JP2004204404A - Ground fabric for airbag, airbag, and method for producing the same - Google Patents

Ground fabric for airbag, airbag, and method for producing the same Download PDF

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Publication number
JP2004204404A
JP2004204404A JP2002376972A JP2002376972A JP2004204404A JP 2004204404 A JP2004204404 A JP 2004204404A JP 2002376972 A JP2002376972 A JP 2002376972A JP 2002376972 A JP2002376972 A JP 2002376972A JP 2004204404 A JP2004204404 A JP 2004204404A
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JP
Japan
Prior art keywords
airbag
fabric
base fabric
base
resin
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JP2002376972A
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Japanese (ja)
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JP4423853B2 (en
Inventor
Atsushi Morimoto
厚志 森本
Yoshiya Honbo
義哉 本母
Tomomichi Fujiyama
友道 藤山
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Toray Industries Inc
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Toray Industries Inc
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Priority to JP2002376972A priority Critical patent/JP4423853B2/en
Application filed by Toray Industries Inc filed Critical Toray Industries Inc
Priority to US10/529,848 priority patent/US8211813B2/en
Priority to CA 2501032 priority patent/CA2501032C/en
Priority to EP20030751321 priority patent/EP1548180B1/en
Priority to PCT/JP2003/012707 priority patent/WO2004031472A1/en
Priority to TW92127372A priority patent/TWI241965B/en
Priority to KR1020057005833A priority patent/KR100680564B1/en
Publication of JP2004204404A publication Critical patent/JP2004204404A/en
Application granted granted Critical
Publication of JP4423853B2 publication Critical patent/JP4423853B2/en
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  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide an airbag for protecting the occupants in the crush of an automobile, having mechanical properties, air-barrierness and compact housing space as an airbag, and producible with little loss of the cloth in cutting to improve the cost performance. <P>SOLUTION: The ground fabric for an airbag has a thermoplastic layer laminated on at least one surface of a woven fabric made of a synthetic fiber. The thickness T1 of the center part of the fabric and the thickness T2 of the coating edge part satisfy the relationship 0.9≤T1/T2, and the width W of the fabric and the width C of the resin-coated part of the fabric satisfy the relationship 0.95≤C/W≤0.99. <P>COPYRIGHT: (C)2004,JPO&NCIPI

Description

【0001】
【発明の属する技術分野】
本発明は、樹脂が積層されているエアバッグ用基布に関するものであり、更に詳しくは、樹脂が織物に積層された基布の厚み差を改善し、かつ織物の耳端部の耳たぶりによる塗工幅の減少を改善した経済性に優れたエアバッグ用基布およびエアバッグおよびその製造方法に関するものである。
【0002】
【従来の技術】
従来、エアバッグには、耐熱性、難燃性、空気遮断性などの機能を付与することを目的に、100〜900デシテックスのナイロン66、ナイロン6またはポリエステルなどのフィラメント糸からなる織物にクロロプレン、シリコーン、ウレタンなどの合成樹脂樹脂を塗布することが一般に行われている。かかる合成樹脂の塗布には一般にナイフコーターやコンマコーターが使用されており、上記のエアバッグの機能を保持し、かつ、収納コンパクト性、コストダウンを目的に、樹脂量をより少なく均一にコートすることが要求されている。しかし、現状では、エアバッグ基布のようなカバーファクターが1,400〜2,300の範囲内にある高密度織物においては製織時に生じる耳たぶりの問題があり、従来の塗布方法ではその耳端部の耳たぶりにより織物の端部に皺が生じ樹脂が塗布できず、実際にエアバッグとして使用できる織物幅は織り幅に対し90%程度になり織物のロスが生じるものである。
【0003】
そこで、近年、このような問題を解消するために、耳端部の織り密度が他本体基布より高くすることや耳端部に増糸が打ち込まれていることを特徴とする耳たぶりを改善する方法が開示されているが(例えば、特許文献1、2参照)十分なものではない。また、耳部にレノ組織とちがう地糸より細い糸で2本を絡み糸の単位として地糸2本と交互に挿入し耳たぶりを改善する方法が開示されているが(例えば、特許文献3参照)、工程が増えコストアップになり十分なものではない。安全部品であるエアバッグにもコストダウンなどの経済的要求が高まっており、製造ロスの少ない経済性に優れたエアバッグが切望されている。
【0004】
【特許文献1】
特開平9−302549号公報
【0005】
【特許文献2】
特開平9−302550号公報
【0006】
【特許文献3】
特開2002−212856号公報
【0007】
【発明が解決しようとする課題】
本発明は、かかる従来のエアバッグの欠点に鑑み、エアバッグとしての機械的特性、空気遮断性、収納コンパクト性を兼ね備え、かつ、裁断時のロスが少なく、コストパフォーマンスに優れたエアバッグ用基布を提供するものである。
【0008】
【課題を解決するための手段】
本発明は、かかる課題を解決するために、次のような手段を採用する。すなわち、
(1)合成繊維からなる織物の少なくとも片面に熱可塑性樹脂が積層されたエアバッグ用基布であって、該基布の中央部の厚みT1と塗工端部の厚みT2との関係が、0.9≦T1/T2であり、かつ、該基布の基布幅Wと樹脂が塗工された塗工幅Cとの関係が0.95≦C/W≦0.99の範囲内にあることを特徴とするエアバッグ用基布。
(2)該基布の中央部の厚みT1と塗工端部の厚みT2との関係が、0.95≦T1/T2であることを特徴とする、(1)に記載のエアバッグ用基布。
(3)JIS L1096 A法に規定される方法で測定した通気度が0.01cc/cm2 /sec以下であることを特徴とする、(1)または(2)のいずれかに記載のエアバッグ用基布。
(4)該熱可塑性樹脂の付着量が5〜30g/m2であることを特徴とする、(1)〜(3)のいずれかに記載のエアバッグ用基布。
(5)(1)〜(4)のいずれかに記載のエアバッグ用基布からなるエアバッグ
(6)合成繊維からなる織物に、熱可塑性樹脂をナイフコーターにより、ナイフと該織物との接圧を1〜15N/cmの範囲内で、かつ、基布張力が500〜3,000N/mの範囲内で塗工することを特徴とするエアバッグ用基布の製造方法。
(7)該織物の精練加工を施さずに該樹脂を塗工することを特徴とする、(6)に記載のエアバッグ用基布の製造方法。
【0009】
【発明の実施の形態】
本発明は、合成繊維からなる織物の少なくとも片面に熱可塑性樹脂が積層されたエアバッグ用基布であって、該基布の中央部の厚みT1と塗工端部の厚みT2との関係が、0.9≦T1/T2であり、かつ、該基布の基布幅Wと樹脂が塗工された塗工幅Cとの関係が0.95≦C/W≦0.99の範囲内にあることを基本とし、これによって、エアバッグとしての機械的特性、空気遮断性、収納コンパクト性を兼ね備え、かつ、裁断時のロスが少なく、コストパフォーマンスを著しく高くすることを達成し、実現したものである。ここで、塗工幅とはコーティング基布としてエアバッグに有効に活用できる基布幅のことをいう。
【0010】
本発明を構成する合成繊維からなる織物としては、ナイロン6・6、ナイロン6、ナイロン12、ナイロン4・6、ナイロン6とナイロン6・6との共重合体、ナイロン6にポリアルキレングリコール、ジカルボン酸やアミンなどを共重合した共重合体等からなるポリアミド繊維、ポリエチレンテレフタレート、ポリブチレンテレフタレートなどのポリエステル繊維、ポリエステルの繰り返し単位を構成する酸成分にイソフタル酸、5−ナトリウムスルホイソフタル酸またはアジピン酸などの脂肪族ジカルボン酸などを共重合した共重合体等からなるポリエステル繊維、パラフェニレンテレフタルアミドおよび芳香族エーテルとの共重合体に代表されるアラミド繊維、レーヨン繊維、サルフォン系繊維、超高分子量ポリエチレン繊維および上記合成繊維を主体とする海島構造を有する高分子配列体繊維から構成される織物が用いられる。これらの織物の中でもポリアミド繊維、ポリエチレンテレフタレート繊維からなる織物が好ましく、さらにはナイロン66繊維、ナイロン6繊維が耐衝撃性の面から好ましい。
【0011】
かかる繊維には、原糸の製造工程や加工工程での生産性あるいは特性改善のために使用される各種添加剤を含んでもよい。たとえば熱安定剤、酸化防止剤、光安定剤、平滑剤、帯電防止剤、可塑剤、増粘剤、顔料、難燃剤などを含有せしめることができる。
【0012】
織物を構成する織糸の繊度は、好ましくは90〜600デシテックスの範囲内、さらに好ましくは150〜470デシテックスの範囲内にあるものが、機械的強度と厚み、重量のバランスから好ましい。すなわち90デシテックス未満では厚み、重量の観点からは好ましいが機械的強度が不足し、600デシテックスを超えると厚み、重量が大きくなり収納性の面で劣る。
【0013】
かかる織糸を構成する繊維の単繊維繊度は、好ましくは1〜6.5デシテックスの範囲内、さらに好ましくは2〜4.5デシテックスの範囲内にあることが収納性、樹脂との接着性の点から良い。1デシテックス未満では糸の生産性が悪化しやすくなるという問題があり、6.5デシテックスを超えると織物が厚くなり、エアバッグ用基布を折り畳むときに基布反発も強く、収納性の面で劣る。
【0014】
また、織糸の単糸断面形状は丸に限らずいずれの形であってもよい。たとえば、扁平、長方形、菱形、繭型のような左右対称型は勿論、左右非対称型でも良く、あるいはそれらの組み合わせ型でも良い。さらに、突起や凹凸、中空糸があっても良い。特に好ましくは断面の長軸と短軸との比、すなわちアスペクト比が1.8〜6の扁平断面糸を用いると基布の厚みを薄くすることができ収納性が向上する面から良い。また、扁平断面糸を用いると織物表面の凹凸が小さくなり、かつ、織物を構成する織り糸間に生じる空隙を小さくすることができ、その空隙を埋めて塗工するには少ない樹脂量で良いので、収納性やコストの面で好ましい。
【0015】
また、織糸は無撚りの方が低塗工の面で好ましい。撚りがかかっていると、マルチフィラメントが収束するため、織物表面の凹凸が増し、樹脂で織物表面の凹凸を埋めるためにはより多くの樹脂量を必要とし、基布重量が大きくなり収納性が悪化するばかりか、樹脂量が多くなるためコストがかかる。
【0016】
本発明の基布を構成する織物を製織する織機は、工業用織物を製織するのに用いられる各種織機から適宜選定すればよく、例えば、シャトル織機、ウォータージェット織機(WJL)、エアージェット織機(AJL)、レピア織機などから選べばよい。そのなかでもエアバッグの難燃性に影響する懸念のある基布の残留油剤を小さくすることや生産性の点で、ウォータージェット織機(WJL)が好ましく用いられる。
【0017】
本発明を構成する織物は、平組織、綾組織、朱子組織及びこれらの変形組織等を使用することができるが、これらに特に限定されるものではない。これらの織組織の中でも、織物コスト及びエアバッグの等方展開性の面から平組織が好ましく使用される。かかる織物としては、対称組織である必然性はなく、非対称組織であってもよい。ここでいう非対称組織としては、例えば、平組織織物でタテ糸とヨコ糸の糸本数が異なるもの、タテ、ヨコの一方の糸種が異なるもの、タテ、ヨコの一方がリップストップや空羽組織になっているもの等の組織が異なるもの等を使用することができる。
【0018】
本発明を構成する織物に積層される熱可塑性樹脂としては、ポリウレタン系、ポリエステル系、ポリアミド系、アクリル系、シリコーン系、フッ素系、ポリエチレン系、スチレンブタジエン系、ニトリルブタジエン系などの合成樹脂の1種以上を用いることができるが、特にこれらに限定されるものではない。また、かかる合成樹脂は、溶剤系、水系、水分散系樹脂のいずれをも適宜使用することができる。 なかでも、シリコーン系樹脂が耐熱性の面から好ましく使用される。
【0019】
本発明における熱可塑性樹脂の付着量は、好ましくは5〜30g/m2の範囲内、より好ましくは8〜20g/m2の範囲内にあるのが、基布の厚さ、重量、空気遮断性、さらに収納性の面から良い。
【0020】
本発明におけるエアバッグ用基布の中央部の厚みT1と塗工端部の厚みT2の関係が、0.9≦T1/T2であり、より好ましくは0.95≦T1/T2である。T1/T2が0.9より小さくなると裁断縫製後のバッグにおいても厚みのばらつきが大きくなり、そのことからバッグを展開させたときに等方的に展開せず、乗員をより速く受け止める高速展開性能が劣る。また、展開時の高温ガスがバッグに不均一にあたるため、バッグが熱による損傷を大きく受ける場合があり良くない。
【0021】
本発明のエアバッグ用基布は、その基布の基布幅Wと樹脂が塗工された塗工幅Cの関係が0.95≦C/W≦0.99であることが好ましい。0.95よりも小さいと、バッグ裁断時のロスが大きく、コストパフォーマンスの面で劣る。0.99よりも大きくなると樹脂塗工後の熱セットで基布の両端を把持する部分が樹脂塗工部となり、皺の原因になり品位面で劣る。
【0022】
本発明のエアバッグ基布の通気度は0.01cc/cm2/sec以下であることが好ましい。かかる通気度に調整することにより、各種部位のエアバッグ設計範囲が広くなり、インフレータブルカーテン、ニーエアバッグ、スマートバッグ等の極めて低い通気度を要求される用途にも好ましく使用することができる。
【0023】
また、本発明のエアバッグ用基布の厚さについては0.35mm以下であることが収納コンパクト性の面から好ましく、剛軟度についてはタテ方向およびヨコ方向ともに100mm以下であることが収納コンパクト性の面から好ましい。また、エアバッグ用基布の引張強力が400N/cm以上、破断伸度が15%以上、引裂強力が80N以上であることがエアバッグとしての機械的特性、つまり破裂防止の点から好ましい。
【0024】
また、本発明のエアバッグ用基布はエアバッグが展開した時にかかる高温ガスが基布に与える熱的損傷などを想定して、FMVSS302に基づいて測定した難燃性が100mm/min未満であることが好ましい。80mm/min未満であればさらに好ましい。
【0025】
本発明のエアバッグ用基布は、運転席用エアバッグ、助手席用エアバッグ、後部座席用エアバッグ、側面用エアバッグ、カーテン用エアバッグ、ニーエアバッグなどに使用することができ、追突保護用のヘッドバッグ、幼児保護用ミニバッグ、脚部保護用バッグ、シートベルト用バッグなど機能的に適用し得る部位にも適用することもでき、形状、容量などは要望される要件を満足するようにすればよい。
【0026】
また、本発明のエアバッグ用基布は、合成繊維からなる織物に、熱可塑性をナイフコーターにより、ナイフと該織物との接圧を1〜15N/cmの範囲内で、かつ、基布張力が500〜3,000N/mの範囲内で塗工することにより製造することができる。ナイフコーターで塗工すると、熱可塑性樹脂の付着量の制御、付着量の安定性が良好となる。塗工時にナイフと織物との接圧を1〜15N/cmの範囲内で行うが、1N/cmより小さいと樹脂量が多く塗工され基布重量が大きく、収納コンパクト性に劣る。また、15N/cmより大きいと織物を構成するマルチフィラメントがナイフで削られて単糸切れをおこす原因となり、品位が劣るばかりか、織物表面を樹脂膜で覆うことができなくなり、低通気性の面で良くない。また、基布張力を500〜3,000N/mの範囲内で塗工することが、塗工時に一時的に織物の耳たぶりを改善し、塗工幅を制御できる点で極めて重要である。基布張力が500N/mより小さいと織物の耳たぶりが改善されず、塗工幅を十分に確保することができない。また、3,000N/mより大きいと織物の幅方向に均一な張力がかからない場合があるばかりか、バッグ作製時の収縮により寸法安定性が劣り良くない。ナイフコーターで塗工する場合の樹脂粘度は5〜20Pa・sの範囲内にあることが好ましい。5Pa・s未満であると粘度が低すぎて、基布内部に樹脂が浸透し低通気性に劣るばかりか、低通気性を達成するためには塗工量が多くなり、収納性の面で良くない。また、20Pa・sより大きくなると粘度が高すぎて、樹脂の塗工量を少なくする(薄く均一に塗工する)ことが困難となり、収納性の面で良くないし、コストもかかる。
【0027】
また、ナイフコーティング法には、ナイフオーバーロール法、ナイフオーバーベルト法、フローティングナイフ法があるが、低塗工量化が可能であるという点からフローティングナイフ法が好ましく用いられる。
【0028】
また、塗工前の精練セット加工は、基布の耳たぶりを軽減させ、塗工をより円滑に行うために実施されるが、本発明においては、基布張力を500〜1,500という高張力で樹脂を塗工するので、耳たぶりを軽減しながら塗工ができる。したがって、精練セット加工を施さず生機あるいは生機セットである織物を用いることが、コストダウンの面から好ましい。
【0029】
【実施例】
次に実施例により、本発明をさらに詳しく説明する。なお、実施例中における各種評価は、下記の方法で測定した。
【0030】
目付(樹脂付着量):JIS L1096(8.4.2法)により求めた。
【0031】
厚み: JIS L1096に基づき測定した。なお、基布の中央部の測定値は基布を幅方向に3分割し、その3分割された真ん中の基布における厚み5点を測定し、その平均値より求めた。また、塗工端部の測定値は塗工された端から基布の内側へ1cm間隔で3点ずつで両端6点の平均値より求めた。
【0032】
引張強力:JIS L1096(8.12.1A法)に基づき、織物幅は3cm、引張つかみ間隔15cm、引張速度200mm/minで引っ張った時の破断強力を測定した。
【0033】
破断伸度:JIS L1096(8.12.1A法)に基づき、織物幅は3cm、引張つかみ間隔15cm、引張速度200mm/minで引っ張った時の破断伸度を測定した。
【0034】
引裂強力:JIS L1096(8.15.2A−2法)に基づき、引張速度200mm/minで引っ張ったときの引裂強力を求めた。
【0035】
剛軟度:JIS L1096(8.19.1A法)により求めた。
【0036】
通気度:JIS L1096 (8.27.1A法)により求めた。
【0037】
難燃性:FMVSS302により求めた。
実施例1、比較例1、2
単糸断面のアスペクト比が1.0であるナイロン66繊維であって、総繊度が470デシテックスで72フィラメントの、強度8.5cN/デシテックス、伸度21%、無撚りの糸を使用してウオータージェットルームでタテ糸とヨコ糸の密度がそれぞれ55本/2.54cmの平織物を製織し、190℃で1分間ヒートセットした。該ヒートセット後の織物を、粘度が15Pa・sの無溶剤系メチルビニルシリコーン樹脂液を用いて次の方法でコーティングした。
(実施例1)せき板ナイフを用いたフローティングナイフコーターにて、ナイフと織物との接圧を10N/m、基布張力を2620N/mに調整しコーティングを行った後、190℃で2分間加硫処理を行い、基布幅が152cmのエアバッグ用基布を得た。
(比較例1)ナイフと織物との接圧を0.6N/mとした以外は、実施例1と同様に処理し、基布幅が152cmのエアバッグ用基布を得た。
(比較例2)基布張力を300N/mとした以外は、実施例1と同様に処理し、エアバッグ用基布を得た。
【0038】
このようにして得られたエアバッグ用基布の特性を表1に示した。実施例1のエアバッグ用基布は、基布幅が152cm、塗工幅が148cm(C/W=0.97)であり、かつ基布の中央部の厚みT1と塗工端部との厚みT2との関係がT1/T2=0.97であったが、比較例1のエアバッグ用基布は、接圧が小さいため、塗工幅が139cmとなり(C/W=0.91)、十分な塗工幅を確保できなかった。また、比較例2のエアバッグ用基布は、塗工時の基布張力が非常に小さいため、基布端部の耳フレアが改善されないまま塗工されたことにより、T1/T2=0.88となり、かつ、基布幅が152cm、塗工幅も142cmとなり(C/W=0.93)、十分な塗工幅を確保できなかった。さらに、塗工端部の1.5cm幅は樹脂量が多く除去しなければならず、塗工幅より小さい有効利用幅となった。実施例1によるものは、十分な塗工幅を確保した経済性に優れたエアバッグ用基布であることがわかる。
【0039】
実施例2、比較例3、4
単糸断面のアスペクト比が3.2であるナイロン66繊維であって、総繊度が350デシテックスで96フィラメントの強度8.0cN/デシテックス、伸度24%、無撚りの糸を使用してウオータージェットルームでタテ糸とヨコ糸の密度がそれぞれ61本/2.54cmの平織物を製織し、190℃で1分間ヒートセットした。ヒートセット後の織物を、粘度が16Pa・sの無溶剤系メチルビニルシリコーン樹脂液を用いて次の方法でコーティングした。
(実施例2)せき板ナイフを用いたフローティングナイフコーターにて、ナイフと織物との接圧を12N/m、基布張力を520N/mになるようにコーティングを行った後、190℃で2分間加硫処理を行い、エアバッグ用基布を得た。
(比較例3)ナイフと織物との接圧を17N/mとした以外は、実施例2と同様に処理し、エアバッグ用基布を得た。
(比較例4)基布張力を3200N/mとした以外は、実施例2と同様に処理し、エアバッグ用基布を得た。
【0040】
このようにして得られたエアバッグ用基布の特性を表1に示した。実施例2のエアバッグ用基布は、基布幅が154cm、塗工幅が148cm(C/W=0.96)であり、かつ基布の中央部の厚みT1と塗工端部との厚みT2との関係がT1/T2=0.96であったが、比較例3のエアバッグ用基布は、接圧が大きいため、織物表面を樹脂膜で十分に覆うことができなくなり、塗工幅が確保できないばかりか、エアバッグとして必要な通気度、難燃性をクリアできない。また、比較例4のエアバッグ用基布は、塗工時の基布張力が非常に大きいため、基布の幅方向において均一な張力がかからず、塗工幅が十分確保できなかった。実施例2は、比較例に比べエアバッグとしての機械的特性に優れかつ、十分な塗工幅を確保した経済性に優れたエアバッグ用基布であることがわかる。
【0041】
【表1】

Figure 2004204404
【0042】
【発明の効果】本発明によれば、エアバッグとしての機械的特性、空気遮断性、収納コンパクト性を兼ね備え、かつ、裁断時のロスが少なく、コストパフォーマンスに優れたエアバッグ用基布を提供するものことができ、エアバッグ乗員保護システムを普及推進させることができる。[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to an airbag base fabric in which a resin is laminated, and more particularly, to improve the thickness difference of a base fabric in which a resin is laminated on a woven fabric, and to reduce the thickness of the ear end portion of the woven fabric by using ear fins. The present invention relates to a base fabric for an airbag, an airbag, and a method for manufacturing the airbag, which has a reduced coating width and is excellent in economy.
[0002]
[Prior art]
Conventionally, for the purpose of imparting functions such as heat resistance, flame retardancy, and air blocking properties to an airbag, chloroprene is added to a woven fabric made of a filament yarn such as nylon 66, nylon 6, or polyester of 100 to 900 dtex. It is common practice to apply a synthetic resin such as silicone or urethane. In general, a knife coater or a comma coater is used for applying such a synthetic resin. The knife coater or the comma coater is used to maintain the function of the above-mentioned airbag, and to coat the resin less uniformly for the purpose of compactness and cost reduction. Is required. However, at present, a high-density woven fabric having a cover factor in the range of 1,400 to 2,300, such as an airbag base cloth, has a problem of ear pallet occurring at the time of weaving. Wrinkles occur at the edges of the woven fabric due to the ears of the parts, so that the resin cannot be applied, and the width of the woven fabric that can be actually used as an airbag is about 90% of the woven width, resulting in loss of the woven fabric.
[0003]
Therefore, in recent years, in order to solve such a problem, the weaving density of the ear end is made higher than that of the other main body base cloth, and the ear lashing which is characterized by the fact that the additional yarn is driven into the ear end is improved. Although a method of performing the above is disclosed (for example, see Patent Documents 1 and 2), it is not sufficient. Further, a method has been disclosed in which two yarns thinner than a ground yarn different from a reno texture are entangled in the ear portion and two ground yarns are alternately inserted as a unit of a yarn to improve ear cling (for example, Patent Document 3). ), The number of processes increases and the cost increases, which is not sufficient. Economic demands such as cost reduction are also increasing for airbags as safety parts, and there is a strong demand for economical airbags with little production loss.
[0004]
[Patent Document 1]
JP-A-9-302549
[Patent Document 2]
JP-A-9-302550
[Patent Document 3]
JP, 2002-212856, A
[Problems to be solved by the invention]
In view of the drawbacks of the conventional airbag, the present invention provides an airbag base having both the mechanical characteristics as an airbag, the air-blocking property, and the compactness of storage, and the loss at the time of cutting is small and excellent in cost performance. Provide cloth.
[0008]
[Means for Solving the Problems]
The present invention employs the following means in order to solve such a problem. That is,
(1) A base fabric for an airbag in which a thermoplastic resin is laminated on at least one surface of a woven fabric made of synthetic fibers, wherein a relationship between a thickness T1 of a central portion of the base fabric and a thickness T2 of a coated end portion is as follows. 0.9 ≦ T1 / T2, and the relationship between the base cloth width W of the base cloth and the coating width C on which the resin is applied is within the range of 0.95 ≦ C / W ≦ 0.99. A base fabric for an airbag, comprising:
(2) The base for an airbag according to (1), wherein the relationship between the thickness T1 of the central portion of the base fabric and the thickness T2 of the coated end portion is 0.95 ≦ T1 / T2. cloth.
(3) The airbag according to any one of (1) and (2), wherein the air permeability measured by a method specified in JIS L1096 A method is 0.01 cc / cm 2 / sec or less. Base cloth.
(4) The base fabric for an airbag according to any one of (1) to (3), wherein the thermoplastic resin has an adhesion amount of 5 to 30 g / m 2 .
(5) An airbag comprising the base fabric for an airbag according to any one of (1) to (4). (6) A thermoplastic resin is applied to a woven fabric made of synthetic fiber using a knife coater to connect the knife to the woven fabric. A method for producing a base fabric for an airbag, wherein the coating is performed at a pressure within a range of 1 to 15 N / cm and a base fabric tension within a range of 500 to 3,000 N / m.
(7) The method for producing a base fabric for an airbag according to (6), wherein the resin is applied without performing a scouring process on the woven fabric.
[0009]
BEST MODE FOR CARRYING OUT THE INVENTION
The present invention relates to an airbag base fabric in which a thermoplastic resin is laminated on at least one surface of a woven fabric made of synthetic fibers, wherein the relationship between the thickness T1 of the central portion of the base fabric and the thickness T2 of the coated end portion is defined. , 0.9 ≦ T1 / T2, and the relationship between the base cloth width W of the base cloth and the coating width C on which the resin is applied is in the range of 0.95 ≦ C / W ≦ 0.99. As a result, the combination of mechanical characteristics as an airbag, air-blocking properties, and compactness of storage is achieved, and the loss at the time of cutting is reduced, resulting in significantly improved cost performance. Things. Here, the coating width refers to a base cloth width which can be effectively used as a coating base cloth for an airbag.
[0010]
Examples of the woven fabric made of the synthetic fibers constituting the present invention include nylon 6.6, nylon 6, nylon 12, nylon 4.6, a copolymer of nylon 6 and nylon 6.6, and nylon 6 with polyalkylene glycol and dicarboxylic acid. Polyamide fibers such as copolymers obtained by copolymerizing acids and amines, polyester fibers such as polyethylene terephthalate and polybutylene terephthalate, and isophthalic acid, 5-sodium sulfoisophthalic acid or adipic acid as acid components constituting repeating units of polyester. Polyester fibers such as copolymers obtained by copolymerizing aliphatic dicarboxylic acids, etc., aramid fibers represented by copolymers with paraphenylene terephthalamide and aromatic ethers, rayon fibers, sulfone fibers, ultrahigh molecular weight Polyethylene fiber and top Fabric composed of synthetic fibers from a polymer array fiber having a sea-island structure mainly is used. Among these woven fabrics, woven fabrics composed of polyamide fibers and polyethylene terephthalate fibers are preferable, and nylon 66 fibers and nylon 6 fibers are more preferable in terms of impact resistance.
[0011]
Such fibers may contain various additives used for improving productivity or characteristics in the production or processing steps of the raw yarn. For example, a heat stabilizer, an antioxidant, a light stabilizer, a leveling agent, an antistatic agent, a plasticizer, a thickener, a pigment, a flame retardant and the like can be contained.
[0012]
The fineness of the woven yarn constituting the woven fabric is preferably in the range of 90 to 600 dtex, more preferably in the range of 150 to 470 dtex, from the viewpoint of the balance between mechanical strength, thickness and weight. That is, a thickness of less than 90 dtex is preferable from the viewpoint of thickness and weight, but the mechanical strength is insufficient, and a thickness of more than 600 dtex increases the thickness and weight and is inferior in terms of storage.
[0013]
The single-fiber fineness of the fibers constituting the woven yarn is preferably in the range of 1 to 6.5 dtex, more preferably in the range of 2 to 4.5 dtex, and the storability and the adhesiveness to the resin are preferable. Good from the point. If it is less than 1 dtex, there is a problem that the productivity of the yarn is liable to deteriorate. If it exceeds 6.5 dtex, the fabric becomes thick, and when the base fabric for airbags is folded, the base fabric rebound is strong, and in terms of storability. Inferior.
[0014]
Further, the cross-sectional shape of the single yarn of the woven yarn is not limited to a circle, but may be any shape. For example, a symmetrical type such as a flat, rectangular, diamond-shaped, or cocoon-shaped type, as well as a bilaterally asymmetric type, or a combination thereof may be used. Further, there may be protrusions, irregularities, and hollow fibers. It is particularly preferable to use a flat cross-section yarn having a ratio between the long axis and the short axis of the cross section, that is, an aspect ratio of 1.8 to 6, since the thickness of the base fabric can be reduced and the storage property is improved. In addition, the use of a flat cross-section yarn reduces irregularities on the surface of the woven fabric, and can reduce voids generated between the woven yarns constituting the woven fabric, so that a small amount of resin is sufficient to fill and apply the voids. This is preferable in terms of storability and cost.
[0015]
In addition, the woven yarn is preferably non-twisted in terms of low coating. If twisting occurs, the multifilaments converge, so the unevenness of the fabric surface increases, and more resin is required to fill the unevenness of the fabric surface with the resin, the base fabric weight increases, and the storage capacity increases. Not only does it worsen, but the cost increases because the amount of resin increases.
[0016]
The loom for weaving the fabric constituting the base fabric of the present invention may be appropriately selected from various looms used for weaving industrial fabrics. For example, a shuttle loom, a water jet loom (WJL), an air jet loom ( AJL), rapier looms and the like. Among them, a water jet loom (WJL) is preferably used from the viewpoint of reducing the residual oil agent of the base fabric which may affect the flame retardancy of the airbag and productivity.
[0017]
As the woven fabric constituting the present invention, a flat texture, a twill texture, a satin texture, a deformed texture thereof, and the like can be used, but the fabric is not particularly limited thereto. Among these woven structures, a flat structure is preferably used from the viewpoint of the fabric cost and the isostatic deployability of the airbag. Such a fabric does not necessarily need to have a symmetrical structure, and may have an asymmetrical structure. Examples of the asymmetrical design used here include a flat-textile woven fabric having a different number of warp yarns and weft yarns, a warp yarn and a weft yarn having a different yarn type, and a warp yarn or a weft fabric having one of a ripstop or hollow fabric. It is possible to use one having a different organization, such as the one shown in FIG.
[0018]
Examples of the thermoplastic resin laminated on the fabric constituting the present invention include one of synthetic resins such as polyurethane, polyester, polyamide, acrylic, silicone, fluorine, polyethylene, styrene butadiene, and nitrile butadiene. More than one kind can be used, but it is not particularly limited to these. As the synthetic resin, any of a solvent-based resin, an aqueous resin, and a water-dispersed resin can be used as appropriate. Among them, silicone resins are preferably used from the viewpoint of heat resistance.
[0019]
The adhesion amount of the thermoplastic resin in the present invention is preferably in the range of 5 to 30 g / m 2 , and more preferably in the range of 8 to 20 g / m 2. It is good in terms of properties and storage.
[0020]
In the present invention, the relationship between the thickness T1 of the central portion of the base fabric for an airbag and the thickness T2 of the coated end portion is 0.9 ≦ T1 / T2, and more preferably 0.95 ≦ T1 / T2. If T1 / T2 is smaller than 0.9, the thickness of the bag after cutting and sewing will vary greatly, and as a result, the bag will not expand isotropically when the bag is deployed, and will quickly catch the occupant faster. Is inferior. In addition, since the hot gas at the time of deployment hits the bag unevenly, the bag may be greatly damaged by heat, which is not good.
[0021]
In the base fabric for an airbag of the present invention, the relation between the base fabric width W of the base fabric and the coating width C on which the resin is applied is preferably 0.95 ≦ C / W ≦ 0.99. When it is smaller than 0.95, the loss at the time of cutting the bag is large, and the cost performance is inferior. If it is larger than 0.99, the portion holding both ends of the base fabric in the heat setting after resin coating becomes a resin coated portion, which causes wrinkles and is inferior in quality.
[0022]
The air permeability of the airbag base fabric of the present invention is preferably 0.01 cc / cm 2 / sec or less. By adjusting to such air permeability, the design range of airbags in various parts is widened, and the airbag can be preferably used for applications requiring extremely low air permeability, such as inflatable curtains, knee airbags, and smart bags.
[0023]
The thickness of the base fabric for an airbag of the present invention is preferably 0.35 mm or less from the viewpoint of compactness in storage, and the rigidity is preferably 100 mm or less in both the vertical and horizontal directions. It is preferable in terms of properties. Further, it is preferable that the tensile strength of the base fabric for an airbag is 400 N / cm or more, the breaking elongation is 15% or more, and the tear strength is 80 N or more from the viewpoint of mechanical properties as an airbag, that is, from the viewpoint of preventing rupture.
[0024]
In addition, the airbag fabric of the present invention has a flame retardancy of less than 100 mm / min measured based on FMVSS302, assuming thermal damage to the fabric caused by the high temperature gas when the airbag is deployed. Is preferred. It is more preferable that the speed is less than 80 mm / min.
[0025]
The base fabric for an airbag of the present invention can be used for a driver seat airbag, a passenger seat airbag, a rear seat airbag, a side airbag, a curtain airbag, a knee airbag, and the like. It can also be applied to functionally applicable parts such as protective head bags, infant protective mini bags, leg protective bags, seat belt bags, etc., satisfying the required requirements in shape, capacity, etc. What should I do?
[0026]
Further, the airbag fabric of the present invention is characterized in that the fabric made of synthetic fiber is thermoplastically coated with a knife coater so that the contact pressure between the knife and the fabric is within a range of 1 to 15 N / cm, and the fabric tension. Can be produced by coating within the range of 500 to 3,000 N / m. When the coating is performed with a knife coater, the control of the attached amount of the thermoplastic resin and the stability of the attached amount are improved. At the time of coating, the contact pressure between the knife and the woven fabric is performed within a range of 1 to 15 N / cm. If it is smaller than 1 N / cm, the amount of resin is large, the weight of the base fabric is large, and the storage compactness is poor. On the other hand, if it is larger than 15 N / cm, the multifilaments constituting the woven fabric may be cut with a knife to cause breakage of the single yarn, and the quality is not only poor, but also the woven fabric surface cannot be covered with the resin film, and the air permeability is low. Not good in terms of aspect. Further, it is extremely important to apply the base fabric tension within the range of 500 to 3,000 N / m in that the ear-tapping of the woven fabric can be temporarily improved during the application and the application width can be controlled. If the base fabric tension is less than 500 N / m, the ear pallets of the woven fabric are not improved, and the coating width cannot be sufficiently secured. On the other hand, if it is larger than 3,000 N / m, not only a uniform tension may not be applied in the width direction of the woven fabric, but also dimensional stability is inferior due to shrinkage during bag production. The resin viscosity when applying with a knife coater is preferably in the range of 5 to 20 Pa · s. When the viscosity is less than 5 Pa · s, the viscosity is too low, and the resin penetrates into the base fabric, so that not only is the air permeability inferior, but also the amount of coating is large in order to achieve the low air permeability. Not good. On the other hand, if it is larger than 20 Pa · s, the viscosity is too high, so that it is difficult to reduce the amount of resin to be applied (coating thinly and uniformly), which is not good in terms of storability and costly.
[0027]
As the knife coating method, there are a knife over roll method, a knife over belt method, and a floating knife method, but the floating knife method is preferably used because the coating amount can be reduced.
[0028]
In addition, the scouring and setting process before coating is performed to reduce the ears of the base cloth and perform the coating more smoothly. In the present invention, the base cloth tension is as high as 500 to 1,500. Because the resin is applied with tension, it is possible to apply while reducing the earlashes. Therefore, it is preferable to use a greige machine or a woven fabric that is a greige machine set without performing the scouring setting process from the viewpoint of cost reduction.
[0029]
【Example】
Next, the present invention will be described in more detail with reference to examples. Various evaluations in the examples were measured by the following methods.
[0030]
Weight per unit area (resin adhesion amount): Determined according to JIS L1096 (8.4.2 method).
[0031]
Thickness: Measured according to JIS L1096. In addition, the measured value of the central part of the base cloth was obtained by dividing the base cloth into three in the width direction, measuring five points of the thickness of the middle part of the divided base cloth, and calculating the average value thereof. The measured value of the coated end was obtained from the average value of 6 points at both ends at three points at 1 cm intervals from the coated end to the inside of the base cloth.
[0032]
Tensile strength: Based on JIS L1096 (8.12.1A method), the breaking strength at the time of pulling at a woven fabric width of 3 cm, a tension grip interval of 15 cm, and a pulling speed of 200 mm / min was measured.
[0033]
Breaking elongation: Based on JIS L1096 (8.12.1A method), the breaking elongation at the time of pulling at a fabric width of 3 cm, a tension gripping interval of 15 cm, and a pulling speed of 200 mm / min was measured.
[0034]
Tear strength: Based on JIS L1096 (8.15.2A-2 method), the tear strength when pulled at a tensile speed of 200 mm / min was determined.
[0035]
Bending resistance: determined according to JIS L1096 (8.19.1A method).
[0036]
Air permeability: determined according to JIS L1096 (8.27.1A method).
[0037]
Flame retardancy: determined by FMVSS302.
Example 1, Comparative Examples 1 and 2
A nylon 66 fiber having an aspect ratio of a single yarn cross section of 1.0, a total fineness of 470 dtex and 72 filaments, a strength of 8.5 cN / decite, an elongation of 21%, and a water-free yarn. In a jet loom, a plain woven fabric having a warp yarn and a weft yarn density of 55 / 2.54 cm, respectively, was woven and heat set at 190 ° C. for 1 minute. The heat-set fabric was coated with a solvent-free methyl vinyl silicone resin solution having a viscosity of 15 Pa · s by the following method.
(Example 1) Coating was performed by adjusting the contact pressure between the knife and the fabric to 10 N / m and the base fabric tension to 2620 N / m using a floating knife coater using a weir plate knife, and then at 190 ° C. for 2 minutes. A vulcanization treatment was performed to obtain a base fabric for an airbag having a base fabric width of 152 cm.
(Comparative Example 1) The same treatment as in Example 1 was carried out except that the contact pressure between the knife and the fabric was 0.6 N / m, to obtain a base fabric for an airbag having a base fabric width of 152 cm.
(Comparative Example 2) Except that the base fabric tension was set to 300 N / m, the same treatment as in Example 1 was performed to obtain a base fabric for an airbag.
[0038]
Table 1 shows the characteristics of the airbag base fabric thus obtained. The base fabric for an airbag of Example 1 has a base fabric width of 152 cm, a coating width of 148 cm (C / W = 0.97), and a thickness T1 of a central portion of the base fabric and a coating end portion. Although the relationship with the thickness T2 was T1 / T2 = 0.97, the coating width of the airbag base fabric of Comparative Example 1 was 139 cm because the contact pressure was small (C / W = 0.91). , A sufficient coating width could not be secured. In addition, the base fabric for an airbag of Comparative Example 2 had a very small base fabric tension at the time of coating, and was applied without improving the ear flare at the end of the base fabric, so that T1 / T2 = 0. 88, the base cloth width was 152 cm, and the coating width was 142 cm (C / W = 0.93), and a sufficient coating width could not be secured. In addition, the 1.5 cm width at the coating end had to be removed because of the large amount of resin, resulting in an effective use width smaller than the coating width. It can be seen that the airbag according to Example 1 is a base fabric for an airbag which ensures a sufficient coating width and is excellent in economy.
[0039]
Example 2, Comparative Examples 3 and 4
Water jet using a non-twisted yarn, a nylon 66 fiber having an aspect ratio of 3.2 of a single yarn cross section and a total fineness of 350 dtex, a 96 filament strength of 8.0 cN / decite, an elongation of 24%, and no twist. In the room, a plain woven fabric having a warp yarn and a weft yarn with a density of 61 / 2.54 cm, respectively, was woven and heat set at 190 ° C. for 1 minute. The heat-set fabric was coated with a solvent-free methyl vinyl silicone resin solution having a viscosity of 16 Pa · s by the following method.
(Example 2) After coating with a floating knife coater using a weir plate knife so that the contact pressure between the knife and the fabric is 12 N / m and the base fabric tension is 520 N / m, the coating is performed at 190 ° C for 2 hours. Vulcanization treatment was performed for a minute to obtain a base fabric for an airbag.
(Comparative Example 3) The same treatment as in Example 2 was carried out except that the contact pressure between the knife and the fabric was set at 17 N / m, to obtain a base fabric for an airbag.
(Comparative Example 4) Except that the base fabric tension was set to 3200 N / m, the same treatment as in Example 2 was performed to obtain a base fabric for an airbag.
[0040]
Table 1 shows the characteristics of the airbag base fabric thus obtained. The base fabric for an airbag of Example 2 had a base fabric width of 154 cm, a coating width of 148 cm (C / W = 0.96), and a thickness T1 of a central portion of the base fabric and a coating end portion. Although the relationship with the thickness T2 was T1 / T2 = 0.96, the base fabric for an airbag of Comparative Example 3 had a large contact pressure, so that the fabric surface could not be sufficiently covered with the resin film, and Not only can the working width not be secured, but the air permeability and flame retardancy required for an airbag cannot be cleared. In the base fabric for an airbag of Comparative Example 4, since the base fabric tension at the time of coating was very large, uniform tension was not applied in the width direction of the base fabric, and a sufficient coating width could not be secured. It can be seen that Example 2 is a base fabric for an airbag which is more excellent in mechanical properties as an airbag than the comparative example, and which has a sufficient coating width and which is excellent in economy.
[0041]
[Table 1]
Figure 2004204404
[0042]
According to the present invention, there is provided an airbag base fabric which has both mechanical properties as an airbag, air blocking properties, and compactness in storage, has little loss at the time of cutting, and is excellent in cost performance. Can promote the spread of the airbag occupant protection system.

Claims (7)

合成繊維からなる織物の少なくとも片面に熱可塑性樹脂が積層されたエアバッグ用基布であって、該基布の中央部の厚みT1と塗工端部の厚みT2との関係が、0.9≦T1/T2であり、かつ、該基布の基布幅Wと樹脂が塗工された塗工幅Cとの関係が0.95≦C/W≦0.99の範囲内にあることを特徴とするエアバッグ用基布。An airbag base fabric in which a thermoplastic resin is laminated on at least one surface of a woven fabric made of synthetic fibers, wherein a relationship between a thickness T1 of a central portion of the base fabric and a thickness T2 of a coated end portion is 0.9. ≦ T1 / T2, and the relationship between the base cloth width W of the base cloth and the coating width C on which the resin is applied is within a range of 0.95 ≦ C / W ≦ 0.99. Characteristic airbag fabric. 該基布の中央部の厚みT1と塗工端部の厚みT2との関係が、0.95≦T1/T2であることを特徴とする、請求項1に記載のエアバッグ用基布。2. The airbag base fabric according to claim 1, wherein a relationship between a thickness T <b> 1 of a central portion of the base fabric and a thickness T <b> 2 of a coated end portion is 0.95 ≦ T1 / T2. 3. JIS L1096 A法に規定される方法で測定した通気度が0.01cc/cm2 /sec以下であることを特徴とする、請求項1または2のいずれかに記載のエアバッグ用基布。And wherein the air permeability measured by the method specified in JIS L1096 A method is less than 0.01cc / cm 2 / sec, an airbag fabric of any of claims 1 or 2. 該熱可塑性樹脂の付着量が5〜30g/m2であることを特徴とする、請求項1〜3のいずれかに記載のエアバッグ用基布。Heat adhesion amount of thermoplastic resin is characterized by a 5 to 30 g / m 2, an airbag fabric according to any one of claims 1 to 3. 請求項1〜4のいずれかに記載のエアバッグ用基布からなるエアバッグ。An airbag comprising the base fabric for an airbag according to claim 1. 合成繊維からなる織物に、熱可塑性樹脂をナイフコーターにより、ナイフと該織物との接圧を1〜15N/cmの範囲内で、かつ、基布張力が500〜3,000N/mの範囲内で塗工することを特徴とするエアバッグ用基布の製造方法。A thermoplastic resin is applied to a woven fabric made of synthetic fibers by a knife coater so that the knife and the woven fabric have a contact pressure of 1 to 15 N / cm and a base fabric tension of 500 to 3,000 N / m. A method for producing a base fabric for an airbag, wherein the base fabric is applied by a coating method. 該織物の精練加工を施さずに該樹脂を塗工することを特徴とする、請求項6に記載のエアバッグ用基布の製造方法。The method for producing a base fabric for an airbag according to claim 6, wherein the resin is applied without performing scouring of the woven fabric.
JP2002376972A 2002-10-04 2002-12-26 Airbag base fabric and airbag Expired - Lifetime JP4423853B2 (en)

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CA 2501032 CA2501032C (en) 2002-10-04 2003-10-03 Coated base fabric for air bags and air bags
EP20030751321 EP1548180B1 (en) 2002-10-04 2003-10-03 Coated base fabric for air bags and air bags
PCT/JP2003/012707 WO2004031472A1 (en) 2002-10-04 2003-10-03 Coated base fabric for air bags and air bags
US10/529,848 US8211813B2 (en) 2002-10-04 2003-10-03 Coated base fabric for air bags and air bags
TW92127372A TWI241965B (en) 2002-10-04 2003-10-03 Coated air bag bottom and air bag
KR1020057005833A KR100680564B1 (en) 2002-10-04 2003-10-03 Coated base fabric for air bags and air bags

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JP2009035834A (en) * 2007-08-01 2009-02-19 Asahi Kasei Chemicals Corp Method for producing base fabric for airbag
JP2012158850A (en) * 2011-02-01 2012-08-23 Asahi Kasei Fibers Corp Woven fabric for airbag
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JP2014514470A (en) * 2011-03-31 2014-06-19 コーロン インダストリーズ インク Expandable double fabric by gas and method for producing the same
JP5679076B2 (en) * 2012-09-27 2015-03-04 東レ株式会社 Woven fabric and its manufacturing method
JPWO2015151358A1 (en) * 2014-03-31 2017-04-13 東洋紡株式会社 Aircraft coat base fabric
JP2018172103A (en) * 2017-03-31 2018-11-08 豊田合成株式会社 Heat-resistant reinforcement fabric for airbag
WO2019017273A1 (en) 2017-07-19 2019-01-24 帝人フロンティア株式会社 Woven fabric for airbags

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