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JPS62299514A - Thermally bondable hollow conjugated yarn - Google Patents

Thermally bondable hollow conjugated yarn

Info

Publication number
JPS62299514A
JPS62299514A JP61134031A JP13403186A JPS62299514A JP S62299514 A JPS62299514 A JP S62299514A JP 61134031 A JP61134031 A JP 61134031A JP 13403186 A JP13403186 A JP 13403186A JP S62299514 A JPS62299514 A JP S62299514A
Authority
JP
Japan
Prior art keywords
hollow
core component
sheath
component
heat
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.)
Pending
Application number
JP61134031A
Other languages
Japanese (ja)
Inventor
Magosaburo Fujiwara
藤原 孫三郎
Hideo Nakajima
秀雄 中島
Kiminori Shigeta
重田 公紀
Toshiyuki Kihara
木原 敏之
Kenjiro Kuhara
久原 健次郎
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.)
Daiwa Boseki KK
Original Assignee
Daiwa Boseki KK
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 Daiwa Boseki KK filed Critical Daiwa Boseki KK
Priority to JP61134031A priority Critical patent/JPS62299514A/en
Publication of JPS62299514A publication Critical patent/JPS62299514A/en
Pending legal-status Critical Current

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  • Multicomponent Fibers (AREA)
  • Nonwoven Fabrics (AREA)

Abstract

PURPOSE:Thermally bondable yarn which is conjugated yarn having eccentrically existing high-melting core part and low-melting sheath part and a hollow part at the core part wherein the center of the hollow part is approximately coincident with the center of the sheath part and provides nonwoven fabric having bulkiness, improved elasticity recovering properties, good flexibility and feeling. CONSTITUTION:In sheath-skin type conjugated yarn, thermally bondable yarn wherein a core part 1 consists of a high-melting polymer and has a hollow part 2 continuing in the longer direction and a sheath part 3 comprises a low- melting polymer having a melting point 20 deg.C lower than the component of the core part 1, the core part 1 eccentrically exists in the sheath part 3 and the center of the hollow part 2 approximately coincides with the center of the sheath part 3. The center ratio is preferably 5-40%. The eccentric ratio of the core part 1 and the hollow part 2 is preferably 0.10-0.70.

Description

【発明の詳細な説明】 3、発明の詳細な説明 (産業上の利用分野) 本発明は嵩高性と弾性回復性に優れ、特に不織布用素材
として好適な熱接着性中空複合繊維に関するものである
[Detailed Description of the Invention] 3. Detailed Description of the Invention (Field of Industrial Application) The present invention relates to a heat-adhesive hollow composite fiber that has excellent bulkiness and elastic recovery properties and is particularly suitable as a material for nonwoven fabrics. .

(従来の技術つ 融点の異なる2成分からなる熱接着性複合繊維は、接着
剤を用いることなく繊維間の結合が可能であるため、接
着剤結合による場合のように乾燥を必要とせず、エネル
ギーの消費量が少なく経済的であり、またホルマリン等
人体に有害な物質の含有を忌避する衛生材料をはじめ各
種の不織布用の繊維素材として介臼ムく用いられている
。殊に例えば特公昭50−4767号公報、特公昭52
−12830号公報あるいは特公昭55−483号公報
にみられるように、ポリプロピレンとポリエチレンとを
並列型または芯鞘型に配したポリオレフィン系の複合繊
維は、有害物質が含有せず、比較的低温で熱接着でき、
風合が柔軟で耐薬品性に優れていることから、この種の
熱接着性繊維は各種の不織用として最も汎用されている
(Conventional technology) Heat-adhesive conjugate fibers made of two components with different melting points can be bonded between fibers without using adhesives, so they do not require drying and require energy It is economical with low consumption, and is widely used as a fiber material for various non-woven fabrics, including sanitary materials that avoid the inclusion of substances harmful to the human body such as formalin. -4767 Publication, Special Publication No. 1977
As seen in Japanese Patent Publication No. 12830 or Japanese Patent Publication No. 55-483, polyolefin composite fibers in which polypropylene and polyethylene are arranged in a parallel type or core-sheath type do not contain harmful substances and can be used at relatively low temperatures. Can be thermally bonded
Because of its soft texture and excellent chemical resistance, this type of thermally adhesive fiber is most commonly used for various nonwovens.

(発明が解決しようとする問題点) しかしながら従来の熱接着性複合繊維は、嵩高性と弾性
回復性において必ずしも満足すべきものではない。例え
ば熱接着性複合繊維を全部又は一部に用いて柔軟μ風合
の不織布を製造する場合、該複合繊維のカードウェブ、
またはランダムウェブに熱風加工またはエンボスロール
加工を施して該複合繊維の低融点成分のみを溶融し、繊
維間接着を行なわしめて強力の向上した不織布とfjす
ものであるが、得られた不織布は熱接着加工前のウェブ
に比べて嵩高性が意外に乏しい。そして上記熱接着加後
の不織布は通常紙管(こ巻き取って出荷あるいは保管さ
れるが、例えば保管後出荷された上記巻き取り物を使用
のために巻き戻しく開度うすると、弾性回復力が小さい
ために巻き取り前に比べて嵩高性が著しく損なわれた状
態となっている。
(Problems to be Solved by the Invention) However, conventional heat-adhesive composite fibers are not necessarily satisfactory in terms of bulk and elastic recovery. For example, when producing a nonwoven fabric with a soft μ texture using heat-adhesive conjugate fibers in whole or in part, a carded web of the conjugate fibers,
Alternatively, a random web is subjected to hot air processing or embossing roll processing to melt only the low melting point components of the composite fibers, and bonding between the fibers is performed to create a nonwoven fabric with improved strength. The bulkiness is surprisingly poor compared to the web before adhesive processing. The nonwoven fabric after being thermally bonded is usually rolled up into a paper tube and shipped or stored. is small, so the bulkiness is significantly impaired compared to before winding.

本発明は、熱接着性複合繊維による不織布の柔軟性、良
好な風合、高強力等の特長を損なうことtく、嵩高性並
びに弾性回復性に富んだ熱接着性複合繊維を提供するも
のである。
The present invention provides a heat-adhesive conjugate fiber that is rich in bulk and elastic recovery without impairing the flexibility, good feel, high strength, and other features of nonwoven fabrics made of heat-adhesive conjugate fibers. be.

(問題点を解決するための手段) 本発明1こよる熱接着性繊維は、繊維形成性熱可塑性重
合体を芯成分とし、該芯成分よりも少なくとも20℃低
い融点を有する繊維形成性熱可塑性重合体を鞘成分とし
、芯成分(こは繊維の長さ方向に中空部が形成されてな
り、該中空部は鞘成分に対して同心の位置にあり、芯成
分に対しては偏心位置に存在した断面構造を有してなり
、中空部の存在によって繊維の曲げモーメントを太き(
し、芯成分に対する中空部の偏心存在によって適度rλ
捲縮が確保され、か(して嵩高性と弾性回復性の優れた
不織布を得ることができるものである。
(Means for Solving the Problems) The thermoadhesive fiber according to the present invention 1 has a fiber-forming thermoplastic polymer as a core component and has a melting point at least 20° C. lower than that of the core component. A polymer is used as a sheath component, and a core component (a hollow part is formed in the length direction of the fiber, and the hollow part is located concentrically with respect to the sheath component and eccentrically with respect to the core component). The bending moment of the fiber is increased due to the presence of the hollow part.
However, due to the presence of eccentricity of the hollow part with respect to the core component, a moderate rλ
The crimp is ensured, and a nonwoven fabric with excellent bulk and elastic recovery properties can be obtained.

本発明の熱接着性複合繊維の芯成分の重合体としては、
ポリプロビレ/、ポリエチレンテレフタレート等が好適
であり、鞘成分の重合体としては、高密度ポリエチレン
、中密度ポリエチレン、低密度ポリエチレン、エチレン
・酢設ビニル共重合体、あるいはポリプロピレノ等が挙
げられる。
As the core component polymer of the heat-adhesive composite fiber of the present invention,
Polypropylene/polyethylene terephthalate and the like are preferred, and examples of the polymer for the sheath component include high density polyethylene, medium density polyethylene, low density polyethylene, ethylene/vinyl acetate copolymer, and polypropylene.

また、これらの異なる2成分からなる熱接着性複合繊維
を用いた繊維集合体や不織布の熱接着加工前に、芯成分
の熱収縮、軟化等が好ましくない影響を避けるため、鞘
成分は芯成分を構成する重合体の融点よりも少fjくと
も20℃低い融点の重合体であることが必要である。
In addition, before thermal bonding processing of fiber aggregates or nonwoven fabrics using heat-adhesive composite fibers made of these two different components, the sheath component is added to the core component in order to avoid undesirable effects such as heat shrinkage and softening of the core component. It is necessary that the melting point of the polymer is at least 20° C. lower than the melting point of the polymer constituting the polymer.

本発明の複合繊維は添付図面に示したごとく、繊維断面
において芯成分(1)の中;こ中空部(2)が形成され
ているが、該中空部(2)は芯成分(1)とは偏心位置
にあり、該芯成分(1)の中心点(0りと中空部(2)
の中心点((12)との距離をlalとし芯成分(1)
の半径をtriとした場合、その偏心比(DIはD−一
で表わされるが、偏心比1(11が0.10未満の場合
においては捲縮の発現性が小さく熱接着加工後の繊維集
合体の嵩高性と弾性回復性が劣ったものとなり、また偏
心比tDlが0.70を越えると中空部(2)の1部が
芯成分(1)の外に露出する恐れがあり、中空部(2)
の1部が芯成分(1)の外に位置した場合には熱接着加
工時に溶融した鞘成分(3)が中空部に流入して嵩高性
および弾性回復性を損なう結果を招(ことから上記偏心
比(D+は0.10〜0.70の範囲であることが望ま
しい。そして加熱処理前の複合繊維に均一な捲縮形態を
付与してカードの通過性を良好ならしめるためには、上
記中空部(2)は鞘成分(3)に対しては同心位置にあ
ることが望ましい。
As shown in the attached drawings, the composite fiber of the present invention has a hollow portion (2) formed in the core component (1) in the cross section of the fiber; is at an eccentric position, and the center point (0 and the hollow part (2) of the core component (1)
The center point (with the distance from (12) as lal, the core component (1)
When the radius of is tri, the eccentricity ratio (DI is expressed as D-1, but when the eccentricity ratio 1 (11) is less than 0.10, the occurrence of crimp is small and the fiber assembly after thermal bonding is The bulkiness and elastic recovery of the body will be poor, and if the eccentricity ratio tDl exceeds 0.70, there is a risk that a part of the hollow part (2) will be exposed outside the core component (1), and the hollow part (2)
If a part of the core component (1) is located outside the core component (1), the sheath component (3) melted during the thermal bonding process will flow into the hollow part, resulting in loss of bulk and elastic recovery (thus, the above-mentioned It is desirable that the eccentricity ratio (D+) be in the range of 0.10 to 0.70.In order to impart a uniform crimp form to the composite fiber before heat treatment and to improve the card passability, the above-mentioned Preferably, the hollow part (2) is in a concentric position with respect to the sheath component (3).

また芯成分(1)に対する中空部(2)の面積率(中空
率〕は5〜40%程度が好ましい。
Further, the area ratio (hollowness ratio) of the hollow portion (2) to the core component (1) is preferably about 5 to 40%.

ここに中空率は次式により求められる。Here, the hollowness ratio is determined by the following formula.

中空率が5%未満では嵩高性、弾性回復性が乏しくなり
、また40%を越えると高荷重丁で中空部がつぶれ易く
嵩高性や弾性回復性が損なわれるという結果を招く。
If the hollowness ratio is less than 5%, bulkiness and elastic recovery properties will be poor, and if it exceeds 40%, the hollow portion will be easily crushed under high load, resulting in loss of bulkiness and elastic recovery properties.

本発明の繊維は不織布用繊維素材等として単独で用いて
もよ(、他種の繊維と混合して用いてもよいが熱液効果
を得るためには30重fft%以上配合するのがよい。
The fibers of the present invention may be used alone as a fiber material for nonwoven fabrics, etc. (or may be used in combination with other types of fibers, but in order to obtain a hot liquid effect, it is preferable to mix 30% by weight or more. .

(作用〕 本発明の芯鞘型複合繊維における鞘成分は、芯成分内に
存在している中空部と実質的に同心円状であるから、芯
成分と中空部との偏心による芯成分の構造的異方性の発
現を抑制し、複合繊維の延伸後のリラックス熱処理によ
る捲縮発現が過度となるのを防止してカード通過性の良
好な適度の捲縮を有した複合繊維となる。その上芯成分
万に中空部が存在しているため熱接着加工の際に鞘成分
が溶融しても中空部がその侭芯成分内に残留し、この中
空部の存在によって繊維の曲げモーメントが大となり、
嵩高性と弾性回復性を向上させる。
(Function) Since the sheath component in the core-sheath type composite fiber of the present invention is substantially concentric with the hollow portion existing within the core component, the structural impact of the core component due to the eccentricity between the core component and the hollow portion It suppresses the development of anisotropy and prevents excessive crimp development due to relaxation heat treatment after drawing the composite fiber, resulting in a composite fiber with moderate crimp and good card passability. Since there is a hollow part in the core component, even if the sheath component melts during thermal bonding, the hollow part remains in the core component, and the presence of this hollow part increases the bending moment of the fiber. ,
Improves bulk and elastic recovery.

また特筆すべきことは、本発明の複合繊維はカードウェ
ブの状態【こおいて嵩高性が優れているだけではfj<
、熱接着加工後の不織布に優れた嵩高性と弾性回復性を
具備させ得ることである。場合)こおいてはカードウェ
ブ状態の嵩高性よりも熱接着加工後の不織布の嵩高性の
方が良好となる。これは熱接着加工によって複合繊維の
鞘成分が溶融したのちにおいては、芯成分に対して中空
部が偏心しているため、鞘成分の束縛から解放された芯
成分が中空部の偏心による構造異方性により三次元的な
立体捲縮を発現することによるものである。
It should also be noted that the composite fiber of the present invention has a carded web state [where fj<
Another object of the present invention is that the nonwoven fabric after being thermally bonded can have excellent bulkiness and elastic recovery properties. case), the bulkiness of the nonwoven fabric after thermal bonding is better than the bulkiness of the carded web state. This is because after the sheath component of the composite fiber is melted by thermal bonding, the hollow part is eccentric with respect to the core component, so the core component released from the constraints of the sheath component exhibits structural anisotropy due to the eccentricity of the hollow part. This is due to the appearance of three-dimensional crimps depending on the nature of the body.

そして一旦嵩高となった不織布は繊維間が接着結合され
ることによって繊維集合体としての形態が安定化され、
繊維自体の弾性回復性と相まって高弾性と良好な回復性
を呈する。
Once bulky, the nonwoven fabric is stabilized as a fiber aggregate by adhesive bonding between the fibers.
Combined with the elastic recovery properties of the fiber itself, it exhibits high elasticity and good recovery properties.

(実施例) 融点が167℃、230℃におけるメルトフロレートが
5のポリプロピレンを芯成分(1)とし、融点力132
℃、メルトインデックスが26、密度0.960の高密
度ポリエチレンを鞘成分(3)として両者を別個の押出
様に供給して溶融押出しを行ない、外径1.2關の中空
ノズル孔を有する複合紡糸口金(ノズル数40)から紡
糸して芯成分中番こ中空部(2)が存在しかつ芯成分(
1)と鞘成分(3)との複合比(断面積比〕が1:1の
芯鞘型中空複合繊維を紡出した。次いで、この芯鞘型中
空複合繊維を加熱して延伸し、スタッファ−ボックス型
捲縮機を付与し、または機械捲縮を付与することなく1
10℃で15分間リラックス熱処理したのち51關の長
さに切断してステープル繊維と1ヱした。
(Example) Polypropylene with a melting point of 167°C and a melt fluorate of 5 at 230°C was used as the core component (1), and a melting point power of 132
℃, high-density polyethylene with a melt index of 26 and a density of 0.960 is used as a sheath component (3), and both are supplied in a separate extrusion manner to perform melt extrusion, and a composite material having a hollow nozzle hole with an outer diameter of about 1.2 is obtained. When spinning from a spinneret (40 nozzles), a hollow part (2) exists in the core component and the core component (
A core-sheath type hollow composite fiber was spun with a composite ratio (cross-sectional area ratio) of 1) and sheath component (3) of 1:1.Then, this core-sheath type hollow composite fiber was heated and stretched to form a staff. 1 with a box crimper or without mechanical crimping.
After relaxing heat treatment at 10° C. for 15 minutes, the fibers were cut into 51-inch lengths and used as staple fibers.

このステープル繊維をローラカードに供給して得たウェ
ブを無荷重下において熱風貫通型熱加工機により140
℃で1分間加熱して鞘成分を溶融し、繊維間が接着結合
した不織布を得た。上記の実施例1−8および比較例1
〜2の結果は第1表の通りであった。
The web obtained by supplying this staple fiber to a roller card is processed by a hot air penetrating thermal processing machine under no load.
The sheath component was melted by heating at .degree. C. for 1 minute to obtain a nonwoven fabric in which the fibers were adhesively bonded. Examples 1-8 and Comparative Example 1 above
-2 results are as shown in Table 1.

次に、融点255℃、極限粘度0.72のポIJ エチ
レンテレフタレートと、融点132℃、メルトインデッ
クス28、密度06955の高密度ポリエチレンとを、
別個の押出機に供給して溶融押出しを行ない、両者を外
径1.3朋の中空ノズル孔を有する複合紡糸口金(ノズ
ル孔数120)に導入して、ポリエチレンテレフタレー
トが芯成分に、高密度ボIJ エチレ/が鞘成分となり
、その芯成分中(こ中空部が存在し、かつ芯成分と鞘成
分との複合比が1=1の芯鞘型中空複合繊維を紡出した
。この紡出糸を所定信性で延伸したのちスタッファ−ボ
ックス型捲縮機で機械捲縮を付与し、または付与せず(
こ115℃で15分間リラックス熱処理をして51mm
の長さに切断し、ステーブル繊維を得た。
Next, polyethylene terephthalate with a melting point of 255°C and an intrinsic viscosity of 0.72 and high-density polyethylene with a melting point of 132°C, a melt index of 28, and a density of 06955 were
They were fed into separate extruders for melt extrusion, and both were introduced into a composite spinneret (number of nozzle holes: 120) having hollow nozzle holes with an outer diameter of 1.3 mm, so that polyethylene terephthalate became the core component and had a high density. A core-sheath type hollow composite fiber was spun, in which BoIJ Echire/ was used as a sheath component, a hollow part existed in the core component, and the composite ratio of the core component and the sheath component was 1=1. After the yarn is drawn to a predetermined reliability, mechanical crimp is applied with or without mechanical crimp using a stuffer box type crimper (
After relaxing heat treatment at 115℃ for 15 minutes, it became 51mm.
The fibers were cut into lengths to obtain stable fibers.

このステープル繊維をカードウェブとなし、これを無荷
1丁で熱風貫通型加工機で140℃にて1分間加熱して
熱接着せしめ、繊維間が結合した不織布となした。
This staple fiber was made into a carded web, which was heated unloaded in a hot air penetrating processing machine for 1 minute at 140° C. to thermally bond it to form a nonwoven fabric in which the fibers were bonded.

上記の実施例9〜10、および比較例3〜4の結果は第
2表の通りであった。
The results of Examples 9 and 10 and Comparative Examples 3 and 4 are shown in Table 2.

第2表 なお、第1表の比較例1および′52表の比較例3の偏
心比は芯成分と鞘成分との偏心比を表わしくこより算出
した。また不織布の厚さは、0.1り2dの荷重下で測
定して得られた値を40 Vrdの目付に換算した値を
示し、不織布の風合は5人のパネラ−によって官能評価
試験を行ない、その平均評価として「軟かい」が◎、「
や\軟かい」が○、「や\硬い゛」がΔ、「硬い」がX
として表示したつまた除重後の厚さは、タテ15cmX
ヨコ150に切り取った不織布片を10枚重ね、目付4
0Hに換算して不織布の巻き取り状態における厚さに相
当するところの1枚当り0.1 mmの厚さまで圧縮し
、−週間後除重し、その状態で24時間放置後、0.1
ダ、七の荷重下で測定した厚さを40 Fiordの目
付に換算した値を示し、嵩高維持率は を表わす。
Table 2 Note that the eccentricity ratio of Comparative Example 1 in Table 1 and Comparative Example 3 in Table '52 was calculated from the eccentricity ratio of the core component and the sheath component. In addition, the thickness of the nonwoven fabric is the value obtained by measuring under a load of 0.1 to 2 d and converted to a basis weight of 40 Vrd, and the texture of the nonwoven fabric is determined by a sensory evaluation test conducted by five panelists. The average rating was ``soft'', and ``soft'' was ◎.
○ for ``ya\soft'', Δ for ``ya\hard゛'', and X for ``hard''
The thickness after removing the tsumata weight is 15 cm vertically.
Layer 10 pieces of nonwoven fabric cut at 150 mm horizontally, and make the fabric weight 4.
It was compressed to a thickness of 0.1 mm per sheet, which corresponds to the thickness of the nonwoven fabric in a rolled state in terms of 0H, and after - weeks, the weight was removed, and after leaving it in that state for 24 hours, it was compressed to a thickness of 0.1 mm.
The value is the value obtained by converting the thickness measured under a load of 40 mm to a basis weight of 40 mm, and the bulk retention rate is expressed as .

(発明の効果) このように本発明による熱接着性中空複合繊維は、長さ
方向に連続した中空部を有する高融点重合体よりflる
芯成分と、該芯成分よりも少なくとも20℃低い融点を
有する低融点重合体よりなる鞘成分とからなり、該中空
部の中心点は該芯成分の中心点から偏心しているから、
機械捲縮の付与の有無に拘らずリラックス熱処理におい
て3次元的な立体捲縮が発現し、カードの通過性が良好
となり、また熱接着加工後の不織布においてもカードウ
ェブと同等もしくはそれ以上の嵩高性を維持する。その
上中空部の存在によって弾性回復性が高くなり、ロール
状に巻き取った不織布を展開した際、嵩高性の回復が顕
著に認められ、風合がソフトであり弾力性(こ富んだ不
織布シートと戸る。
(Effects of the Invention) As described above, the heat-adhesive hollow conjugate fiber according to the present invention has a core component that is higher than a high melting point polymer having a continuous hollow portion in the length direction, and a melting point that is at least 20° C. lower than that of the core component. and a sheath component made of a low melting point polymer having
Regardless of whether or not mechanical crimping is applied, three-dimensional crimping occurs during the relaxing heat treatment, resulting in good card passage properties, and the nonwoven fabric after thermal bonding has a bulk that is equal to or greater than that of the carded web. maintain sexuality. In addition, the presence of hollow parts increases elastic recovery, and when the nonwoven fabric wound into a roll is rolled out, the bulkiness is significantly recovered, the texture is soft, and the nonwoven fabric is highly elastic. Toru.

したがって本発明による熱接着性中空複合繊維でもっで
あるいは該中空複合繊維を混入して得られる不織布は、
ソフトな風合と嵩高性が要求される衛生材料として好適
であり、また良好な弾性復元性は吸収芯材中の液体の逆
流防止作用を奏することから、吸収芯材の表面材として
特に好都合である。
Therefore, the nonwoven fabric obtained by using the heat-adhesive hollow conjugate fiber according to the present invention or by mixing the hollow conjugate fiber with the heat-adhesive hollow conjugate fiber is as follows:
It is suitable as a sanitary material that requires a soft texture and bulkiness, and its good elastic resilience prevents the backflow of liquid in the absorbent core material, making it particularly suitable as a surface material for the absorbent core material. be.

更に、本発明の中空複合繊維を用いた不織布は弾性回復
性に富んでいるから、不織布の製造工程において紙管に
巻き取ったまま長期間保管しても展開すると嵩高性が回
復し、圧縮巻き取りにより嵩高性が減殺されるという不
都合の解消に役立つ。
Furthermore, since the nonwoven fabric using the hollow composite fibers of the present invention has high elastic recovery properties, even if it is stored for a long period of time while being rolled up in a paper tube during the manufacturing process of the nonwoven fabric, its bulkiness is restored when it is unfolded, and it can be compressed and rolled. This helps eliminate the inconvenience that bulkiness is reduced due to removal.

その上、従来の熱接着性繊維と同等の熱接着性能を具備
しているから、衛生材料用不織布のみならす、嵩高性と
弾性回復性が要求される各種分野の繊維製品の用途に適
合する。
Furthermore, since it has thermal adhesive performance equivalent to that of conventional thermal adhesive fibers, it is suitable for use not only in nonwoven fabrics for sanitary materials, but also in textile products in various fields that require bulkiness and elastic recovery.

【図面の簡単な説明】[Brief explanation of drawings]

図面は本発明の複合繊維の断面拡大図であり(1)は芯
成分、(2)は中空部、(3)は鞘成分である。
The drawing is an enlarged cross-sectional view of the composite fiber of the present invention, in which (1) is a core component, (2) is a hollow part, and (3) is a sheath component.

Claims (13)

【特許請求の範囲】[Claims] (1)長さ方向に連続した中空部を有する高融点重合体
よりをよる芯成分と、該芯成分よりも少なくとも20℃
低い融点を有する低融点重合体よりなる鞘成分とからな
り、該中空部の中心点は芯成分の中心点から偏心し鞘成
分の中心点とほぼ一致していることを特徴とする熱接着
性中空複合繊維
(1) A core component made of a high melting point polymer having a hollow part continuous in the length direction, and at least 20°C higher than the core component.
and a sheath component made of a low melting point polymer having a low melting point, and the center point of the hollow portion is eccentric from the center point of the core component and almost coincides with the center point of the sheath component. hollow composite fiber
(2)上記中空部の芯成分に対する中空率が5〜40%
である上記特許請求の範囲第1項記載の熱接着性中空複
合繊維。
(2) The hollow ratio of the above hollow part to the core component is 5 to 40%
The heat-adhesive hollow composite fiber according to claim 1.
(3)繊維断面における芯成分と鞘成分との面積比が1
:1〜2:1である上記特許請求の範囲第1項記載の熱
接着性中空複合繊維。
(3) The area ratio of the core component and sheath component in the fiber cross section is 1
The heat-adhesive hollow composite fiber according to claim 1, wherein the ratio is 1 to 2:1.
(4)芯成分と中空部との偏心比が0.10〜0.70
である上記特許請求の範囲第1項記載の熱接着性中空複
合繊維。
(4) Eccentricity ratio between core component and hollow part is 0.10 to 0.70
The heat-adhesive hollow composite fiber according to claim 1.
(5)芯成分がポリプロピレン、鞘成分が高密度ポリエ
チレンよりなる上記特許請求の範囲第1項記載の熱接着
性中空複合繊維。
(5) The heat-adhesive hollow conjugate fiber according to claim 1, wherein the core component is polypropylene and the sheath component is high-density polyethylene.
(6)芯成分がポリプロピレン、鞘成分が中密度ポリエ
チレンよりなる上記特許請求の範囲第1項記載の熱接着
性中空複合繊維。
(6) The thermoadhesive hollow conjugate fiber according to claim 1, wherein the core component is polypropylene and the sheath component is medium density polyethylene.
(7)芯成分がポリプロピレン、鞘成分が低密度ポリエ
チレンよりなる上記特許請求の範囲第1項記載の熱接着
性中空複合繊維。
(7) The heat-adhesive hollow composite fiber according to claim 1, wherein the core component is polypropylene and the sheath component is low-density polyethylene.
(8)芯成分がポリプロピレン、鞘成分がエチレン・酢
酸ビニル共重合体よりなる上記特許請求の範囲第1項記
載の熱接着性中空複合繊維。
(8) The heat-adhesive hollow conjugate fiber according to claim 1, wherein the core component is polypropylene and the sheath component is an ethylene/vinyl acetate copolymer.
(9)芯成分がポリエチレンテレフタレート、鞘成分が
高密度ポリエチレンよりなる上記特許請求の範囲第1項
記載の熱接着性中空複合繊維。
(9) The heat-adhesive hollow composite fiber according to claim 1, wherein the core component is polyethylene terephthalate and the sheath component is high-density polyethylene.
(10)芯成分がポリエチレンテレフタレート、鞘成分
が中密度ポリエチレンよりなる上記特許請求の範囲第1
項記載の熱接着性中空複合繊維。
(10) Claim 1 above wherein the core component is polyethylene terephthalate and the sheath component is medium density polyethylene.
The heat-adhesive hollow composite fiber described in .
(11)芯成分がポリエチレンテレフタレート、鞘成分
が低密度ポリエチレンよりなる上記特許請求の範囲第1
項記載の熱接着性中空複合繊維。
(11) Claim 1 above wherein the core component is polyethylene terephthalate and the sheath component is low density polyethylene.
The heat-adhesive hollow composite fiber described in .
(12)芯成分がポリエチレンテレフタレート、鞘成分
がエチレン・酢酸ビニル共重合体よりなる上記特許請求
の範囲第1項記載の熱接着性中空複合繊維。
(12) The heat-adhesive hollow conjugate fiber according to claim 1, wherein the core component is polyethylene terephthalate and the sheath component is an ethylene/vinyl acetate copolymer.
(13)芯成分がポリエチレンテレフタレート鞘成分が
ポリプロピレンよりなる上記特許請求の範囲第1項記載
の熱接着性中空複合繊維。
(13) The thermoadhesive hollow composite fiber according to claim 1, wherein the core component is polyethylene terephthalate and the sheath component is polypropylene.
JP61134031A 1986-06-10 1986-06-10 Thermally bondable hollow conjugated yarn Pending JPS62299514A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61134031A JPS62299514A (en) 1986-06-10 1986-06-10 Thermally bondable hollow conjugated yarn

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61134031A JPS62299514A (en) 1986-06-10 1986-06-10 Thermally bondable hollow conjugated yarn

Publications (1)

Publication Number Publication Date
JPS62299514A true JPS62299514A (en) 1987-12-26

Family

ID=15118756

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61134031A Pending JPS62299514A (en) 1986-06-10 1986-06-10 Thermally bondable hollow conjugated yarn

Country Status (1)

Country Link
JP (1) JPS62299514A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01213452A (en) * 1988-02-16 1989-08-28 Chisso Corp Production of bulky nonwoven fabric
JPH01272823A (en) * 1988-04-25 1989-10-31 Chisso Corp Three-dimensional curl filament
JPH0253914A (en) * 1988-08-11 1990-02-22 Kuraray Co Ltd hot melt adhesive fiber
JPH02191718A (en) * 1989-01-19 1990-07-27 Toyobo Co Ltd Heat bondable conjugate yarn
JPH02191717A (en) * 1989-01-19 1990-07-27 Toyobo Co Ltd Heat bondable conjugate yarn
JPH03814A (en) * 1989-05-25 1991-01-07 Toyobo Co Ltd Heat bonding conjugate yarn
JPH0369614A (en) * 1989-06-15 1991-03-26 Toyobo Co Ltd Thermally adhesive hollow conjugate fiber
JPH03241055A (en) * 1990-02-20 1991-10-28 Toyobo Co Ltd Bulky filament non-woven fabric
JPH03287848A (en) * 1990-04-03 1991-12-18 Toyobo Co Ltd Bulky nonwoven fabric
US6878650B2 (en) 1999-12-21 2005-04-12 Kimberly-Clark Worldwide, Inc. Fine denier multicomponent fibers
US7238423B2 (en) 2004-12-20 2007-07-03 Kimberly-Clark Worldwide, Inc. Multicomponent fiber including elastic elements
JP2013252330A (en) * 2012-06-08 2013-12-19 Unicharm Corp Absorbing body and absorbing article with the same
CN105200664A (en) * 2015-09-25 2015-12-30 佛山市南海必得福无纺布有限公司 Spun-bonded hollow double-component non-woven fabric
JP2017526834A (en) * 2014-07-02 2017-09-14 ヒュービス カンパニー リミテッド Thermal adhesive composite fiber for nonwoven fabric binder

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4825005A (en) * 1971-07-31 1973-04-02
JPS4889077A (en) * 1972-03-01 1973-11-21
JPS58180614A (en) * 1982-04-12 1983-10-22 Daiwa Spinning Co Ltd Polyolefin type eccentric composite fiber and preparation apparatus therefor
JPS6119815A (en) * 1984-07-04 1986-01-28 Daiwa Spinning Co Ltd Bicomponent conjugated hollow fiber and its production

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4825005A (en) * 1971-07-31 1973-04-02
JPS4889077A (en) * 1972-03-01 1973-11-21
JPS58180614A (en) * 1982-04-12 1983-10-22 Daiwa Spinning Co Ltd Polyolefin type eccentric composite fiber and preparation apparatus therefor
JPS6119815A (en) * 1984-07-04 1986-01-28 Daiwa Spinning Co Ltd Bicomponent conjugated hollow fiber and its production

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01213452A (en) * 1988-02-16 1989-08-28 Chisso Corp Production of bulky nonwoven fabric
JPH01272823A (en) * 1988-04-25 1989-10-31 Chisso Corp Three-dimensional curl filament
JPH0253914A (en) * 1988-08-11 1990-02-22 Kuraray Co Ltd hot melt adhesive fiber
JPH02191718A (en) * 1989-01-19 1990-07-27 Toyobo Co Ltd Heat bondable conjugate yarn
JPH02191717A (en) * 1989-01-19 1990-07-27 Toyobo Co Ltd Heat bondable conjugate yarn
JPH03814A (en) * 1989-05-25 1991-01-07 Toyobo Co Ltd Heat bonding conjugate yarn
JPH0369614A (en) * 1989-06-15 1991-03-26 Toyobo Co Ltd Thermally adhesive hollow conjugate fiber
JPH03241055A (en) * 1990-02-20 1991-10-28 Toyobo Co Ltd Bulky filament non-woven fabric
JPH03287848A (en) * 1990-04-03 1991-12-18 Toyobo Co Ltd Bulky nonwoven fabric
US6878650B2 (en) 1999-12-21 2005-04-12 Kimberly-Clark Worldwide, Inc. Fine denier multicomponent fibers
US7238423B2 (en) 2004-12-20 2007-07-03 Kimberly-Clark Worldwide, Inc. Multicomponent fiber including elastic elements
JP2013252330A (en) * 2012-06-08 2013-12-19 Unicharm Corp Absorbing body and absorbing article with the same
JP2017526834A (en) * 2014-07-02 2017-09-14 ヒュービス カンパニー リミテッド Thermal adhesive composite fiber for nonwoven fabric binder
CN105200664A (en) * 2015-09-25 2015-12-30 佛山市南海必得福无纺布有限公司 Spun-bonded hollow double-component non-woven fabric

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