EP0132110A2 - Process for producing composite monofilaments - Google Patents
Process for producing composite monofilaments Download PDFInfo
- Publication number
- EP0132110A2 EP0132110A2 EP84304721A EP84304721A EP0132110A2 EP 0132110 A2 EP0132110 A2 EP 0132110A2 EP 84304721 A EP84304721 A EP 84304721A EP 84304721 A EP84304721 A EP 84304721A EP 0132110 A2 EP0132110 A2 EP 0132110A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- composite
- component
- sheath
- melting
- 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.)
- 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
Definitions
- This invention relates to a process for producing composite monofilaments (hereinafter abbreviated to "composite MF”) having heat-adhesive properties and excellent strengths. More particularly it relates to a process for producing composite MF of polyolefin resins having heat-adhesive properties and excellent strengths, obtained by using a low melting polyolefin resin component on the sheath side and a high melting polypropylene (hereinafter abbreviated to "high melting PP”) component on the core side, and melt-extruding these components through a sheath-and-core type spinneret, followed by cooling, solidifying and stretching.
- composite MF composite monofilaments
- high melting PP high melting polypropylene
- monofilaments as a single component obtained by melt-extruding a polyolefin resin, followed by cooling and then stretching are superior in mechanical strengths, chemical strengths, corrosion resistance, water resistance, moldability, etc.; hence they have been fabricated into ropes, materials of fishing such as fishermen's nets, nets for land such as insect screening, windbreak net, golf net, light-shielding net, filter, sheet for public works, etc. and the resulting products have been widely used.
- the object of the present invention is to provide a process for producing composite MF having heat-adhesive properties, superior strengths, no curl and no peeling between the layers thereof.
- the present invention resides in
- HDPE and polypropylene used in the present invention
- homopolymer of ethylene or propylene is not only used, but also copolymers of ethylene with propylene, butene-1, etc. composed mainly of ethylene or copolymers of propylene with ethylene, butene-1, etc. composed mainly of propylene may be preferably used.
- added additives which are usually added to polyolefin resins, such as stabilizers, e.g. antioxidant, ultraviolet absorber, etc., coloring agent, lubricant, antistatic agent, delustering agent, etc.
- mixing may be carried out employing a conventional means such as extruder, Banbury mixer, tumbler mixer, Henschel mixer, etc. and in a conventional manner.
- a conventional means such as extruder, Banbury mixer, tumbler mixer, Henschel mixer, etc. and in a conventional manner.
- composite extrusion method and apparatus although known techniques may be employed such as composite extrusion by means of two extruders and composite spinnerets of side- by-side or sheath-and-core type, it is preferred in the present invention to employ composite spinnerets of sheath-and-core type which is advantageous in the aspects of spinning, stretching stability and peel resistance of the boundary surface layer between the sheath component and the core component of stretched composite MF.
- the high melting PP and the low melting PP are based on MFR measured according to ASTM D 1238 (L), and HDPE and LLDPE are based on MI measured according to ASTM D 1238(E).
- the melt flow index (MFR) of the high melting PP used on the core side of the composite MF may be in the range of 0.3 to 15 which has been used for ordinary MF, but its melting point is required to be 150°C or higher, and as for the FR ratio of the low melting polyolefin resin component on the sheath side to the high melting PP on the core side, when the ratio is'in the range of 1.5 to 7, the effectiveness of the present invention is remarkable. If the melting point of the core component is lower than 150°C, its strength as a basic performance of the core component is reduced, and also its shrink properties increase so that when a net prepared by knitting or weaving the above composite MF is subjected to heat set, shrink- deformation is notable.
- the FR ratio is lower than 1.5, spinning and stretching properties are unstable and the resulting net is inferior in heat-adhesive properties. If it is higher than 7, the fluidity of the sheath component in the nozzle is different from that of the core component therein, and also there occurs a large stress strain due to the difference in the crystallization behavior between the two components or the difference in the volume shrinkage between the two components during the process from molten state to cooling and solidification, so that extruded unstretched MF bends or curls at the exit of the nozzle to make spinnability inferior. Further since the difference between the stretching stresses applied to the sheath and core components increases; hence stretching troubles such as stretching breakage, curling of stretched MF, etc. are liable to occur.
- the low melting polyolefin resin used as the sheath component constitutes a component by which adhesive properties due to heat-melt adhesion are imparted to composite MF, and the effectiveness is fully exhibited by single use of HDPE, LLDPE or a low melting PP, but even when two or more kinds thereof are used in admixture, the same effectiveness as in the single use is exhibited. In this case, as for the combination of the components, combinations of polymers having similar fluidities are preferred. When a low melting PP is used as the sheath component, its melting point is necessary to be 135°C or lower.
- the melting point of the low melting polyolefin resin is preferably 80°C or higher and more preferably 100°C or higher.
- the composite ratio of the sheath component to the core component is preferably in the range of 30 70 to 60 :40. If the sheath component is less than 30%, spinnability and stretchability are liable to be inferior, and also since the amount of the heat-adhesive component of the composite MF is reduced, the bonding force at the adhesion part of the mesh of the net becomes weak. On the other hand, if the core component is less than 40%, the strength of the core component as a basic element of the role thereof is reduced.
- the stretching in the present invention general apparatus and process for stretching may be employed which have been employed for ordinary MF.
- the stretch ratio is suitably in the range of 6 to 9 times the original length.
- composite MF since its strength is structurally somewhat lower than that of ordinary MF, if the ratio is lower than 6 times, its strength is low, while if it exceeds 9 times, its strength is sufficient, but due to the fact that composite MF is poor in the compatibility of polymers at the boundary surface thereof, the difference in stretchability between the sheath component and the core component becomes remarkable so that troubles such as turnover or peel of the sheath component occur during the stretching step and also it is liable to curl after stretching, which causes troubles of bad take-up during the take-up step such as bad take-up shape or getting out of take-up shape.
- the composite MF of the present invention may usually be preferably used in a thickness of 100 to 1,000 d.
- the composite MF obtained according to the present invention retains strength characteristics similar to those of ordinary MF and is at the same time provided with heat-adhesive properties.
- the net-form product having its mesh part bonded together by heat- adhesion obtained by subjecting a net-form material prepared by knitting or weaving the above composite MF, to heat treatment by way of a general means such as heating roll, heating calender, hot air, steam treatment, etc., retains strengths similar to those of net-form products consisting of ordinary MF and hardly causes mesh deformation.
- melt-extrusion was carried out at an extrusion temperature on the core side of 260°C, at an extrusion temperature on the sheath side of 240°C and at a composite spinneret temperature of 260°C, followed by spinning through cooling to obtain an unstretched composite filament of sheath-and-core type having a composite ratio of 50 :50, which was then stretched to 5 to 10 times by means of a wet type, heat stretching apparatus to obtain various kinds of composite MF of 450 d.
- PP having a m.p. of 161°C and a MFR of 3.1 Using as a core component, PP having a m.p. of 161°C and a MFR of 3.1, and as a sheath component, either one of HDPE, LLDPE or PP of m.p. 128°, spinning was carried out under the same conditions as in Example 1 to obtain various unstretched composite filaments of sheath-and-core type, which were then stretched by means of a wet type, heat stretching apparatus to obtain composite MFs of 450 d. The spinnability and stretchability of the resulting composite MFs and evaluations of the heat-adhesive properties and the residual strength of net-form products prepared from the above composite MFs in the same manner as in Example 1 are shown in Table 3.
- a PP having a m.p. of 161°C and a MFR of 3.1 was used as a core component, and three kinds of mixed resins obtained by mixing the respective two of HDPE, LLDPE or a PP of m.p. 128°C in a ratio of 1 :1 by means of a Henschel mixer, followed by extruding and granulating the mixtures by means of an extruder having a bore diameter of 40 mm were used as a sheath component, respectively. Evaluation was made as in Example 1. The results are shown in Table 5.
- PPs having similar MFRs and various melting points were used as a core component, and HDPE, LLDPE or a PP of m.p. 128°C was singly used as a sheath component. Evaluation was made as in Example 1. The results are shown in Table 6.
Abstract
Description
- This invention relates to a process for producing composite monofilaments (hereinafter abbreviated to "composite MF") having heat-adhesive properties and excellent strengths. More particularly it relates to a process for producing composite MF of polyolefin resins having heat-adhesive properties and excellent strengths, obtained by using a low melting polyolefin resin component on the sheath side and a high melting polypropylene (hereinafter abbreviated to "high melting PP") component on the core side, and melt-extruding these components through a sheath-and-core type spinneret, followed by cooling, solidifying and stretching.
- In general, monofilaments as a single component (hereinafter abbreviated to "ordinary MF") obtained by melt-extruding a polyolefin resin, followed by cooling and then stretching are superior in mechanical strengths, chemical strengths, corrosion resistance, water resistance, moldability, etc.; hence they have been fabricated into ropes, materials of fishing such as fishermen's nets, nets for land such as insect screening, windbreak net, golf net, light-shielding net, filter, sheet for public works, etc. and the resulting products have been widely used.
- Among them, nets for land have been in most cases knitted or woven and the resulting knitted or woven products have been used, and their specific feature for practical use consists in their high mechanical strengths. However, since the intersecting parts of warps and wefts of the nets (hereinafter referred to as "mesh") are not bonded together, but relatively free, the meshes shift at the time of knitting or weaving or at the time of applying net products or depending on the practical state of the nets; thus such drawbacks occur that the shielding or protecting effect of net products as their main object is lost or a good appearance thereof is damaged.
- On the other hand, there have been known a technique of molding polymers directly into the form of net by melt-extrusion through a specific rotating spinneret to obtain a net having the meshes bonded together and a technique of further stretching the net product obtained above in both the longitudinal and lateral directions. However, as to the monofilaments (hereinafter abbreviated to."MF") constituting these nets, as compared with conventional nets wherein the strength of each MF in the longitudinal direction and that in the lateral direction are both 3g/d or more, the strength of each MF of the above particular nets in the longitudinal and that in the lateral direction are both 1.5 g/d or less, that is, extremely lower; thus a problem has been raised that the particular nets could have been applied only to extremely limited uses such as use for packaging simple, light-weight goods.
- Further, in the field of non-woven fabrics, those obtained by processing composite fibers having a hot-melt adhesive function imparted thereto, into a bag form material, which is then subjected to heat-treatment to bring the mesh parts to hot-melt adhesion, have been in recent years applied to various uses. However, since hot-melt adhesive composite fibers used therefor have as very small a fineness as about 1 to 30 d, if it is intended to use such composite fibers in the form of a thick material having 100 d or more which has been used for ordinary MF, then it is necessary to process composite fibers into a fiber bundle; hence drawbacks occur that the process is complicated and accordingly very expensive.
- The object of the present invention is to provide a process for producing composite MF having heat-adhesive properties, superior strengths, no curl and no peeling between the layers thereof.
- The present invention resides in
- a process for producing a composite MF having heat-adhesive properties and superior strengths which comprises
- subjecting a low melting polyolefin resin selected from the group consisting of high density polyethylene (hereinafter abbreviated to "HDPE"), linear chain, low density polyethylene (hereinafter abbreviated to "LLDPE"), polypropylene having a melting point of 135°C or. lower (hereinafter abbreviated to "low melting PP") and mixtures of the foregoing, and a high melting polypropylene having a melting point of 150°C or higher, to a sheath-and-core type composite spinning using the former low melting polyolefin resin as the sheath component and the latter high melting polypropylene as the core component, into an unstretched composite MF,
- the melt flow index ratio (hereinafter abbreviated to "FR ratio") of the former low melting polyolefin resin component to the latter high melting polypropylene component being in the range of 1.5 to 7, and the composite ratio being in the range of 30 70 to 60 :40; and
- stretching the unstretched composite MF to 6 to 9 times the original length.
- As for HDPE and polypropylene (hereinafter abbreviated to "PP") used in the present invention, homopolymer of ethylene or propylene is not only used, but also copolymers of ethylene with propylene, butene-1, etc. composed mainly of ethylene or copolymers of propylene with ethylene, butene-1, etc. composed mainly of propylene may be preferably used. Further, to these polymers or mixtures thereof may be, if necessary, added additives which are usually added to polyolefin resins, such as stabilizers, e.g. antioxidant, ultraviolet absorber, etc., coloring agent, lubricant, antistatic agent, delustering agent, etc.
- In the present invention, in the case where HDPE, LLDPE or low melting PP is mixed with each other and the mixture is used as the sheath component, mixing may be carried out employing a conventional means such as extruder, Banbury mixer, tumbler mixer, Henschel mixer, etc. and in a conventional manner. Further, as for the composite extrusion method and apparatus, although known techniques may be employed such as composite extrusion by means of two extruders and composite spinnerets of side- by-side or sheath-and-core type, it is preferred in the present invention to employ composite spinnerets of sheath-and-core type which is advantageous in the aspects of spinning, stretching stability and peel resistance of the boundary surface layer between the sheath component and the core component of stretched composite MF.
- As to the FR ratio in the present invention, the high melting PP and the low melting PP are based on MFR measured according to ASTM D 1238 (L), and HDPE and LLDPE are based on MI measured according to ASTM D 1238(E).
- The melt flow index (MFR) of the high melting PP used on the core side of the composite MF may be in the range of 0.3 to 15 which has been used for ordinary MF, but its melting point is required to be 150°C or higher, and as for the FR ratio of the low melting polyolefin resin component on the sheath side to the high melting PP on the core side, when the ratio is'in the range of 1.5 to 7, the effectiveness of the present invention is remarkable. If the melting point of the core component is lower than 150°C, its strength as a basic performance of the core component is reduced, and also its shrink properties increase so that when a net prepared by knitting or weaving the above composite MF is subjected to heat set, shrink- deformation is notable. If the FR ratio is lower than 1.5, spinning and stretching properties are unstable and the resulting net is inferior in heat-adhesive properties. If it is higher than 7, the fluidity of the sheath component in the nozzle is different from that of the core component therein, and also there occurs a large stress strain due to the difference in the crystallization behavior between the two components or the difference in the volume shrinkage between the two components during the process from molten state to cooling and solidification, so that extruded unstretched MF bends or curls at the exit of the nozzle to make spinnability inferior. Further since the difference between the stretching stresses applied to the sheath and core components increases; hence stretching troubles such as stretching breakage, curling of stretched MF, etc. are liable to occur.
- The low melting polyolefin resin used as the sheath component constitutes a component by which adhesive properties due to heat-melt adhesion are imparted to composite MF, and the effectiveness is fully exhibited by single use of HDPE, LLDPE or a low melting PP, but even when two or more kinds thereof are used in admixture, the same effectiveness as in the single use is exhibited. In this case, as for the combination of the components, combinations of polymers having similar fluidities are preferred. When a low melting PP is used as the sheath component, its melting point is necessary to be 135°C or lower. If it is higher than 135°C, when the resulting net is subjected to heat set, this is necessarily carried out at a high temperature and for a long time; hence even if heat adhesion is effected, the orientation of the core component of the composite MF is lost by the heat at the time of the heat set, to reduce its strength and thereby damage the strength-retaining characteristic of the core component.
- The melting point of the low melting polyolefin resin is preferably 80°C or higher and more preferably 100°C or higher.
- The composite ratio of the sheath component to the core component is preferably in the range of 30 70 to 60 :40. If the sheath component is less than 30%, spinnability and stretchability are liable to be inferior, and also since the amount of the heat-adhesive component of the composite MF is reduced, the bonding force at the adhesion part of the mesh of the net becomes weak. On the other hand, if the core component is less than 40%, the strength of the core component as a basic element of the role thereof is reduced.
- As to the stretching in the present invention, general apparatus and process for stretching may be employed which have been employed for ordinary MF. The stretch ratio is suitably in the range of 6 to 9 times the original length. In the case of composite MF, since its strength is structurally somewhat lower than that of ordinary MF, if the ratio is lower than 6 times, its strength is low, while if it exceeds 9 times, its strength is sufficient, but due to the fact that composite MF is poor in the compatibility of polymers at the boundary surface thereof, the difference in stretchability between the sheath component and the core component becomes remarkable so that troubles such as turnover or peel of the sheath component occur during the stretching step and also it is liable to curl after stretching, which causes troubles of bad take-up during the take-up step such as bad take-up shape or getting out of take-up shape. In order to improve the shrinkabilityof stretched filament after the stretching step, it may be also preferred to apply annealing for relaxation thereto employing a general apparatus and process.
- The composite MF of the present invention may usually be preferably used in a thickness of 100 to 1,000 d.
- The composite MF obtained according to the present invention retains strength characteristics similar to those of ordinary MF and is at the same time provided with heat-adhesive properties. Further, the net-form product having its mesh part bonded together by heat- adhesion, obtained by subjecting a net-form material prepared by knitting or weaving the above composite MF, to heat treatment by way of a general means such as heating roll, heating calender, hot air, steam treatment, etc., retains strengths similar to those of net-form products consisting of ordinary MF and hardly causes mesh deformation.
-
- Using as a core component, various kinds of PP having a melting point of 161°C and various MFR values and as a sheath component, HDPE or LLDPE having various MI values or PP having a melting point of 128°C, and employing two extruders each having a bore diameter of 40 mm and a composite spinneret of sheath-and-core type having a nozzle diameter of 1.5 mm, melt-extrusion was carried out at an extrusion temperature on the core side of 260°C, at an extrusion temperature on the sheath side of 240°C and at a composite spinneret temperature of 260°C, followed by spinning through cooling to obtain an unstretched composite filament of sheath-and-core type having a composite ratio of 50 :50, which was then stretched to 5 to 10 times by means of a wet type, heat stretching apparatus to obtain various kinds of composite MF of 450 d. The results as to the spinnability and stretchability of the extruded, unstretched filament and the peeling properties of the sheath layer from the core layer are shown in Table 1. Further, various kinds of composite MF prepared according to the above process were each woven into a net-form product having a woven density of 5 warps/ 25 mm x5 wefts/25 mm, which was then heat-set in a hot air-heating vessel at 140°C for 1.5 minute, taken out and subjected to evaluations of the heat-adhesive properties at the mesh parts and the residual strength of the composite MF. The results are shown in Table 2.
- From these Tables it is seen that when a high melting PP of m.p. 161°C is used as a core component and either one of HDPE or LLDPE or a low melting PP of m.p. 128°C is used as a sheath component, if the FR ratio is in the range of 1.5 to 7.0 and the stretch ratio is in the range of 6 to 9 times, it is possible to obtain a stretched MF having a stabilized composite structure without any peel, and also that among the above cases, when a low melting PP is used as a sheath component, a composite MF which is particularly difficult to peel is obtained. Further it is also seen that net-form products obtained by heat-setting net-form materials prepared from the above composite MF have the mesh parts bonded together by heat adhesion and have a sufficiently retained strength.
- Using as a core component, PP having a m.p. of 161°C and a MFR of 3.1, and as a sheath component, either one of HDPE, LLDPE or PP of m.p. 128°, spinning was carried out under the same conditions as in Example 1 to obtain various unstretched composite filaments of sheath-and-core type, which were then stretched by means of a wet type, heat stretching apparatus to obtain composite MFs of 450 d. The spinnability and stretchability of the resulting composite MFs and evaluations of the heat-adhesive properties and the residual strength of net-form products prepared from the above composite MFs in the same manner as in Example 1 are shown in Table 3.
- From Table 3 it is seen that when the composite ratio of the sheath and core components is in the range of 30 70 to 60 :40, the spinning and stretching stabilities of composite MF and the heat-adhesive properties and the residual strength of net-form products prepared from composite MF are superior.
- Using as a core component, PP having a m.p. of 161°C and a MFR of 3.1 and as a sheath component, various low melting PPs having a MFR of 15.5 and various melting points, composite MFs were prepared under the same conditions as in Example 1. The heat-adhesive properties and the residual strength of net-form products prepared from the above composite MFs were evaluated. The results are shown in Table 4.
- From Table 4 it is seen that in the case where a low melting PP is used as the sheath component, if its melting point exceeds 135°C, the contrary properties to each other of the heat-adhesive properties and the residual strength become greater depending on the heat setting conditions of net-form products, and as the melting point becomes higher, the heat-adhesive properties become inferior, and if the heat setting temperature is raised in order to improve heat-adhesive properties, the strength of composite MF after heat adhesion processing contrarily becomes too low.
- A PP having a m.p. of 161°C and a MFR of 3.1 was used as a core component, and three kinds of mixed resins obtained by mixing the respective two of HDPE, LLDPE or a PP of m.p. 128°C in a ratio of 1 :1 by means of a Henschel mixer, followed by extruding and granulating the mixtures by means of an extruder having a bore diameter of 40 mm were used as a sheath component, respectively. Evaluation was made as in Example 1. The results are shown in Table 5.
- From Table 5 it is seen that even when mixed resins of HDPE, LLDPE or a low melting PP are used as a sheath component, the same effectiveness as in the case of single use thereof is obtained.
- PPs having similar MFRs and various melting points were used as a core component, and HDPE, LLDPE or a PP of m.p. 128°C was singly used as a sheath component. Evaluation was made as in Example 1. The results are shown in Table 6.
-
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58128666A JPS6021908A (en) | 1983-07-14 | 1983-07-14 | Manufacture of composite monofilament |
JP128666/83 | 1983-07-14 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0132110A2 true EP0132110A2 (en) | 1985-01-23 |
EP0132110A3 EP0132110A3 (en) | 1985-06-05 |
EP0132110B1 EP0132110B1 (en) | 1988-01-07 |
Family
ID=14990434
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84304721A Expired EP0132110B1 (en) | 1983-07-14 | 1984-07-11 | Process for producing composite monofilaments |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0132110B1 (en) |
JP (1) | JPS6021908A (en) |
KR (1) | KR870000442B1 (en) |
DE (1) | DE3468448D1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0260607A2 (en) * | 1986-09-12 | 1988-03-23 | Chisso Corporation | Heat-adhesive composite fibers and method for making the same |
EP0311860A2 (en) * | 1987-10-02 | 1989-04-19 | Unitika Ltd. | Nonwoven fabric made of heat bondable fibers |
EP0339410A1 (en) * | 1988-04-23 | 1989-11-02 | Henkel Kommanditgesellschaft auf Aktien | Detergent product |
EP0340763A1 (en) * | 1988-05-05 | 1989-11-08 | Danaklon A/S | Bicomponent synthetic fibre and process for producing same |
US6878650B2 (en) | 1999-12-21 | 2005-04-12 | Kimberly-Clark Worldwide, Inc. | Fine denier multicomponent fibers |
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 |
Families Citing this family (17)
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 | ||
JPH07103507B2 (en) * | 1988-08-23 | 1995-11-08 | ユニチカ株式会社 | Nonwoven fabric made of heat-bondable long fibers |
JP2612350B2 (en) * | 1989-11-27 | 1997-05-21 | 宇部日東化成 株式会社 | Elastic composite fiber |
US5382400A (en) | 1992-08-21 | 1995-01-17 | Kimberly-Clark Corporation | Nonwoven multicomponent polymeric fabric and method for making same |
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 |
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 |
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 |
JPH06330444A (en) * | 1993-05-21 | 1994-11-29 | Ube Nitto Kasei Co Ltd | Polypropylene fiber mat |
JP3814289B2 (en) * | 1997-03-25 | 2006-08-23 | 三井化学株式会社 | Binding material |
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 |
JP6743266B1 (en) * | 2019-12-25 | 2020-08-19 | 宇部エクシモ株式会社 | Black synthetic fiber yarn |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2358484A1 (en) * | 1972-11-25 | 1974-06-12 | Chisso Corp | UNWOVEN MATS AND METHOD OF MANUFACTURING THEREOF |
JPS5386836A (en) * | 1976-12-29 | 1978-07-31 | Chisso Corp | Crimpless, hot melt conjugate fiber and its production |
US4211819A (en) * | 1977-05-24 | 1980-07-08 | Chisso Corporation | Heat-melt adhesive propylene polymer fibers |
US4285748A (en) * | 1977-03-11 | 1981-08-25 | Fiber Industries, Inc. | Selfbonded nonwoven fabrics |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6024205B2 (en) * | 1979-04-11 | 1985-06-12 | チッソ株式会社 | Flame-retardant composite fiber and its manufacturing method |
JPS5658009A (en) * | 1979-10-09 | 1981-05-20 | Chisso Corp | Preparation of flame-retardant composite fiber |
JPS607722B2 (en) * | 1980-08-20 | 1985-02-26 | チッソ株式会社 | Flame-retardant composite fiber and its manufacturing method |
JPS57101023A (en) * | 1980-12-10 | 1982-06-23 | Daiwa Spinning Co Ltd | Sheath-core composite polyolefin fiber containing inorganic material and its preparation |
-
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 |
---|---|---|---|---|
DE2358484A1 (en) * | 1972-11-25 | 1974-06-12 | Chisso Corp | UNWOVEN MATS AND METHOD OF MANUFACTURING THEREOF |
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 |
US4211819A (en) * | 1977-05-24 | 1980-07-08 | Chisso Corporation | Heat-melt adhesive propylene polymer fibers |
Non-Patent Citations (1)
Title |
---|
PATENTS ABSTRACTS OF JAPAN, vol.2, no.122 page 2429 C 78, 13-10-1978 & JP-A 53 86 836 (CHISSO K.K.) (31-07-1978) * |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0260607A2 (en) * | 1986-09-12 | 1988-03-23 | Chisso Corporation | Heat-adhesive composite fibers and method for making the same |
EP0260607A3 (en) * | 1986-09-12 | 1989-11-23 | Chisso Corporation | Heat-adhesive composite fibers and method for making the same |
EP0311860A2 (en) * | 1987-10-02 | 1989-04-19 | Unitika Ltd. | Nonwoven fabric made of heat bondable fibers |
EP0311860A3 (en) * | 1987-10-02 | 1990-07-04 | Unitika Ltd. | Heat-bondable filament and nonwoven fabric made of said filament |
EP0339410A1 (en) * | 1988-04-23 | 1989-11-02 | Henkel Kommanditgesellschaft auf Aktien | Detergent product |
WO1989010394A1 (en) * | 1988-04-23 | 1989-11-02 | Henkel Kommanditgesellschaft Auf Aktien | Detergent |
US5116524A (en) * | 1988-04-23 | 1992-05-26 | Henkel Kommanditgesellschaft Auf Aktien | Detergent product including a water-insoluble, water-permeable bag made form sheathed bicomponent fibers |
EP0340763A1 (en) * | 1988-05-05 | 1989-11-08 | Danaklon A/S | Bicomponent synthetic fibre and process for producing same |
WO1989010989A1 (en) * | 1988-05-05 | 1989-11-16 | Danaklon A/S | Bicomponent synthetic fibre and process for producing same |
US5456982A (en) * | 1988-05-05 | 1995-10-10 | Danaklon A/S | Bicomponent synthesis fibre and process for producing same |
US6878650B2 (en) | 1999-12-21 | 2005-04-12 | Kimberly-Clark Worldwide, Inc. | Fine denier multicomponent fibers |
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 |
Also Published As
Publication number | Publication date |
---|---|
JPS633969B2 (en) | 1988-01-27 |
EP0132110B1 (en) | 1988-01-07 |
DE3468448D1 (en) | 1988-02-11 |
EP0132110A3 (en) | 1985-06-05 |
KR870000442B1 (en) | 1987-03-10 |
KR850001316A (en) | 1985-03-18 |
JPS6021908A (en) | 1985-02-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0132110B1 (en) | Process for producing composite monofilaments | |
DE60313305T2 (en) | REVERSIBLE, THERMOFIXED, ELASTIC FIBERS, PRODUCTION METHOD AND ARTICLES PRODUCED THEREFROM | |
KR930011950B1 (en) | Process for the manufacture of polyester industrial yarn | |
DE3315360C2 (en) | Melt-adhesive fibers made from polyethylene and their use in composite fibers | |
US5032442A (en) | Fibrillated weatherproof webs having network structure, nonwoven fabrics made from the webs, and processes for the production of the webs and nonwoven fabrics | |
US4315881A (en) | Process for producing composite fibers of side by side type having no crimp | |
KR900702096A (en) | Stretched polyethylene terephthalate yarn manufacturing process and stretched polyethylene terephthalate multifilament yarn manufactured therefrom | |
JP4365249B2 (en) | Woven fabric and its woven fabric processed products | |
DE2739782A1 (en) | PROCESS FOR MANUFACTURING A STIFF, PERMEABLE FABRIC AND THE SUBSTANCES PRODUCED BY THIS PROCESS | |
US4297413A (en) | Concentric composite conjugate yarns and a process for manufacturing same | |
JPH07238417A (en) | Thread-or belt-shaped plastically deformable polyethylene material and its production | |
US20190203382A1 (en) | Conjugated fiber | |
JP2003089942A (en) | Net-formed product | |
JPS633968B2 (en) | ||
KR100523265B1 (en) | Tarpaurin by using polyolefin group split yarn and method thereof | |
JP2000144562A (en) | Meshed article comprising coated synthetic fiber yarns | |
JPS6197416A (en) | Special monofilament having high strength and its production | |
WO2020203286A1 (en) | Drawn composite fibers, non-woven cloth, and production method for drawn composite fibers | |
JPH0641648B2 (en) | Manufacturing method of latent bulky multifilament and its spinneret | |
JPH02446B2 (en) | ||
JP4081338B2 (en) | Polypropylene-based fluid disturbed fiber and method for producing the same | |
KR102144201B1 (en) | Polypropylene filament elastic yarns, fabric thereof and manufacture method | |
JPH0151570B2 (en) | ||
KR101850628B1 (en) | Rayon-like polyester composite yarn having excellent drapability and high elasticity and manufacturing method thereof | |
JPS61113852A (en) | Fabric for reinforcing tire |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19840719 |
|
AK | Designated contracting states |
Designated state(s): DE FR GB SE |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Designated state(s): DE FR GB SE |
|
17Q | First examination report despatched |
Effective date: 19860220 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB SE |
|
REF | Corresponds to: |
Ref document number: 3468448 Country of ref document: DE Date of ref document: 19880211 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
EAL | Se: european patent in force in sweden |
Ref document number: 84304721.8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19970702 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19970709 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19970716 Year of fee payment: 14 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19980711 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19980712 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19980711 |
|
EUG | Se: european patent has lapsed |
Ref document number: 84304721.8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990331 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20010702 Year of fee payment: 18 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20030201 |