JPH0249219B2 - - Google Patents
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- Publication number
- JPH0249219B2 JPH0249219B2 JP57120354A JP12035482A JPH0249219B2 JP H0249219 B2 JPH0249219 B2 JP H0249219B2 JP 57120354 A JP57120354 A JP 57120354A JP 12035482 A JP12035482 A JP 12035482A JP H0249219 B2 JPH0249219 B2 JP H0249219B2
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- Prior art keywords
- glass
- glass fabric
- tex
- warp
- weft
- 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.)
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Classifications
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K1/00—Printed circuits
- H05K1/02—Details
- H05K1/03—Use of materials for the substrate
- H05K1/0313—Organic insulating material
- H05K1/0353—Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement
- H05K1/0366—Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement reinforced, e.g. by fibres, fabrics
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- Laminated Bodies (AREA)
Description
本発明は、熱硬化性樹脂を結合剤として複数の
ガラス織物を積層形成してなる積層板に関し、さ
らに詳しくは、寸法安定性、機械的強度、電気特
性、耐熱性および耐薬品性のみならず特に冷間打
抜加工性に優れた、ガラス織物を補強用基材とす
る積層板に関する。
従来、極めて高品質が要求される電子機器、電
気通信機等に利用される電気絶縁板または印刷回
路用銅張積層板の補強用基材としては、主として
ガラス織物が用いられている。ガラス織物を基材
とする積層板は、この分野において最も要求され
る寸法安定性、機械的強度、電気特性、耐熱性、
耐薬品性等の特性において非常に優れているから
である。しかしながら、ガラス織物を基材とする
積層板は冷間打抜加工が困難であり、ドリル加工
等の機械加工性に極めて劣るという欠点がある。
一方、基材としてガラス織物、ガラスペーパ
ー、ガラスストランドマツト、ガラス繊維等を使
用した積層板も広く知られている。これらの基材
は、ガラス織物基材と比較して面方向の補強効果
が弱いため、積層板の機械加工法、特に冷間打抜
加工性に優れているものの、その反面、最優先さ
れるべき寸法安定性、機械的強度、電気特性、耐
薬品性等の特性はガラス織物基材のものと比べて
かなり劣つている。さらに、機械的強度その他の
いくつかの特性の向上を目的として無機充填材含
有ガラス不織巾、ガラスペーパー等を基材とした
積層板が提案されている。この積層板は、冷間打
抜加工性に優るとされ、機械的強度、電気特性に
もわずかな向上が認められるものの、寸法安定
性、耐熱性等の特性は依然満足できるものではな
い。
また、積層板両表面層の基材にはガラス織物を
使用し、中間層の基材には無機充填材含有ガラス
不織巾、ガラスペーパー等を使用したいわゆるコ
ンポジツトタイプの積層板が考案された。これら
の積層板は冷間打抜加工性が優れており、機械的
強度、電気特性、耐熱性の特性においてもかなり
の性能を有しているものの、冷間打抜性以外の諸
特性はガラス織物を基材とする積層板には到底及
ばないのが現状である。特に、これらの積層板は
平面方向だけでなくZ軸方向の寸法安定性が悪い
ため、そりねじりを生じたり、スルーホールメツ
キの切断が生じる等の致命的な欠陥がある。さら
に、耐熱性、耐薬品性等も満足できるとは言い難
い。
本発明者らは、従来のガラス織物のみを基材と
して用いた積層板と比較して殆んど遜色のない寸
法安定性、機械的強度、電気特性、耐熱性、耐薬
品性などの特性を保有し、且つ非常に優れた冷間
打抜加工性を有するガラス織物補強積層板を開発
すべく鋭意研究した結果、基材のガラス織物を構
成している糸の強度を抑制することにより上記の
目的が達せられることを見い出した。このガラス
織物補強積層板は、「熱硬化性樹脂を結合剤とし
て複数のガラス織物を積層成形してなる積層板に
おいて、ガラス織物を構成するガラス糸の引張強
度が経糸および緯糸とも10gf/tex未満で且つ
両者の和が15gf/tex未満であることを特徴と
する」ものであつて、出願人は本特許出願と同日
付で特許出願を行つた。
上述の特許出願に係る積層板は、冷間打抜加工
性に優るとともに、寸法安定性、耐熱性その他の
特性において満足すべき水準を維持している。し
かしながら、機械的強度、特に曲げ強度において
通常のG−10およびFR−4(いずれも米国
HEMA規格)と比較して若干劣つている。本願
発明の目的は、曲げ強度を始めとする機械的強度
においても通常のG−10およびFR−4と何ら遜
色のない、冷間打抜加工性に優れたガラス織物入
に積層板を提供するにある。
本発明に係るガラス織物入り積層板は、熱硬化
性樹脂を結合剤として複数のガラス織物を積層成
形してなる積層板において、
A ガラス織物を構成するガラス糸の引張強度が
経糸および緯糸とも10gf/tex以上であるガ
ラス織物を少くとも1枚と、
B ガラス織物を構成するガラス糸の引張強度が
経糸および緯糸とも10gf/tex未満で且つ両
者の和が15gf/tex未満であるガラス織物を
少くとも1枚重ねてなることを特徴とする。
本発明において「ガラス織物を構成するガラス
糸の引張強度」とは、熱硬化性樹脂を結合剤とし
て積層成形する直前においてガラス織物を構成し
ているガラス糸の引張強度を指す。すなわち、一
般に、ガラス織物は経糸と緯糸とが交織されてな
るものであるが、ガラス織物は原糸の紡糸時およ
び経糸整経時に収束剤として用いたバインダー
(糊剤)が付着しているため、通常製織後ヒート
クリーニングや洗浄などの方法で脱糊する。さら
に、脱糊したガラス織物は、通常熱硬化性樹脂と
の結合を強化するためカツプリング剤(例えば、
エポキシ樹脂との結合を強化するためにはシラン
化合物などのカツプリング剤が用いられる)で表
面処理された後に、積層成形される。本発明にお
けるガラス糸の引張強度とは、このような標準的
予備処理を行う場合には、そのような処理を経た
後積層成形される直前のガラス織物を構成してい
るガラス糸の引張強度を指す。
一般に、通常のガラス織物を構成しているガラ
ス糸の引張強度は脱糊処理後において経糸および
緯糸ともに10〜14gf/tex程度であり、さらに、
カツプリング剤による表面処理後、即ち、積層成
形に供用する直前においては16〜20gf/tex程
度である。
本発明の積層板の基材であるガラス織物のうち
少なくとも一枚は、それを構成するガラス糸の引
張強度が、熱硬化性樹脂を結合剤として積層成形
に供給する直前において経糸および緯糸とともに
10gf/tex未満であり且つ両者の和が15gf/
tex未満であつて、従来のガラス織物基材と比較
するとかなり低い。このように本発明のガラス織
物基材の少なくとも1層の糸の引張強度が従来の
ガラス織物基材の糸と比較してかなり低いにもか
かわらず、本発明のガラス織物基材積層板が従来
のガラス織物基材積層板と比較して遜色のない寸
法安定性、機械的強度、電気特性、耐熱性、耐薬
品性などの特性を有すること、および、従来のガ
ラス織物基材積層板と比較して遥かに優れた冷間
打抜加工性を示すことは驚くべきことである。
本発明で結合剤として用いる熱硬化性樹脂とし
ては、従来ガラス織物を基材とする積層板の製造
に常用されるエポキシ樹脂、ポリイミド樹脂、フ
エノール樹脂、ポリエステル樹脂、シリコン樹
脂、ポリウレタン樹脂、ポリビニルブチラール樹
脂等が使用できるが、もとよりこれらのもののみ
に限定されるものではない。
また、添加剤として無機充填剤その他常用され
る添加剤を熱硬化性樹脂にブレンドすることがで
きる。
本発明で基材として用いるガラス織物に使用さ
れる糸は、ガラス長繊維であれば単糸径、収束本
数等に制限はない。また、ガラスの組成も格別の
制限はないが、一般的に電気絶縁板または印刷回
路基板用のガラスには、アルカリ成分の少いEガ
ラスや誘電率の低いDガラスが有利に用いられ
る。ガラス織物は、通常経糸と緯糸が交織されて
なり、織組織には平織り、綾織り、朱子織り等が
あるが、本発明に用いられるガラス織物の組織は
特に限定されない。
ガラス織物には原糸紡糸時および経糸整経時に
収束剤として用いたデンプン、ポリビニルアルコ
ール等を主成分とするバインダー(糊剤)が付着
しているが、通常製織後にヒートクリーニングや
洗浄などの方法で脱糊する。さらに、脱糊した後
に、シラン化合物のようなカツプリング剤で表面
処理されて積層板用基材となる。カツプリング剤
は、ガラスと樹脂結合剤との架橋効果を発揮し、
両者間の結合力を高める。適当なカツプリング剤
は使用する樹脂結合剤にあうように選択される。
例えば、エポキシ樹脂結合剤に対し適合するカツ
プリング剤ははシラン化合物の中から選ぶことが
できる。
本発明のガラス織物基材積層板を構成する基材
層のうち少なくとも一層のガラス糸は前述のよう
に引張強度が非常に低いことを特徴としており、
その引張強度はJIS・R・3413−3.2(3)に規定され
たガラス系の引張強さに比較し大巾に低い。
一般的に、ガラス糸の引張強度は糊剤付着量、
カツプリング剤付着量、ヒートクリーニングの温
度が時間に依存して変動するものの、本発明に使
用されるような低強度のガラス織物を得るために
は特別の低強度化処理を必要とする。低強度化処
理としては、400℃以上の高温度で比較的長時間
ヒートクリーニングを行う方法、酸またはアルカ
リ液中に浸漬する方法なども可能であるが、前者
の方法は特別な炉で長時間処理するため工業的に
はあまり有利でなく、また、後者の方法は最終的
に得られるガラス織物基材積層板の電気的性質な
どに悪影響を及ぼすという問題がある。特に好ま
しい低強度化処理方法は、テトラアルコキシシラ
ン、トリアルコキシシラン、ジアルコキシシラン
のような特定のシラン化合物の稀薄溶液をガラス
織物に適用し、微量の該シラン化合物が付着した
状態でガラス織物を加熱する方法である。このよ
うな方法で非常に効果的且つ工業的有利に低強度
化を達成することができる。
上述の特定のシラン化合物の適用は糊剤を除去
するためのヒートクリーニングに先立つて行うこ
とが望ましい。この適用はシラン化合物の稀薄溶
液中にガラス織物を浸漬するか、稀薄溶液をガラ
ス織物に散布すればよい。上述のようなシラン化
合物の適用量とヒートクリーニング加熱温度とは
ガラス糸の引張強度の低下量と正の相関を有し、
適用量とヒートクリーニング加熱温度を変えるこ
とによつてガラス糸の引張強度を任意に制御する
ことができる。
なお、上述のような低強度ガラス織物を構成す
るガラス糸の引張強度の下限は、得られる積層板
の寸法安定性、機械的強度その他の特性および積
層成形工程での適合性が満足できるものである限
り格別限定されないが、経糸の引張強度が約5g
f/tex以上であることが望ましい。
本発明に係る積層板は、上述のような低強度ガ
ラス織物の少くとも1枚と、ガラス織物を構成す
るガラス糸の引張強度が経糸および緯糸とも10g
f/tex以上である従来と同様なガラス織物(以
下、「高強度ガラス織物」という。)の少くとも1
枚とを積層成形してなる。積層板の基材を構成す
るガラス織物の積層数は格別限定されるものでは
なく、積層板の用途に依存して変わる。一般に
は、少くとも3枚のガラス織物を積層して構成
し、そして、高強度ガラス織物が少くとも一方の
表面層側に配置されている積層構造が好ましい。
特に、高強度ガラス織物が両表面側にそれぞれ一
枚宛配置されている積層構造は最良である。
積層板の回転は常法に従つて行うことができ
る。即ち、一般的にはガラス織物に樹脂を含浸さ
せて半硬化したプリプレグを重ね合わせ、圧縮加
熱成形を行う。また、注型による方法や、低圧加
熱の方法も可能である。印刷回路基板用には銅箔
等の金属膜を積層板の一面または両面に貼着形成
するが、アデイテイブ法のごとく、回路形成材を
成形後に付着する方法も可能である。
以下、ガラスを実施例および比較例について具
体的に説明する。実施例中「部」は重量部を意味
する。
実施例 1
経糸及び緯糸がECG75 1/0(67.5tex)で構
成され、密度が経糸44本/25mm緯糸32本25mmから
なるガラス織物を製織した。
本ガラス織物の引張強度は経糸が110Kgf/25
mm、緯糸が80Kgf/25mmであつた。このガラス織
物を次の2通りの方法で加工した。
即ち、
(A) 400℃の加熱炉中で20時間ヒートクリーニン
グした。
(B) (A)の方法で得られたガラス織物をテトラエト
キシシラン5c.c./に水溶液に浸漬し、絞液後
乾燥し、再度400℃の加熱炉で20時間ヒートク
リーニングした。
(A),(B)で得られたガラス織物を次にエポキシシ
ラン5g/の水溶液に浸漬し乾燥した。(A)のエ
ポキシシラン処理織物の引張強度は経糸50Kgf/
25mm、緯糸40Kgf/25mmで、tex当りでは経糸
16.9gf/tex、緯糸18.5gf/texであり、(B)の
それは経糸22.3Kgf/25mm、緯糸15.1Kgf/25mm
で、tex当りでは経糸7.5gf/tex緯糸7.0gf/
texである。
これらのガラス織物に下記配合のエポキシ樹脂
ワニスを含浸させ、160℃で加熱乾燥して、プリ
プレグを作成した。次に、(A)の織物からなるプリ
プレグを上下表層に合計2枚、(B)の織物からなる
プリプレグを中間に6枚挾んで重ねあわせ、更に
その両表面に35μの銅箔を重ねて175℃、40Kg/
cm2で圧縮成形して、1.6mm厚の銅張積層板を得た。
樹脂ワニス組成 AER−711(旭化成製エポキシ
樹脂) 100部
ジシアンジアミド 3部
ベンジルジメチルアミン 0.2部
ジメチルホルムアミド 20部
メチルエチルケトン 100部
得られた積層板の諸性質は表1の如くであり、
パンチング性、ハンダ耐熱性、耐薬品性、厚み方
向線膨張率などの非常に良好であり且つ曲げ強度
も一般のガラス織物補強積層板と同等レベルにあ
る。
実施例 2
実施例1と同じガラス織物を更に別の2通りの
方法で加工した。
即ち
(C) 625℃の高温炉中に6秒間曝して付着糊剤を
部分的に焼燃し、これを更に400℃の加熱炉中
で20時間ヒートクリーニングした後、5g/
のエポキシシラン水溶液に浸漬し、乾燥した。
(D) 625℃の高温炉中に6秒間曝して付着糊剤を
部分的に燃焼したガラス織物をつくり、これを
テトラエトキシシラン10g/の水溶液に浸漬
し、絞液後乾燥した。次に、これを400℃の加
熱炉中で20時間ヒートクリーニングした後、5
g/のエポキシシラン水溶液に浸漬して乾燥
した。
(C)の方法で得られたガラス織物の引張強度は経
糸48Kgf/25mm、緯糸38Kgf/25mmであり、tex
当りでは経糸16.1gf/tex、緯糸17.6gf/tex
であり、(D)の方法で得られたガラス織物の引張強
度は経糸29.5Kgf/25mm、緯糸9.7Kgf/25mmで、
tex当りでは経糸9.7gf/tex緯糸5.0gf/tex
であつた。
次に、(C)の織物からなるプリプレグを上下両表
面に各1枚、(D)の織物からなるプリプレグを中間
に6枚はさんで重ねあわせ実施例1と同様にして
銅張積層板を得た。
実施例 3
経糸及び緯糸がECG37−1/0(135tex)で構
成され、密度が経緯とも25本/25mmからなるガラ
ス織物を製織した。本ガラスの織物の引張強度は
経糸が125Kgf/25mm、緯糸が110Kgf/25mmであ
つた。これを比較的2の(D)と同一の方法で加工し
たところ引張強度は経糸30.5Kgf/25mm、緯糸
17.8Kgf/25mmで、tex当りでは経糸が9.0gf/
tex、緯糸が5.3gf/texであつた。
次に実施例2の(C)で得られたガラス織物からな
るプリプレグを上下両表面に各1枚、本例で得ら
れたガラス織物からなるプリプレグを中間に4枚
はさんで重ねあわせ、実施例1と同様にして銅張
積層板を得た。
比較例 1
経糸および緯糸がECG75 1/0(67.5tex)で
構成され、密度が経44本/25mm、緯32本/25mmか
らなるガラス織物を製織した。本ガラス織物の引
張強度は経が110Kgf/25mm、緯が80Kgf/25mm
であつた。次にこの織物を400℃の加熱炉中で20
時間ヒートクリーニングし付着糊剤を燃焼した。
次に、このガラス織物をテトラエトキシシラン5
c.c./の水溶液に浸漬した。絞液し、乾燥した
後、再度このガラス織物を400℃の加熱炉で20時
間ヒートクリーニングし、次にカツプリング剤と
してエポキシシラン5g/の水溶液に浸漬し、
乾燥した。このように処理されたガラス織物の引
張強度は経糸22.3Kgf/25mm、緯糸15.1Kgf/25
mmで、tex当りでは経糸7.5gf/tex緯糸7.0g
f/texであつた。
このガラス織物に実施例1のエポキシ樹脂ワニ
スを含浸させ、160℃にて加熱乾燥させてプリプ
レグを作成した。このプリプレグ8枚と表面に
35μの銅箔を重ねて175℃、40Kg/cm2で圧縮成形
して1.6mm厚の銅張積層板を得た。
比較例 2
比較例1において、最初に400℃の加熱炉中で
20時間ヒートクリーニングしたガラス織物を直ち
にエポキシシラン5g/の水溶液に浸漬し、乾
燥して表面処理されたガラス織物を得た。このガ
ラス織物の引張強度は、経糸50Kgf/25mm、緯糸
40Kgf/25mmで、tex当りでは、経糸16.9gf/
tex、緯糸18.5gf/texであつた。次に実施例1
と同様にして銅張積層板を得た。
比較例 3
目付70g/m2、単繊維径9μの湿式抄紙された
ガラスペーパーに実施例1の樹脂ワニスを含浸、
乾燥してプリプレグを作成した。このプリプレグ
10枚と表面に35μの銅箔を重ねて、175℃、40
Kg/cm2で圧縮成形して1.6mm厚の銅張積層板を得
た。
比較例 4
比較例3のプリプレグを中間層に8枚、上下表
層に比較例2のプリプレグを2枚重ね、表面に
35μの銅箔を重ねて、175℃、40Kg/cm2で圧縮成
形して、1.6mm厚の銅張積層板を得た。
各実施例および比較例で用いたガラス織物およ
び得られた積層板の特性は下記表1のとおりであ
つた。
The present invention relates to a laminate formed by laminating a plurality of glass fabrics using a thermosetting resin as a binder. In particular, the present invention relates to a laminate having glass fabric as a reinforcing base material, which has excellent cold punching workability. Conventionally, glass fabric has been mainly used as a reinforcing base material for electrical insulating boards or copper-clad laminates for printed circuits used in electronic devices, telecommunications equipment, etc. that require extremely high quality. Glass fabric-based laminates have the most required dimensional stability, mechanical strength, electrical properties, heat resistance, and
This is because it has excellent properties such as chemical resistance. However, laminates made of glass fabric as a base material have the disadvantage that cold punching is difficult and machinability such as drilling is extremely poor. On the other hand, laminates using glass fabric, glass paper, glass strand mat, glass fiber, etc. as the base material are also widely known. These substrates have a weak reinforcing effect in the planar direction compared to glass fabric substrates, so although they are superior in laminate machining methods, especially cold punching, on the other hand, they are given top priority. Properties such as dimensional stability, mechanical strength, electrical properties, and chemical resistance are considerably inferior to those of glass fabric substrates. Furthermore, laminates using glass non-woven cloths containing inorganic fillers, glass paper, etc. as base materials have been proposed for the purpose of improving mechanical strength and other properties. Although this laminate is said to have excellent cold punching properties, and slight improvements in mechanical strength and electrical properties are observed, properties such as dimensional stability and heat resistance are still unsatisfactory. In addition, so-called composite-type laminates have been devised in which glass fabric is used as the base material for both surface layers of the laminate, and non-woven glass cloth containing inorganic fillers, glass paper, etc. are used as the base material for the intermediate layer. Ta. Although these laminates have excellent cold punching properties and have considerable performance in terms of mechanical strength, electrical properties, and heat resistance, their properties other than cold punching properties are inferior to that of glass. At present, it is nowhere near as good as laminates based on textiles. In particular, these laminates have poor dimensional stability not only in the planar direction but also in the Z-axis direction, resulting in fatal defects such as warpage, twisting, and breakage of through-hole plating. Furthermore, it is difficult to say that heat resistance, chemical resistance, etc. are also satisfactory. The present inventors have developed properties such as dimensional stability, mechanical strength, electrical properties, heat resistance, and chemical resistance that are almost comparable to conventional laminates using only glass fabric as a base material. As a result of intensive research to develop a glass fabric-reinforced laminate with excellent cold punching properties, we succeeded in achieving the above-mentioned properties by suppressing the strength of the threads that make up the base glass fabric. I have found that my purpose can be achieved. This glass fabric reinforced laminate is a laminate made by laminating and molding a plurality of glass fabrics using a thermosetting resin as a binder, and the tensile strength of the glass threads constituting the glass fabric is less than 10 gf/tex for both warp and weft. and the sum of both is less than 15 gf/tex, and the applicant filed the patent application on the same date as the present patent application. The laminate according to the above-mentioned patent application has excellent cold punching workability and maintains satisfactory levels of dimensional stability, heat resistance, and other properties. However, in terms of mechanical strength, especially bending strength, G-10 and FR-4 (both US
Slightly inferior to the HEMA standard). The purpose of the present invention is to provide a laminated sheet containing glass fabric that is comparable in mechanical strength including bending strength to ordinary G-10 and FR-4 and has excellent cold punching workability. It is in. The glass fabric-containing laminate according to the present invention is a laminate formed by laminating and molding a plurality of glass fabrics using a thermosetting resin as a binder, and A. The tensile strength of the glass threads constituting the glass fabric is 10 gf for both warp and weft. B. At least one glass fabric whose tensile strength is less than 10 gf/tex for both the warp and weft, and the sum of both is less than 15 gf/tex. Both are characterized by being made of one layer. In the present invention, "the tensile strength of the glass threads constituting the glass fabric" refers to the tensile strength of the glass threads constituting the glass fabric immediately before lamination molding using a thermosetting resin as a binder. In other words, in general, glass fabrics are made by interweaving warp and weft yarns, but glass fabrics have a binder (sizing agent) attached to them that is used as a binding agent during spinning of raw yarns and warping of warp yarns. After weaving, the size is usually removed by heat cleaning or washing. In addition, desized glass fabrics are typically treated with coupling agents (e.g.,
After the surface is treated with a coupling agent such as a silane compound (a coupling agent such as a silane compound is used to strengthen the bond with the epoxy resin), it is laminated and molded. In the present invention, the tensile strength of the glass threads refers to the tensile strength of the glass threads constituting the glass fabric immediately before being laminated and formed after such standard pretreatment. Point. Generally, the tensile strength of glass threads constituting ordinary glass fabrics is about 10 to 14 gf/tex for both warp and weft after desizing treatment, and further,
After surface treatment with a coupling agent, that is, immediately before use for lamination molding, it is about 16 to 20 gf/tex. At least one of the glass fabrics that is the base material of the laminate of the present invention is such that the tensile strength of the glass threads constituting it is lower than that of the warp and weft immediately before being supplied to the laminate molding using a thermosetting resin as a binder.
less than 10gf/tex and the sum of both is 15gf/tex
tex, which is considerably lower than that of conventional glass fabric substrates. Although the tensile strength of the yarns in at least one layer of the glass fabric substrate of the present invention is considerably lower than that of the yarns of the conventional glass fabric substrate, the glass fabric substrate laminate of the present invention is It has properties such as dimensional stability, mechanical strength, electrical properties, heat resistance, and chemical resistance that are comparable to those of conventional glass fabric-based laminates, and compared to conventional glass fabric-based laminates. It is surprising that this material exhibits far superior cold punching workability. Thermosetting resins used as binders in the present invention include epoxy resins, polyimide resins, phenolic resins, polyester resins, silicone resins, polyurethane resins, and polyvinyl butyral, which are conventionally used in the production of laminates based on glass fabrics. Although resins and the like can be used, the material is not limited to these materials. Additionally, inorganic fillers and other commonly used additives can be blended with the thermosetting resin. As long as the yarn used in the glass fabric used as the base material in the present invention is a long glass fiber, there are no restrictions on the single yarn diameter, number of converged yarns, etc. Furthermore, there are no particular restrictions on the composition of the glass, but E glass with a low alkali content and D glass with a low dielectric constant are generally advantageously used as glasses for electrical insulating boards or printed circuit boards. Glass fabrics are usually made of warp and weft interwoven, and weave structures include plain weave, twill weave, satin weave, etc., but the structure of the glass fabric used in the present invention is not particularly limited. Glass fabrics have a binder (sizing agent) mainly composed of starch, polyvinyl alcohol, etc. used as a binding agent during yarn spinning and warping, but they are usually processed by heat cleaning, washing, etc. after weaving. Deglue with. Furthermore, after de-sizing, the surface is treated with a coupling agent such as a silane compound to form a base material for a laminate. The coupling agent exerts a crosslinking effect between the glass and the resin binder,
Increase the bond between the two. A suitable coupling agent is selected to match the resin binder used.
For example, compatible coupling agents for epoxy resin binders can be selected from among silane compounds. As mentioned above, the glass threads in at least one layer of the base material layers constituting the glass fabric base material laminate of the present invention are characterized by extremely low tensile strength,
Its tensile strength is much lower than that of glass as defined in JIS R 3413-3.2(3). Generally, the tensile strength of glass thread is determined by the amount of adhesive applied,
Although the amount of coupling agent deposited and the temperature of heat cleaning vary depending on time, a special strength-lowering treatment is required to obtain a low-strength glass fabric as used in the present invention. Other methods of reducing strength include heat cleaning at a high temperature of 400°C or higher for a relatively long period of time, or immersion in an acid or alkali solution, but the former method requires a long period of time in a special furnace. The latter method is not very advantageous from an industrial perspective because of its processing, and the latter method has the problem of adversely affecting the electrical properties of the glass fabric base laminate finally obtained. A particularly preferred strength-lowering treatment method is to apply a dilute solution of a specific silane compound such as tetraalkoxysilane, trialkoxysilane, or dialkoxysilane to the glass fabric, and then remove the glass fabric with a trace amount of the silane compound attached. This is a heating method. By such a method, it is possible to reduce the strength very effectively and industrially. It is desirable that the specific silane compound described above be applied prior to heat cleaning to remove the sizing agent. This application can be accomplished by dipping the glass fabric in a dilute solution of the silane compound or by spraying the glass fabric with a dilute solution. The amount of the silane compound applied and the heat cleaning heating temperature as described above have a positive correlation with the amount of decrease in the tensile strength of the glass thread.
By changing the application amount and heat cleaning heating temperature, the tensile strength of the glass thread can be arbitrarily controlled. Note that the lower limit of the tensile strength of the glass threads constituting the low-strength glass fabric as described above is such that the dimensional stability, mechanical strength, and other properties of the resulting laminate and compatibility in the laminate molding process are satisfied. There is no particular limitation as long as the tensile strength of the warp is approximately 5g.
It is desirable that it is f/tex or more. The laminate according to the present invention includes at least one sheet of the above-mentioned low-strength glass fabric, and the tensile strength of the glass threads constituting the glass fabric is 10 g for both warp and weft.
At least one of the conventional glass fabrics (hereinafter referred to as "high-strength glass fabrics") having a f/tex or higher
It is made by laminating and molding the sheets. The number of laminated glass fabrics constituting the base material of the laminate is not particularly limited, and varies depending on the use of the laminate. Generally, a laminated structure in which at least three glass fabrics are laminated and a high-strength glass fabric is disposed on at least one surface layer side is preferred.
In particular, a laminated structure in which one high-strength glass fabric is placed on each surface is best. Rotation of the laminate can be carried out according to conventional methods. That is, generally, semi-cured prepregs made by impregnating glass fabric with a resin are stacked on top of each other, and compression and heating molding is performed. Further, a casting method and a low pressure heating method are also possible. For printed circuit boards, a metal film such as copper foil is attached to one or both sides of the laminate, but a method such as an additive method in which the circuit forming material is attached after molding is also possible. Examples and comparative examples of glasses will be specifically described below. In the examples, "parts" mean parts by weight. Example 1 A glass fabric was woven in which the warp and weft were made of ECG75 1/0 (67.5 tex) and the density was 44 warp/25 mm and 32 weft 25 mm. The tensile strength of this glass fabric is 110Kgf/25 for the warp.
mm, and the weft was 80Kgf/25mm. This glass fabric was processed using the following two methods. That is, (A) Heat cleaning was performed in a heating furnace at 400° C. for 20 hours. (B) The glass fabric obtained by the method of (A) was immersed in an aqueous solution of 5 c.c. of tetraethoxysilane, squeezed, dried, and heat-cleaned again in a heating furnace at 400° C. for 20 hours. The glass fabrics obtained in (A) and (B) were then immersed in an aqueous solution containing 5 g of epoxysilane and dried. The tensile strength of the epoxy silane treated fabric (A) is 50Kgf/warp
25mm, weft 40Kgf/25mm, warp per tex
16.9gf/tex, weft 18.5gf/tex, and that of (B) is warp 22.3Kgf/25mm, weft 15.1Kgf/25mm
So, per tex, warp 7.5gf/tex weft 7.0gf/
It is tex. These glass fabrics were impregnated with an epoxy resin varnish having the following composition, and heated and dried at 160°C to prepare prepregs. Next, a total of two prepregs made of the woven fabric of (A) are placed on top and bottom surfaces, and six prepregs made of the woven fabric of (B) are sandwiched in the middle. °C, 40Kg/
Compression molding was performed to obtain a copper-clad laminate with a thickness of 1.6 mm. Resin varnish composition AER-711 (epoxy resin manufactured by Asahi Kasei) 100 parts dicyandiamide 3 parts benzyldimethylamine 0.2 parts dimethylformamide 20 parts methyl ethyl ketone 100 parts The properties of the obtained laminate are as shown in Table 1,
It has very good punching properties, solder heat resistance, chemical resistance, coefficient of linear expansion in the thickness direction, etc., and its bending strength is on the same level as general glass fabric reinforced laminates. Example 2 The same glass fabric as in Example 1 was processed in two additional ways. That is, (C) the adhering adhesive was partially burnt out by exposing it to a high-temperature furnace at 625°C for 6 seconds, and then heat-cleaned it in a heating furnace at 400°C for 20 hours, and then 5 g/
It was immersed in an aqueous epoxy silane solution and dried. (D) A glass fabric was prepared by exposing it to a high-temperature oven at 625°C for 6 seconds to partially burn out the adhering adhesive, and immersed it in an aqueous solution of 10 g of tetraethoxysilane, squeezed the liquid, and dried it. Next, after heat cleaning this in a heating furnace at 400℃ for 20 hours,
It was immersed in an aqueous solution of epoxy silane of 100 g/g and dried. The tensile strength of the glass fabric obtained by method (C) is 48Kgf/25mm for the warp and 38Kgf/25mm for the weft.
At hit, warp 16.1gf/tex, weft 17.6gf/tex
The tensile strength of the glass fabric obtained by method (D) is 29.5 Kgf/25 mm for the warp and 9.7 Kgf/25 mm for the weft.
Warp 9.7gf/tex Weft 5.0gf/tex
It was hot. Next, one prepreg made of the woven fabric of (C) was placed on both the upper and lower surfaces, and six prepregs made of the woven fabric of (D) were sandwiched in the middle to form a copper-clad laminate in the same manner as in Example 1. Obtained. Example 3 A glass fabric was woven in which the warp and weft were made of ECG37-1/0 (135 tex) and the density was 25 threads/25 mm in both warp and weft. The tensile strength of the glass fabric was 125 Kgf/25 mm for the warp and 110 Kgf/25 mm for the weft. When this was processed using the same method as 2 (D), the tensile strength was 30.5Kgf/25mm for the warp and 30.5Kgf/25mm for the weft.
17.8Kgf/25mm, warp is 9.0gf/tex
tex and weft were 5.3gf/tex. Next, one prepreg made of the glass fabric obtained in (C) of Example 2 was stacked on each of the upper and lower surfaces, and four prepregs made of the glass fabric obtained in this example were sandwiched in the middle. A copper-clad laminate was obtained in the same manner as in Example 1. Comparative Example 1 A glass fabric was woven whose warp and weft were made of ECG75 1/0 (67.5 tex) and whose density was 44 warps/25 mm and weft 32 threads/25 mm. The tensile strength of this glass fabric is 110Kgf/25mm for warp and 80Kgf/25mm for weft.
It was hot. Next, this fabric was placed in a heating oven at 400℃ for 20 minutes.
Heat cleaning was performed for a period of time to burn off the adhering adhesive.
Next, this glass fabric was coated with tetraethoxysilane 5
It was immersed in an aqueous solution of cc/. After squeezing and drying, this glass fabric was heat-cleaned again in a heating furnace at 400°C for 20 hours, and then immersed in an aqueous solution of 5 g of epoxy silane as a coupling agent.
Dry. The tensile strength of the glass fabric treated in this way is 22.3Kgf/25mm for the warp and 15.1Kgf/25mm for the weft.
mm, warp 7.5gf/tex weft 7.0g per tex
It was f/tex. This glass fabric was impregnated with the epoxy resin varnish of Example 1 and dried by heating at 160°C to produce a prepreg. 8 sheets of prepreg and the surface
A 1.6 mm thick copper clad laminate was obtained by stacking 35 μm copper foil and compression molding at 175° C. and 40 Kg/cm 2 . Comparative Example 2 In Comparative Example 1, the sample was first heated in a heating furnace at 400°C.
The glass fabric heat-cleaned for 20 hours was immediately immersed in an aqueous solution containing 5 g of epoxy silane and dried to obtain a surface-treated glass fabric. The tensile strength of this glass fabric is 50Kgf/25mm for warp and 25mm for weft.
40Kgf/25mm, warp 16.9gf/tex
The weft was 18.5 gf/tex. Next, Example 1
A copper-clad laminate was obtained in the same manner as above. Comparative Example 3 Wet-made glass paper with a basis weight of 70 g/m 2 and a single fiber diameter of 9 μ was impregnated with the resin varnish of Example 1.
It was dried to create a prepreg. This prepreg
Layer 10 sheets and 35μ copper foil on the surface and heat at 175℃ for 40 minutes.
A copper-clad laminate with a thickness of 1.6 mm was obtained by compression molding at Kg/cm 2 . Comparative Example 4 Eight sheets of prepreg from Comparative Example 3 were stacked on the middle layer, two sheets of prepreg from Comparative Example 2 were stacked on the upper and lower surface layers, and
A 1.6 mm thick copper clad laminate was obtained by layering 35 μm copper foil and compression molding at 175° C. and 40 Kg/cm 2 . The properties of the glass fabrics and the resulting laminates used in each of the Examples and Comparative Examples are shown in Table 1 below.
【表】
ハンダ耐熱性 4時間煮沸で異常な
同 左 同 左 同左
同左 ふくれ ふくれ発生
(煮沸後の260℃ハンダ浴20秒 し
発生
浸漬テスト)
絶縁抵抗 6.2×1012
4.8×1012 9.1×1011 5.5
× 5.2× 3.9× 4.1×1011
(C−96/20/65+D−2/100)
1012
1012 109
厚み方向線膨張係数 2.6×10−5
2.4×10−5 8.2×10−5 2
×10−5 2.2× 1.2× 10−4
(20℃〜80℃;cm/cm/deg)
10−5 10−4
耐薬品性
(塩化メチレン浸漬後260℃ハ 異常なし
異常なし 異常なし 異常な
し 〃 ふくれ ややふくれ発生
ンダ浴浸漬)
多発
[Table] Solder heat resistance Abnormal after 4 hours of boiling
Same left Same left Same left
Same as left Blisters Blisters occur
(260℃ solder bath for 20 seconds after boiling)
occurrence
immersion test)
Insulation resistance 6.2×10 12
4.8×10 12 9.1×10 11 5.5
× 5.2× 3.9× 4.1×10 11
(C-96/20/65+D-2/100)
10 12
10 12 10 9
Linear expansion coefficient in thickness direction 2.6×10 −5
2.4×10 −5 8.2×10 −5 2
×10 −5 2.2× 1.2× 10 −4
(20℃~80℃;cm/cm/deg)
10 -5 10 -4
chemical resistance
(260℃ after immersion in methylene chloride) No abnormality
No abnormality No abnormality No abnormality 〃 Blistering Slightly blistering (soaked in bath)
frequent occurrence
Claims (1)
物を積層成形してなる積層板において、 A ガラス織物を構成するガラス糸の引張強度が
経糸および緯糸とも10gf/tex以上であるガ
ラス織物を少くとも1枚と、 B ガラス織物を構成するガラス糸の引張強度が
経糸および緯糸とも10gf/tex未満で且つ両
者の和が15gf/tex未満であるガラス織物を
少くとも1枚重ねてなることを特徴とするガラ
ス織物入り積層板。 2 少くとも3枚のガラス織物を重ねてなる積層
板であつて、ガラス糸の引張強度が経糸および緯
糸ともに10gf/tex以上であるガラス織物が少
くとも一方の表面層側に配置されている特許請求
の範囲第1項記載の積層板。 3 ガラス糸の引張強度が経糸および緯糸ともに
10gf/tex以上であるガラス織物が両表面層に
配置されてなる特許請求の範囲第2項記載の積層
板。 4 少なくとも1方の表面に金属膜が形成されて
なる特許請求の範囲第1項から第3項までのいず
れかに記載のガラス織物入り積層板。[Scope of Claims] 1. A laminate formed by laminating and molding a plurality of glass fabrics using a thermosetting resin as a binder, A. The tensile strength of the glass threads constituting the glass fabrics is 10 gf/tex or more for both warp and weft. At least one glass fabric and at least one glass fabric in which the tensile strength of the glass threads constituting the glass fabric are less than 10 gf/tex for both warp and weft, and the sum of both is less than 15 gf/tex. A laminated board containing glass fabric that is characterized by the fact that it becomes 2. A patent for a laminate made by stacking at least three glass fabrics, in which a glass fabric whose tensile strength is 10 gf/tex or more for both warp and weft is arranged on at least one surface layer side. A laminate according to claim 1. 3 The tensile strength of glass threads for both warp and weft
3. The laminate according to claim 2, wherein glass fabric having a density of 10 gf/tex or more is disposed on both surface layers. 4. A glass fabric-containing laminate according to any one of claims 1 to 3, wherein a metal film is formed on at least one surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12035482A JPS5911244A (en) | 1982-07-10 | 1982-07-10 | Laminated board containing glass textile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12035482A JPS5911244A (en) | 1982-07-10 | 1982-07-10 | Laminated board containing glass textile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5911244A JPS5911244A (en) | 1984-01-20 |
| JPH0249219B2 true JPH0249219B2 (en) | 1990-10-29 |
Family
ID=14784139
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12035482A Granted JPS5911244A (en) | 1982-07-10 | 1982-07-10 | Laminated board containing glass textile |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5911244A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0491417U (en) * | 1990-12-22 | 1992-08-10 |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6364740A (en) * | 1986-09-08 | 1988-03-23 | 東芝ケミカル株式会社 | Copper-lined laminated board |
| JP7250149B2 (en) * | 2019-08-26 | 2023-03-31 | 三菱電機株式会社 | Double-sided metal-clad laminates, printed wiring boards, printed wiring devices |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5114967A (en) * | 1974-07-27 | 1976-02-05 | Sumitomo Bakelite Co | |
| JPS533487A (en) * | 1976-06-30 | 1978-01-13 | Matsushita Electric Works Ltd | Laminates |
-
1982
- 1982-07-10 JP JP12035482A patent/JPS5911244A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0491417U (en) * | 1990-12-22 | 1992-08-10 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5911244A (en) | 1984-01-20 |
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