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US3616129A - Longitudinally stretchable nonwoven material - Google Patents

Longitudinally stretchable nonwoven material Download PDF

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Publication number
US3616129A
US3616129A US3616129DA US3616129A US 3616129 A US3616129 A US 3616129A US 3616129D A US3616129D A US 3616129DA US 3616129 A US3616129 A US 3616129A
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Prior art keywords
threads
cross
nonwoven material
web
warp threads
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Karl E Sager
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Kimberly Clark Corp
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Kimberly Clark Corp
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    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/05Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in another pattern, e.g. zig-zag, sinusoidal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074Strand or strand-portions
    • Y10T428/24083Nonlinear strands or strand-portions
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074Strand or strand-portions
    • Y10T428/24091Strand or strand-portions with additional layer[s]
    • Y10T428/24099On each side of strands or strand-portions
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24802Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
    • Y10T428/24826Spot bonds connect components
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/26Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/266Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension of base or substrate
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/60Nonwoven fabric [i.e., nonwoven strand or fiber material]
    • Y10T442/608Including strand or fiber material which is of specific structural definition

Definitions

  • ABSTRACT A longitudinally stretchable, nonwoven material and the method of making same are disclosed.
  • a plurality of spaced-apart, substantially parallel wa'rp threads are drawn from their respective supply cans and over an adhesive applicator.
  • the warp threads are laterally oscillated and deposited on the surface of a carrier sheet moving into a thread cross-laying apparatus to produce a generally sinusoidal pattern of threads on the carrier sheet.
  • a plurality of spaced-apart, substantially parallel cross threads are then laid generally straight across the carrier sheet in a transverse direction as it moves through the cross layer and the cross threads are adhesively bonded to the warp threads where they cross one another. Provision is also made for introducing and laminating top and bottom layers of sheet material to the iongitudinally stretchable, nonwoven material.
  • the present invention relates generally to nonwoven material and more particularly concerns longitudinally stretchable nonwoven materials and methods of making same.
  • creped cellulosic wadding has considerably higher stretch and strength properties in the longitudinal direction than in the cross direction and this makes it difficult to match the creped wadding with a reinforcing scrim having the desired properties of stretch and strength in both the longitudinal and transverse directions.
  • a more particular object is to provide a longitudinally stretchable nonwoven reinforcing scrim in which the warp threads are disposed in a generally sinusoidal pattern.
  • the longitudinally stretchable, nonwoven material of the present invention includes a plurality of spaced-apart, sub stantially parallel warp threads which extend generally 1ongitudinally in a sinusoidal pattern and a plurality of spacedapart, substantially parallel cross threads which extend generally straight across the warp threads with the warp threads and cross threads bonded together where they cross one another.
  • the warp threads are first drawn from their respective supply cans and aligned in spaced-apart, substantially parallel relation and, after application of adhesive, are laterally oscillated and deposited on the surface of a carrier sheet moving into a cross-laying apparatus where the cross threads are laid straight across the sinusoidally disposed warp threads.
  • the warp threads and cross threads are of multifilament low twist construction having an overall denier in the range of between about and 150 and a twist ratio of not more than 6 turns per inch and are spaced apart between about 2 and 12 threads per inch.
  • the invention also contemplates the use of monofilament threads which, preferably, have a denier in the range of 15 and for certain applications.
  • a preferred laminated longitudinally stretchable nonwoven material includes a longitudinally sinusoidal scrim as described above adhesively bonded to one or more layers of sheet material having appreciably more 1ongitudinal than transverse stretch characteristics such as creped cellulosic wadding.
  • the creped wadding layers are each preferably formed of at least one ply having a basis weight before creping of between about 4 and 12 pounds per 2,880- square-foot ream and have a residual stretch ratio of between about 1.2 and 1.5 after stretching and ironing.
  • FIG. 11 is a schematic side elevation of a cross-laying apparatus which may be utilized to practice the method of the present invention.
  • FIG. 2 is an enlarged fragmentary front elevation view of the adhesive application roll
  • FIG. 3 is an enlarged fragmentary section taken substantially along line 3-3 in FIG. 2;
  • FIG. 4i is a projection ofone ofthe grooves in the cylindrical surface of the adhesive application roll shown in FIG. 2;
  • FIG. 5 is an enlarged fragmentary plan view of one form of longitudinally stretchable, nonwoven material made on the apparatus shown in FIG. 11 with the various layers broken away to show the internal details of the multicomponent construction.
  • the illustrated apparatus 110 includes a generally cylindrical mandrel 11 around which an endless belt 112 is helically wound through a plurality of turns.
  • the mandrel Jill is preferably in the form of a hollow cylindrical shell having a plurality of air discharge openings therein and the interior of the mandrel is supplied with air under pressure in order to floatingly support the belt 12 on the surface of the mandrel.
  • the belt 112 makes three turns or wraps on the mandrel 11 and the belt is further supported by a plurality of guide rollers and turning bars M-IIl mounted in a suitable frame (not shown).
  • roller 15 not only guides and supports the belt 112 as it moves off the mandrel, but also drives the belt around the helical turns through suita' ble means (not shown).
  • the belt is also guided by roller 116 and 19 andturning bars 17 and 118, which are preferably ofthe air-floating type, as it returns from drive roll 15 to guide roll 14.
  • a plurality of threads 21) are drawn from their respective supply spools which are located, for example, in a creel room 21.
  • the threads 21 pass through a comb 22 to align them in spaced-apart, substantially parallel relation.
  • the threads 21) are then drawn over a grooved adhesive applicator roll 23 which coats the threads with a thin layer of flexible adhesive.
  • the applicator roll is partially submerged in liquid adhesive contained in a supply trough 24 and excess adhesive is removed from the surface of the roll by a suitable doctor blade 25.
  • the surface of the applicator roll 23 is provided with a plurality of axially spaced, self returning grooves 27, each of which, in cylindrical projection, define a sinusoidal pattern (see FIG. d).
  • Suitable means (not shown) are provided for rotating the applicator roll 23 and, as it rotates, the grooves 27 impart a laterally oscillating sinusoidal movement to the threads 20.
  • the applicator roll 23 is preferably rotated with a differential surface speed relative to the movement of the threads 20 to help avoid wrap-up of the threads on the roll and! to enhance the lateral force imparted to the threads by the grooves 27.
  • the threads are deposited on the upper surface of a carrier sheet 30 moving into the cross-laying apparatus 11).
  • the carrier sheet comprises a web of creped wadding drawn from a supply roll 311 and around guide rollers 32 and 33 onto the upper surface of the belt 112.
  • the roller 33 is positioned such that the web 30 ofcreped wadding intersects the threads 20 at a slight angle and the adhesive on the threads is sufficiently tacky to hold the threads on the web surface in the predetermined sinusoidal pattern imparted by the adhesive applicator
  • a serving ring 35 is rotated about the mandrel 11 in the direction of the arrow 36 in timed relation to the helical movement of the belt 12 around the mandrel.
  • a plurality of reinforcing threads 37 are drawn from respective supply cones 38 are helically wound about the mandrel 11 and belt 12, with the threads 37 disposed in spacedapart, substantially parallel relation and extending generally straight across the web 30 in a transverse direction.
  • the precise spacing of the threads 37 and their angular orientation relative to the web 30, of course, depend upon the number of threads served by the ring 35, the rotational speed of the ring relative to the belt as well as the helical angle of the belt.
  • the reinforcing threads 37 are partially embedded and held in their parallel, spaced-apart relation by the adhesive on the threads 20 where the threads 37 and 20 cross one another.
  • another web 40 is preferably introduced in registry with the belt 12 and web 30 is wound about a subsequent helical turn on the mandrel 11.
  • the web 40 is drawn from a supply roll 41 and is trained around guide rolls 42, 43 and 44 which guide the web 40 to the mandrel in registry with the belt 12 and web 30 as they travel around the mandrel. The web 40 thus overlies the threads 37 and imprisons them against the sinusoidal threads 20 and the lower web 30.
  • the top web 40 preferably makes at least one complete helical turn on the mandrel 11 and a slitter 48 is disposed along the edges of the web 40 and belt 12 to cut the cross threads 37 into transverse segments after they are imprisoned between the webs 30 and 40.
  • the belt 12 and composite web comprising the bottom wadding layer 30, sinusoidal threads 20, cross threads 37 and top web 40 travel off the mandrel 11 in the direction of the belt drive and support roller 15.
  • the composite web is then separated from the belt 12 and, in the illustrated apparatus 10, is wound around the surface of a preheat drum 50 before being directed into the nip of a pair of calender rolls and 52.
  • the preheat drum serves to at least partially cure or dry the adhesive in the composite web and brings the adhesive to the desired condition for final bonding of the assembled components.
  • the required surface temperature will depend on the type of adhesive employed as well as the length of time the web remains in contact with the heated drum surface. While various adhesives may be employed, advantages reside in the use of plastisols which, as is well known, are colloidal dispersions of synthetic resins in a suitable organic ester plasticizer. While many adhesives of this nature are known, those found particularly useful for incorporation in the product of this invention include vinyl chloride polymers, and copolymers of vinyl chloride with other vinyl resins, plasticized by organic phthalates, sebacates, or adipates.
  • the steel drum 50 is heated to a temperature of about 250 to 350 F., to advance the curing or drying of the adhesive.
  • Hot calender rolls 51 and 52 operate at temperatures of 300-375 F. and serve to complete the curing or drying of the adhesive while firmly bonding the cross threads 37 and sinusoidal threads to the bottom web 50 and top web 40.
  • the composite web then passes over a series of cooling drums 53 and 54 prior to being wound on a take-up roll 55.
  • the top web 40 is formed of creped cellulose wadding similar to the bottom web 30. Such a material is shown, in somewhat exaggerated form, in FIG. 5.
  • the creped wadding layers are each preferably formed of at least one ply having a basis weight before creping of between about 4 and 12 pounds per 2,880-square-foot ream and have a residual stretch ratio of between about 1.2 and 1.5 after stretching and ironing.
  • the under surface of the top web can also be printed with adhesive and for this purpose, an offset adhesive printer, indicated generally at 60, is provided.
  • the warp threads 20 and cross threads 37 are preferably of multifilament low twist construction having an overall denier in the range of between about l5 and and a twist ratio of not more than 6 turns per inch and preferably not more than 2 turns per inch. Both the warp threads and cross threads are disposed in spaced-apart parallel relation between about 2 and 12 threads per inch. It will be understood, of course, that the sinusoidal disposition of the warp threads 20 is selected to afford a longitduinal stretch characteristic within the range of and preferably identical to the residual stretch ratio of the creped wadding layers 30 and 40.
  • the present invention also contemplates the method of producing cross-thread-reinforced fiber webs which does not require the addition of a top layer of cellulose wadding.
  • this method it is desirable to introduce holddown threads on each side of the slitter as disclosed, for example, in U.S. Pat. No. 3,025,196. If such holddown threads are employed, the edges of the composite material are subsequently trimmed off to remove the holddown threads so as not to impair the longitudinal stretch characteristics of the material
  • the bottom wadding layer 30 may also be initially eliminated, if desired, to produce a longitudinally stretchable, cross-thread-reinforced nonwoven material.
  • the adhesively coated threads 20 are discharged in a sinusoidal pattern directly on the release-coated surface of the carrier belt 12.
  • holddown threads such as disclosed in the above mentioned U.S. Pat. No. 3,025,196 are preferably introduced on each side of the slitter 48.
  • the belt 12 may also be heated by means (not shown) to partially cure or dry the adhesive to the point where the threads 20 release cleanly from the belt.
  • One or more wadding layers may subsequently be applied to the previously formed nonwoven scrim as, for example just prior to wrapping it around the preheat drum 50.
  • a longitudinally stretchable, nonwoven material comprising, in combination:
  • warp thrdads extendimg generakly n he longhtudimfl diqebsion $0lof the material and in a generally sinusoidal pattern;
  • said warp and cross threads being of multifilament low twist construction
  • top and bottom layers of sheet material having appreciably more longitudinal than transverse stretch characteristics
  • cross threads being adhesively bonded to said warp threads where they cross one another, and said top and bottom layers being adhesively bonded to at least said warp threads.

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Nonwoven Fabrics (AREA)
  • Manufacturing Of Multi-Layer Textile Fabrics (AREA)

Abstract

A longitudinally stretchable, nonwoven material and the method of making same are disclosed. A plurality of spaced-apart, substantially parallel warp threads are drawn from their respective supply cans and over an adhesive applicator. The warp threads are laterally oscillated and deposited on the surface of a carrier sheet moving into a thread cross-laying apparatus to produce a generally sinusoidal pattern of threads on the carrier sheet. A plurality of spaced-apart, substantially parallel cross threads are then laid generally straight across the carrier sheet in a transverse direction as it moves through the cross layer and the cross threads are adhesively bonded to the warp threads where they cross one another. Provision is also made for introducing and laminating top and bottom layers of sheet material to the longitudinally stretchable, nonwoven material.

Description

United States Patent [72] Inventor Karl E. Sager Appleton, Wis. [21] Appl. No. 813,982 [22] Filed Apr. 7, 1969 [45] Patented Oct. 26, 1971 [73] Assignee Kimberly-Clark Corporation Neenah, Wis.
[54] LONGITUDINALLY STRETCHABLE NONWOVEN MATERIAL 7 Claims, 5 Drawing Figs.
[52] US. Cl. 161/57, 156/175,156/177,156/178,156/183,161/129, 161/141,161/143,161/156,161/157 [51] Int.Cl B32b5/l2 [50] Field ofSearch 161/57, 58, 59,129,142,156,157,143,141;156/175,]76, 177,178,181,183
[56] References Cited UNITED STATES PATENTS 2,502,514 4/1950 Ewer l54/1.76
2,604,424 7/1952 Mathes 161/128 3,479,244 11/1969 Burnett 156/181 X 3,523,056 9/1970 Horning 156/183 X Primary Examiner-Robert F. Burnett Assistant Examiner-Raymond O. Linker, Jr. Attorney-Wolfe, Hubbard, Leydlg, Voit & Osann, Ltd.
ABSTRACT: A longitudinally stretchable, nonwoven material and the method of making same are disclosed. A plurality of spaced-apart, substantially parallel wa'rp threads are drawn from their respective supply cans and over an adhesive applicator. The warp threads are laterally oscillated and deposited on the surface of a carrier sheet moving into a thread cross-laying apparatus to produce a generally sinusoidal pattern of threads on the carrier sheet. A plurality of spaced-apart, substantially parallel cross threads are then laid generally straight across the carrier sheet in a transverse direction as it moves through the cross layer and the cross threads are adhesively bonded to the warp threads where they cross one another. Provision is also made for introducing and laminating top and bottom layers of sheet material to the iongitudinally stretchable, nonwoven material.
PATENTEnnm 26 I9?! SHEET 10F 2 LONGITIJDINALLY STRETCI-IABLE NONWOVEN MATERIAL BACKGROUND OF THE INVENTION The present invention relates generally to nonwoven material and more particularly concerns longitudinally stretchable nonwoven materials and methods of making same.
It haspreviously been proposed, for example in Hirschy U.S. Pat. No. 2,841,202 and in Burger U.S. Pat. No. 3,025,196 to provide thread cross-laying apparatus for making a cross thread reinforced nonwoven material in which both the 1ongitudinally extending warp threads and the generally transverselyextending cross threads are adhesively bonded together at their crossings in spaced-apart, parallel and substantially straight condition. Such a nonwoven scrim, of course, has utility of its own, but more often it is used to longitudinally and transversely reinforce one or more layers of sheet material which otherwise have relatively low strength characteristics. One very practical application of such scrim-reinforced materials employing outer layers of creped cellulosic wadding is in the fabrication of disposable garments, sheets, coverings, toweling and the like. Normally, however, such creped wadding has considerably higher stretch and strength properties in the longitudinal direction than in the cross direction and this makes it difficult to match the creped wadding with a reinforcing scrim having the desired properties of stretch and strength in both the longitudinal and transverse directions.
Accordingly, it is the primary aim of the present invention to provide a method of making a cross-reinforced nonwoven material which has a controlled and predetermined amount of longitudinal stretch built into it.
It is a further object to provide such a longitudinally stretchable nonwoven reinforcing material whichcan be easily matched with the stretch requirements of various surfacing webs.
A more particular object is to provide a longitudinally stretchable nonwoven reinforcing scrim in which the warp threads are disposed in a generally sinusoidal pattern.
SUMMARY OF THE INVENTION The longitudinally stretchable, nonwoven material of the present invention includes a plurality of spaced-apart, sub stantially parallel warp threads which extend generally 1ongitudinally in a sinusoidal pattern and a plurality of spacedapart, substantially parallel cross threads which extend generally straight across the warp threads with the warp threads and cross threads bonded together where they cross one another. The warp threads are first drawn from their respective supply cans and aligned in spaced-apart, substantially parallel relation and, after application of adhesive, are laterally oscillated and deposited on the surface of a carrier sheet moving into a cross-laying apparatus where the cross threads are laid straight across the sinusoidally disposed warp threads.
in the preferred embodiment, the warp threads and cross threads are of multifilament low twist construction having an overall denier in the range of between about and 150 and a twist ratio of not more than 6 turns per inch and are spaced apart between about 2 and 12 threads per inch. However, the invention also contemplates the use of monofilament threads which, preferably, have a denier in the range of 15 and for certain applications. A preferred laminated longitudinally stretchable nonwoven material includes a longitudinally sinusoidal scrim as described above adhesively bonded to one or more layers of sheet material having appreciably more 1ongitudinal than transverse stretch characteristics such as creped cellulosic wadding. The creped wadding layers are each preferably formed of at least one ply having a basis weight before creping of between about 4 and 12 pounds per 2,880- square-foot ream and have a residual stretch ratio of between about 1.2 and 1.5 after stretching and ironing.
BRIEF DESCRIPTION OF THE DRAWINGS In the drawings:
FIG. 11 is a schematic side elevation of a cross-laying apparatus which may be utilized to practice the method of the present invention;
FIG. 2 is an enlarged fragmentary front elevation view of the adhesive application roll;
FIG. 3 is an enlarged fragmentary section taken substantially along line 3-3 in FIG. 2;
FIG. 4i is a projection ofone ofthe grooves in the cylindrical surface of the adhesive application roll shown in FIG. 2; and,
FIG. 5 is an enlarged fragmentary plan view of one form of longitudinally stretchable, nonwoven material made on the apparatus shown in FIG. 11 with the various layers broken away to show the internal details of the multicomponent construction.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Turning now to the drawings, there is shown schematically in FIG. 11 an apparatus for making longitudinally stretchable, nonwoven material according to the present invention. The illustrated apparatus 110 includes a generally cylindrical mandrel 11 around which an endless belt 112 is helically wound through a plurality of turns. The mandrel Jill is preferably in the form of a hollow cylindrical shell having a plurality of air discharge openings therein and the interior of the mandrel is supplied with air under pressure in order to floatingly support the belt 12 on the surface of the mandrel. In the present instance, the belt 112 makes three turns or wraps on the mandrel 11 and the belt is further supported by a plurality of guide rollers and turning bars M-IIl mounted in a suitable frame (not shown).
It will be understood that the location and disposition of the roller M relative to the mandrell 11 determines the approach angle of the best 12 to the mandrel and thus the angle of the helical turns. In the illustrated embodiment, roller 15 not only guides and supports the belt 112 as it moves off the mandrel, but also drives the belt around the helical turns through suita' ble means (not shown). The belt is also guided by roller 116 and 19 andturning bars 17 and 118, which are preferably ofthe air-floating type, as it returns from drive roll 15 to guide roll 14.
Pursuant to the present invention, a plurality of threads 21) are drawn from their respective supply spools which are located, for example, in a creel room 21. The threads 21 pass through a comb 22 to align them in spaced-apart, substantially parallel relation. The threads 21) are then drawn over a grooved adhesive applicator roll 23 which coats the threads with a thin layer of flexible adhesive. The applicator roll is partially submerged in liquid adhesive contained in a supply trough 24 and excess adhesive is removed from the surface of the roll by a suitable doctor blade 25.
As shown in greater detail in FIGS. 2 and 3, the surface of the applicator roll 23 is provided with a plurality of axially spaced, self returning grooves 27, each of which, in cylindrical projection, define a sinusoidal pattern (see FIG. d). Suitable means (not shown) are provided for rotating the applicator roll 23 and, as it rotates, the grooves 27 impart a laterally oscillating sinusoidal movement to the threads 20. The applicator roll 23is preferably rotated with a differential surface speed relative to the movement of the threads 20 to help avoid wrap-up of the threads on the roll and! to enhance the lateral force imparted to the threads by the grooves 27.
From the adhesive applicator roll 23, the threads are deposited on the upper surface of a carrier sheet 30 moving into the cross-laying apparatus 11). In the illustrated embodiment the carrier sheet comprises a web of creped wadding drawn from a supply roll 311 and around guide rollers 32 and 33 onto the upper surface of the belt 112. Desirably the roller 33 is positioned such that the web 30 ofcreped wadding intersects the threads 20 at a slight angle and the adhesive on the threads is sufficiently tacky to hold the threads on the web surface in the predetermined sinusoidal pattern imparted by the adhesive applicator A serving ring 35 is rotated about the mandrel 11 in the direction of the arrow 36 in timed relation to the helical movement of the belt 12 around the mandrel. As the serving ring rotates, a plurality of reinforcing threads 37 are drawn from respective supply cones 38 are helically wound about the mandrel 11 and belt 12, with the threads 37 disposed in spacedapart, substantially parallel relation and extending generally straight across the web 30 in a transverse direction. The precise spacing of the threads 37 and their angular orientation relative to the web 30, of course, depend upon the number of threads served by the ring 35, the rotational speed of the ring relative to the belt as well as the helical angle of the belt. The reinforcing threads 37 are partially embedded and held in their parallel, spaced-apart relation by the adhesive on the threads 20 where the threads 37 and 20 cross one another.
Following the helical wrapping of the threads 37 over the sinusoidal threads 20 on the web 30, another web 40 is preferably introduced in registry with the belt 12 and web 30 is wound about a subsequent helical turn on the mandrel 11. In the illustrated apparatus 10, the web 40 is drawn from a supply roll 41 and is trained around guide rolls 42, 43 and 44 which guide the web 40 to the mandrel in registry with the belt 12 and web 30 as they travel around the mandrel. The web 40 thus overlies the threads 37 and imprisons them against the sinusoidal threads 20 and the lower web 30. The top web 40 preferably makes at least one complete helical turn on the mandrel 11 and a slitter 48 is disposed along the edges of the web 40 and belt 12 to cut the cross threads 37 into transverse segments after they are imprisoned between the webs 30 and 40.
After the slitting operation, the belt 12 and composite web comprising the bottom wadding layer 30, sinusoidal threads 20, cross threads 37 and top web 40 travel off the mandrel 11 in the direction of the belt drive and support roller 15. The composite web is then separated from the belt 12 and, in the illustrated apparatus 10, is wound around the surface of a preheat drum 50 before being directed into the nip of a pair of calender rolls and 52.
The preheat drum serves to at least partially cure or dry the adhesive in the composite web and brings the adhesive to the desired condition for final bonding of the assembled components. The required surface temperature will depend on the type of adhesive employed as well as the length of time the web remains in contact with the heated drum surface. While various adhesives may be employed, advantages reside in the use of plastisols which, as is well known, are colloidal dispersions of synthetic resins in a suitable organic ester plasticizer. While many adhesives of this nature are known, those found particularly useful for incorporation in the product of this invention include vinyl chloride polymers, and copolymers of vinyl chloride with other vinyl resins, plasticized by organic phthalates, sebacates, or adipates. These combinations provide a fast-curing plastisol adhesive characterized by relatively low viscosity, low migration tendencies, and minimum volatility. Such adhesives remain soft and flexible after curing, can be reactivated by the application of heat and pressure, such as by hot-calendering, and insure that the resultant laminated product retains the desired softness, and proper hand and feel. Although plastisols are preferred, polyvinyl resins per se, plasticized or unplasticized, such as polyvinyl acetate, and copolymers may also be used. Other flexible adhesive may also be used, including acrylic resins such as the alkyl acrylates, and butadiene resins such as butadiene-styrene and butadiene acrylonitriles.
When using the preferred plastisol adhesives described above, the steel drum 50 is heated to a temperature of about 250 to 350 F., to advance the curing or drying of the adhesive. Hot calender rolls 51 and 52 operate at temperatures of 300-375 F. and serve to complete the curing or drying of the adhesive while firmly bonding the cross threads 37 and sinusoidal threads to the bottom web 50 and top web 40. The composite web then passes over a series of cooling drums 53 and 54 prior to being wound on a take-up roll 55.
In the preferred embodiment, the top web 40 is formed of creped cellulose wadding similar to the bottom web 30. Such a material is shown, in somewhat exaggerated form, in FIG. 5. The creped wadding layers are each preferably formed of at least one ply having a basis weight before creping of between about 4 and 12 pounds per 2,880-square-foot ream and have a residual stretch ratio of between about 1.2 and 1.5 after stretching and ironing. If desired, the under surface of the top web can also be printed with adhesive and for this purpose, an offset adhesive printer, indicated generally at 60, is provided.
The warp threads 20 and cross threads 37 are preferably of multifilament low twist construction having an overall denier in the range of between about l5 and and a twist ratio of not more than 6 turns per inch and preferably not more than 2 turns per inch. Both the warp threads and cross threads are disposed in spaced-apart parallel relation between about 2 and 12 threads per inch. It will be understood, of course, that the sinusoidal disposition of the warp threads 20 is selected to afford a longitduinal stretch characteristic within the range of and preferably identical to the residual stretch ratio of the creped wadding layers 30 and 40.
The present invention also contemplates the method of producing cross-thread-reinforced fiber webs which does not require the addition of a top layer of cellulose wadding. However, in practicing this method it is desirable to introduce holddown threads on each side of the slitter as disclosed, for example, in U.S. Pat. No. 3,025,196. If such holddown threads are employed, the edges of the composite material are subsequently trimmed off to remove the holddown threads so as not to impair the longitudinal stretch characteristics of the material The bottom wadding layer 30 may also be initially eliminated, if desired, to produce a longitudinally stretchable, cross-thread-reinforced nonwoven material. To produce a nonwoven material of this character, the adhesively coated threads 20 are discharged in a sinusoidal pattern directly on the release-coated surface of the carrier belt 12. After the cross threads 37 are wound around the helically traveling threads 20, holddown threads such as disclosed in the above mentioned U.S. Pat. No. 3,025,196 are preferably introduced on each side of the slitter 48. In this instance the belt 12 may also be heated by means (not shown) to partially cure or dry the adhesive to the point where the threads 20 release cleanly from the belt. One or more wadding layers may subsequently be applied to the previously formed nonwoven scrim as, for example just prior to wrapping it around the preheat drum 50.
While the invention has been described and illustrated in connection with certain preferred embodiments and procedures, it is not intended to limit the invention to those specific embodiments and procedures. Rather, it is intended to cover such other alternative and equivalent embodiments and procedures as fall within the spirit and scope of the present invention.
I claim as my invention:
1. A longitudinally stretchable, nonwoven material comprising, in combination:
a plurality of spaced-apart, substantially parallel warp thrdads extendimg generakly n he longhtudimfl diqebsion $0lof the material and in a generally sinusoidal pattern;
a plurality of spaced-apart, substantially parallel cross threads extending generally straight across the material in a. transverse direction;
said warp and cross threads being of multifilament low twist construction;
top and bottom layers of sheet material having appreciably more longitudinal than transverse stretch characteristics;
said cross threads being adhesively bonded to said warp threads where they cross one another, and said top and bottom layers being adhesively bonded to at least said warp threads.
2. A nonwoven material as defined in claim 1 wherein said warp threads have an overall denier in the range of between about 15 and 150 and a twist ratio of not more than 6 turns per inch.
5. A nonwoven material as defined in claim 4 wherein said l plies of wadding each have a basis weight before creping of between about 4 and 12 pounds per 2,.880-square-foot ream.
6. A nonwoven material as defined. in claim 1 wherein said warp threads are spaced apart between 2 and 12 threads per inch.
7. A nonwoven material as defined in claim 1 wherein said cross threads are spaced apart between 2 and 12 threads per inch.
UNITEe STATES PATENT OFFICE CERNFICATE 8F (IQRRECTIGN Patent No. 3, 1 9 D d October 26, 1971 Inventor(s) Karl E. Sager It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
In the Specification:
Col. 2, l. 34 change mandrell" to -rnandre1-;
i. 75 after 'appiicatoredd roll 23.
Co}. 3, 1. 18 after Web 30 add -and In the Claims Claim 1, 11. 4 and 5, change "thrdads extendimg generakly n he ionghizudim [I diqebsion $01 to e threads extending general ly in the longitudinal direction.
Signed and sealed this 28th day of November 1972.
(SEAL) Attest:
EDWARD MJLETCHER ,JR ROBERT GOTTSCHALK A ttesting Officer Commissione r' of Pa ten ts

Claims (6)

  1. 2. A nonwoven material as defined in claim 1 wherein said warp threads have an overall denier in the range of between about 15 and 150 and a twist ratio of not more than 6 turns per inch.
  2. 3. A nonwoven material as defined in claim 1 wherein said cross threads have an overall denier in the range of between about 30 and 100 and a twist ratio of not more than 2 turns per inch.
  3. 4. A nonwoven material as defined in claim 1 wherein said top and bottom layers are each formed of at least one ply of creped cellulosic wadding having a residual stretch ratio of between about 1.2 and 1.5.
  4. 5. A nonwoven material as defined in claim 4 wherein said plies of wadding each have a basis weight before creping of between about 4 and 12 pounds per 2,880-square-foot ream.
  5. 6. A nonwoven material as defined in claim 1 wherein said warp threads are spaced apart between 2 and 12 threads per inch.
  6. 7. A nonwoven material as defined in claim 1 wherein said cross threads are spaced apart between 2 and 12 threads per inch.
US3616129D 1969-04-07 1969-04-07 Longitudinally stretchable nonwoven material Expired - Lifetime US3616129A (en)

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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3816231A (en) * 1972-05-25 1974-06-11 Kendall & Co Reinforced nonwoven fabrics
US4360555A (en) * 1979-12-14 1982-11-23 Orcon Corporation Fill strand transfer process for making non woven fabrics
US4769202A (en) * 1985-11-29 1988-09-06 The B. F. Goodrich Company Process of making a conveyor belt
US5523141A (en) * 1993-08-09 1996-06-04 The Charles Stark Draper Laboratory, Inc. Extensible composite fabric and method and apparatus for making it
US6387471B1 (en) 1999-03-31 2002-05-14 Kimberly-Clark Worldwide, Inc. Creep resistant composite elastic material with improved aesthetics, dimensional stability and inherent latency and method of producing same
US6503855B1 (en) 1998-10-02 2003-01-07 3M Innovative Properties Company Laminated composites
US6547915B2 (en) 1999-04-15 2003-04-15 Kimberly-Clark Worldwide, Inc. Creep resistant composite elastic material with improved aesthetics, dimensional stability and inherent latency and method of producing same
US20030109842A1 (en) * 2001-12-12 2003-06-12 Louis Raymond Gerard St. Separated targeted elastic zone for improved process and product function
US20030114824A1 (en) * 2001-12-19 2003-06-19 Odorzynski Thomas W. Three dimensional profiling of an elastic hot melt pressure sensitive adhesive to provide areas of differential tension
US20030124331A1 (en) * 2001-12-28 2003-07-03 Charles Morell Elastic strand bonded laminate
US20040005834A1 (en) * 2002-07-02 2004-01-08 Peiguang Zhou Elastomeric adhesive
US20040006324A1 (en) * 2002-07-02 2004-01-08 Peiguang Zhou Garment including an elastomeric composite laminate
US6833179B2 (en) 2000-05-15 2004-12-21 Kimberly-Clark Worldwide, Inc. Targeted elastic laminate having zones of different basis weights
US6969441B2 (en) 2000-05-15 2005-11-29 Kimberly-Clark Worldwide, Inc. Method and apparatus for producing laminated articles
US20060258249A1 (en) * 2005-05-11 2006-11-16 Fairbanks Jason S Elastic laminates and process for producing same
US20070042663A1 (en) * 2005-08-18 2007-02-22 Gerndt Robert J Cross-direction elasticized composite material and method of making it
US7316842B2 (en) 2002-07-02 2008-01-08 Kimberly-Clark Worldwide, Inc. High-viscosity elastomeric adhesive composition
US7316840B2 (en) 2002-07-02 2008-01-08 Kimberly-Clark Worldwide, Inc. Strand-reinforced composite material
US7601657B2 (en) 2003-12-31 2009-10-13 Kimberly-Clark Worldwide, Inc. Single sided stretch bonded laminates, and methods of making same
US8182457B2 (en) 2000-05-15 2012-05-22 Kimberly-Clark Worldwide, Inc. Garment having an apparent elastic band

Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3816231A (en) * 1972-05-25 1974-06-11 Kendall & Co Reinforced nonwoven fabrics
US4360555A (en) * 1979-12-14 1982-11-23 Orcon Corporation Fill strand transfer process for making non woven fabrics
US4769202A (en) * 1985-11-29 1988-09-06 The B. F. Goodrich Company Process of making a conveyor belt
US5523141A (en) * 1993-08-09 1996-06-04 The Charles Stark Draper Laboratory, Inc. Extensible composite fabric and method and apparatus for making it
US6503855B1 (en) 1998-10-02 2003-01-07 3M Innovative Properties Company Laminated composites
US20030104746A1 (en) * 1998-10-02 2003-06-05 3M Innovative Properties Company Laminated composites
US20050084647A1 (en) * 1998-10-02 2005-04-21 3M Innovative Properties Company Laminated composites
US6835256B2 (en) 1998-10-02 2004-12-28 3M Innovative Properties Company Laminated composites
US6387471B1 (en) 1999-03-31 2002-05-14 Kimberly-Clark Worldwide, Inc. Creep resistant composite elastic material with improved aesthetics, dimensional stability and inherent latency and method of producing same
US6547915B2 (en) 1999-04-15 2003-04-15 Kimberly-Clark Worldwide, Inc. Creep resistant composite elastic material with improved aesthetics, dimensional stability and inherent latency and method of producing same
US6833179B2 (en) 2000-05-15 2004-12-21 Kimberly-Clark Worldwide, Inc. Targeted elastic laminate having zones of different basis weights
US8182457B2 (en) 2000-05-15 2012-05-22 Kimberly-Clark Worldwide, Inc. Garment having an apparent elastic band
US6969441B2 (en) 2000-05-15 2005-11-29 Kimberly-Clark Worldwide, Inc. Method and apparatus for producing laminated articles
US20030109842A1 (en) * 2001-12-12 2003-06-12 Louis Raymond Gerard St. Separated targeted elastic zone for improved process and product function
US6939334B2 (en) 2001-12-19 2005-09-06 Kimberly-Clark Worldwide, Inc. Three dimensional profiling of an elastic hot melt pressure sensitive adhesive to provide areas of differential tension
US20030114824A1 (en) * 2001-12-19 2003-06-19 Odorzynski Thomas W. Three dimensional profiling of an elastic hot melt pressure sensitive adhesive to provide areas of differential tension
US20030124331A1 (en) * 2001-12-28 2003-07-03 Charles Morell Elastic strand bonded laminate
US6902796B2 (en) 2001-12-28 2005-06-07 Kimberly-Clark Worldwide, Inc. Elastic strand bonded laminate
US6978486B2 (en) 2002-07-02 2005-12-27 Kimberly-Clark Worldwide, Inc. Garment including an elastomeric composite laminate
US6967178B2 (en) 2002-07-02 2005-11-22 Kimberly-Clark Worldwide, Inc. Elastic strand laminate
US20040005835A1 (en) * 2002-07-02 2004-01-08 Peiguang Zhou Elastic strand laminate
US20040005834A1 (en) * 2002-07-02 2004-01-08 Peiguang Zhou Elastomeric adhesive
US7015155B2 (en) 2002-07-02 2006-03-21 Kimberly-Clark Worldwide, Inc. Elastomeric adhesive
US7316842B2 (en) 2002-07-02 2008-01-08 Kimberly-Clark Worldwide, Inc. High-viscosity elastomeric adhesive composition
US7316840B2 (en) 2002-07-02 2008-01-08 Kimberly-Clark Worldwide, Inc. Strand-reinforced composite material
US7923505B2 (en) 2002-07-02 2011-04-12 Kimberly-Clark Worldwide, Inc. High-viscosity elastomeric adhesive composition
US20040006324A1 (en) * 2002-07-02 2004-01-08 Peiguang Zhou Garment including an elastomeric composite laminate
US7601657B2 (en) 2003-12-31 2009-10-13 Kimberly-Clark Worldwide, Inc. Single sided stretch bonded laminates, and methods of making same
US8043984B2 (en) 2003-12-31 2011-10-25 Kimberly-Clark Worldwide, Inc. Single sided stretch bonded laminates, and methods of making same
US20060258249A1 (en) * 2005-05-11 2006-11-16 Fairbanks Jason S Elastic laminates and process for producing same
US20070042663A1 (en) * 2005-08-18 2007-02-22 Gerndt Robert J Cross-direction elasticized composite material and method of making it

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NL7004897A (en) 1970-10-09
FR2038300A7 (en) 1971-01-08
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AU1342170A (en) 1971-11-07
DE2017784A1 (en) 1970-11-05

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