JPS6021908A - Manufacture of composite monofilament - Google Patents
Manufacture of composite monofilamentInfo
- Publication number
- JPS6021908A JPS6021908A JP58128666A JP12866683A JPS6021908A JP S6021908 A JPS6021908 A JP S6021908A JP 58128666 A JP58128666 A JP 58128666A JP 12866683 A JP12866683 A JP 12866683A JP S6021908 A JPS6021908 A JP S6021908A
- Authority
- JP
- Japan
- Prior art keywords
- composite
- melting point
- sheath
- core
- component
- 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
Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D5/00—Formation of filaments, threads, or the like
- D01D5/28—Formation of filaments, threads, or the like while mixing different spinning solutions or melts during the spinning operation; Spinnerette packs therefor
- D01D5/30—Conjugate filaments; Spinnerette packs therefor
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F8/00—Conjugated, i.e. bi- or multicomponent, artificial filaments or the like; Manufacture thereof
- D01F8/04—Conjugated, i.e. bi- or multicomponent, artificial filaments or the like; Manufacture thereof from synthetic polymers
- D01F8/06—Conjugated, i.e. bi- or multicomponent, artificial filaments or the like; Manufacture thereof from synthetic polymers with at least one polyolefin as constituent
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Multicomponent Fibers (AREA)
- Treatment Of Fiber Materials (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は熱接着性を有し隼かつ強度の優れた複合モノフ
ィラメント(以下「複合MFJと略記する。)の製造法
に関するものである。更に詳しくは、鞘側に低融点ポリ
オレフィン樹脂成分を、芯側に融点の高いポリプロピレ
ン(以下[高融点PPJと略記する。)を使用して、鞘
芯型の口金を用いて溶融押出し冷却固化後延伸してなる
熱接着性を有し、かつ強度の優れたポリオレフィン樹脂
複合MPの製造法である。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing a composite monofilament (hereinafter abbreviated as "composite MFJ") that has thermal adhesive properties and excellent strength. Thermal adhesiveness is obtained by melt-extruding a melting point polyolefin resin component using a core side of polypropylene with a high melting point (hereinafter abbreviated as high melting point PPJ) using a sheath-core type die, cooling, solidifying, and stretching. This is a method for producing a polyolefin resin composite MP having the same properties and excellent strength.
一般にポリオレフィン樹脂を溶融押出し冷却後延伸して
なる単一成分のモノフィラメント(以下「通常MFJと
略記する。)は機械的強度、耐薬品性、耐腐食性、耐水
性、成形性等が優れていることから、ロープ、漁網等の
水産資材及び防虫網、防風網、ゴルフネット、遮光ネッ
ト、フィルター・1、土木シート等の陸上用ネット類に
加工され巾広く使用されている。In general, single-component monofilament (hereinafter abbreviated as MFJ), which is made by melt-extruding polyolefin resin, cooling and drawing it, has excellent mechanical strength, chemical resistance, corrosion resistance, water resistance, moldability, etc. Therefore, it is widely used and processed into marine materials such as ropes and fishing nets, as well as land nets such as insect nets, windbreak nets, golf nets, shading nets, Filter 1, and civil engineering sheets.
ところで陸上用ネット類は主に編織加工して使用されそ
の機械的強度が強いことが実用上の特徴となっているが
編織物の縦、横交絡部(以下「網目」と言う。)は結合
されておらず比較的に自由な為、編、織加工時及びネッ
ト製品の施行時あるいは実用状態によっては網目がずれ
てネット製品の主たる目的である遮蔽あるいは保護効果
を逸失したり外観の見映えが悪くなシ美観を損う等の欠
点がある。By the way, nets for land use are mainly used by knitting and weaving, and their mechanical strength is strong in practical use. Because it is relatively free, the mesh may shift during knitting, weaving, and when the net product is used or depending on the actual state of use, resulting in the loss of the shielding or protective effect that is the main purpose of the net product, or the appearance of the net product. There are disadvantages such as poor appearance and poor appearance.
一方、特殊回転口金を用い溶融押出しにより直接ネット
状に成形し網目が結合されたネット又はこのネット成形
品を更に縦横方向に延伸して得られるネット類の製網技
術が公知となっている。しかし、これらのモノフィラメ
ント(以下「MFJと略記する。)は、通常MF’から
なるネメト類の縦、横1本々々のMF強度が3t/d以
上であるのに比較して・共に1,5 t’/a以下と極
端に強度が低いためきわめて限られた簡易軽量物包装用
等にしか適用できない問題がある。On the other hand, there are well-known techniques for making nets that are directly formed into a net shape by melt extrusion using a special rotary die and have meshes joined together, or for nets obtained by further stretching this net molded product in the longitudinal and lateral directions. However, these monofilaments (hereinafter abbreviated as "MFJ") have a MF strength of 1,000 t/d or more in both vertical and horizontal directions, compared to the normal MF' nemets, which have a vertical and horizontal MF strength of 3 t/d or more. Since the strength is extremely low at less than 5 t'/a, there is a problem that it can only be applied to a very limited number of simple and lightweight packaging applications.
又、不織布分野に於いては、近年熱融着性機能を付与し
た複合繊維を使、用して布状にした後熱処理を施し網目
部を熱融着させたものが種々の用途に利用されているが
、これに使用される熱融着性複合繊維は繊度がほぼ1〜
30デニールと非常に細いため、通常MPとして使用さ
れている繊度100デニール以上の太物としてその複合
繊維を利用する場合は、繊維集束体とする必要があるか
ら、加工が繁雑になりそれにつれてコストが非常に高く
なる欠点がある。In addition, in the field of non-woven fabrics, in recent years composite fibers with heat-fusible properties have been used for various purposes, made into cloth-like fabrics and then heat-treated to heat-seal the mesh parts. However, the fineness of the heat-fusible composite fibers used for this is approximately 1~1.
Because the composite fiber is very thin at 30 denier, when using it as a thick material with a fineness of 100 denier or more, which is normally used as MP, it needs to be made into a fiber bundle, which requires complicated processing and costs accordingly. The disadvantage is that it is very high.
本発明の目的は、熱接着性を有し、強度が優れかつカー
ルがなく、層間剥離のない複合MFの製造方法を提供す
ることである。An object of the present invention is to provide a method for producing a composite MF that has thermal adhesive properties, excellent strength, no curling, and no delamination.
即ち、本発明は高密度ポリエチレン(以下jHDPEJ
と略記する。)又は直鎖状低密度ポリエチレン(以下[
LLDPEJと略記すム)もしくは、融点が135℃以
下のポリプロピレン(以下「低融点PPJと略記する。That is, the present invention uses high-density polyethylene (hereinafter referred to as jHDPEJ).
It is abbreviated as ) or linear low-density polyethylene (hereinafter [
(abbreviated as LLDPEJ) or polypropylene with a melting point of 135°C or less (hereinafter abbreviated as "low melting point PPJ").
)又はそれらの混合物である一低融点ポリオレフイン樹
脂と融点が150℃以上の高融点ポリプロピレンとを前
者を鞘、後者を芯とする鞘芯型に複合紡糸して得られる
複合MF未延伸糸であって、その低融点ポリオレフィン
樹脂成分と高融点PP成分との溶融流動指数比(以下1
’−FR比」と略記する。)が1.5以上7以下であり
、かつ複合比が30 : 70〜60:40であるもの
を、6本発明に用いるHDPB及びポリプロピレン(以
下[PPJと略記する。)は、いずれもエチレン又はプ
ロピレンの単独重合体のみならずエチレンを主体とした
プロピレン、ブテン−1等との共重合体又はプロピノン
を主体としたエチレン・ブテン−1等との共重合体も好
ましく用いることができる。又これらの重合体又はこれ
らの混合物には通常ポリオレフィン樹脂に添加される酸
化防止剤、紫外線吸収剤等の安定剤や着色剤、滑剤、帯
電防止剤、艶消剤2等の添加剤を必要に応じて添加する
ことができる。) or a mixture thereof, a low melting point polyolefin resin and a high melting point polypropylene having a melting point of 150° C. or higher, and a composite MF undrawn yarn obtained by composite spinning into a sheath-core type having the former as a sheath and the latter as a core. The melt flow index ratio of the low melting point polyolefin resin component and the high melting point PP component (hereinafter 1
It is abbreviated as '-FR ratio'. ) is 1.5 or more and 7 or less, and the composite ratio is 30:70 to 60:40.6 HDPB and polypropylene (hereinafter abbreviated as PPJ) used in the present invention are both ethylene or polypropylene. Not only a homopolymer of propylene but also a copolymer of propylene mainly composed of ethylene with 1-butene, etc., or a copolymer of ethylene and 1-butene mainly composed of propylene can be preferably used. In addition, these polymers or mixtures thereof require additives such as antioxidants, stabilizers such as ultraviolet absorbers, colorants, lubricants, antistatic agents, matting agents, etc. that are usually added to polyolefin resins. It can be added accordingly.
本発明に於いて鞘成分としてHDPE%LLDPE又は
低融点pp等を混合して用いる場合の混合方法は押出機
、パンパシーミキサー、タンブラ−ミキサー・ヘンシェ
ルミキサー等の通常の装置、方法で可能である。又複合
押出紡糸方法や装置は・2台の押出機と並列型あるいは
鞘芯型の複合口金を用いて複合押出しする等の公知の技
術で可能であるが、本発明に於いては紡糸、延伸安定性
及び延伸された複合MPの鞘芯成分境界面層の難剥離性
等の面で有利となる鞘芯型複合口金を使用することが好
ましい。In the present invention, when HDPE%LLDPE or low melting point PP, etc. are mixed and used as a sheath component, the mixing method can be carried out using conventional equipment and methods such as an extruder, a Panpassie mixer, a tumbler mixer, a Henschel mixer, etc. . In addition, the composite extrusion spinning method and device are possible using known techniques such as composite extrusion using two extruders and a parallel type or sheath-core type composite spinneret, but in the present invention, spinning, drawing, etc. It is preferable to use a sheath-core type composite cap, which is advantageous in terms of stability and difficulty in peeling off the sheath-core component interface layer of the drawn composite MP.
複合MFの芯側に使用される高融点PPの溶融流動指数
は通常MPに使用される0、3〜15の範囲のものでよ
いが、その融点は150℃以上を必要とし、これと複合
される鞘側の低融点ポリオレフィン樹脂成分とのFR比
は1.5以上7以下で本発明の効果が顕著となる。即ち
、芯成分の融点が150℃以下では芯成分の基本的性能
である強度が低下し、更には収縮性が大きくなりネット
状に編、織加工した後のヒートセット時に於いて収縮・
変形が激しくなシ好ましくない。FI’L比は、1,5
以下では紡糸、延伸性が不安定でしかもネットの熱接着
性に劣り、7以上になると鞘成分と芯成分のノズル内で
の流動性が異り、又画成分間の結晶化挙動差あるいは溶
融状態から冷却固化に到る過程の鞘芯層の体積収縮差に
よる応力歪が大きくなり押出未延伸糸がノズル出口で湾
曲あるいはカール状に&D可紡性が悪化する。又鞘芯成
分に掛かる延伸応力の差が大きくな9延伸切れ又は延伸
糸がカールし易くなり延伸トラブルが発生し易くなる。The melt flow index of the high melting point PP used for the core side of the composite MF may be in the range of 0, 3 to 15, which is normally used for MP, but its melting point needs to be 150°C or higher, and the The effect of the present invention becomes remarkable when the FR ratio with respect to the low melting point polyolefin resin component on the sheath side is 1.5 or more and 7 or less. That is, if the melting point of the core component is below 150°C, the strength, which is the basic performance of the core component, will decrease, and furthermore, the shrinkability will increase, causing shrinkage and shrinkage during heat setting after knitting and weaving into a net shape.
Severe deformation is not desirable. FI'L ratio is 1.5
Below 7, the spinning and drawing properties are unstable, and the net thermal adhesion is poor, and above 7, the fluidity of the sheath component and core component in the nozzle is different, and there is also a difference in crystallization behavior between the fraction components or melting. The stress strain due to the difference in volume shrinkage of the sheath-core layer in the process of cooling and solidifying increases, and the extruded undrawn yarn becomes curved or curled at the nozzle exit, deteriorating spinnability. In addition, if the difference in stretching stress applied to the sheath-core components is large, stretching breakage or curling of the drawn yarn becomes more likely, and stretching troubles are more likely to occur.
鞘成分として使用される低融点ポリオレフィン樹脂は複
合MPに熱融着による接着性を付与させる成分となるも
のであシ、HDPE%LLDPE、低融点PPの単独使
用で充分効果が顕われるがそれらの2種類以上の混合使
用によっても単独使用と同様の効果が顕われ、その場合
の成分の組合わせは、同程度の流動性を持つものの組合
せが好ましい。鞘成分として低融点PPセットする場合
必然的に高温長時間となシ・熱接着ができたとしてもヒ
ートセット時の熱により複合MP芯成分の配向が戻り強
度が低下し、芯成分の受け持つ強度維持特性を損うこと
になるので好ましくない。The low melting point polyolefin resin used as the sheath component is a component that imparts adhesive properties to the composite MP by heat fusion.Although the use of HDPE%LLDPE and low melting point PP alone is sufficient, the effect is apparent. The same effect as using a mixture of two or more types can be obtained, and in this case, it is preferable to use a combination of components that have the same fluidity. When setting low-melting-point PP as a sheath component, it is inevitably necessary to use high temperature for a long time.Even if thermal bonding is possible, the orientation of the composite MP core component returns due to the heat during heat setting and the strength decreases, reducing the strength that the core component is responsible for. This is not preferable because it will impair the maintenance characteristics.
鞘成分と芯成分の鞘/芯の複合比は・30ニアo〜60
: 40の範囲が好ましい。鞘成分が30%以下では
紡糸、延伸性が不良になり易く更に複合MPの熱接着成
分が少なくなりネットの網目接着部の結合力が弱くなり
好ましくない。The sheath/core composite ratio of the sheath component and core component is ・30 near o to 60
: A range of 40 is preferred. If the sheath component is less than 30%, the spinning and drawing properties tend to be poor, and furthermore, the thermal adhesive component of the composite MP decreases and the bonding strength of the mesh bonding portion of the net becomes weak, which is not preferable.
他方芯成分が40チ以下になると芯成分の受け持つ基本
要素である強度が低下して好ましくない。On the other hand, if the core component is less than 40 inches, the strength, which is a basic element of the core component, decreases, which is not preferable.
本発明に於ける延伸は、通常MFでとられている一般的
な装置及び方法で可能であり、その延伸倍率は6〜9倍
が適当である。複合MPの場合通常MFに比べて構造的
に強度嘉低目になる為6倍以下では強度が低く、9倍以
上になると強度は充分であるφ;、複合構造特有の重合
体間境界面の相溶性が乏しいことに起因して鞘芯成分の
延伸性の差が著るしくなり延伸過程に於いて鞘成分のメ
クレあるいは剥離等のトラブルが発生し、又延伸後にカ
ールし易くなり巻工程での巻姿不良又は巻りズレ等の巻
取不良トラブルの原因になり好ましくない。尚延伸工程
の後に延伸糸の収縮性を改善する目的で一般的な装置及
び方法によシ緩和アニールを施ずことも好ましく用いる
ことができる。Stretching in the present invention can be carried out using the general equipment and method normally used in MF, and the appropriate stretching ratio is 6 to 9 times. In the case of composite MP, the strength is structurally lower than that of normal MF, so if it is less than 6 times the strength is low, and if it is more than 9 times the strength is sufficient. Due to poor compatibility, the difference in stretchability between the sheath and core components becomes significant, causing problems such as curling or peeling of the sheath components during the stretching process, and the sheath components tend to curl after stretching, resulting in the sheath core components becoming more easily drawn during the winding process. This is undesirable as it may cause problems such as poor winding appearance or winding misalignment. In order to improve the shrinkability of the drawn yarn after the drawing process, it is also preferable to perform relaxation annealing using a general apparatus and method.
本発明によって得られた複合MPは通常MP並みの強度
特性を維持しかつ熱接着性を兼ね備えたものである。こ
の複合MPを用いて編・織加工されたネット状物を熱ロ
ール又、熱カレンダーあるいは熱風又はスチーム処理等
の一般的な方法で熱処理を施すことにより得られた網目
部が熱接着結合されたネット状物は、通常MFからなる
ネット状物盤みの強度を保持し、がっ網目部の目ズレが
起きにくいネット状製品となる。The composite MP obtained by the present invention maintains strength characteristics comparable to those of ordinary MP and has thermal adhesive properties. A net-like article knitted and woven using this composite MP is heat-treated by a general method such as a heat roll, a heat calender, or a hot air or steam treatment, and the resulting mesh parts are bonded by thermal adhesive. The net-like material maintains the strength of the net-like material usually made of MF, and becomes a net-like product in which mesh portions are less likely to shift.
以下に実施例及び比較例によシ本発明について説明する
。伺評価の基準及び表中の記号は下記の如くである。The present invention will be explained below using Examples and Comparative Examples. The criteria for evaluation and the symbols in the table are as follows.
1)MI・・・・・・・・・・・ポリエチレン樹脂の溶
融流動指数(AS TMD−1238(L)による。即
ち、オリフィス孔径2.092±0.002閣、温度1
90℃、荷重2.16 Of 、の条件下で1o分間押
し出した試料の重量を
1数で表したもの)
2)MFR・・・・・・・・・・・・ポリプロピレン樹
脂の溶融流動指数(温度を230℃とする以外は
1)と同様である。)
3)FR比・・・・・・・・・・・・鞘成分と芯成分の
溶融流動指数の比(1)及び2)で測定したMIとMP
Rとの比)
4)複合比・・・・・・・・・・・・鞘芯成分を各単独
に押出しその未延伸糸の単位時間当りの重量測定
を行なった鞘芯成分の重量比率
5)紡糸性・・・・・・・・・・・・押出未延伸糸の状
態O:正常。1) MI・・・・・・・・・Melt flow index of polyethylene resin (according to AS TMD-1238 (L). That is, orifice hole diameter 2.092±0.002mm, temperature 1
The weight of the sample extruded for 10 minutes under the conditions of 90°C and 2.16 of The procedure is the same as in 1) except that the temperature is 230°C. ) 3) FR ratio・・・・・・・・・MI and MP measured by the ratio of melt flow index of sheath component and core component (1) and 2)
(ratio with R) 4) Composite ratio: Weight ratio of the sheath-core components obtained by extruding each sheath-core component individually and measuring the weight per unit time of the undrawn yarn: 5 ) Spinnability: Condition of extruded undrawn yarn: O: Normal.
Δ:未延伸−系がノズル出口で湾曲する。Δ: Unstretched - the system curves at the nozzle exit.
×:未延伸糸がノズル出口で湾曲し、 紡糸が不能になる。×: The undrawn yarn is curved at the nozzle exit, Spinning becomes impossible.
6)延伸性・・・・・・・・・・・・延伸の状態で評価
した。尚、*印は延伸不能を表わす。6) Stretchability: Evaluation was made in the stretched state. Note that the * mark indicates that stretching is not possible.
○:延伸糸においても延伸プロセスに おいても正常。○: Even in drawn yarn, the drawing process It is normal to leave it on.
△:延伸糸が白化状になる。Δ: The drawn yarn becomes white.
X:延伸切れ又はカール状になり巻 取トラブルを発生し易い。X: Stretched or curled Easy to cause trouble when handling.
7)複合MPの剥離性・・・・・・・・・・・・鞘芯成
分の層間分離性
○:強制的に鞘層を剥ごうとしても
剥離しない。7) Peelability of composite MP: Separability between layers of sheath-core component ○: The sheath layer does not peel off even if an attempt is made to forcibly peel it off.
△:強制的に鞘層な剥げば剥離する が通常では問題なし。△: If the sheath layer is forcibly peeled off, it will peel off. But normally there is no problem.
×:延伸巻取工程にて剥離し易くな る。×: Easy to peel off during stretching and winding process Ru.
8)ネット状物のヒートセット(熱接着)法・・・複合
MFを使い通常の方法で織った
ネット状物を140〜150℃の熱
風加熱槽内に1.5分間放置する。8) Heat-setting (thermal bonding) method for net-like material: A net-like material woven using a composite MF in a conventional manner is left in a hot air heating tank at 140 to 150° C. for 1.5 minutes.
9)熱接着加工後の複合MP強度・・・・・・・・・・
・・網目部が熱接着されたネット状物から複合
MPを採取し引張強度を測定し評価
した。9) Composite MP strength after thermal bonding process...
...Composite MP was sampled from a net-like material whose mesh portions were thermally bonded, and its tensile strength was measured and evaluated.
○: 4.Ot/dより大
△: 3.0〜4.Of/d
X : 3.Of/dより小
注)引張強度測定条件
■引張試験機 東洋ボールドウィン社製・テンンロン■
型
■チャック間 200mn
■引張速度 200wII/min
■室 温 23℃
■湿 度 50チ
10)ネット状物の網目部の接着性・・・・・・・・・
・・・網目郡部の接着強力を測定
Q:接着強力30Ofより大
△: 〃 10 o〜300 f
X: // 100より小(−窓付い
ているが接着性微弱なものが含ま
れる。)
実施例−1及び比較例−1
芯成分として融点が161℃でMFRが種々のPPを、
鞘成分として種々なMIのHDPEもしくはLLDPE
又は融点が128℃のPPを、各単独(二用いて口径4
0wnの押出機2台及び口径が1.5mの鞘芯型複合口
金を用い、窓側押出温度を260℃、鞘側押出温度を2
40℃・複合口金温度260℃として溶融押出し冷却に
よる紡糸を行い、複合比が50:50の鞘芯型複合未延
伸糸を得た。これを湿式加熱延伸装置により5〜1o倍
に延伸し、450デニールの各種複合MFを得た。その
ときの押出未延伸糸の紡糸性と延伸性及び複合MPの鞘
芯層間剥離性についての結果を第1表に示す。更に上記
プロセスでつくられた各種複合MFを用いて織り密度が
タテ5本/ 25 mm X 5本/ 25 mmのネ
ット状物に成織した後140℃の熱風加熱槽にて1.5
分間ヒートセットして取り出して網目部の熱接着性と複
合MFの残存強度を評価した結果を第2表に示す。○: 4. Greater than Ot/d: 3.0-4. Of/dX: 3. Smaller than Of/d Note) Tensile strength measurement conditions ■Tensile tester Tennron manufactured by Toyo Baldwin ■
Mold ■Chuck distance 200mm ■Tension speed 200wII/min ■Room temperature 23℃ ■Humidity 50cm 10) Adhesion of the mesh part of the net-like material...
...Measure the adhesive strength of the mesh area Q: Adhesive strength greater than 30Of △: 〃 10 o ~ 300 f Example-1 and Comparative Example-1 PP with a melting point of 161°C and various MFRs was used as a core component.
HDPE or LLDPE of various MI as sheath component
Or PP with a melting point of 128℃, each singly (using two with a diameter of 4
Using two 0wn extruders and a sheath-core composite nozzle with a diameter of 1.5 m, the window side extrusion temperature was 260°C and the sheath side extrusion temperature was 260°C.
Spinning was performed by melt extrusion cooling at 40° C. and composite die temperature of 260° C. to obtain a sheath-core composite undrawn yarn with a composite ratio of 50:50. This was stretched 5 to 10 times using a wet heating stretching device to obtain various composite MFs of 450 denier. Table 1 shows the results regarding the spinnability and drawability of the extruded undrawn yarn and the peelability between the sheath and core layers of the composite MP. Furthermore, the various composite MFs produced by the above process were woven into a net-like material with a weaving density of 5 vertical fibers/25 mm x 5 fibers/25 mm, and then woven in a hot air heating tank at 140°C to a density of 1.5
Table 2 shows the results of evaluating the thermal adhesion of the mesh portion and the residual strength of the composite MF after heat setting for a minute and taking it out.
これらの表から161℃の高融点PPを芯成分とし、H
DPE又はLLDPB又は融点が128℃の低融点PP
を各単独に鞘成分とした場合・FR比が1.5〜7.0
及び延伸が6〜9倍の範囲に於いて剥離のない安定した
複合構造の延伸MPが得られることがわかり、そのうち
でも鞘成分を低融点PPとした場合は特(=剥離し難い
複合MFが得られることがわかる。更(二それらの複合
MPによるネット状物をヒートセットすることにより得
られたネット状物は網目部が熱接着によシ結合され、強
度も充分維持されていることがわかる。From these tables, PP with a high melting point of 161°C is used as the core component, and H
DPE or LLDPB or low melting point PP with a melting point of 128°C
When each is individually used as a sheath component, the FR ratio is 1.5 to 7.0
It was found that a stretched MP with a stable composite structure without peeling can be obtained in the stretching range of 6 to 9 times, and among these, when the sheath component is low melting point PP, it is especially possible to obtain a stretched MP with a stable composite structure (= composite MF that is difficult to peel off). Furthermore, in the net-like material obtained by heat-setting the net-like material made of these composite MPs, the mesh portions are bonded together by thermal adhesion, and the strength is sufficiently maintained. Recognize.
実施例−2及び比較例−2
芯成分として融点が161℃でMFRが3.1のPPを
鞘成分としてHDPB、LLDPB又は融点が128℃
のPPを各単独に用いて、実施例−1と同じ条件による
紡糸を行い、複合比が種々の鞘芯型複合、未延伸糸を得
た。これを湿式加熱延伸装置により延伸し、450デニ
ールの複合MFを得た。そのときの未延伸糸の紡糸性と
延伸性並びに得られた複合MFi二ついて実施例−1と
同様にネット状物の熱接着性と残存強度の評価を行った
。その結果を第3表(二示す。Example-2 and Comparative Example-2 PP with a melting point of 161°C and MFR of 3.1 as a core component and HDPB, LLDPB or a melting point of 128°C as a sheath component
Each of these PPs was used individually and spinning was performed under the same conditions as in Example 1 to obtain sheath-core type composite, undrawn yarns with various composite ratios. This was stretched using a wet heating stretching device to obtain a composite MF of 450 denier. The spinnability and drawability of the undrawn yarn and the resulting composite MFi were evaluated for the thermal adhesion and residual strength of the net-like material in the same manner as in Example-1. The results are shown in Table 3.
第3表から鞘芯成分の複合比は、30 : ’i’0〜
60:40の範囲で、紡糸延伸安定性及び複合M、Fに
よるネット状物の熱接着性と残存強度が優れていること
がわかる。From Table 3, the composite ratio of sheath-core components is 30:'i'0~
It can be seen that within the range of 60:40, the spinning drawing stability and the thermal adhesion and residual strength of the composite M and F net-like products are excellent.
実施例−3及び比較例−3
芯成分として融点が161℃でMFRが3.1のPPと
鞘成分にMFRが15.5で融点の異る種々の低融点P
Pを各単独に用いて、実施例−1と同じ条件により複合
MFをつくり、ネット状物の熱接着性と残存強度につい
て評価した。Example-3 and Comparative Example-3 A core component of PP with a melting point of 161°C and an MFR of 3.1, and a sheath component of various low melting point Ps with an MFR of 15.5 and different melting points.
Composite MFs were prepared using P alone under the same conditions as in Example 1, and the thermal adhesion and residual strength of the net-like materials were evaluated.
その結果を第4表に示す。The results are shown in Table 4.
第4表から、鞘成分に低融点PPを使う場合、融点が1
35℃以上になるとネット状物のヒートセット条件によ
り熱接着性と残存強度の相反性が大きくなり融点が高く
なるにつれて熱接着性が悪くなり熱接着性を良くするた
めにヒートセット温度を上げると逆に熱接着加工後の複
合MP強度が低くなり過ぎることがわかる。From Table 4, when using low melting point PP for the sheath component, the melting point is 1.
When the temperature exceeds 35℃, the reciprocity between thermal adhesion and residual strength increases depending on the heat setting conditions of the net-like material, and as the melting point increases, the thermal adhesion deteriorates.In order to improve the thermal adhesion, increasing the heat setting temperature On the contrary, it can be seen that the composite MP strength after thermal bonding becomes too low.
実施例−4
融点が161℃でMFRが3゜1のPPを芯成分に、H
DPB、LLDPE又は融点が128℃のPPを各1:
1の比率でヘンンエルミキサーで混合したのち、口径4
0咽の押出機で押出造粒した混合樹脂を鞘成分として実
施例−1と同様の評価をした。その結果を第5表に示す
。Example-4 H
1 each of DPB, LLDPE or PP with a melting point of 128°C:
After mixing in a Hennel mixer at a ratio of 1:1,
The same evaluation as in Example 1 was carried out using the mixed resin extruded and granulated using a zero-throat extruder as the sheath component. The results are shown in Table 5.
第5表から、鞘成分をHDPK、LLDPE及び低融点
PPの混合物とした場合でも単独成分と同様の効果があ
ることがわかる。Table 5 shows that even when the sheath component is a mixture of HDPK, LLDPE, and low melting point PP, it has the same effect as the single component.
実施例−5及び比較例−4
芯成分としてMFRが同程度で融点が種々のPP′ta
0:、鞘成分としてHDPE、LLDPE又は融点が1
28℃のPPを、各単独に用い、実施例−1と同様に評
価した結果を第6表に示す。Example-5 and Comparative Example-4 PP'ta with similar MFR and various melting points as core components
0: HDPE, LLDPE or melting point 1 as the sheath component
Table 6 shows the results of evaluation in the same manner as in Example-1 using 28° C. PP alone.
第6表から、芯成分の融点が150℃以下になると熱接
着性は問題ないが残存強度の低下が著しいことがわかる
。From Table 6, it can be seen that when the melting point of the core component is 150° C. or lower, there is no problem in thermal adhesion, but the residual strength is significantly reduced.
Claims (1)
は融点が130℃以下のポリプロピレン又はそれらの混
合物である低融点ポリオレフィン樹脂と融点が150℃
以上のポリプロピレンとを前者を鞘、後者を芯とした鞘
芯型に複合紡糸して得られる複合モノフィラメント未延
伸糸であって、その低融点ポリオレフィン樹脂成分と融
点が150℃以上のポリプロピレン成分との溶融流動指
数比が1.5以上7.○以下であシ・かつ鞘/芯の複合
比が30:’i’o〜6o:4oであるものを6〜9倍
に延伸することを特徴とする熱接着性を有し、かつ強度
の優れた複合モノフィラメントの製造法。Low melting point polyolefin resin, which is high density polyethylene, linear low density polyethylene, polypropylene with a melting point of 130°C or less, or a mixture thereof, and a melting point of 150°C
A composite monofilament undrawn yarn obtained by composite spinning the above polypropylene into a sheath-core type with the former as a sheath and the latter as a core, comprising a low melting point polyolefin resin component and a polypropylene component having a melting point of 150°C or higher. 7. Melt flow index ratio is 1.5 or more. ○ A material with thermal adhesive properties and strength characterized by stretching 6 to 9 times as follows and the sheath/core composite ratio is 30:'i'o to 6o:4o. A superior method for producing composite monofilaments.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58128666A JPS6021908A (en) | 1983-07-14 | 1983-07-14 | Manufacture of composite monofilament |
DE8484304721T DE3468448D1 (en) | 1983-07-14 | 1984-07-11 | Process for producing composite monofilaments |
EP84304721A EP0132110B1 (en) | 1983-07-14 | 1984-07-11 | Process for producing composite monofilaments |
KR1019840004154A KR870000442B1 (en) | 1983-07-14 | 1984-07-14 | Multi-monofilament's producing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58128666A JPS6021908A (en) | 1983-07-14 | 1983-07-14 | Manufacture of composite monofilament |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6021908A true JPS6021908A (en) | 1985-02-04 |
JPS633969B2 JPS633969B2 (en) | 1988-01-27 |
Family
ID=14990434
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58128666A Granted JPS6021908A (en) | 1983-07-14 | 1983-07-14 | Manufacture of composite monofilament |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0132110B1 (en) |
JP (1) | JPS6021908A (en) |
KR (1) | KR870000442B1 (en) |
DE (1) | DE3468448D1 (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61194221A (en) * | 1985-02-18 | 1986-08-28 | Chisso Corp | Elastic conjugated yarn and cloth using same |
JPS63266688A (en) * | 1987-04-24 | 1988-11-02 | Hitachi Ltd | Magnetic recording device |
JPS63280543A (en) * | 1987-05-13 | 1988-11-17 | Nec Corp | Communication control equipment |
JPS643549U (en) * | 1987-06-29 | 1989-01-10 | ||
JPS6426754A (en) * | 1987-07-22 | 1989-01-30 | Showa Denko Kk | Cloth for shrink packaging |
JPS6417758U (en) * | 1987-07-24 | 1989-01-30 | ||
JPH0261156A (en) * | 1988-08-23 | 1990-03-01 | Unitika Ltd | Nonwoven fabric comprising hot adhesive filaments |
JPH03167314A (en) * | 1989-11-27 | 1991-07-19 | Ube Nitto Kasei Co Ltd | Elastic conjugated yarn |
JPH06330444A (en) * | 1993-05-21 | 1994-11-29 | Ube Nitto Kasei Co Ltd | Polypropylene fiber mat |
JPH10266035A (en) * | 1997-03-25 | 1998-10-06 | Taniyama Kagaku Kogyo Kk | Complex type plastic deformation product and its production |
US6878650B2 (en) | 1999-12-21 | 2005-04-12 | Kimberly-Clark Worldwide, Inc. | Fine denier multicomponent fibers |
JP2021102821A (en) * | 2019-12-25 | 2021-07-15 | 宇部エクシモ株式会社 | Black synthetic fiber |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0819570B2 (en) * | 1986-09-12 | 1996-02-28 | チッソ株式会社 | Heat-bondable composite fiber and method for producing the same |
JPH0192415A (en) * | 1987-10-02 | 1989-04-11 | Unitika Ltd | Heat-bondable fiber and nonwoven fabric thereof |
DE3813773A1 (en) * | 1988-04-23 | 1989-11-02 | Henkel Kgaa | DETERGENT PRODUCTS |
DK245488D0 (en) * | 1988-05-05 | 1988-05-05 | Danaklon As | SYNTHETIC FIBER AND PROCEDURES FOR PRODUCING THEREOF |
US5382400A (en) | 1992-08-21 | 1995-01-17 | Kimberly-Clark Corporation | Nonwoven multicomponent polymeric fabric and method for making same |
US5405682A (en) | 1992-08-26 | 1995-04-11 | Kimberly Clark Corporation | Nonwoven fabric made with multicomponent polymeric strands including a blend of polyolefin and elastomeric thermoplastic material |
US5336552A (en) | 1992-08-26 | 1994-08-09 | Kimberly-Clark Corporation | Nonwoven fabric made with multicomponent polymeric strands including a blend of polyolefin and ethylene alkyl acrylate copolymer |
CA2092604A1 (en) | 1992-11-12 | 1994-05-13 | Richard Swee-Chye Yeo | Hydrophilic, multicomponent polymeric strands and nonwoven fabrics made therewith |
US5482772A (en) | 1992-12-28 | 1996-01-09 | Kimberly-Clark Corporation | Polymeric strands including a propylene polymer composition and nonwoven fabric and articles made therewith |
CN107988654B (en) * | 2017-12-19 | 2020-08-04 | 广东蒙泰高新纤维股份有限公司 | High-strength PE-PP double-component sheath-core structure composite filament and preparation method thereof |
CN114150411A (en) * | 2021-10-26 | 2022-03-08 | 浙江龙仕达科技股份有限公司 | Preparation method of high-strength composite covering yarn |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55137220A (en) * | 1979-04-11 | 1980-10-25 | Chisso Corp | Flame-retardant composite fiber and its production |
JPS5658009A (en) * | 1979-10-09 | 1981-05-20 | Chisso Corp | Preparation of flame-retardant composite fiber |
JPS5739216A (en) * | 1980-08-20 | 1982-03-04 | Chisso Corp | Flame retardant composite fiber and its preparation |
JPS57101023A (en) * | 1980-12-10 | 1982-06-23 | Daiwa Spinning Co Ltd | Sheath-core composite polyolefin fiber containing inorganic material and its preparation |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5212830B2 (en) * | 1972-11-25 | 1977-04-09 | ||
JPS5386836A (en) * | 1976-12-29 | 1978-07-31 | Chisso Corp | Crimpless, hot melt conjugate fiber and its production |
US4285748A (en) * | 1977-03-11 | 1981-08-25 | Fiber Industries, Inc. | Selfbonded nonwoven fabrics |
JPS53147816A (en) * | 1977-05-24 | 1978-12-22 | Chisso Corp | Hot-melt fiber of polypropylene |
-
1983
- 1983-07-14 JP JP58128666A patent/JPS6021908A/en active Granted
-
1984
- 1984-07-11 DE DE8484304721T patent/DE3468448D1/en not_active Expired
- 1984-07-11 EP EP84304721A patent/EP0132110B1/en not_active Expired
- 1984-07-14 KR KR1019840004154A patent/KR870000442B1/en not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55137220A (en) * | 1979-04-11 | 1980-10-25 | Chisso Corp | Flame-retardant composite fiber and its production |
JPS5658009A (en) * | 1979-10-09 | 1981-05-20 | Chisso Corp | Preparation of flame-retardant composite fiber |
JPS5739216A (en) * | 1980-08-20 | 1982-03-04 | Chisso Corp | Flame retardant composite fiber and its preparation |
JPS57101023A (en) * | 1980-12-10 | 1982-06-23 | Daiwa Spinning Co Ltd | Sheath-core composite polyolefin fiber containing inorganic material and its preparation |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61194221A (en) * | 1985-02-18 | 1986-08-28 | Chisso Corp | Elastic conjugated yarn and cloth using same |
JPS63266688A (en) * | 1987-04-24 | 1988-11-02 | Hitachi Ltd | Magnetic recording device |
JPS63280543A (en) * | 1987-05-13 | 1988-11-17 | Nec Corp | Communication control equipment |
JPS643549U (en) * | 1987-06-29 | 1989-01-10 | ||
JPS6426754A (en) * | 1987-07-22 | 1989-01-30 | Showa Denko Kk | Cloth for shrink packaging |
JPH0529886Y2 (en) * | 1987-07-24 | 1993-07-30 | ||
JPS6417758U (en) * | 1987-07-24 | 1989-01-30 | ||
JPH0261156A (en) * | 1988-08-23 | 1990-03-01 | Unitika Ltd | Nonwoven fabric comprising hot adhesive filaments |
JPH03167314A (en) * | 1989-11-27 | 1991-07-19 | Ube Nitto Kasei Co Ltd | Elastic conjugated yarn |
JPH06330444A (en) * | 1993-05-21 | 1994-11-29 | Ube Nitto Kasei Co Ltd | Polypropylene fiber mat |
JPH10266035A (en) * | 1997-03-25 | 1998-10-06 | Taniyama Kagaku Kogyo Kk | Complex type plastic deformation product and its production |
US6878650B2 (en) | 1999-12-21 | 2005-04-12 | Kimberly-Clark Worldwide, Inc. | Fine denier multicomponent fibers |
JP2021102821A (en) * | 2019-12-25 | 2021-07-15 | 宇部エクシモ株式会社 | Black synthetic fiber |
Also Published As
Publication number | Publication date |
---|---|
KR870000442B1 (en) | 1987-03-10 |
DE3468448D1 (en) | 1988-02-11 |
EP0132110A2 (en) | 1985-01-23 |
JPS633969B2 (en) | 1988-01-27 |
EP0132110A3 (en) | 1985-06-05 |
EP0132110B1 (en) | 1988-01-07 |
KR850001316A (en) | 1985-03-18 |
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