JP3462914B2 - Thread for airbag - Google Patents

Thread for airbag

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Publication number
JP3462914B2
JP3462914B2 JP27085694A JP27085694A JP3462914B2 JP 3462914 B2 JP3462914 B2 JP 3462914B2 JP 27085694 A JP27085694 A JP 27085694A JP 27085694 A JP27085694 A JP 27085694A JP 3462914 B2 JP3462914 B2 JP 3462914B2
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JP
Japan
Prior art keywords
yarn
airbag
fiber
sheath
core
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 - Fee Related
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JP27085694A
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Japanese (ja)
Other versions
JPH08134721A (en
Inventor
和典 橋本
幸治 角本
等 内田
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Unitika Ltd
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Unitika Ltd
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Publication of JPH08134721A publication Critical patent/JPH08134721A/en
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Description

【発明の詳細な説明】 【0001】 【産業上の利用分野】本発明は、機械的特性と柔軟性に
優れたエアバッグ基布を得ることできる、エアバッグ用
糸条に関するものである。 【0002】 【従来の技術】自動車の安全装置として用いられるエア
バッグは、現在、ナイロン66を用いた合成繊維織物に
ゴム類を被覆した基布により形成されたものが主流であ
る。 【0003】エアバッグは衝撃吸収性とともに、通常、
非常に小さな場所に収納するために、柔軟性にも優れて
いることが要求される。 【0004】しかしながら、この合成繊維織物にゴム類
を被覆した基布は、ゴム類の被覆によって、耐熱性や気
密性を向上させることはできるが、基布が硬くなるた
め、収納性が悪いという問題がある。 【0005】この問題を解決し、製造コストを下げる目
的で、最近では、ゴムを被覆しないノンコートタイプの
エアバッグの開発が進められており、素材もナイロン6
6より安価で耐熱性のよいポリエステルを使用すること
が検討されている。 【0006】しかしながら、ポリエステルはナイロン6
6と比較して弾性率が高いため、製織して基布にする
と、柔軟性に欠けるという欠点があり、特に、気密性を
上げるために高密度に織ると、コンパクトに収納するこ
とがより困難になるという問題が生じる。 【0007】特開平3-167312号公報には、エアバッグ用
ポリエステル繊維として、タフネス、結節強度の向上し
た繊維が提案されており、この繊維より得られるエアバ
ッグ基布は、耐衝撃性や耐久性に優れ、基布の平坦性も
改善されたものである。 【0008】しかしながら、この繊維より得られる基布
は、柔軟性が十分でなく、特に気密性を上げるために高
密度に織ると、収納性に劣るものとなるという欠点があ
った。 【0009】このように、強度や耐久性を保持したうえ
でポリエステル糸条に柔軟性を付与することは容易では
なく、強度や耐久性に優れると同時に柔軟なエアバッグ
基布を得ることのできるポリエステル糸条は未だ開発さ
れていない。 【0010】 【発明が解決しようとする課題】本発明は、上記のよう
な問題点を解決し、エアバッグ基布として必要な機械的
特性と柔軟性を同時に有する基布を得ることのできるエ
アバッグ用糸条を提供することを技術的な課題とするも
のである。 【0011】 【課題を解決する手段】本発明者らは、上記の課題を解
決するために鋭意検討した結果、本発明に到達した。 【0012】すなわち、本発明は、芯成分が固有粘度が
0.8 以上のポリエチレンテレフタレート、鞘成分がポリ
エチレンテレフタレートとポリブチレンテレフタレート
が85/15〜90/10のモル比率で共重合された共重合体よ
り構成され、芯/鞘比率が重量比で50/50〜70/30の芯
鞘構造の繊維からなる糸条であって、単糸繊度が1〜3
d、総繊度が200 〜500 d、引張強度が8〜8.8g/
破断伸度が15〜17.6%、曲げ剛性が(1)式の範囲
にあることを特徴とするエアバッグ用糸条。 (1) B≦ 5.5×10-6×TD B :曲げ剛性(g・cm2/糸条) TD:総繊度(d) 【0013】(1) B≦ 5.5×10-6×TD B :曲げ剛性(g・cm2 /糸条) TD:総繊度(d) 以下、本発明について詳細に説明する。 【0014】本発明のエアバッグ用糸条は、芯鞘構造の
複合繊維からなるものであり、芯成分はポリエチレンテ
レフタレート(PET)、鞘成分はPETとポリブチレ
ンテレフタレート(PBT)の共重合体よりなるもので
ある。 【0015】ポリエステル本来の性質を損なわない程度
において、PETに耐熱剤、難燃剤、艶消剤等の第3成
分が混合されていてもよい。 【0016】まず、繊維の芯成分は、固有粘度が0.8 以
上のPETとする。ここで、固有粘度は、フェノールと
テトラクロロエタンの等重量混合溶剤を用いて、20℃で
測定した値である。固有粘度が0.8 未満であると、強度
や耐久性に劣った繊維となり、好ましくない。また、固
有粘度の上限は特に限定されるものではないが、操業性
よく紡糸するためには、固有粘度の範囲を0.8 〜1.1 と
することが好ましい。鞘成分は、PETとPBTが85/
15〜90/10のモル比率で共重合された共重合体よりなる
ものであり、共重合体の固有粘度は0.7 〜0.85の範囲が
好ましい。 【0017】鞘成分をこのように、PETとPBTから
なる共重合体とすることで、繊維の表層は、PETを成
分とする内層より柔軟になり、繊維を曲げたときの、内
側の圧縮に要するエネルギーが小さく、曲げ剛性が小さ
くなり、一方、繊維の内層は、高度に配向しているの
で、繊維軸方向に強度の高い繊維とすることができる。
鞘成分のPETとPBTの共重合比率は、85/15〜90/
10のモル比率とする必要があるが、この範囲よりPET
が多い場合、繊維の柔軟性が十分に発現されず、曲げ剛
性が大きくなり、PBTが多い場合、強度や耐久性が不
足する繊維となる。 【0018】芯成分と鞘成分の比率は重量比で50/50〜
70/30の範囲とする必要がある。芯成分がこの範囲より
多いと、曲げ剛性が大きい繊維となり、鞘成分がこの範
囲より多いと、強度や耐久性が不足するものとなる。 【0019】単糸繊度については、1〜3dとすること
が必要である。単糸繊度が3dより大きいと、繊維の曲
げ剛性が大きくなり、得られる布帛が柔軟なものとなら
ず、一方、1dより小さいと強度に劣り、また、芯、鞘
成分が剥離しやすくなるため、耐疲労性も悪い繊維とな
る。 【0020】総繊度は200 〜 500dの範囲のものとする
必要がある。総繊度が 500dより大きいと、高密度に織
る場合、柔軟性に欠けた基布となり、 200dより小さい
と、引裂強力の弱い基布となる。 【0021】糸条の曲げ剛性は、単糸繊度とフィラメン
ト数により値が変わるが、本発明では、製編織した布帛
に十分な柔軟性を付与するために、(1)式を満足させ
る必要がある。 【0022】さらに、引張強度は8〜8.8g/d、破断
伸度は15〜17.6%の糸条とすることが必要である。引張
強度が8g/dより小さいと、引裂強力の弱い基布とな
り、破断伸度が15%より小さいと、エアバッグ作動時の
衝撃に耐える耐衝撃性を有した基布を得ることができな
い。 【0023】次に、本発明のエアバッグ用糸条の製法例
について説明する。 【0024】まず、通常のエクストルーダー型の複合紡
糸機を用い、紡糸温度を295 〜305℃の範囲で紡糸し、
紡出直後の糸条を、雰囲気温度が300 ℃以上の加熱ゾー
ンを通過させた後、糸条の外周から中心に向かって冷却
風を吹き付けて冷却し、冷却固化直後に油剤を付与して
集束する。 【0025】集束した糸条を引き取った後、延伸を施し
て、引張強度が8〜8.8g/dの糸条を得るが、延伸工
程は、生産性をよくするため、紡糸に引き続き連続して
行うことが好ましいので、引取速度を400〜600m/分の
範囲とし、延伸時に繊維表層にかかる応力を低減できる
ように、加熱温度が200℃以上の加熱水蒸気を吹き付け
たり、ヒートプレート等を使用して加熱しながら、延伸
倍率4.5〜5.5倍で延伸する。 【0026】 【実施例】次に、本発明を実施例により具体的に説明す
る。なお、本発明における特性値の測定法は次のとおり
である。 【0027】(a) 強伸度 島津製作所製オートグラフS−100 を用い、試料長25c
m、引っ張り速度30cm/分の条件で測定した。 【0028】(b) 曲げ剛性 カトーテック社製純曲げ試験機KES−FB2を用いて
測定した。 【0029】(c) 柔軟性 JIS L-1096 6.19.1A法(45°カンチレバー法)
で測定した。 【0030】なお、エアバッグ用の基布として十分な柔
軟性は、60mm以下である。 【0031】実施例1〜2、比較例1〜5 固有粘度が0.9 のPETチップと、固有粘度が0.75で共
重合比率が表1に示すモル比であるPET/PBT共重
合体のチップを、エクストルーダーを2機備えた複合溶
融紡糸機にそれぞれ供給し、表1に示す芯鞘比で紡出し
た。 【0032】吐出温度を305 ℃とし、紡出した糸条を、
雰囲気温度が400 ℃に保たれた長さ10cmの加熱筒を通
過させた後に、円筒型の冷却風吹付装置により、風温20
℃、風速30m/分の冷却風を吹付けて冷却固化し、油剤
を付与した後、表面速度が480 m/分の引取ローラで引
き取った。 【0033】続いて、表面温度が220 ℃の延伸ローラに
送り、その際、引取ローラと延伸ローラとの間で400 ℃
の加熱水蒸気を吹き付け、延伸倍率5.2 倍で延伸を行
い、表面温度が160 ℃の弛緩ローラにより3%の弛緩処
理を施し、2500m/分の速度で巻き取った。 【0034】得られた糸条の総繊度、単糸繊度、引張強
度、破断伸度、曲げ剛性の値を表1に示す。 【0035】実施例1、2で得られた糸条は、いずれも
曲げ剛性が小さく、強度、伸度ともにエアバッグ用糸条
として十分な値であった。 【0036】一方、比較例1で得られた糸条は芯成分の
比率が低いため、強度が低く、比較例2で得られた糸条
は鞘成分の比率が低いため、曲げ剛性が大きかった。 【0037】比較例3で得られた糸条は鞘成分のPBT
の比率が高いため、強度が低く、比較例4で得られた糸
条は単糸繊度が小さいため、延伸時に毛羽が多発し採取
できず、比較例5で得られた糸条は単糸繊度が大きいた
め、曲げ剛性が大きかった。 比較例6 固有粘度が0.9 のPETチップを単一のエクストルーダ
ーを備えた溶融紡糸機に供給し、PETを単一成分とす
る繊維とした以外は、実施例1と同様に行った。 【0038】得られた糸条の総繊度、単糸繊度、引張強
度、破断伸度、曲げ剛性の値を表1に示す。 【0039】比較例6で得られた糸条は、PETの単一
成分からなるものであるため、曲げ剛性が大きかった。 【0040】 【表1】【0041】実施例3、比較例7 実施例1及び比較例6の糸条を用いて、経、緯密度とも
に48本/2.54cmの平組織の織物を製織し、柔軟性を測定
した。 【0042】得られた織物の柔軟性の測定値を表2に示
す。 【0043】 【表2】 【0044】実施例3で得られた織物は、柔軟性に優れ
るものであったが、比較例7で得られた織物は、曲げ剛
性が大きい糸条を用いたものであるため、柔軟性に劣
り、エアバッグ用基布としての収納性が不十分なもので
あった。 【0045】 【発明の効果】本発明のエアバッグ用糸条は、製編織す
れば、エアバッグ基布として必要な強度や伸度の機械特
性を有し、かつ柔軟性も有する布帛とすることが可能と
なる。 【0046】
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a thread for an airbag which can obtain an airbag base fabric having excellent mechanical properties and flexibility. 2. Description of the Related Art At present, airbags used as safety devices for automobiles are mainly formed of a base fabric obtained by coating a synthetic fiber woven fabric using nylon 66 with rubbers. [0003] Airbags, together with shock absorption, are usually
In order to store it in a very small place, it is required to have excellent flexibility. [0004] However, the base fabric in which the synthetic fiber woven fabric is covered with rubber can improve heat resistance and airtightness by covering with rubber, but the base fabric is hardened, so that the storage property is poor. There's a problem. [0005] In order to solve this problem and reduce the manufacturing cost, a non-coated type airbag which is not coated with rubber has recently been developed.
The use of a polyester that is less expensive than 6 and has good heat resistance has been studied. [0006] However, polyester is nylon 6
6 has a drawback of lacking flexibility when woven into a base fabric, especially when woven at high density to increase airtightness, it is more difficult to store compactly. Problem arises. Japanese Patent Application Laid-Open No. Hei 3-167312 proposes a fiber having improved toughness and knot strength as a polyester fiber for an airbag, and an airbag base fabric obtained from this fiber has improved impact resistance and durability. It has excellent properties and the flatness of the base fabric is also improved. [0008] However, the base fabric obtained from these fibers has a drawback that the flexibility is not sufficient, and if the fabric is woven at a high density in order to increase the airtightness, the storability is poor. As described above, it is not easy to impart flexibility to the polyester yarn while maintaining strength and durability, and it is possible to obtain a flexible airbag base fabric which is excellent in strength and durability and at the same time. Polyester yarn has not yet been developed. [0010] The present invention solves the above-mentioned problems and provides an airbag capable of obtaining a base cloth having both the mechanical properties and flexibility required for an airbag base cloth. An object of the present invention is to provide a bag thread. Means for Solving the Problems The present inventors have made intensive studies to solve the above problems, and as a result, have reached the present invention. That is, according to the present invention, the core component has an intrinsic viscosity.
0.8 or more polyethylene terephthalate, wherein the sheath component is composed of a copolymer obtained by copolymerizing polyethylene terephthalate and polybutylene terephthalate in a molar ratio of 85/15 to 90/10, and the core / sheath ratio is 50/50 to 50/50 by weight. A yarn made of fibers having a core / sheath structure of 70/30, having a single yarn fineness of 1 to 3.
d, total fineness is 200-500 d, tensile strength is 8-8.8 g /
d . An airbag yarn characterized by having a breaking elongation of 15 to 17.6% and a bending rigidity in the range of the formula (1). (1) B ≦ 5.5 × 10 −6 × TD B: Bending rigidity (g · cm 2 / thread) TD: Total fineness (d) (1) B ≦ 5.5 × 10 −6 × TD B: Bending Rigidity (g · cm 2 / thread) TD: Total fineness (d) Hereinafter, the present invention will be described in detail. The yarn for an airbag of the present invention is composed of a conjugate fiber having a core-sheath structure. The core component is polyethylene terephthalate (PET), and the sheath component is a copolymer of PET and polybutylene terephthalate (PBT). It becomes. To the extent that the intrinsic properties of the polyester are not impaired, a third component such as a heat-resistant agent, a flame retardant, or a matting agent may be mixed with PET. First, the core component of the fiber is PET having an intrinsic viscosity of 0.8 or more. Here, the intrinsic viscosity is a value measured at 20 ° C. using a mixed solvent of an equal weight of phenol and tetrachloroethane. If the intrinsic viscosity is less than 0.8, the fiber becomes poor in strength and durability, which is not preferable. Although the upper limit of the intrinsic viscosity is not particularly limited, the range of the intrinsic viscosity is preferably set to 0.8 to 1.1 in order to perform spinning with good operability. The sheath component is PET / PBT 85 /
It is composed of a copolymer copolymerized in a molar ratio of 15 to 90/10, and the intrinsic viscosity of the copolymer is preferably in the range of 0.7 to 0.85. By making the sheath component a copolymer of PET and PBT in this way, the surface layer of the fiber becomes more flexible than the inner layer containing PET, and the inner layer is compressed when the fiber is bent. The required energy is small and the bending stiffness is small. On the other hand, since the inner layer of the fiber is highly oriented, the fiber can have high strength in the fiber axis direction.
The copolymerization ratio of the sheath component PET and PBT is 85/15 to 90 /
It is necessary to set the molar ratio to 10;
When the amount is too large, the flexibility of the fiber is not sufficiently exhibited, and the bending rigidity is increased. When the amount of PBT is large, the fiber has insufficient strength and durability. The ratio between the core component and the sheath component is 50/50 to 50% by weight.
It must be in the range of 70/30. If the core component is more than this range, the fiber will have high flexural rigidity, and if the sheath component is more than this range, the strength and durability will be insufficient. It is necessary that the fineness of the single yarn is 1 to 3d. If the single yarn fineness is larger than 3d, the bending rigidity of the fiber becomes large, and the obtained fabric is not flexible. On the other hand, if it is smaller than 1d, the strength is inferior and the core and sheath components are easily peeled off. The fibers also have poor fatigue resistance. The total fineness must be in the range of 200 to 500 d. When the total fineness is larger than 500d, the base fabric lacks flexibility when weaving at a high density, and when the total fineness is smaller than 200d, the base fabric has low tear strength. The value of the bending stiffness of the yarn varies depending on the fineness of the single yarn and the number of filaments. In the present invention, in order to impart sufficient flexibility to the knitted and woven fabric, it is necessary to satisfy the expression (1). is there. Further, it is necessary that the yarn has a tensile strength of 8 to 8.8 g / d and a breaking elongation of 15 to 17.6% . If the tensile strength is less than 8 g / d, the base fabric will have a weak tear strength, and if the elongation at break is less than 15%, it will not be possible to obtain an impact resistant base fabric that can withstand the impact during airbag operation. Next, an example of a method for producing the yarn for an airbag of the present invention will be described. First, using an ordinary extruder-type composite spinning machine, spinning is performed at a spinning temperature in the range of 295 to 305 ° C.
After passing the yarn immediately after spinning through a heating zone with an ambient temperature of 300 ° C or more, the yarn is cooled by blowing cooling air from the outer periphery to the center of the yarn, and is applied with an oil agent immediately after cooling and solidifying to bundle it. I do. After the collected yarn is taken out, the yarn is stretched to obtain a yarn having a tensile strength of 8 to 8.8 g / d. In order to improve the productivity, the stretching process is performed continuously after the spinning. Since it is preferable to carry out the process, the take-up speed is set in the range of 400 to 600 m / min, and a heating temperature of 200 ° C. or more is sprayed, or a heat plate or the like is used so that the stress applied to the fiber surface layer during drawing can be reduced. The film is stretched at a stretching ratio of 4.5 to 5.5 while heating. Next, the present invention will be described specifically with reference to examples. In addition, the measuring method of the characteristic value in this invention is as follows. (A) High elongation Using an Autograph S-100 manufactured by Shimadzu Corporation, sample length 25c
m, and a tensile speed of 30 cm / min. (B) Flexural rigidity The flexural rigidity was measured using a pure bending tester KES-FB2 manufactured by Kato Tech. (C) Flexibility JIS L-1096 6.19.1A method (45 ° cantilever method)
Was measured. The flexibility sufficient as a base fabric for an airbag is 60 mm or less. Examples 1 and 2 and Comparative Examples 1 to 5 A PET chip having an intrinsic viscosity of 0.9 and a PET / PBT copolymer chip having an intrinsic viscosity of 0.75 and a copolymerization ratio shown in Table 1 were used. The extruders were supplied to a composite melt spinning machine equipped with two extruders, and were spun at a core-sheath ratio shown in Table 1. At a discharge temperature of 305 ° C., the spun yarn is
After passing through a 10 cm long heating cylinder maintained at an ambient temperature of 400 ° C., a cylindrical cooling air blowing device is used to adjust the air temperature to 20 ° C.
After cooling and solidifying by blowing cooling air at a temperature of 30 ° C. and a wind speed of 30 m / min, and applying an oil agent, it was taken up by a take-off roller having a surface speed of 480 m / min. Subsequently, the film is fed to a stretching roller having a surface temperature of 220 ° C., where 400 ° C. is applied between the take-up roller and the stretching roller.
The film was stretched at a stretching ratio of 5.2 times, subjected to a 3% relaxation treatment with a relaxation roller having a surface temperature of 160 ° C., and wound at a speed of 2500 m / min. Table 1 shows the values of total fineness, single yarn fineness, tensile strength, breaking elongation and bending rigidity of the obtained yarn. The yarns obtained in Examples 1 and 2 each had a low bending rigidity, and both the strength and the elongation were sufficient values for airbag yarns. On the other hand, the yarn obtained in Comparative Example 1 had a low strength due to a low ratio of the core component, and the yarn obtained in Comparative Example 2 had a high bending rigidity due to a low ratio of the sheath component. . The yarn obtained in Comparative Example 3 was composed of PBT as a sheath component.
Is high, the strength obtained is low, and the yarn obtained in Comparative Example 4 has a small single-fiber fineness. , The bending rigidity was large. Comparative Example 6 The same operation as in Example 1 was carried out except that a PET chip having an intrinsic viscosity of 0.9 was supplied to a melt spinning machine equipped with a single extruder to make a fiber having PET as a single component. Table 1 shows the total fineness, single yarn fineness, tensile strength, elongation at break, and flexural rigidity of the obtained yarn. Since the yarn obtained in Comparative Example 6 was composed of a single component of PET, the yarn had high flexural rigidity. [Table 1] Example 3, Comparative Example 7 Using the yarns of Example 1 and Comparative Example 6, woven fabrics having a flat structure with a warp and weft density of 48 yarns / 2.54 cm were measured, and the flexibility was measured. Table 2 shows the measured values of the flexibility of the obtained woven fabric. [Table 2] The woven fabric obtained in Example 3 was excellent in flexibility, but the woven fabric obtained in Comparative Example 7 was obtained by using a yarn having high flexural rigidity. It was inferior, and the storage property as a base fabric for an airbag was insufficient. The yarn for an airbag of the present invention, when knitted and woven, has a mechanical property of strength and elongation required for an airbag base fabric, and is a fabric having flexibility. Becomes possible. [0046]

───────────────────────────────────────────────────── フロントページの続き (58)調査した分野(Int.Cl.7,DB名) D01F 8/14 ──────────────────────────────────────────────────続 き Continued on the front page (58) Field surveyed (Int.Cl. 7 , DB name) D01F 8/14

Claims (1)

(57)【特許請求の範囲】 【請求項1】 芯成分が固有粘度が0.8 以上のポリエチ
レンテレフタレート、鞘成分がポリエチレンテレフタレ
ートとポリブチレンテレフタレートが85/15〜90/10の
モル比率で共重合された共重合体より構成され、芯/鞘
比率が重量比で50/50〜70/30の芯鞘構造の繊維からな
る糸条であって、単糸繊度が1〜3d、総繊度が200〜5
00d、引張強度が8〜8.8g/d破断伸度が15〜17.6
、曲げ剛性が(1)式の範囲にあることを特徴とする
エアバッグ用糸条。 (1) B≦ 5.5×10-6×TD B :曲げ剛性(g・cm2/糸条) TD:総繊度(d)
(57) [Claims 1] A core component is copolymerized with polyethylene terephthalate having an intrinsic viscosity of 0.8 or more, and a sheath component is copolymerized with polyethylene terephthalate and polybutylene terephthalate in a molar ratio of 85/15 to 90/10. A core / sheath fiber having a core / sheath ratio of 50/50 to 70/30 by weight, having a single yarn fineness of 1 to 3d and a total fineness of 200 to Five
00d, tensile strength of 8 to 8.8 g / d , elongation at break of 15 to 17.6
% , An airbag yarn characterized by having a flexural rigidity in the range of the expression (1). (1) B ≦ 5.5 × 10 −6 × TD B: Bending rigidity (g · cm 2 / thread) TD: Total fineness (d)
JP27085694A 1994-11-04 1994-11-04 Thread for airbag Expired - Fee Related JP3462914B2 (en)

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JP27085694A JP3462914B2 (en) 1994-11-04 1994-11-04 Thread for airbag

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JP3462914B2 true JP3462914B2 (en) 2003-11-05

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000153743A (en) * 1998-11-20 2000-06-06 Takata Corp Base cloth for air bag
CN105586714A (en) * 2016-03-17 2016-05-18 东莞市亿茂滤材有限公司 High-static long fiber non-woven fabric and making method thereof
CN111148871B (en) 2017-09-29 2022-10-28 世联株式会社 Base fabric for non-coated airbag and airbag
CN111467879A (en) * 2020-04-09 2020-07-31 立赫产业有限公司 Multifunctional electrostatic electret filter material and preparation method thereof

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