US3568428A - Sheath/core composite yarns - Google Patents

Sheath/core composite yarns Download PDF

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Publication number
US3568428A
US3568428A US797224A US3568428DA US3568428A US 3568428 A US3568428 A US 3568428A US 797224 A US797224 A US 797224A US 3568428D A US3568428D A US 3568428DA US 3568428 A US3568428 A US 3568428A
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US
United States
Prior art keywords
fibres
yarn
sheath
stretch
broken
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 - Lifetime
Application number
US797224A
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English (en)
Inventor
Richard Stentiford
Alan Roebuck
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.)
Imperial Chemical Industries Ltd
Original Assignee
Imperial Chemical Industries Ltd
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Filing date
Publication date
Application filed by Imperial Chemical Industries Ltd filed Critical Imperial Chemical Industries Ltd
Application granted granted Critical
Publication of US3568428A publication Critical patent/US3568428A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/36Cored or coated yarns or threads
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/02Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyamides

Definitions

  • the present invention relates to bulky sheath/ core composite yarns.
  • an especially useful and novel tension-stable bulky sheath/core yarn may be formed of stretch broken fibres, preferably uncrimped, forming a core surrounded by a sheath of crimped staple fibres.
  • the present invention provides a bulked tension-stable core yarn comprising stretchbroken synthetic fibres located substantially centrally of the yarn to form a core portion and crimped staple fibres substantially surrounding the said stretch-broken synthetic fibres to form a sheath portion, the yarn having an extension of not more than when measured by the method as hereinafter defined.
  • the stretch-broken fibres may be formed from a tow of polyamide filaments, for example polyhexamethylene adipamide filaments, or other synthetic filaments and is preferably free of crimp, although some crimp may be imparted to the tow to assist in processing.
  • polyamide filaments for example polyhexamethylene adipamide filaments, or other synthetic filaments and is preferably free of crimp, although some crimp may be imparted to the tow to assist in processing.
  • any natural or synthetic fibre may be employed as the staple fibre sheath component, conveniently this may be formed from a crimped tow of polyamide by conventional crush cutting equipment, for example on a Pacific converter.
  • the tow will normally be crimped in known stuffer box equipment.
  • a bulky tension stable yarn is a textile spun yarn which has a high resistance to extension at relatively low loads of the order of 0.025 g./den.
  • a method of assessing this is to subject a 4 fold 8s worsted count spun yarn to a load of 100 g. Under such conditions we have found that the yarns of our invention have an extension of less than 10%.
  • the yarn of the present invention may be obtained by first blending slivers of stretch-broken synthetic fibres and staple fibres together to form a blended sliver and then drafting and spinning in a conventional worsted processing system. During the latter process the relatively uncrimped stretch-broken fibres tend to migrate to the centre of the yarn to form a core. Additional migration also may take place when the yarn is secured and dyed as a result of slight shrinkage differences which may exist between the components; yarn bulk is also increased during scouring and dyeing.
  • the present invention provides a process for the manufacture of a bulked tension-stable core yarn as defined above wherein slivers of stretch-broken synthetic fibres and crimped staple fibres are blended together and the blend drafted and spun into a yarn which is subsequently scoured and dyed.
  • STRETCH-BROKEN COMPONENT A 300,000 denier unset tow having a crimp of 10 c.p.i. (crimps per inch) and an extension at break of 45% formed from 6 d.p.f. (denier per filament) polyhexamethylene adipamide filaments is subjected to stretch breaking on a Turbo-Stapler machine. The heat stretch zone is maintained at 350-400 F. and the total machine draft at 4.6. The tow is subjected to re-breaking after stretch-breaking and the resultant sliver has a fibre length of 2-8".
  • STAPLE FIBRE COMPONENT A 1,800,000 denier tow having a crimp of 15 c.p.i. and an extension at break of 50% is formed from 10 d.p.f. polyhexamethylene adipamide fibres and cut to 6" staple fibres in a Pacific-Converter.
  • the tow is assembled from eighteen 100,000 denier tows and is steam set at 25 p.s.i.g. in a Sanderson steam cabinet for 7 minutes.
  • Example 1 A sheath/ core yarn was produced by procedure of Example 1 except that the ratio of staple fibre to stretchibroken fibres was 40% 60%. The spun yarn had an extension of 8.0%.
  • Fabrics knitted from the sheath/core yarns of the above examples showed properties of good recovery from deformation, a high area/weight ratio being comparable to that of wool and a resilient handle.
  • Examples 3 and 4 (comparative) Yarns were prepared by the procedure of Example 1 except that the amount of the stretch-broken component was reduced. The details of the yarns, their extension properties and the results of washing trials on fabrics knitted therefrom are shown in Table 1.
  • Example 5 Yarns were again prepared according to the procedure detailed in Example 1 except that the stretch-broken component was formed from a 10 denier per filament polyhexamethylene adipamide tow, and the tow had an extension at break of 54%. Details of the yarn and its properties are given in Table 2.
  • a bulked tension-stable core yarn comprising stretch-broken synthetic fibres located substantially centrally of the yarn to form a core portion and crimped staple fibres substantially surrounding the said stretchbroken synthetic fibres to form a sheath portion, the yarn having an extension of not more than 10% when measured by the method as hereinbefore defined.
  • a yarn according to claim 1 consisting wholly of fibres of polyhexamethylene adipamide.
  • a yarn according to claim 2 wherein the crimped staple fibres are 10 denier P r filament, have 15 crimps per inch and an extension at break of 50%, the stretch broken fibres are 6 denier per filament and comprise at least 40% of the yarn.
  • a yarn according to claim 2 wherein the crimped staple fibres are 10 denier per filament, have 15 crimps per inch and an extension at break of 50% and the stretch-broken fibres are 10 denier per filament and comprise at least 30% of the yarn.
  • a process for the manufacture of a bulked tensionstable core yarn comprising stretch-broken synthetic fibres located substantially centrally of the yarn to form a core portion and crimped staple fibres substantially surrounding the said stretch-broken synthetic fibres to form a sheath portion, the yarn having an extension of not more than 10% when measured by the method as hereinbefore defined wherein slivers of stretch-broken synthetic fibres and crimped staple fibres are blended together and the blend drafted and spun into a yarn which is subsequently scoured and dyed, the stretch-broken fibres being formed from a 300,000 denier 6 denier per filament polyhexamethylene adipamide tow at a breaking extension of 45% and a temperature of 400 F.
  • crimped staple fibres are formed from 18 X 100,000 denier polyhexamethylene adipamide tows which are crimped steam set at 25 p.s.i.g. and cut to 6" staple fibres.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
US797224A 1968-02-15 1969-02-06 Sheath/core composite yarns Expired - Lifetime US3568428A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7461/68A GB1194796A (en) 1968-02-15 1968-02-15 Improvements in or relating to Sheath/Core Composite Yarns

Publications (1)

Publication Number Publication Date
US3568428A true US3568428A (en) 1971-03-09

Family

ID=9833531

Family Applications (1)

Application Number Title Priority Date Filing Date
US797224A Expired - Lifetime US3568428A (en) 1968-02-15 1969-02-06 Sheath/core composite yarns

Country Status (6)

Country Link
US (1) US3568428A (en))
BE (1) BE728460A (en))
DE (1) DE1906768A1 (en))
FR (1) FR2001979A1 (en))
GB (1) GB1194796A (en))
NL (1) NL6902152A (en))

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4307566A (en) * 1979-02-05 1981-12-29 Teijin Limited Bulky spun yarn and a method for manufacturing the same from a combination of thermally extensible and thermally shrinkable fibers
US4719744A (en) * 1982-06-07 1988-01-19 Burlington Industries, Inc. Vacuum spinning method
US4928464A (en) * 1982-06-07 1990-05-29 Burlington Industries, Inc. Yarn produced by spinning with vacuum
US5392588A (en) * 1982-06-07 1995-02-28 Burlington Industries, Inc. Spinning with hollow rotatable shaft and air flow

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3107689B1 (fr) 2020-02-27 2023-05-26 Psa Automobiles Sa Véhicule avec structure montrant une troisième voie d’effort entre le berceau et un brancard avant

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4307566A (en) * 1979-02-05 1981-12-29 Teijin Limited Bulky spun yarn and a method for manufacturing the same from a combination of thermally extensible and thermally shrinkable fibers
US4719744A (en) * 1982-06-07 1988-01-19 Burlington Industries, Inc. Vacuum spinning method
US4928464A (en) * 1982-06-07 1990-05-29 Burlington Industries, Inc. Yarn produced by spinning with vacuum
US5392588A (en) * 1982-06-07 1995-02-28 Burlington Industries, Inc. Spinning with hollow rotatable shaft and air flow

Also Published As

Publication number Publication date
NL6902152A (en)) 1969-08-19
GB1194796A (en) 1970-06-10
FR2001979A1 (en)) 1969-10-03
DE1906768A1 (de) 1969-09-18
BE728460A (en)) 1969-08-14

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