JPH08134721A - Filament yarn for air bag - Google Patents
Filament yarn for air bagInfo
- Publication number
- JPH08134721A JPH08134721A JP27085694A JP27085694A JPH08134721A JP H08134721 A JPH08134721 A JP H08134721A JP 27085694 A JP27085694 A JP 27085694A JP 27085694 A JP27085694 A JP 27085694A JP H08134721 A JPH08134721 A JP H08134721A
- Authority
- JP
- Japan
- Prior art keywords
- yarn
- sheath
- core
- fineness
- filament yarn
- 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.)
- Granted
Links
Landscapes
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Multicomponent Fibers (AREA)
- Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)
- Air Bags (AREA)
- Artificial Filaments (AREA)
Abstract
Description
【0001】[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。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a yarn for an airbag capable of obtaining an airbag base fabric having excellent mechanical properties and flexibility.
【0002】[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。2. Description of the Related Art At present, air bags used as a safety device for automobiles are mainly made of a base fabric obtained by coating a synthetic fiber woven fabric using nylon 66 with rubbers.
【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。[0003] Airbags, together with shock absorption, usually
It also needs to be flexible so that it can be stored in a very small space.
【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。However, the base fabric obtained by coating the synthetic fiber woven fabric with rubber can improve heat resistance and airtightness by coating with rubber, but the base fabric becomes hard, so that the storage property is poor. There's a problem.
【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。In order to solve this problem and reduce the manufacturing cost, recently, a non-coated type airbag not covered with rubber has been developed, and the material is nylon 6
It is considered to use polyester which is cheaper than No. 6 and has good heat resistance.
【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。However, polyester is nylon 6
Since it has a higher elastic modulus than that of 6, when it is woven into a base fabric, it has a drawback that it lacks in flexibility. Especially, when it is woven at a high density to improve airtightness, it is more difficult to store it compactly. The problem arises that
【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。Japanese Patent Laid-Open No. 3-167312 proposes a fiber having improved toughness and knot strength as a polyester fiber for an air bag, and an air bag base fabric obtained from this fiber has impact resistance and durability. The flatness of the base fabric is improved.
【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。However, the base fabric obtained from this fiber has a drawback that it is not sufficiently flexible, and if it is woven at a high density in order to increase the airtightness, the storage property becomes poor.
【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。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 while being excellent in strength and durability. Polyester yarn has not been developed yet.
【0010】[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。DISCLOSURE OF THE INVENTION The present invention solves the above-mentioned problems and is capable of obtaining a base cloth having the mechanical properties and flexibility required for an air bag base cloth at the same time. Providing articles is a technical issue.
【0011】[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。The present inventors have arrived at the present invention as a result of extensive studies to solve the above problems.
【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8g/d以上、
破断伸度が15%以上で、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。That is, according to the present invention, the core component has an intrinsic viscosity
It is composed of polyethylene terephthalate of 0.8 or more, the sheath component is a copolymer of polyethylene terephthalate and polybutylene terephthalate in a molar ratio of 85/15 to 90/10, and the core / sheath ratio is 50/50 to a weight ratio. A yarn consisting of 70/30 core-sheath structure fibers with a single yarn fineness of 1 to 3
d, total fineness of 200 to 500 d, tensile strength of 8 g / d or more,
A yarn for an airbag, which has a breaking elongation of 15% or more and a bending rigidity within the range of the formula (1).
【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。(1) B ≦ 5.5 × 10 −6 × TD B: Flexural rigidity (g · cm 2 / thread) TD: Total fineness (d) The present invention will be described in detail below.
【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。The yarn for an air bag of the present invention comprises a composite 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 will be.
【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。A third component such as a heat-resistant agent, a flame retardant and a matting agent may be mixed with PET to the extent that the original properties of polyester are not impaired.
【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。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 equal weight of phenol and tetrachloroethane. When the intrinsic viscosity is less than 0.8, the fiber is inferior in strength and durability, which is not preferable. Further, the upper limit of the intrinsic viscosity is not particularly limited, but it is preferable to set the intrinsic viscosity in the range of 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 at 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.
【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。By making the sheath component a copolymer composed of PET and PBT in this way, the surface layer of the fiber becomes softer than the inner layer containing PET, and when the fiber is bent, the inner layer is compressed. The required energy is low and the bending rigidity is low. 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, but PET is more than this range.
When the content is large, the flexibility of the fiber is not sufficiently expressed and the flexural rigidity becomes large, and when the content of PBT is large, the fiber has insufficient strength and durability.
【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。The ratio of the core component to the sheath component is 50/50 by weight.
It should be in the range of 70/30. When the core component is more than this range, the fiber has high bending rigidity, and when the sheath component is more than this range, the strength and durability are insufficient.
【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。The single yarn fineness needs to be 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, while if it is smaller than 1d, the strength is poor and the core and sheath components are easily peeled off. The fiber also has poor fatigue resistance.
【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。The total fineness should be in the range of 200 to 500 d. If the total fineness is larger than 500d, the base fabric will lack flexibility when woven at a high density, and if it is smaller than 200d, the base fabric will have a weak tear strength.
【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。The flexural rigidity of the yarn varies depending on the single yarn fineness and the number of filaments, but in the present invention, it is necessary to satisfy the formula (1) in order to impart sufficient flexibility to the woven and knitted fabric. is there.
【0022】さらに、引張強度は8g/d以上、破断伸
度は15%以上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。Further, it is necessary that the tensile strength is 8 g / d or more and the breaking elongation is 15% or more. If the tensile strength is less than 8 g / d, the base fabric will have a weak tear strength,
If the elongation at break is less than 15%, it is not possible to obtain a base fabric having impact resistance capable of withstanding the impact when the airbag is operated.
【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。Next, an example of a method of manufacturing the yarn for airbag of the present invention will be described.
【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。First, using an ordinary extruder type composite spinning machine, spinning was carried out at a spinning temperature in the range of 295 to 305 ° C.,
The yarn immediately after spinning is passed through a heating zone with an ambient temperature of 300 ° C or higher, then cooled by blowing cooling air from the outer periphery of the yarn toward the center, and immediately after cooling and solidification, an oil agent is applied to focus the yarn. To do.
【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8g/d以上の糸条を得るが、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 〜600 m/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。After drawing the bundled yarn, it is stretched to obtain a yarn having a tensile strength of 8 g / d or more, but the stretching process should be continuously performed after spinning in order to improve productivity. Is preferable, so that the take-up speed is in the range of 400 to 600 m / min, and heating steam at a heating temperature of 200 ° C or higher is sprayed or a heat plate is used so that the stress applied to the fiber surface layer during stretching can be reduced. While heating, stretch at a stretch ratio of 4.5 to 5.5.
【0026】[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。EXAMPLES Next, the present invention will be specifically described by way of examples. In addition, the measuring method of the characteristic value in this invention is as follows.
【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。(A) Tensile strength Using Autograph S-100 manufactured by Shimadzu Corporation, sample length 25c
m, and the pulling speed was 30 cm / min.
【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。(B) Bending rigidity Measurement was carried out using a pure bending tester KES-FB2 manufactured by Kato Tech.
【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。(C) Flexibility JIS L-1096 6.19.1A method (45 ° cantilever method)
It was measured at.
【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。The softness sufficient as a base fabric for an airbag is 60 mm or less.
【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。Examples 1 and 2, Comparative Examples 1 to 5 PET chips having an intrinsic viscosity of 0.9 and PET / PBT copolymer chips having an intrinsic viscosity of 0.75 and a copolymerization ratio shown in Table 1 were used. Each was supplied to a composite melt spinning machine equipped with two extruders and spun at the core-sheath ratio shown in Table 1.
【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。The discharge temperature was 305 ° C., and the spun yarn was
After passing through a heating cylinder with a length of 10 cm that was kept at an ambient temperature of 400 ° C, the air temperature of 20
After being cooled and solidified 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-up roller having a surface speed of 480 m / min.
【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。Subsequently, it is sent to a stretching roller having a surface temperature of 220 ° C., and at that time, 400 ° C. between the take-up roller and the stretching roller.
The heated steam was sprayed, the film was drawn at a draw ratio of 5.2 times, subjected to a relaxation treatment of 3% by a relaxation roller having a surface temperature of 160 ° C., and wound at a speed of 2500 m / min.
【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。Table 1 shows the values of total fineness, single yarn fineness, tensile strength, elongation at break, and bending rigidity of the obtained yarn.
【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。Each of the yarns obtained in Examples 1 and 2 had a small bending rigidity, and both the strength and the elongation were values sufficient as a yarn for an airbag.
【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。On the other hand, the yarn obtained in Comparative Example 1 had a low ratio of the core component and thus the strength was low, and the yarn obtained in Comparative Example 2 had a low ratio of the sheath component and thus had a large bending rigidity. .
【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。The yarn obtained in Comparative Example 3 had a sheath component of PBT.
The yarn obtained in Comparative Example 4 has a small single yarn fineness because of a high ratio, and thus the yarn obtained in Comparative Example 5 cannot be collected due to a large number of fluffs during the drawing, and the yarn obtained in Comparative Example 5 has a single yarn fineness. Has a large bending rigidity. Comparative Example 6 The procedure of Example 1 was repeated, except that PET chips having an intrinsic viscosity of 0.9 were supplied to a melt spinning machine equipped with a single extruder to prepare fibers having PET as a single component.
【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。Table 1 shows the values of total fineness, single yarn fineness, tensile strength, elongation at break, and bending rigidity of the obtained yarn.
【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。Since the yarn obtained in Comparative Example 6 was composed of a single component of PET, it had a large bending rigidity.
【0040】[0040]
【表1】 [Table 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。Example 3, Comparative Example 7 Using the yarns of Example 1 and Comparative Example 6, a woven fabric having a flat design with both warp and weft densities of 48 yarns / 2.54 cm was woven and the flexibility was measured.
【0042】得られた織物の柔軟性の測定値を表2に示
す。Table 2 shows the measured values of the flexibility of the obtained woven fabric.
【0043】[0043]
【表2】 [Table 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。The woven fabric obtained in Example 3 was excellent in flexibility, but the woven fabric obtained in Comparative Example 7 was made of a yarn having a large bending rigidity, and therefore was not flexible. Inferior, the storability as an airbag base fabric was insufficient.
【0045】[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。EFFECTS OF THE INVENTION The yarn for an airbag of the present invention can be made into a fabric having the mechanical properties of strength and elongation required for an airbag base fabric and flexibility, if it is woven or knitted. Become.
【0046】[0046]
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 // D01F 6/84 301 H ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification number Office reference number FI technical display location // D01F 6/84 301 H
Claims (1)
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 〜
500 d、引張強度が8g/d以上、破断伸度が15%以上
で、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)1. A core comprising a polyethylene terephthalate having an intrinsic viscosity of 0.8 or more, and a sheath comprising a copolymer of polyethylene terephthalate and polybutylene terephthalate in a molar ratio of 85/15 to 90/10. A yarn consisting of fibers having a core / sheath structure with a weight ratio of / sheath of 50/50 to 70/30, with a single yarn fineness of 1 to 3 d and a total fineness of 200 to
A yarn for an airbag, which has a tensile strength of 500 g, a tensile strength of 8 g / d or more, a breaking elongation of 15% or more, and a bending rigidity in the range of the formula (1). (1) B ≦ 5.5 × 10 −6 × TD B: Flexural rigidity (g · cm 2 / thread) TD: Total fineness (d)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP27085694A JP3462914B2 (en) | 1994-11-04 | 1994-11-04 | Thread for airbag |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP27085694A JP3462914B2 (en) | 1994-11-04 | 1994-11-04 | Thread for airbag |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH08134721A true JPH08134721A (en) | 1996-05-28 |
JP3462914B2 JP3462914B2 (en) | 2003-11-05 |
Family
ID=17491935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP27085694A Expired - Fee Related JP3462914B2 (en) | 1994-11-04 | 1994-11-04 | Thread for airbag |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3462914B2 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2344358A (en) * | 1998-11-20 | 2000-06-07 | Takata Corp | Airbag base fabric |
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 |
WO2019065895A1 (en) * | 2017-09-29 | 2019-04-04 | セーレン株式会社 | Base fabric for non-coated air bag, and air bag |
WO2021203494A1 (en) * | 2020-04-09 | 2021-10-14 | 立赫产业有限公司 | Multifunctional electrostatic electret filter and preparation method therefor |
-
1994
- 1994-11-04 JP JP27085694A patent/JP3462914B2/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2344358A (en) * | 1998-11-20 | 2000-06-07 | Takata Corp | Airbag base fabric |
US6458725B1 (en) | 1998-11-20 | 2002-10-01 | Takata Corporation | Airbag base fabric |
GB2344358B (en) * | 1998-11-20 | 2003-02-12 | Takata Corp | Airbag base fabric |
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 |
WO2019065895A1 (en) * | 2017-09-29 | 2019-04-04 | セーレン株式会社 | Base fabric for non-coated air bag, and air bag |
JPWO2019065895A1 (en) * | 2017-09-29 | 2020-09-17 | セーレン株式会社 | Base cloth and airbags for non-coated airbags |
US11752969B2 (en) | 2017-09-29 | 2023-09-12 | Seiren Co., Ltd. | Non-coated air bag base cloth and air bag |
WO2021203494A1 (en) * | 2020-04-09 | 2021-10-14 | 立赫产业有限公司 | Multifunctional electrostatic electret filter and preparation method therefor |
Also Published As
Publication number | Publication date |
---|---|
JP3462914B2 (en) | 2003-11-05 |
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