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JPH031427B2 - - Google Patents
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JPH031427B2 - - Google Patents

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Publication number
JPH031427B2
JPH031427B2 JP61131361A JP13136186A JPH031427B2 JP H031427 B2 JPH031427 B2 JP H031427B2 JP 61131361 A JP61131361 A JP 61131361A JP 13136186 A JP13136186 A JP 13136186A JP H031427 B2 JPH031427 B2 JP H031427B2
Authority
JP
Japan
Prior art keywords
weft
interlining
knitted fabric
composite
yarns
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
Application number
JP61131361A
Other languages
Japanese (ja)
Other versions
JPS62289677A (en
Inventor
Noboru Matsui
Zenji Yoshida
Nobuhiro Tanaka
Tatsuro Inoe
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.)
Japan Vilene Co Ltd
Original Assignee
Japan Vilene Co Ltd
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 Japan Vilene Co Ltd filed Critical Japan Vilene Co Ltd
Priority to JP61131361A priority Critical patent/JPS62289677A/en
Publication of JPS62289677A publication Critical patent/JPS62289677A/en
Publication of JPH031427B2 publication Critical patent/JPH031427B2/ja
Granted legal-status Critical Current

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  • Details Of Garments (AREA)
  • Manufacturing Of Multi-Layer Textile Fabrics (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

〔産業上の利用分野〕 本発明は衣服などに使用する芯地に関し、とく
に繊維ウエブと編織物とを複合した複合芯地に関
する。 〔従来技術〕 一般に芯地には編織物芯地と不織布芯地とが使
用されているが、その性質には一長一短がある。
例えば編織物芯地は編織物を構成する糸条の交点
が結合されていないので、融通性に優れ、表地に
沿つた動きができる反面、保形性や寸法安定性に
は劣つており着くずれが生じやすい。また編織物
芯地は糸条からなるので、張りや腰などはある
が、糸条によつて囲まれる空間が、不織布の繊維
どうしの間にできる空間よりも大きいため、接着
芯地として用いたとき逆しみが起き易いという欠
点がある。 これとは逆に不織布芯地は繊維交点が結合され
ているので、保形性や寸法安定性には優れている
が、融通性に乏しく、また、樹脂加工を施すなど
ある程度風合のソフトさを犠性にしないと張りや
腰が得られないという欠点がある。 このため、編織物芯地と不織布芯地の各々の短
所を補い、長所のみを利用すべく編織物と不織布
との複合芯地が種々検討された。 従来、この複合芯地としては編織物と繊維ウエ
ブとを積層し、ニードルパンチにより絡合一体化
したものや絡合後、接着剤や予め繊維ウエブ中に
含ませておいた接着繊維などの接着手段により繊
維間を結合したものが提案されている。前者の芯
地は比較的融通性があるが、繊維間が実質的に結
合されていないので、外力による変形を受け易
く、保形性に問題が残り、一方、後者の芯地は繊
維間が接着手段により結合されているので保形性
は得られるが、編織物が繊維ウエブ層に固定され
ることから融通性に乏しく、結局、満足できるも
のは得られなかつた。また、いずれの芯地もニー
ドルパンチによる絡合工程をとるため薄物の複合
芯地を得ることは困難であつた。 〔発明の目的〕 本発明は上記従来技術の欠点を解消すべくなさ
れたものであり、風合がソフトで、張りや腰を有
するとともに、従来その両立が困難であつた融通
性と保形性とを兼ね備えた複合芯地を提供するこ
とを目的とする。 〔発明の構成〕 本発明は熱可塑性繊維20〜100重量%を含む繊
維ウエブ層中に、該熱可塑性繊維よりも融点の高
い糸条からなる粗目織物またはよこ糸挿入編物
(以下「粗目編織物」という)が配置されてなる
積層物が、熱圧着部を部分的に設けることにより
一体化されており、かつ上記粗目編織物のよこ糸
が上記熱圧着部により実質的に固定さないことを
特徴とする複合芯地である。 すなわち、本発明の複合芯地においては、繊維
ウエブ層中に配される粗目編織物の少なくともよ
こ糸が繊維ウエブ層に固定されることなく動くこ
とができ、一方、部分的な熱圧着部により、この
よこ糸の動きうる範囲が限定されているので、本
発明の複合芯地は表地に沿う適度な融通性と、着
くずれなどを生じさせない保形性とを同時に満足
させることができるのである。また、本発明の複
合芯地は、この粗目編織物がある程度の範囲で動
きを持つことにより、外力が加わつたときに組織
内に復元可能なずれをおこすことができ、かつ結
合が部分的な結合によるため、風合が非常にソフ
トであり、しかも、粗目編織物を内挿しているこ
とによる張りや腰、とくによこ張りのある芯地と
なるのである。 本発明に使用する繊維ウエブ層は公知の乾式
法、湿式法、溶融紡糸法などにより形式され、ウ
エブ層中には20〜100重量%の熱可塑性繊維が含
まれる。この熱可塑性繊維は熱圧着を施した部分
において溶融してフイルム化し、実質的に構成繊
維間を結合する働きをする。このため、ウエブ層
中に含まれる熱可塑性繊維の量が20重量%未満で
あると十分な結合力が得られず、ウエブ層に剥離
が生じたり、芯地として必要な強度や耐久性を満
たすことができなくなつてしまう。 上記の熱可塑性繊維にはポリアミド系繊維、ポ
リエステル系繊維、ポリオレフイン系繊維、アク
リル系繊維などの合成繊維や、融点の異なる2成
分以上の樹脂からなる複合繊維などが好適に使用
される。また、熱可塑性繊維とともにウエブ層を
構成する繊維はとくに限定されず、合成繊維、再
生繊維、天然繊維など種々の繊維が用いられる
が、通常、衣料用に用いられる繊維がとくに好ま
しい。繊維ウエブ層の目付は10〜60g/m2の範囲
にある事が望ましく、10g/m2未満ではウエブ層
を用いる効果が少なく、十分な保形性を得ること
ができず、とくに接着芯地として用いた場合に逆
しみが生じるおそれがあり、一方、60g/m2を越
えると厚くなりすぎて芯地に適さなくなるうえ
に、粗目編織物を挿入した効果が薄れ、融通性の
乏しいものとなる。 本発明の複合芯地は上述の繊維ウエブ層中に粗
目編織物が配置された構造となつているが、これ
は例えば、予じめカーデイングにより作成した2
つの繊維ウエブ層の間に粗目編織物を挾んで積層
することなどにより得られる。本発明に使用する
粗目編織物とは粗目織物またはよこ糸挿入編物で
あるが、粗目織物としては、たて糸及びよこ糸の
打ち込み本数が5〜40本/インチ、繊度が40〜
200デニールのものが使用され、よこ糸挿入編物
としては、挿入されるよこ糸の打ち込み本数が5
〜40本/インチ、繊度が80〜300デニール、編糸
の繊度が20〜40デニールのものが使用される。こ
こで、粗目編織物のよこ糸の打ち込み本数が5〜
40本/インチのものが望ましいとされる理由は、
5本/インチ未満では粗目編織物を挿入した効果
が少なく、得られる芯地に張りや腰、とくに横張
りが出にくいからであり、一方、40本/インチを
越えると熱圧着部がよこ糸の上にくる割合が高く
なり、熱圧着をよこ糸に阻害されることにより、
熱圧着部において繊維どうしが十分に結合され
ず、層間剥離をおこし易く実用に耐えないものと
なつてしまうからである。また、よこ糸の打ち込
み本数が40本/インチを越える編織物を用いた場
合、得られる複合芯地の風合は非常に硬いものに
なる。とくに好ましい粗目編織物のよこ糸の打ち
込み本数は10〜25本/インチである。上記粗目編
織物のうち、とくによこ糸挿入編物を用いた複合
芯地は、よこ方向にはよこ糸による張りが得ら
れ、たて方向には編み構造によるドレープ性や伸
縮性が得られるので、前身頃用の芯として好適に
使用できる。 なお、通常、肩部、胸部、ウエスト部、裾部な
どは複数の芯地を組み合わせて、各部位ごとに異
なつた張りや硬さを出しているが、本発明の複合
芯地では使用する粗目編織物に硬さや厚さの変化
するものを選ぶことにより一枚の芯地でまかなう
ことができる。すなわち、粗目編織物のよこ糸の
打ち込み密度やよこ糸の太さを連続的にまたは段
階的に使用する部位に合わせて変化させることに
より、各部位に所望の厚さや硬さを持つた複合芯
地を得ることができるのである。 上述の粗目編織物を構成する糸条には、例えば
ポリエステル系、ポリアミド系などの合成繊維糸
やレーヨン糸などの再生繊維糸、あるいは木綿
糸、麻糸などの天然繊維糸など種々の糸が使用で
きるが、この糸が、熱可塑性繊維の融着する条件
でともに融着性を示すと、結果的に編織物が繊維
ウエブ層に固定されてしまつて、融通性がなく、
風合の硬い芯地となるので、この糸は熱可塑性繊
維が融着する条件下で、融着性を示さないもので
なければならない。従つて、編織物を構成する糸
条は熱可塑性繊維よりも融点の高いものでなけれ
ばならず、少なくとも5℃以上、好ましくは20℃
以上融点の高いものがよい。 本発明の複合芯地は、粗目編織物を挾持した繊
維ウエブ層を部分的に熱圧着することにより製造
される。この部分的な熱圧着は、例えば、点、
線、円、三角形、四角形、多角形などの形状が適
宜分布された1平方センチメートル当り10〜150
個の凸部を有するエンボスロールなどにより加熱
加圧することにより行われる。この様にして形成
された熱圧着部においては、熱可塑性繊維の融着
により繊維が結合される。この熱圧着部の総面積
が複合芯地の面積に占める割合は5〜30%の範囲
にあることが望ましく、5%未満では芯地として
必要な耐久性や強度を得ることができず、30%を
超えると風合が硬く、融通性の乏しい芯地となつ
てしまう。とくに好ましい熱圧着部の面積の割合
は8〜20%である。 また、本発明においては粗目編織物のよこ糸が
熱圧着部により実質的に固定されないものでなけ
ればならない。ここで実質的に固定されないと
は、熱圧着部がよこ糸上にない場合、及びよこ糸
上にあつてもよこ糸がほぼ自由に動きうる場合を
さし、この場合、熱圧着部がよこ糸上にくる割合
が10%以下であるのが望ましい。これは、この割
合が10%を越えると粗目編織物が繊維ウエブ層に
固定されて得られる芯地の融通性がなくなり、し
かも糸条の上にきた熱圧着部では繊維が十分に結
合されず、外力が加わると容易に破壊されて得ら
れる芯地の強度や耐久性が低下するからである。
熱圧着部が粗目編織物のよこ糸の上にくる割合を
10%以下としておけば、よこ糸自体は融着性を持
たず、熱圧着部においても完全にはウエブ層に固
定されないため、実質的によこ糸の大部分は熱圧
着部と熱圧着部との間で移動が可能であり、一
方、それ以上の移動は制限されるので、複合芯地
全体としては適度な融通性と保形性とを両立させ
ることができるのである。この割合は、好ましく
は5%以下、とくに好ましくは0%であるのがよ
い。なお、ここで熱圧着部が粗目編織物のよこ糸
の上にくる割合とは、熱圧着部の総数に対する粗
目編織物のよこ糸の上にくる熱圧着部の数の割合
を百分率で示したものであり、例えば単位面積当
り100個の熱圧着部があり、そのうちよこ糸の上
にある熱圧着部の数が10個であれば10%となるわ
けである。ただし、この熱圧着部の数は、芯地上
の任意の場所を10点選び、各々の場所で1辺1cm
の正方形内に入る熱圧着部の総数とよこ糸上にく
る熱圧着部の数をかぞえ、その平均値により示し
ている。本発明においてとくによこ糸について熱
圧着部が上にくる割合を限定したのは、芯地、と
くに前身頃芯などではよこ方向の張りが重視さ
れ、一般にたて糸に比してよこ糸は同じか、もし
くは太いものが使用されるので、よこ糸が固定さ
れると編織物の動きが著しく妨げられ、またよこ
糸の上にくる熱圧着部の結合は外力により破壊さ
れ易く、強度や耐久性に与える影響が大きいから
である。 この粗目編織物のよこ糸の上にくる熱圧着部の
割合を10%以下とするためには、熱圧着部を形成
する際によこ糸が熱圧着するための凸部に押えら
れない様に、外力がかかると動いてずれる様にし
ておけばよく、例えば、熱圧着の際によこ糸に張
力がかからなくなるとか、よこ糸に繊度の太いも
のを使用するとかすればよい。また、もちろん、
できるだけ編目や織目と、熱圧着を施こすロール
の凸部の分布とを同調させ、よこ糸の上に熱圧着
部がこない様に調節することも効果的である。 なお、好ましくはよこ糸の上だけでなく、たて
糸の上にも熱圧着部はない方がよいが、本発明に
おいては、粗目編織物が熱可塑性繊維よりも融点
の高い糸条により構成されているので、たて糸の
上にある程度熱圧着部がきても、粗目編織物が繊
維ウエブ層に固定されて融通性を失うことはな
い。とくによこ糸挿入編物の場合には、編み組織
が部分的に固定されても、熱圧着部と熱圧着部と
の間の編み構造による伸縮性があるので、よこ糸
さえ動きうる状態にあれば十分な融通性を示す。 本発明の複合芯地は、上述のように融通性と保
形性とを有するので、そのまま縫製などにより表
地と一体化してもよいが、片面もしくは両面にポ
リアミド系樹脂、ポリエステル系樹脂、ポリオレ
フイン系樹脂などのいわゆる熱融着性樹脂をドツ
ト状、粉末状、フイラメント状などの形態で付着
させて接着芯地として使用してもよい。 〔実施例〕 実施例 1 6ナイロン繊維(繊維長44mm、繊度1.5デニー
ル、融点221℃)100重量%よりなる繊維ウエブ層
15g/m2を2層作成し、この層間に繊度120デニ
ール(44番手)のポリエステル糸(融点258℃)
からなるよこ糸を1インチ当り20本打ち込んだよ
こ糸挿入編物(編組織は30デニールのポリエステ
ル糸を用いたベンビステツチからなる)30g/m2
を配して、積層物を形成する。 次いで、この積層物に、小円形状の断面を有す
る凸部がたて方向に1インチ当り20個、(1cm2
り62個)面積割合にして10%となるように分布し
たエングレイブロールを用いて、上記の凸部がよ
こ糸とよこ糸の間にくる様に調節して、温度200
℃で部分熱圧着を施し、複合芯地を得た。なお、
このときよこ糸挿入編物のよこ糸の上に熱圧着部
のくる割合はほぼ0%であつた。 得られた複合芯地のせん断力、曲げ剛性、引張
強伸度、洗濯強さ、ドライクリーニング強さを下
記の試験法により測定し、第1表及び第2表に示
した。 (せん断力) 引張り・せん断試験機((株)加藤鉄工所製)を使
用して、試験片のせん断ずり量とせん断荷重との
関係を求めてグラフ化し、その傾きからせん断力
を求める。 せん断荷重の測定は、20cm平方の試験片を用意
し、この試験片を測定実寸法が5cm×20cmとなる
ように5cmの間隔をあけた2つの平行なチヤツク
間に固定し、一方のチヤツクを移動させることに
より試験片を一定のせん断ずり量だけずらし、そ
れに対応するせん断荷重を測定することにより行
なつた。なお、せん断ずり量はせん断角により表
示され、例えば、5cm間隔の測定実寸法の場合、
せん断角が2゜のとき、せん断ずり量は1.746mm
( 50mm×tan2゜)となる。 このせん断力は、布地にずれが生じる際の抵抗
を示すので、これが小さいほど融通性が大きいこ
とを表わす。 (曲げ剛性) 純曲げ試験機((株)加藤鉄工所製)を使用して試
験片の曲率と曲げモーメントとの関係を求めてグ
ラフ化し、その傾きから曲げ剛性を求める。 この測定は20cm平方の試験片を固定チヤツクと
移動チヤツクにはさみ、移動チヤツクを動かすこ
とで試験片を一定の曲率に曲げ、それに対応する
曲げモーメントを測定することにより行なつた。 (引張り強伸度)JIS−L−1085準用 5cm×20cmの試験片をたて、よこ方向にそれぞ
れ5枚採取し、これを引張り試験機(東洋ボール
ドウイン社製)により、チヤツク間距離10cm、引
張り速度30cm/分の条件で引張り、破断時の強度
(Kg)および伸度(%)を測り平均値で示す。 (ドライクリーニング強さ) 25cm×25cmの試験片をナイロンタフタに包み、
これを商業用パークレンクリーナーを用いて、洗
濯物重量が1Kgになるように負荷布を加え、洗濯
温度25℃で8分間洗濯し、排液1分間、脱液4分
間、乾燥5分間(60℃)および脱臭2分間の工程
を3回繰り返す。 次いで、この試験片の曲げ剛性を測定して物性
の変化を調べるとともに、試験片の形態の変化を
観察し、下記の基準により評価した。 (試料片の形態変化) 5級:クリーニング前後で変化なし 4級:クリーニング前後で変化がわずかにある 3級:クリーニング前後で変化が目立つ 2級:クリーニング前後で変化がかなり目立つ 1級:クリーニング前後で変化が著しい (洗濯強さ) 25cm×25cmの試験片をナイロンタフタで包み、
これを40±3℃の0.5マルセル石けん溶液を20
以上入れた家庭用洗濯機に入れ、毎分500回の回
転速度で15分間操作した後、水洗脱水し、常温で
乾燥する。 次いで、乾燥した試験片の曲げ剛性を調べると
ともに、形態の変化を観察し、ドライクリーニン
グと同様の基準により評価した。 (着用試験) 試験片を前身頃芯として用いた上衣を作成し、
これを90日間着用した後の外観変化を調べた後、
これをドライクリーニングして更に90日間着用し
た後の外観変化を調べた。 比較例 1 6ナイロン繊維(繊維長47mm、繊度1.5デニー
ル)100重量%よりなる繊維ウエブ層60g/m2に、
実施例1と同様のエングレイブロールを用いて、
温度200℃で部分熱圧着を施し、不織布芯地を得
た。 得られた芯地の物性を実施例1と同様にして測
定し、その結果を第1表及び第2表に示した。 実施例 2 実施例1と同様の繊維ウエブ層とよこ糸挿入編
物とからなる積層物を、実施例1で用いたロール
と同様のロールで、よこ糸挿入編物のよこ糸上に
凸部が一部重なるのを許した状態で熱圧着を施
し、複合芯地を得た。なお、このとき、熱圧着部
62個/cm2のうち、5個/cm2がよこ糸上にきてお
り、熱圧着部のうち8%がよこ糸上にあつた。 上記複合芯地の物性を実施例1と同様にして測
定し、その結果を第1表及び第2表に示した。 比較例 2 実施例1と同様の繊維ウエブ層とよこ糸挿入編
物とからなる積層物を、実施例1で用いたロール
と同様のロールで、よこ糸挿入編物のよこ糸上に
凸部が一部重なるのを許した状態で、かつよこ糸
の張力のかかつた状態で熱圧着を施し複合芯地を
得た。なお、このとき熱圧着部62個/cm2のうち、
12個/cm2がよこ糸上にきており、熱圧着部のうち
19%がよこ糸上にあつた。 上記複合芯地の物性を実施例1と同様にして測
定し、その結果を第1表及び第2表に示した。 実施例 3 6ナイロン繊維(繊維長47mm、繊度1.5デニー
ル、融点220℃)70重量%とポリエステル繊維
(繊維長38mm、繊度1.5デニール、融点255℃)30
重量%とからなる繊維ウエブ層20g/m2を2層作
成し、この層間に繊度120デニールのポリエステ
ル糸(融点260℃)からなるよこ糸と繊度80デニ
ールのポリエステル糸(融点260℃)からなるた
て糸を各々、1インチ当り23本打ち込んだ織物を
配して積層物を形成した。 次いで、この積層物に長方形状の断面を有する
凸部が、たて方向に1インチ当り23個(1cm2当り
82個)、面積割合にして13%となるように分布し
たエングレイブロールを用い、上記凸部がよこ糸
とよこ糸の間にくる様に調節して、温度205℃で
部分熱圧着し、複合芯地を得た。なお、このとき
織物のよこ糸の上に熱圧着部はほとんどなかつ
た。 得られた複合芯地の物性を実施例1と同様にし
て測定し、その結果を第1表及び第2表に示し
た。 比較例 3 実施例3と同じ配合の繊維ウエブ層20g/m2
2層作成し、この層間に繊度120デニールのポリ
エステル糸からなるよこ糸と、繊度80デニールの
ポリエステル糸からなるたて糸を各々1インチ当
り42本打ち込んだ織物を配して積層物を形成し
た。 次いで、この積層物に長方形状の断面を有する
凸部が、たて方向に1インチ当り42個(1cm2当り
139個)、面積割合にして18%となるように分布し
たエングレイブロールを用いて、温度205℃で部
分熱圧着を施したが、織物の織目部分の空隙が小
さく、上層と下層との繊維を融着することが困難
であつた。このため得られた複合芯地は層間で容
易に剥離を生じ、使用に適さないものであつた。 実施例 4 実施例1で得た複合芯地の片面にポリアミド樹
脂15g/m2を点状に付着させ、接着芯地を得た。 この接着芯地は表地と接着する際に逆しみが全
く生じず、作業性に優れていた。また、表地と接
着する際に表地の形状に良く沿い、接着後は着用
によつて型くずれがなく保形性も良好であつた。
さらに、この芯地を前身頃芯に用いて衣服を作用
したところ、よこ方向には適度な張りがあり、た
て方向にはドレープ性があり、風合もソフトなの
で、着用感に優れていた。 実施例 5 ポリエステル糸からなるよこ糸を1インチ当り
20本打ち込んだよこ糸挿入編物(編組織は30デニ
ールのポリエステル糸を用いたくさり編みからな
る)であつて、たて方向に15cm、20cm、30cmの幅
において、よこ糸の太さが250デニール、180デニ
ール、130デニールと段階的に変化するよこ糸挿
入編物を用いたこと以外は、実施例1と同様にし
て複合芯地を作成した。 これを、よこ糸の太さの太い側から、肩部、胸
部、腹部に当るように、紳士服の前身頃芯として
使用したところ、一枚の複合芯地で各部に必要な
張りが得られ、従来のように手間のかかる縫製作
業を省略することができた。 実施例 6 繊度150デニールのポリエステル糸からなるよ
こ糸を、たて方向に15cm、20cm、30cmの幅におい
て、打ち込み本数を段階的に25本/インチ、20
本/インチ、15本/インチと変化させたよこ糸挿
入編物(編組織は30デニールのポリエステル糸を
用いたくさり編みからなる)を用いたこと以外
は、実施例1と同様にして複合芯地を作成した。 これを打ち込み本数の多い側から、肩部、胸
部、腹部に当るように紳士服の前身頃芯として使
用したところ、一枚の複合芯地で各部に必要な張
りと融通性とが得られた。
[Industrial Field of Application] The present invention relates to interlining used for clothing and the like, and particularly to a composite interlining made of a composite of a fiber web and a knitted fabric. [Prior Art] Generally, knitted fabric interlinings and non-woven fabric interlinings are used as interlining materials, but their properties have advantages and disadvantages.
For example, interlining for knitted fabrics does not have the intersecting points of the threads that make up the knitted fabric, so it has excellent flexibility and can move along the outer fabric, but it has poor shape retention and dimensional stability, so it may slip when worn. is likely to occur. In addition, knitted fabric interlining is made of yarn, so it has tension and stiffness, but the space surrounded by the yarn is larger than the space created between the fibers of non-woven fabric, so it is used as an adhesive interlining. The disadvantage is that reverse staining is likely to occur. On the other hand, nonwoven interlining has excellent shape retention and dimensional stability because the fiber intersections are bonded together, but it lacks flexibility, and the texture is soft to some extent due to resin processing. The disadvantage is that you cannot gain tension or lower back without sacrificing. For this reason, various composite interlinings of knitted fabrics and nonwoven fabrics have been investigated in order to compensate for the disadvantages of each of the interlinings of knitted fabrics and nonwoven fabrics, and to take advantage of only their advantages. Conventionally, this composite interlining has been produced by laminating knitted fabrics and fiber webs and intertwining them into one piece using needle punching, or by bonding with adhesive or adhesive fibers pre-impregnated in the fiber web after entanglement. It has been proposed that the fibers are bonded by means. The former interlining is relatively flexible, but since the fibers are not substantially bonded, it is easily deformed by external forces, leaving problems with shape retention. Since they are bonded by adhesive means, shape retention can be achieved, but since the knitted fabric is fixed to the fiber web layer, flexibility is poor, and in the end, a satisfactory product could not be obtained. Furthermore, since both interlinings require an entangling process using needle punching, it has been difficult to obtain a thin composite interlining. [Object of the Invention] The present invention has been made in order to eliminate the drawbacks of the above-mentioned prior art, and has a soft texture, firmness and firmness, as well as flexibility and shape retention, which were previously difficult to achieve at the same time. The purpose is to provide a composite interlining that combines the following. [Structure of the Invention] The present invention provides a coarse woven fabric or a weft-inserted knitted fabric (hereinafter referred to as a "coarse knitted fabric") consisting of yarns having a higher melting point than the thermoplastic fibers in a fibrous web layer containing 20 to 100% by weight of thermoplastic fibers. ) are arranged and are integrated by partially providing thermocompression bonding parts, and the weft of the coarse knitted fabric is not substantially fixed by the thermocompression bonding parts. It is a composite interlining material. That is, in the composite interlining of the present invention, at least the weft of the coarsely knitted fabric disposed in the fiber web layer can move without being fixed to the fiber web layer, while the partial thermocompression bonding portion Since the range of movement of the weft yarn is limited, the composite interlining of the present invention can simultaneously satisfy appropriate flexibility along the outer fabric and shape retention that does not cause slippage. In addition, in the composite interlining of the present invention, the loosely knitted fabric has movement within a certain range, so that when an external force is applied, a reversible shift can be caused in the tissue, and the bonding is only partial. Because it is bonded, it has a very soft texture, and the interlining of the coarsely knitted fabric gives it firmness and firmness, especially in the interlining. The fiber web layer used in the present invention is formed by a known dry method, wet method, melt spinning method, etc., and the web layer contains 20 to 100% by weight of thermoplastic fibers. The thermoplastic fibers are melted into a film in the thermocompression bonded area, and serve essentially to bond the constituent fibers together. For this reason, if the amount of thermoplastic fibers contained in the web layer is less than 20% by weight, sufficient bonding strength may not be obtained, resulting in peeling of the web layer or the strength and durability required for interlining. I end up not being able to do anything. As the above-mentioned thermoplastic fibers, synthetic fibers such as polyamide fibers, polyester fibers, polyolefin fibers, acrylic fibers, and composite fibers made of two or more resins having different melting points are preferably used. Further, the fibers constituting the web layer together with the thermoplastic fibers are not particularly limited, and various fibers such as synthetic fibers, recycled fibers, and natural fibers may be used, but fibers normally used for clothing are particularly preferred. It is desirable that the basis weight of the fiber web layer is in the range of 10 to 60 g/m 2 .If it is less than 10 g/m 2 , the effect of using the web layer will be small and sufficient shape retention will not be obtained, especially for adhesive interlining. On the other hand, if it exceeds 60g/ m2 , it becomes too thick and is not suitable for interlining, and the effect of inserting coarse knitted fabric is weakened, resulting in poor flexibility. Become. The composite interlining of the present invention has a structure in which a coarsely knitted fabric is arranged in the above-mentioned fibrous web layer.
It can be obtained by sandwiching and laminating a coarsely knitted fabric between two fibrous web layers. The coarse knitted fabric used in the present invention is a coarse fabric or a weft inserted knitted fabric, and the coarse fabric has a warp and weft yarn count of 5 to 40 per inch and a fineness of 40 to 40.
200 denier is used, and the number of inserted weft threads is 5 for knitting with weft thread insertion.
~40 yarns/inch, fineness of 80 to 300 deniers, and knitting yarns with fineness of 20 to 40 deniers are used. Here, the number of weft threads of the coarse knitted fabric is 5 to 5.
The reason why 40 lines/inch is desirable is that
If it is less than 5 yarns/inch, the effect of inserting the coarsely knitted fabric will be small, and the resulting interlining will have difficulty exhibiting tension, stiffness, and especially lateral tension.On the other hand, if it exceeds 40 yarns/inch, the thermo-compression bonding part will not be as strong as the weft yarns. The proportion of the material coming to the top increases, and thermocompression bonding is obstructed by the weft threads.
This is because the fibers are not sufficiently bonded to each other in the thermocompression bonded portion, and delamination is likely to occur, making the product impractical. Furthermore, when a knitted fabric with a weft count of more than 40 per inch is used, the resulting composite interlining will have a very hard texture. The number of weft yarns in the coarsely knitted fabric is particularly preferably 10 to 25 yarns/inch. Among the above-mentioned coarse knitted fabrics, composite interlinings using weft yarn insertion knit fabrics provide tension in the weft direction due to the weft yarns, and provide drapability and stretchability due to the knitted structure in the warp direction. It can be suitably used as a core. Normally, multiple interlining materials are combined for the shoulders, chest, waist, hem, etc. to create different tension and stiffness for each area, but the composite interlining of the present invention uses a coarse interlining material. By choosing knitted fabrics that vary in hardness and thickness, you can cover all your needs with a single piece of interlining. In other words, by changing the weft thread density and weft thickness of the coarsely knitted fabric, either continuously or stepwise, depending on the area where it will be used, it is possible to create a composite interlining that has the desired thickness and hardness for each area. You can get it. Various yarns can be used as the yarns constituting the above-mentioned coarse knitted fabric, such as synthetic fiber yarns such as polyester and polyamide yarns, recycled fiber yarns such as rayon yarn, or natural fiber yarns such as cotton yarn and hemp yarn. However, if this yarn exhibits fusibility under the conditions where thermoplastic fibers are fused together, the knitted fabric will end up being fixed to the fiber web layer, resulting in no flexibility.
Since this results in an interlining with a hard feel, the yarn must not exhibit fusibility under the conditions in which the thermoplastic fibers are fused. Therefore, the yarns constituting the knitted fabric must have a higher melting point than the thermoplastic fibers, at least 5°C or higher, preferably 20°C.
Those with higher melting points are preferred. The composite interlining of the present invention is produced by partially thermocompressing fibrous web layers sandwiching a coarsely knitted fabric. This partial thermocompression bonding, for example, points,
10 to 150 shapes such as lines, circles, triangles, squares, and polygons are distributed appropriately per square centimeter.
This is done by applying heat and pressure using an embossing roll or the like having several convex portions. In the thermocompression bonded portion formed in this manner, the fibers are bonded by fusing the thermoplastic fibers. It is desirable that the ratio of the total area of this thermocompression bonded part to the area of the composite interlining is in the range of 5 to 30%; if it is less than 5%, it will not be possible to obtain the necessary durability and strength as an interlining. If it exceeds %, the interlining material will have a hard texture and poor flexibility. A particularly preferable area ratio of the thermocompression bonded portion is 8 to 20%. Further, in the present invention, the weft threads of the coarsely knitted fabric must not be substantially fixed by the thermocompression bonding part. Here, "not substantially fixed" refers to cases where the thermocompression-bonded part is not on the weft thread, or cases where the weft thread can move almost freely even if it is on the weft thread, in which case the thermocompression-bonded part is on the weft thread. It is desirable that the ratio is 10% or less. This is because if this ratio exceeds 10%, the coarsely knitted fabric will be fixed to the fiber web layer and the interlining will lose its flexibility, and the fibers will not be bonded sufficiently at the thermocompression bonded part above the yarn. This is because when an external force is applied, the interlining is easily destroyed and the strength and durability of the resulting interlining are reduced.
The ratio of the thermocompression bonding part to the weft of the coarsely knitted fabric
If it is set to 10% or less, the weft yarn itself does not have fusion properties and is not completely fixed to the web layer even at the thermocompression bonding section, so the majority of the weft yarn is essentially bonded between the thermocompression bonding sections. However, since further movement is restricted, the composite interlining as a whole can achieve both appropriate flexibility and shape retention. This proportion is preferably 5% or less, particularly preferably 0%. Note that the ratio of the thermocompression-bonded parts to the weft of the coarsely knitted fabric here refers to the ratio of the number of thermocompression-bonded parts that are above the weft of the coarsely knitted fabric to the total number of thermocompression-bonded parts, expressed as a percentage. For example, if there are 100 thermocompression bonded parts per unit area, and the number of thermocompression bonded parts on the weft is 10, it will be 10%. However, the number of thermocompression bonding parts is determined by selecting 10 arbitrary locations on the core surface and 1 cm on each side at each location.
The total number of thermocompression bonded parts that fall within the square and the number of thermocompression bonded areas that fall on the weft are counted, and the average value is shown. In the present invention, the ratio of the thermocompression bonded part to the top of the weft yarns is specifically limited because the tension in the weft direction is important for interlining materials, especially front body cores, and generally the weft yarns are the same or thicker than the warp yarns. If the weft is fixed, the movement of the knitted fabric will be significantly hindered, and the bond of the thermo-compression bonded part above the weft is easily destroyed by external force, which has a large effect on strength and durability. It is. In order to keep the proportion of the thermocompression bonded part above the weft of this coarse knitted fabric to 10% or less, when forming the thermocompression bonding part, external force must be applied so that the weft yarn is not pressed by the convex part for thermocompression bonding. What is necessary is to make it move and shift when pressure is applied, for example, by removing tension from the weft thread during thermocompression bonding, or by using a weft thread with a thicker fineness. Also, of course,
It is also effective to synchronize the stitches and weave as much as possible with the distribution of the convex portions of the roll that applies thermocompression bonding, so that the thermocompression bonded portions do not come on top of the weft threads. Preferably, there should be no thermocompression bonded parts not only on the weft yarns but also on the warp yarns, but in the present invention, the coarsely knitted fabric is composed of yarns having a higher melting point than the thermoplastic fibers. Therefore, even if a thermocompression bonded part is formed on the warp yarns to some extent, the coarsely knitted fabric will not be fixed to the fiber web layer and lose its flexibility. Particularly in the case of weft inserted knitted fabrics, even if the knitting structure is partially fixed, there is elasticity due to the knitting structure between the thermocompression bonded parts, so as long as the weft yarn is in a state where it can move, it is sufficient. Show flexibility. The composite interlining of the present invention has flexibility and shape retention as described above, so it may be integrated with the outer material by sewing or the like, but one or both sides may be made of polyamide resin, polyester resin, or polyolefin resin. A so-called heat-fusible resin such as a resin may be attached in the form of dots, powder, filament, etc. and used as an adhesive interlining. [Example] Example 1 Fiber web layer consisting of 100% by weight of 6 nylon fibers (fiber length 44 mm, fineness 1.5 denier, melting point 221°C)
Two layers of 15g/m 2 were created, and between these layers was a polyester yarn with a fineness of 120 denier (44th count) (melting point 258℃).
A weft-inserted knitted fabric with 20 wefts per inch (the knitting structure consists of Benbi stitch using 30 denier polyester yarn) 30g/m 2
to form a laminate. Next, this laminate was coated with an engraving roll in which convex portions having a small circular cross section were distributed in the vertical direction so that 20 convex portions per inch (62 convex portions per 1 cm 2 ) were distributed at an area ratio of 10%. Adjust the above protrusion so that it is between the weft threads, and set the temperature to 200.
Partial thermocompression bonding was performed at ℃ to obtain a composite interlining. In addition,
At this time, the proportion of the thermocompression-bonded portion above the weft of the weft-inserted knitted material was approximately 0%. The shear force, bending rigidity, tensile strength and elongation, washing strength, and dry cleaning strength of the obtained composite interlining were measured by the following test methods and are shown in Tables 1 and 2. (Shear force) Using a tensile/shear tester (manufactured by Kato Iron Works Co., Ltd.), determine the relationship between the shear amount of the test piece and the shear load, graph it, and determine the shear force from the slope. To measure the shear load, prepare a 20 cm square test piece, fix this test piece between two parallel chucks spaced 5 cm apart so that the actual measurement dimensions are 5 cm x 20 cm, and hold one chuck in place. This was done by shifting the test piece by a certain amount of shear shear by moving it, and measuring the corresponding shear load. The amount of shear shear is expressed by the shear angle. For example, in the case of measured actual dimensions at 5 cm intervals,
When the shear angle is 2°, the shear amount is 1.746mm
(50mm×tan2゜). This shear force indicates the resistance to shearing of the fabric, so the smaller the shear force, the greater the flexibility. (Bending rigidity) Using a pure bending tester (manufactured by Kato Iron Works Co., Ltd.), the relationship between the curvature of the test piece and the bending moment is determined and graphed, and the bending rigidity is determined from the slope of the graph. This measurement was performed by sandwiching a 20 cm square test piece between a fixed chuck and a moving chuck, bending the test piece to a certain curvature by moving the moving chuck, and measuring the corresponding bending moment. (Tensile strength and elongation) Applicable to JIS-L-1085. 5 cm x 20 cm test pieces were set up and 5 pieces were taken in the horizontal direction. These were tested using a tensile tester (manufactured by Toyo Baldwin Co., Ltd.) with a distance between chucks of 10 cm, Tensile strength (Kg) and elongation (%) at break were measured at a tensile speed of 30 cm/min and are shown as average values. (Dry cleaning strength) Wrap a 25cm x 25cm test piece in nylon taffeta.
Using a commercial Perclean cleaner, load cloth was added so that the laundry weight was 1 kg, washed at a washing temperature of 25°C for 8 minutes, drained for 1 minute, dehydrated for 4 minutes, and dried for 5 minutes (60 minutes). C) and deodorization for 2 minutes are repeated three times. Next, the bending rigidity of this test piece was measured to examine changes in physical properties, and changes in the form of the test piece were observed and evaluated according to the following criteria. (Change in shape of sample piece) Grade 5: No change before and after cleaning Grade 4: Slight change before and after cleaning Grade 3: Noticeable change before and after cleaning Grade 2: Significant change before and after cleaning Grade 1: Before and after cleaning (washing strength) A 25cm x 25cm test piece was wrapped in nylon taffeta.
Add 0.5 Marcel soap solution at 40±3℃ for 20 minutes.
Put it in a household washing machine with the above contents, run it at a rotation speed of 500 times per minute for 15 minutes, then rinse it with water, dehydrate it, and dry it at room temperature. Next, the bending rigidity of the dried test piece was examined, changes in morphology were observed, and evaluation was made using the same criteria as for dry cleaning. (Wearing test) A jacket was created using the test piece as the front core,
After examining the appearance change after wearing this for 90 days,
This was dry cleaned and the change in appearance was examined after wearing it for an additional 90 days. Comparative Example 1 A fiber web layer of 60 g/m 2 consisting of 100% by weight of 6 nylon fibers (fiber length 47 mm, fineness 1.5 denier),
Using the same engraving roll as in Example 1,
Partial thermocompression bonding was performed at a temperature of 200°C to obtain a nonwoven interlining. The physical properties of the obtained interlining were measured in the same manner as in Example 1, and the results are shown in Tables 1 and 2. Example 2 A laminate consisting of a fiber web layer and a weft-inserted knitted fabric as in Example 1 was rolled using a roll similar to that used in Example 1 so that the convex portion partially overlapped the weft of the weft-inserted knitted fabric. A composite interlining was obtained by thermocompression bonding while allowing this. In addition, at this time, the thermocompression bonding part
Of the 62 pieces/cm 2 , 5 pieces/cm 2 were on the weft thread, and 8% of the thermocompression bonded parts were on the weft thread. The physical properties of the above composite interlining were measured in the same manner as in Example 1, and the results are shown in Tables 1 and 2. Comparative Example 2 A laminate consisting of a fiber web layer and a weft-inserted knitted fabric as in Example 1 was rolled using a roll similar to that used in Example 1 so that the convex portion partially overlapped the weft of the weft-inserted knitted fabric. A composite interlining was obtained by thermocompression bonding with the weft yarns under tension. At this time, out of 62 thermocompression bonded parts/ cm2 ,
12 pieces/cm 2 are on the weft thread, and in the thermocompression bonding part
19% was on the weft thread. The physical properties of the above composite interlining were measured in the same manner as in Example 1, and the results are shown in Tables 1 and 2. Example 3 6 Nylon fiber (fiber length 47 mm, fineness 1.5 denier, melting point 220°C) 70% by weight and polyester fiber (fiber length 38 mm, fineness 1.5 denier, melting point 255°C) 30
Two fiber web layers of 20 g/m 2 are created between the layers, and between these layers are a weft made of polyester yarn with a fineness of 120 denier (melting point 260°C) and a warp made of polyester yarn with a fineness of 80 denier (melting point 260°C). A laminate was formed by placing 23 woven fabrics per inch in each case. Next, on this laminate, 23 protrusions with a rectangular cross section are formed per inch (per cm2 ) in the vertical direction.
Using engraving rolls distributed so that the area ratio is 13%, the convex portions are adjusted so that they are between the weft yarns, and the composite interlining is bonded by partial thermocompression at a temperature of 205℃. I got it. In addition, at this time, there were almost no thermocompression bonded parts on the weft of the fabric. The physical properties of the obtained composite interlining were measured in the same manner as in Example 1, and the results are shown in Tables 1 and 2. Comparative Example 3 Two fiber web layers of 20 g/m 2 having the same composition as in Example 3 were created, and between these layers, a weft yarn made of polyester yarn with a fineness of 120 denier and a warp yarn made of polyester yarn with a fineness of 80 denier were placed between the layers of 1 inch each. A laminate was formed by arranging 42 woven fabrics per thread. Next, this laminate has 42 protrusions per inch (per 1 cm2) in the vertical direction.
Partial thermocompression bonding was performed at a temperature of 205℃ using engraving rolls distributed so that the area ratio was 18%, but the voids in the weave of the fabric were small and the fibers between the upper and lower layers were It was difficult to fuse. For this reason, the resulting composite interlining easily peeled off between layers, making it unsuitable for use. Example 4 On one side of the composite interlining obtained in Example 1, 15 g/m 2 of polyamide resin was attached in dots to obtain an adhesive interlining. This adhesive interlining did not cause any reverse staining when bonded to the outer material, and had excellent workability. Furthermore, when bonded to the outer material, it conformed well to the shape of the outer material, and after adhesion did not lose its shape when worn, and had good shape retention.
Furthermore, when this interlining material was used as the front core of a garment, it had moderate tension in the horizontal direction, drape in the vertical direction, and had a soft texture, making it extremely comfortable to wear. . Example 5 Weft yarn made of polyester yarn per inch
It is a knitted fabric with 20 weft threads inserted (the knitting structure is made of a pile knit using 30 denier polyester yarn), and the weft thickness is 250 denier and 180 denier at widths of 15 cm, 20 cm, and 30 cm in the warp direction. A composite interlining was produced in the same manner as in Example 1, except that a weft insertion knitted fabric whose denier gradually changed from 130 denier to 130 denier was used. When this was used as a core for the front body of men's clothing, starting from the thicker side of the weft and hitting the shoulders, chest, and abdomen, the necessary tension was obtained in each part with a single piece of composite interlining. The time-consuming sewing work required in the conventional method can be omitted. Example 6 Weft yarns made of polyester yarn with a fineness of 150 denier were set in widths of 15 cm, 20 cm, and 30 cm in the warp direction, and the number of weft yarns was set in stages to 25 yarns/inch and 20 yarns/inch.
A composite interlining was fabricated in the same manner as in Example 1, except that a knitted fabric with weft insertion (the knitting structure consisted of a double knit using 30 denier polyester yarn) with different weft threads per inch and 15 threads per inch was used. Created. When this material was used as a core for the front body of men's clothing, covering the shoulders, chest, and abdomen, starting from the side with the most number of threads, it was possible to obtain the necessary tension and flexibility for each part with a single piece of composite interlining. .

【表】【table】

【表】【table】

〔発明の効果〕〔Effect of the invention〕

本発明の複合芯地は融通性と保形性とを両立し
たものであるので、衣服を作成する際に使用部位
に合わせて丸みを出すなどの整形効果が高く、美
しいシルエツトを出すことができる。 また、外力の歪みを吸収する融通性は有する
が、一度定められた形状は容易に崩れないので、
着用による着崩れも生じにくい。一方、本発明の
複合芯地は風合がソフトであるにもかかわらず、
強度や耐久性に優れ、しかも張りや腰、とくに横
張りがあり、前身頃芯などに好適に利用できる。 更に、本発明の複合芯地においては、使用する
粗目編織物としてよこ糸の打ち込み密度や太さを
変化させたものを用いることにより、芯地の厚み
や硬さを変化させ、本来複数枚の芯地でまかなわ
れる肩部、胸部、腹部の芯地を、一枚の芯地でま
かなうこともできる。 この様に本発明の複合芯地は、従来の芯地には
なかつた優れた性質を持つので、衣服用芯地とし
て極めて有用なものである。
Since the composite interlining of the present invention is both flexible and shape-retaining, it has a high shaping effect such as rounding according to the area of use when making clothes, and can create a beautiful silhouette. . In addition, although it has the flexibility to absorb distortion from external forces, once the shape is determined, it does not easily collapse.
It also doesn't easily fall apart when worn. On the other hand, although the composite interlining of the present invention has a soft texture,
It has excellent strength and durability, and has good tension and waist tension, especially horizontal tension, so it can be used suitably for the core of the front body. Furthermore, in the composite interlining of the present invention, the thickness and hardness of the interlining can be changed by using coarsely knitted fabrics with varying weft implant density and thickness. It is also possible to cover the shoulders, chest, and abdomen with a single piece of interlining. As described above, the composite interlining of the present invention has excellent properties not found in conventional interlining, and is therefore extremely useful as an interlining for clothing.

Claims (1)

【特許請求の範囲】 1 熱可塑性繊維20〜100重量%を含む繊維ウエ
ブ層中に、該熱可塑性繊維よりも融点の高い糸条
からなる粗目織物またはよこ糸挿入編物が配置さ
れてなる積層物が、熱圧着部を部分的に設けるこ
とにより一体化されており、かつ上記粗目織物ま
たはよこ糸挿入編物のよこ糸が上記熱圧着部によ
り実質的に固定されていないことを特徴とする複
合芯地。 2 粗目織物のよこ糸及びたて糸の打ち込み本数
が5〜40本/インチである特許請求の範囲第1項
記載の複合芯地。 3 よこ糸挿入編物のよこ糸の打ち込み本数が5
〜40本/インチである特許請求の範囲第1項記載
の複合芯地。 4 粗目織物またはよこ糸挿入編物のよこ糸の打
ち込み密度が規則的に変化している特許請求の範
囲第1項ないし第3項のいずれかに記載の複合芯
地。 5 粗目織物またはよこ糸挿入編物のよこ糸の太
さが規則的に変化している特許請求の範囲第1項
ないし第3項のいずれかに記載の複合芯地。
[Scope of Claims] 1. A laminate comprising a fibrous web layer containing 20 to 100% by weight of thermoplastic fibers and a coarse woven fabric or a weft-inserted knitted fabric made of threads having a higher melting point than the thermoplastic fibers. A composite interlining characterized in that it is integrated by partially providing a thermocompression bonding part, and the weft of the coarse woven fabric or the weft insertion knitted fabric is not substantially fixed by the thermocompression bonding part. 2. The composite interlining according to claim 1, wherein the number of weft and warp yarns of the coarse woven fabric is 5 to 40 yarns/inch. 3 The number of weft threads for weft insertion knitting is 5.
The composite interlining according to claim 1, wherein the interlining is ~40 lines/inch. 4. The composite interlining according to any one of claims 1 to 3, wherein the weft density of the coarse woven fabric or the weft-inserted knitted fabric changes regularly. 5. The composite interlining according to any one of claims 1 to 3, in which the thickness of the weft yarns of the coarse woven fabric or the weft insertion knitted fabric changes regularly.
JP61131361A 1986-06-05 1986-06-05 Composite core cloth Granted JPS62289677A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61131361A JPS62289677A (en) 1986-06-05 1986-06-05 Composite core cloth

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61131361A JPS62289677A (en) 1986-06-05 1986-06-05 Composite core cloth

Publications (2)

Publication Number Publication Date
JPS62289677A JPS62289677A (en) 1987-12-16
JPH031427B2 true JPH031427B2 (en) 1991-01-10

Family

ID=15056128

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61131361A Granted JPS62289677A (en) 1986-06-05 1986-06-05 Composite core cloth

Country Status (1)

Country Link
JP (1) JPS62289677A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110996703A (en) * 2017-09-05 2020-04-10 日东纺绩株式会社 Adhesive interlining and laminated composite material

Also Published As

Publication number Publication date
JPS62289677A (en) 1987-12-16

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