US3568428A - Sheath/core composite yarns - Google Patents
Sheath/core composite yarns Download PDFInfo
- 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
- Authority
- 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
Links
- 239000002131 composite material Substances 0.000 title description 3
- 238000002156 mixing Methods 0.000 abstract description 3
- 238000009987 spinning Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 11
- 229920002994 synthetic fiber Polymers 0.000 description 10
- 229920002302 Nylon 6,6 Polymers 0.000 description 7
- 239000004744 fabric Substances 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 238000005406 washing Methods 0.000 description 3
- 239000004952 Polyamide Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229920002647 polyamide Polymers 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000004043 dyeing Methods 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000009991 scouring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
Classifications
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
- D02G3/00—Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
- D02G3/22—Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
- D02G3/36—Cored or coated yarns or threads
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2331/00—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
- D10B2331/02—Fibres 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)
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)
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)
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 |
-
1968
- 1968-02-15 GB GB7461/68A patent/GB1194796A/en not_active Expired
-
1969
- 1969-02-06 US US797224A patent/US3568428A/en not_active Expired - Lifetime
- 1969-02-11 DE DE19691906768 patent/DE1906768A1/de active Pending
- 1969-02-11 NL NL6902152A patent/NL6902152A/xx unknown
- 1969-02-14 FR FR6903749A patent/FR2001979A1/fr not_active Withdrawn
- 1969-02-14 BE BE728460D patent/BE728460A/xx unknown
Cited By (4)
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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