化性又は熱可塑性樹脂(以下
強化用プラスチックス)で積層板を製作するに当り、補
強材に多数の小孔(3.0mm孔径以下)を開孔率が1
.0〜20%となるよう搾孔することにより強化用プラ
スチックスを介し立体綱目状を構成する強化複合プラス
チックス。
(1) When manufacturing a laminate using thermosetting or thermoplastic resin (hereinafter referred to as reinforcing plastics) using an airtight metal foil or metal film/sheet-like flat plate as the reinforcing material, many The opening rate of small holes (3.0 mm or less) is 1.
.. Reinforced composite plastics that forms a three-dimensional mesh shape through reinforcing plastics by drilling the holes to 0 to 20%.
(2)前項1の記載において補強材としてプラスチック
スを用い、強化用プラスチックスとして熱硬化性樹脂を
用いる組合せで立体綱目状を構成する複合強化プラスチ
ックス。
(2) A composite reinforced plastic that constitutes a three-dimensional mesh shape by using a plastic as a reinforcing material and a thermosetting resin as a reinforcing plastic as described in the preceding item 1.
JP18156888A 1988-07-22 1988-07-22 Composite reinforced plastic prepared by laminating air-tight reinforcing material Pending JPH0232840A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18156888A JPH0232840A (en) 1988-07-22 1988-07-22 Composite reinforced plastic prepared by laminating air-tight reinforcing material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18156888A JPH0232840A (en) 1988-07-22 1988-07-22 Composite reinforced plastic prepared by laminating air-tight reinforcing material

Publications (1)

Publication Number Publication Date
JPH0232840A true JPH0232840A (en) 1990-02-02

Family

ID=16103079

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18156888A Pending JPH0232840A (en) 1988-07-22 1988-07-22 Composite reinforced plastic prepared by laminating air-tight reinforcing material

Country Status (1)

Country Link
JP (1) JPH0232840A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002081201A1 (en) * 2001-04-03 2002-10-17 Meng Chen Decorative metal composite panal

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002081201A1 (en) * 2001-04-03 2002-10-17 Meng Chen Decorative metal composite panal

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