Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6346180B2 - - Google Patents
[go: Go Back, main page]

JPS6346180B2 - - Google Patents

Info

Publication number
JPS6346180B2
JPS6346180B2 JP18952881A JP18952881A JPS6346180B2 JP S6346180 B2 JPS6346180 B2 JP S6346180B2 JP 18952881 A JP18952881 A JP 18952881A JP 18952881 A JP18952881 A JP 18952881A JP S6346180 B2 JPS6346180 B2 JP S6346180B2
Authority
JP
Japan
Prior art keywords
forming
yarn
sheath
thread
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
Application number
JP18952881A
Other languages
Japanese (ja)
Other versions
JPS5891841A (en
Inventor
Kunio Shibata
Tomoji Kanemura
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.)
Mitsubishi Chemical Corp
Original Assignee
Mitsubishi Rayon Co Ltd
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 Mitsubishi Rayon Co Ltd filed Critical Mitsubishi Rayon Co Ltd
Priority to JP18952881A priority Critical patent/JPS5891841A/en
Publication of JPS5891841A publication Critical patent/JPS5891841A/en
Publication of JPS6346180B2 publication Critical patent/JPS6346180B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は新規な特殊複合糸の製造方法に関する
ものである。 一般に意匠効果を目的とした複合糸の製造方法
は多岐多様であり、紡績糸の場合はスラブ糸、ネ
ツプ糸等、紡績工程で糸条に変化を与えることに
よつて得られるが複雑な技術もしくは工程が必要
であり、且つ意匠性での多様化は望め得ず、原理
的に生産性も低い。又フイラメント糸については
生産性と新規な糸条形態が得られる点で加圧流体
を利用した各種方法が提案されているが、これも
主として糸条の混繊・交絡方式であるため機構が
複雑で品質の安定性に問題があり、且つ単能機で
ある場合が多く、糸条形態に大きな変化を与え得
ないという欠点がある。更に、意匠撚糸機を利用
する紡績糸もしくはフイラメント糸から成るいわ
ゆる意匠撚糸と呼ばれる複合糸は、その多様性に
おいて優れているが、複雑な機構・技術を必要と
し、原理的に生産性が著しく低いという重大な欠
陥が解決されるに到つていない。 本発明者等はかかる従来法の問題点を解消すべ
く鋭意検討した結果本発明に到達したものであつ
て、その発明の要旨とするところは、周面の接線
方向に空気流入孔を有し、その内部中心軸上に中
空円錘体と環状体とを対向して設けた旋回渦流発
生の為の円筒体を2ケ直列に配置し各円筒体を吸
引により負圧状態として芯部形成用糸条を各円筒
体の中心軸に沿つて走行せしめると共に、鞘部形
成用糸条を各円筒体の空気流入孔より少くとも1
本づつ芯部形成用糸条の走行速度以上の速度で供
給し、中空円錘体の先端部で負圧旋回渦流の作用
により各鞘部形成用糸条を芯部形成用糸条の周囲
に加撚状態で絡合せしめることを特徴とする特殊
複合糸の製法にある。 以下図面に従つて本発明を詳細に説明すると、
第1図は本発明の実施に使用する装置の一例を示
す側面図で、同図において、芯部形成用糸条1は
張力調整装置4及び負圧源15に連結された旋回
渦流発生円筒8,11の糸条導入孔7を経て該旋
回渦流発生円筒8,11の中心軸に沿つて走行す
る一方これとは別の鞘部形成用糸条2は張力調整
装置4′、フイードローラー5,5′、糸条ガイド
9を経て、前述旋回流発生円筒8の周面接線方向
に設けられた空気流入孔10から該旋回渦流発生
円筒8内に供給される。同様にこれとは別の鞘部
形成糸条3も張力調整装置4″、フイードローラ
ー6,6′、糸条ガイド12を経て旋回渦流発生
円筒11の周面接線方向に設けられた空気流入孔
13から該旋回渦流発生円筒11内に供給され
る。 このようにしてそれぞれの旋回渦流発生円筒
8,11内に供給された鞘部形成用糸条2,3は
それぞれ芯部形成用糸条1に負圧旋回渦流の作用
により加撚絡合されて孔出し孔14を経て特殊複
合糸16となり、捲き取り装置によりチーズ17
として捲き取られる。 そこで、前述特殊複合糸16の形成過程を第2
図及び第3図により更に詳細に説明すると、鞘部
形成用糸条2,3はそれぞれ空気流入孔10,1
3から吸引気流に導かれ、芯部形成用糸条1以上
好ましくは数倍以上の過剰供給が行なわれて旋回
渦流発生円筒8,11内に供給されるため、該旋
回渦流発生円筒8,11内で適度なたるみを生じ
つつ、負圧旋回渦流作用によりループ群19,2
2がそれぞれ連続的に発生する。これらループ群
は更に負圧旋回渦流作用により旋回渦流発生円筒
8,11内の中心部に設けられた環状体18,2
1上方の中空円錘体20,23の先端部で芯部形
成用糸条1の周面に先ず鞘部形成用糸条2が続い
て鞘部形成用糸条3が加撚状態で連続的に絡合さ
れて特殊複合糸16を形成する。尚、この時、旋
回渦流発生円筒8,11が同一のもので鞘部形成
用糸条2,3が同一種類、同一供給量であれば特
殊複合糸16は嵩高性に優れた均整なものとな
り、鞘部形成用糸条2,3を異種類とするか、或
いは供給量をそれぞれ変更することにより形状変
化に富んだ多様な特殊複合糸とすることができ
る。 又旋回渦流発生円筒8,11の空気流入孔1
0,13を互いに逆方向の負圧旋回渦流を生ずる
ように設けると、例えば芯部形成用糸条1に対し
て、先ず円筒8により鞘部形成用糸条2を右撚加
撚状態で絡合せしめた後、円筒11により鞘部形
成用糸条3を左撚加撚状態で絡合せしめて第4図
ロの如きスラブ調複合糸を製造することができ
る。 上述の如く構成された本発明によれば、吸引に
よる高速の負圧旋回渦流を有効利用するものであ
るため、従来方法のような複雑な機構・技術を必
要とせず、従つて経済的で高生産性が得られると
いう利点と多種類の糸形態の製造に適応でき、且
つ加撚状態の糸構造となるため形態の安定性、品
質に優れるなど、多大の工業的効果を奏するもの
である。 実施例 1 空気流入孔10,13を同方向の旋回渦流を生
ずるように設けた第1図の装置により主な条件を
第1表の通り設定して、特殊複合糸の製造を行な
つたところ、しなやかできわめて嵩高な紬調意匠
効果に優れた第4図イの如き特殊複合糸が得られ
た。
The present invention relates to a method for producing a novel special composite yarn. In general, there are a wide variety of methods for producing composite yarns for the purpose of design effects, and in the case of spun yarns, slub yarns, net yarns, etc. can be obtained by changing the threads during the spinning process, but complex yarns or It requires a lot of steps, does not allow for diversification in terms of design, and has low productivity in principle. In addition, various methods using pressurized fluid have been proposed for filament yarns in order to increase productivity and obtain new yarn forms, but these methods are also complicated in mechanism because they mainly involve blending and entangling the yarns. However, there is a problem with quality stability, and in many cases it is a single-function machine, which has the disadvantage of not being able to significantly change the yarn form. Furthermore, composite yarns called so-called designed twisted yarns, which are made of spun yarn or filament yarn using a designed yarn twisting machine, are excellent in their versatility, but require complicated mechanisms and techniques, and in principle have extremely low productivity. This serious flaw has not yet been resolved. The present inventors have arrived at the present invention as a result of intensive studies to solve the problems of the conventional method. , Two cylindrical bodies are arranged in series to generate a swirling vortex flow, with a hollow conical body and an annular body facing each other on the internal central axis, and each cylindrical body is brought into a negative pressure state by suction to form the core. The yarn is made to run along the central axis of each cylinder, and the sheath forming yarn is placed at least one point closer to the air inflow hole of each cylinder.
The threads for forming the sheath are fed one by one at a speed higher than the traveling speed of the thread for forming the core, and each thread for forming the sheath is wrapped around the thread for forming the core by the action of a negative pressure swirling vortex at the tip of the hollow cone. The method of manufacturing a special composite yarn is characterized by intertwining the yarn in a twisted state. The present invention will be described in detail below with reference to the drawings.
FIG. 1 is a side view showing an example of an apparatus used in carrying out the present invention, in which a core forming yarn 1 is connected to a swirling vortex generating cylinder 8 connected to a tension adjusting device 4 and a negative pressure source 15. , 11, and runs along the central axis of the swirling vortex generating cylinders 8, 11, while another sheath forming yarn 2 is connected to a tension adjusting device 4' and a feed roller 5. , 5', and the yarn guide 9, and is supplied into the swirling vortex generating cylinder 8 from the air inflow hole 10 provided in the direction of the circumferential surface of the swirling vortex generating cylinder 8. Similarly, another sheath-forming yarn 3 is also connected to an air inlet provided in the direction of the circumferential surface of the swirling vortex generating cylinder 11 via a tension adjusting device 4'', feed rollers 6, 6', and a yarn guide 12. The yarns 2 and 3 for forming the sheath part are supplied into the swirling vortex generating cylinder 11 through the hole 13. 1 is twisted and entangled by the action of a negative pressure swirling vortex flow, passes through the hole 14, becomes a special composite yarn 16, and is turned into a cheese 17 by a winding device.
It is rolled up as. Therefore, the process of forming the special composite yarn 16 described above was performed in a second manner.
To explain in more detail with reference to FIG. 3 and FIG.
3, the core forming yarn is supplied in excess of one or more times, preferably several times or more, and is supplied into the swirling vortex generating cylinders 8, 11. The loop groups 19,2
2 occur consecutively. These loop groups are further formed by annular bodies 18 and 2 provided at the center of the swirling vortex generation cylinders 8 and 11 by the negative pressure swirling vortex action.
At the tip of the hollow conical bodies 20 and 23 above 1, the sheath forming yarn 2 is first attached to the circumferential surface of the core forming yarn 1, and then the sheath forming yarn 3 is continuously twisted in a twisted state. are intertwined to form a special composite yarn 16. At this time, if the swirling vortex generating cylinders 8 and 11 are the same, and the sheath forming yarns 2 and 3 are of the same type and supplied in the same amount, the special composite yarn 16 will be well-balanced with excellent bulk. By using different types of sheath-forming yarns 2 and 3 or by changing their supply amounts, a variety of special composite yarns with a variety of shapes can be obtained. Also, the air inflow holes 1 of the swirling vortex generating cylinders 8 and 11
0 and 13 are provided so as to generate negative pressure swirling vortices in opposite directions, for example, first the sheath forming yarn 2 is entwined with the core forming yarn 1 in a right-handed twisted state by the cylinder 8. After being combined, the sheath forming yarns 3 are intertwined in a left-handed twisted state using the cylinder 11 to produce a slab-like composite yarn as shown in FIG. 4B. According to the present invention configured as described above, since it effectively utilizes the high-speed negative pressure swirling vortex flow caused by suction, it does not require complicated mechanisms and techniques as in the conventional method, and is therefore economical and high cost. It has the advantage of high productivity, can be applied to the manufacture of many types of yarn forms, and has a twisted yarn structure, which has excellent stability of form and quality, and has many industrial effects. Example 1 A special composite yarn was manufactured using the apparatus shown in Fig. 1, in which the air inflow holes 10 and 13 were arranged to generate swirling vortices in the same direction, and the main conditions were set as shown in Table 1. A special composite yarn as shown in Fig. 4A, which is flexible, extremely bulky, and has an excellent pongee-like design effect, was obtained.

【表】【table】

【表】 実施例 2 空気流入孔10,13を第4図A,Bの如く逆
方向の旋回渦流を生ずるように設けた第1図の装
置により主な条件を第2表の通り設定して特殊複
合糸の製造を行なつたところ、スラブ調意匠効果
に優れ且つスラブ状部分が堅牢で安定な工程通過
性に優れる第4図ロの如き特殊複合糸が得られ
た。
[Table] Example 2 The main conditions were set as shown in Table 2 using the device shown in Fig. 1, in which the air inflow holes 10 and 13 were provided so as to produce swirling vortices in opposite directions as shown in Fig. 4 A and B. When a special composite yarn was manufactured, a special composite yarn as shown in FIG. 4B was obtained which had an excellent slab-like design effect, a solid slab-like portion, and excellent processability.

【表】【table】

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

第1図は本発明の実施に使用する装置の一例を
示す斜視図、第2図は第1図の円筒体8,11部
分の縦断面図、第3図は第2図のA−A′線断面
図、第4図イ,ロは本発明にて得られた複合糸の
各種例を示す側面図で、第1図〜第3図におい
て、1は芯部形成用糸条、2,3は鞘部形成用糸
条、8,11は旋回渦流円筒、10,13は空気
流入孔、20,23は中空円錘体、18,21は
環状体である。
FIG. 1 is a perspective view showing an example of an apparatus used to carry out the present invention, FIG. 2 is a longitudinal sectional view of the cylindrical bodies 8 and 11 in FIG. 1, and FIG. 3 is a line A-A' in FIG. 2. Line sectional views and FIGS. 4A and 4B are side views showing various examples of composite yarns obtained by the present invention. In FIGS. 1 to 3, 1 is a core forming yarn; 8 and 11 are swirling swirl cylinders, 10 and 13 are air inflow holes, 20 and 23 are hollow conical bodies, and 18 and 21 are annular bodies.

Claims (1)

【特許請求の範囲】[Claims] 1 周面の接線方向に空気流入孔を有し、その内
部中心軸上に中空円錘体と環状体とを対向して設
けた旋回渦流発生の為の円筒体を2ケ直列に配置
し、各円筒体を吸引により負圧状態として芯部形
成用糸条を各円筒体の中心軸に沿つて走行せしめ
ると共に鞘部形成用糸条を各円筒体の空気流入孔
より少くとも1本づつ芯部形成用糸条の走行速度
以上の速度で供給し、中空円錘体の先端部で負圧
旋回渦流の作用により各鞘部形成用糸条を芯部形
成用糸条の周囲に加撚状態で絡合せしめることを
特徴とする特殊複合糸の製法。
1. Two cylindrical bodies for generating swirling vortices are arranged in series, each having an air inflow hole in the tangential direction of the circumferential surface, and a hollow conical body and an annular body facing each other on the central axis of the cylindrical body, Each cylindrical body is brought into a negative pressure state by suction, and the thread for forming the core portion is made to run along the central axis of each cylindrical body, and at least one thread for forming the sheath portion is inserted into the core from the air inflow hole of each cylindrical body. The sheath forming threads are fed at a speed higher than the running speed of the sheath forming threads, and each sheath forming thread is twisted around the core forming thread by the action of a negative pressure swirling vortex at the tip of the hollow cone. A method for producing a special composite yarn that is characterized by intertwining.
JP18952881A 1981-11-26 1981-11-26 Manufacturing method of special composite yarn Granted JPS5891841A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18952881A JPS5891841A (en) 1981-11-26 1981-11-26 Manufacturing method of special composite yarn

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18952881A JPS5891841A (en) 1981-11-26 1981-11-26 Manufacturing method of special composite yarn

Publications (2)

Publication Number Publication Date
JPS5891841A JPS5891841A (en) 1983-05-31
JPS6346180B2 true JPS6346180B2 (en) 1988-09-13

Family

ID=16242795

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18952881A Granted JPS5891841A (en) 1981-11-26 1981-11-26 Manufacturing method of special composite yarn

Country Status (1)

Country Link
JP (1) JPS5891841A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105316831B (en) * 2014-07-25 2017-07-28 江苏天地化纤有限公司 A kind of mariages winding shaping device

Also Published As

Publication number Publication date
JPS5891841A (en) 1983-05-31

Similar Documents

Publication Publication Date Title
US3978648A (en) Helically wrapped yarn
US4070815A (en) Textured multifilament yarn
US3113413A (en) Apparatus and method for producing volumized slub yarn
US4069565A (en) Process and apparatus for producing textured multifilament yarn
US4003194A (en) Method and apparatus for producing helically wrapped yarn
JPH0544117A (en) Apparatus for spinning
JPH0153366B2 (en)
JPS6143447B2 (en)
JPH0319929A (en) Open-end spun yarn
JPS6346180B2 (en)
US3823541A (en) Effect voluminous yarn
US3438186A (en) Method and apparatus for producing a novelty loop yarn
US3492803A (en) Process and apparatus for making yarns of polymeric material
DE1906844A1 (en) Pneumatic false real twisting
JPS6040529B2 (en) Manufacturing method of pongee yarn style composite yarn
JPS6018338B2 (en) nozzle
KR20020081662A (en) Method and device as well as the utilization of the device to produce a blended yarn or a composite yarn
JPH036257B2 (en)
JPS60126340A (en) Production of core yarn
JPS5936685B2 (en) Manufacturing method of composite string
JPS58109637A (en) Twisting apparatus of open end spinning frame
JP2517616Y2 (en) Spinning equipment
JPS6347812B2 (en)
JPH08269833A (en) Production device for fancy yarn
JPS5933691B2 (en) Manufacturing method of pongee yarn style composite yarn