WO2009025643A1 - Composite élastique, et système et procédé pour fabriquer le composite élastique - Google Patents

Composite élastique, et système et procédé pour fabriquer le composite élastique Download PDF

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Publication number
WO2009025643A1
WO2009025643A1 PCT/US2007/018576 US2007018576W WO2009025643A1 WO 2009025643 A1 WO2009025643 A1 WO 2009025643A1 US 2007018576 W US2007018576 W US 2007018576W WO 2009025643 A1 WO2009025643 A1 WO 2009025643A1
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WO
WIPO (PCT)
Prior art keywords
web
elastic
strand
webs
moving
Prior art date
Application number
PCT/US2007/018576
Other languages
English (en)
Inventor
Anne Smid
Patrick King Yu Tsang
Andrew C. Wright
William S. Sayers
Kuo-Shu Edward Chang
Original Assignee
Dsg Technology Holdings Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dsg Technology Holdings Ltd filed Critical Dsg Technology Holdings Ltd
Priority to CA2697023A priority Critical patent/CA2697023C/fr
Priority to PCT/US2007/018576 priority patent/WO2009025643A1/fr
Priority to MX2010002055A priority patent/MX337926B/es
Publication of WO2009025643A1 publication Critical patent/WO2009025643A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/144—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers using layers with different mechanical or chemical conditions or properties, e.g. layers with different thermal shrinkage, layers under tension during bonding
    • A—HUMAN NECESSITIES
    • A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F13/00—Bandages or dressings; Absorbent pads
    • A61F13/15—Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators
    • A61F13/45—Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators characterised by the shape
    • A61F13/49—Absorbent articles specially adapted to be worn around the waist, e.g. diapers
    • A61F13/49007—Form-fitting, self-adjusting disposable diapers
    • A61F13/49009—Form-fitting, self-adjusting disposable diapers with elastic means
    • A61F13/4902—Form-fitting, self-adjusting disposable diapers with elastic means characterised by the elastic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/18—Handling of layers or the laminate
    • B32B38/1875—Tensioning
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING 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
    • D04H13/00—Other non-woven fabrics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2555/00—Personal care
    • B32B2555/02—Diapers or napkins

Definitions

  • the present invention relates generally to elastic composites. More particularly, the present invention relates to an elastic composite that can be employed in one or more areas of a garment, other textile or fabric structures, similar material structures, and the like. The present invention also relates to a system and method of making the elastic composite and a garment, other textile or fabric structures, and the like, employing the elastic component.
  • the elastic composite and the system and method for making the elastic composite are particularly suited for use with or on disposable absorbent garments or articles such as baby diapers and training pants. To illustrate the invention, exemplary and preferred embodiments described in the context of disposable absorbent garments.
  • Disposable absorbent garments contemplated by the invention include disposable diapers, disposable pull-on garments, and the like.
  • the principal elements of a- typical disposable absorbent garment include a liquid permeable inner layer (or topsheet), a liquid impermeable outer layer (or backsheet), and an absorbent core sandwiched between the inner and outer layers.
  • Elastic members may be incorporated into different parts of the garment. For example, elastic members may be positioned longitudinally along a diaper, generally outboard of the absorbent core to effect a seal around the buttocks, legs, or both of the users.
  • elastic members e.g., in the form of elongated elastic threads or strands
  • waist regions including the side waist regions
  • elastication allows the garment to stretch when it is put on and then during wear. In this way, the garment can stretch to accommodate variations in waist size and leg size of the user, while fitting snugly about the waist and legs.
  • elastic components When elastic members are incorporated into a part or area of the garment, that part or area typically becomes a distinct, functional component of the garment.
  • These elastic components include the side panels or ear portions, the waistband, and fastening tabs.
  • the elastic components to which the present invention is directed is generally elongated, and may be a distinct portion of a larger, unitary piece, or a separate, attachable component.
  • the elastic component typically contains one or more sections or layers in addition to the elastic members.
  • such an elastic component may be referred to as an elastic composite.
  • These elastic composites are typically functional components that have an important impact on the fit and sealability of the garment.
  • these elastic composites typically require a dedicated sub-process for manufacture which must be accommodated by the larger garment manufacturing process.
  • the elastic composite may be manufactured independently and fed into the larger process as a complete product.
  • the design and construction of the elastic composite represents, therefore, a significant portion of the cost of manufacturing a disposable absorbent garment, as well as the quality and utility of the finished product.
  • the term "elastic band” or “elastic composite” refers to a multi-layer construction.
  • a plurality of elastic members such as threads or strands, are disposed adjacent one or more layers, e.g., backsheet and topsheet.
  • the elastic members impart elasticity to the adjacent layers and thus, to that part of the garment or other textile structure.
  • Such an elastic structure may be a distinct attachable component of the garment or textile structure or may be a distinct portion or section of the garment body or textile structure or a larger, unitary component of the garment body or textile structure.
  • a method of making an elastic composite for incorporation into a disposable absorbent garment, textile or fabric structure, and the like comprises the steps of: conveying a first web of material along a first web plane moving path; conveying a second web of material along a second web plane moving path generally parallel with the first web plane moving direction; and applying a section of a continuous strand of elastic element onto both the first web and the second web along a direction generally transverse to the web plane moving paths.
  • another method of making an elastic composite comprises the steps of: conveying a first web, whereby the first web moves along a predefined path; applying a first section of a first elastic strand onto the first web and generally transversely to the moving web; applying a second section of a second elastic strand onto the first web and generally transversely to the moving web; and repeating the applying steps while performing the conveying step, thereby arranging a plurality of first and second elastic elements on the first web, in generally parallel relation to one another.
  • the present application is also directed to systems of making an elastic composite, suitable for employment with the above-described methods.
  • FIG. 1 is a plan view of a disposable absorbent garment in the unfolded configuration
  • FIG. 2 is a plan view of an elastic composite
  • FIG. 3 is a plan view of the elastic composite of FIG. 2 shown in an extended, stretchable condition;
  • FIG. 4 is a perspective view of the elastic composite of FIG. 2 with a cut-out detail to show an elastic construction;
  • FIG. 5 is a simplified schematic of a system for manufacturing the elastic composite according to the present invention
  • FIG. 6 is a top view of an elastic element applicator assembly for use with the system of FIG. 5;
  • FIG. 7 is a side view of the assembly of FIG. 6;
  • FIG. 8 is a simplified process illustration of making the elastic composite according to the invention.
  • FIG. 9 is a plan view of an alternative elastic composite according to the present invention.
  • FIG. 10 is a top view of an alternative elastic element applicator assembly for use with the system of FIG. 5, according to the invention.
  • FIG. 11 is a simplified illustration of a folding guide assembly for use with the system and method according to the invention.
  • FIG. 12A is a perspective view of an elastic composite used for reference
  • FIG. 12B is a perspective view of an elastic composite, according to one embodiment of the present invention.
  • FIG. 13A is a perspective view of another elastic composite used for reference
  • FIG. 13B is a perspective view of an alternative elastic composite, according to another embodiment of the present invention.
  • FIG. 14A is a top view of a system for making an elastic composite, according to an embodiment of the present invention.
  • FIG. 14B is a side view of the system in FIG. 14A;
  • FIG. 15A is a top view of a system for.making an elastic composite, according to an alternative embodiment of the invention.
  • FIG. 15B is a side view of the system in FIG. 15 A;
  • FIG. 16A is a cross-sectional view through line AA in FIG. 14B;
  • FIG. 16B is a cross-sectional view through line BB in FIG: 14B;
  • FIG. 16C is a cross-sectional view through line CC in FIG. 19B;
  • FIG. 16D is a cross-sectional view through a web output of elastic composite, according to the present invention.
  • FIG. 17 is a simplified flow chart illustrating basics steps of a method of making an elastic composite, according to the present invention.
  • FIG. 18 is a top view of a system for making an elastic composite, according to an embodiment of the present invention.
  • FIG. 19 is a perspective view of the system in FIG. 18; [0036] FIG. 2OA is a cross-sectional view through line AA in FIG. 18; [0037] FIG. 2OB is a cross-sectional view through line BB in FIG. 18; [0038] FIG. 2OC is a cross-sectional view through line CC in FIG. 18;
  • FIG. 21 is a cross-sectional view of a web output of elastic composite, according to the present invention.
  • FIG. 22 is a simplified flow chart illustrating basic steps of a method of making an elastic composite, according to the present invention.
  • FIG. 23 A is a perspective view of an elastic composite having dual elasticized regions;
  • FIG. 23B is a perspective view of another elastic composite having dual elasticized regions
  • FIG. 23C is a perspective view of an elastic composite having dual elasticized regions, according to another embodiment of the present invention.
  • FIG. 24A is a simplified illustration and front view of an alternative elastic element applicator in the form of a spinhead, according to the present invention.
  • FIG. 24B is a simplified illustration and top view of a web substrate conveyed in a method of making an alternative elastic composite, according to the present invention
  • FIG. 25 A is a simplified illustration and front view of an alternative elastic element applicator in the form of a spinhead, according to the present invention
  • FIG. 25B is a simplified illustration and top view of a web substrate conveyed in a method of making an alternative elastic composite, according to the present invention.
  • FIG. 1 a disposable absorbent garment 110 is shown that is suitable for the invention and in the form of a diaper having one or more elastic composites incorporated therein.
  • the elastic composite in FIGS. 1-4 and FIG. 9 have side and end edges and, thus, may be referred to herein as elastic composite bands.
  • FIG. 5 illustrates a system and process of making the elastic composite (and a garment having the elastic composite) in accordance with a previously described concept.
  • FIGS. 12-15 and 24-25 are now provided to illustrate another method(s) or process(es) of making an elastic composite (and a garment having the elastic composite), and a system for making or manufacturing the elastic composite, in accordance with the present invention.
  • FIGS. 1-10 also embody various aspects of the present invention in the form a novel elastic composite, a web output of the elastic composite, and/or a material structure, such as a disposable absorbent garment, textile or fabric structure, similar material structures, and the like, and into which the elastic composite is incorporated.
  • the described system and process are particularly focused on the application or integration of the elastic elements upon or with one of the layers of the composite.
  • FIGS. 16-23 are also provided to illustrate yet another method(s) or process(es) of making an elastic composite (and a garment having the elastic composite), and a system for making or manufacturing the elastic composite, in accordance with an alternative embodiment of the present invention.
  • These figures also embody various aspects of the present invention in the form a novel elastic composite, a web output of the elastic composite, and/or a material structure, such as a disposable absorbent garment, textile or fabric structure, and he like, into which the elastic composite is incorporated.
  • the described system and process are particularly focused on the application or integration of the elastic elements upon or with one of the layers of the composite.
  • the disposable absorbent garment 110 in FIG. 1 is of a type that can be placed against or in proximity to the body of a wearer so as to absorb and to contain various bodily exudates.
  • the present invention is applicable to a variety of disposable absorbent articles and garments, including training pants and a variety of adult incontinence products.
  • the inventive elastic composite or elastic composite band may provide a side panel or ear portion, a waistband, a fastening tab or band, . or other distinct elastic component of the garment or article.
  • the inventive elastic composite may also be incorporated into an ear portion to elasticate the ear portion or to supplement the ear portion with an elasticated fastening tab.
  • the present invention is not intended to be limited to the structures and the processes specifically described and illustrated herein. For purposes of description, however, the following discussion will be directed to an exemplary disposable diaper only.
  • the invention will be described in the context of its various configurations and aspects. It should be appreciated that alternative arrangements of the inventive disposable absorbent garment and such an elastic composite band may comprise various combinations, which include one or more of the various configurations and aspects of the invention.
  • FIG. 1 is introduced to illustrate some basic features of a disposable diaper 110, most of which are also applicable to other disposable absorbent garments contemplated by the invention.
  • the diaper 110 includes three main regions aligned along an imaginary longitudinal axis or plane AA. These regions include a first waist region 112 (typically at the front of the user when the garment 1 10 is worn), a back waist region 114, and a crotch region 116.
  • the diaper 110 is also characterized by a front edge 140, a back longitudinal edge 142, a first lateral or side edge or side margin 144, and a second lateral or side edge or side margin 146.
  • the diaper 110 includes ear regions or ear portions
  • the waist regions 112, 114 and crotch region 116 may be referred to as forming a central body portion 120 of the garment 110 that is positioned within side edges 144, 146.
  • the body portion 120 may also be referred to as being formed by a liquid permeable inner layer or topsheet 152, a liquid impermeable outer layer or backsheet (not shown), and an absorbent core 154 sandwiched between the two layers.
  • the ear portions 118 further include fastening tabs 124 for attaching the waist regions 112, 114 together.
  • the diaper 110 also has an elastic waistband 130 positioned generally along the back edge 142 to facilitate fastening and to enhance the fit and seal of the diaper 110.
  • the crotch region 116 fits about the crotch of the wearer, and the front and back waist regions, 112 and 114, fit about the corresponding waist areas.
  • the ear portions 118 wrap about the wearer and the fastening tabs 124 engage to form a complete, all-around waistline of the diaper 110.
  • FIG. 2 depicts a typical elastic composite band 210. More particularly, the elastic composite band 210 is one particularly suited for use as a side panel or fastening tab of a disposable absorbent garment (see, e.g., Fig. 1).
  • FIG. 4 provides a perspective view and partial cut-out of the elastic composite band 210.
  • the elastic composite band 210 may be characterized by an imaginary centerline LL. In one aspect of the invention, the centerline LL preferably corresponds with the machine direction of the elastic composite band 210 during manufacture.
  • the elastic band 210 also has side or longitudinally extending side edges 210a and 210b and laterally extending end edges 210c and 21Od. In FIG.
  • the elastic composite band 210 is shown in the stretched state as, for example, when a garment incorporating the elastic composite band 210 is worn. In this state, the elastic composite band 210 stretches, in the lateral or cross-machine direction (denoted by arrows XX).
  • the term “machine” direction refers to the direction at which the component, or more particularly, the material web from which the elastic composite is derived (e.g., cut from) is driven in an assembly line during manufacturing.
  • the cross machine direction is the direction XX extending laterally or perpendicularly relative to the longitudinal line LL.
  • the elastic composite band 210 has a central region 214 in which an elastic construction is situated. Extending laterally from this central elastic or elasticized region 214 are regions 216 and 218, which are substantially non-elasticized.
  • the regions 216, 218 occupy the expanse between the central elastic region 214 and the side edges 210a, 210b.
  • the elastic composite band 210 has a top layer 318 and a bottom or base layer 320.
  • the two layers 318, 320 preferably extend the total width and length of the elastic composite band 210, thereby providing the side edges 210a, 210b, and the end edges 210c, 21Od.
  • Both the base layer 320 and the top layer 318 are preferably non-woven, breathable, disposable materials such as propylene, non-woven fabric, breathable polyethylene/polypropylene films, or non-porous films (or combinations of these materials).
  • the base layer 320 and top layer 318 adhere to one another, thereby sandwiching and securing a plurality of elastic strands 322 therebetween.
  • the elastic strands 322 may be substituted, in alternative embodiments, by suitable elastic elements such as elastic strands, threads, ribbons, and elastic glue beads.
  • the elastic elements or strands 322 are distributed along a direction that extend between the side edges 210a, 210b and parallel with (or corresponding to) center line LL.
  • each elastic element 322 is generally aligned or oriented in a direction corresponding with the lateral or cross-machine direction, i.e., in a direction generally perpendicular to the longitudinal center line LL and intersecting the side edges 210a, 210b.
  • the strands 322 are disposed in generally parallel relation and spaced apart generally equally along the longitudinal direction. More preferably, the elastic strands 322 are of generally equal length. Accordingly, when the elastic composite band 210 is worn, the strands 322 impart elasticity into the structure which allows the band 210 to stretch in the lateral or cross-machine direction XX.
  • the elastic strands 322 are preferably tensioned during securement between the top and base layers 318, 320.
  • FIG. 3 illustrates the elastic composite band 210 in a laterally stretched condition.
  • the central elastic region 214 has a width that is almost equal to the non-elasticized zones 216 and 218.
  • the central elastic region 214 contracts and crimps to a substantially reduced width.
  • the contracted elastic strands 322 shirrs the elastic composite 210 and provide pleats 234 in the contracted elastic region 214.
  • the disposable absorbent garment 110 employs one or more elastic composite bands.
  • the disposable absorbent garment 110 employs in each of the ear portions 118, a fastening tab 124 having the elastic composite construction.
  • the elastic composite band is configured such that one non-elasticized region 124a is attached to and overlaps the central body 120 of the garment 110 while a second non-elasticized region 124b is situated outboard of the side margins 144, 146.
  • An elasticized region 124c as shown in FIG. 1, provides elasticity, and thus, stretch in the lateral or cross-machine direction (of the elastic composite).
  • the elasticity or stretch provided by the central elastic region 124c directed along a direction that is generally perpendicular to the longitudinal center line AA of the garment 110, and corresponds with a direction that wraps about the waistline of the user.
  • the disposable absorbent garment 110 in FIG. 1 also provides an elastic composite, as the waistband 130.
  • the waistband 130 is situated centrally in the waist region 114.
  • the elastic composite waistband 130 is disposed such that non-elasticized regions 130a, 130b are positioned outwardly of the longitudinal line AA of the garment 110, while an elasticized region 130c is positioned centrally across the longitudinal center line AA.
  • the elasticized region 130c is configured such that the elastic strands are aligned or oriented in a direction that is generally perpendicular to the longitudinal center line AA. In this way, the elastic composite waistband 130 imparts elasticity about the waist region 114 of the garment 110, and in a direction corresponding with the direction of waistline about the user.
  • FIG. 9 depicts an alternative elastic composite band.
  • the elastic composite band 710 illustrated therein differs from the previously described elastic composite band (see e.g. FIGS. 2 and 2a) in that the elastic composite band 710 includes two elasticized regions 714a and 714b.
  • the elasticized region 714a, 714b are preferably equidistantly spaced apart on either side of the longitudinal centerline AA.
  • the spacing of the elasticized regions 714a, 714b creates right and left non-elasticized or dead regions 716, 718, as well as central non- elasticized region 750.
  • the elasticized regions 714a, 714b imparts elasticity to elastic composite band 710a in the lateral directions XX, and in the central non-elasticized region 750, also in the opposite lateral direction VV.
  • FIGS. 5-8 and 10-11 depict a system and system components, and illustrate a method or process of making or manufacturing the elastic composite.
  • Two elastic composite web outputs 1031 are produced from four separate non-woven web inputs 1003a, 1003b,
  • a system 1001 includes four separate non-woven web inputs 1003a-1003d, which provide a web or roll of non-woven material for the elastic composite.
  • the system further includes an output assembly or reel 1005 that receives two elastic composite webs 1031 from the rest of the process. These two separate elastic webs may be fixed together to produce the kind of composite described in respect to FIG. 4 (or maintained separately).
  • a conveyor assembly 1009 Central to the system 1001 are a conveyor assembly 1009 for receiving, manipulating, and conveying each of the non-woven web inputs.
  • the conveyor assembly 1009 is positioned and operatively associated with an elastic element applicator such as a spinning head assembly 1007, that applies elastic fibers or strands upon, onto, and or integrally with the non- woven web inputs.
  • the spinning head assembly 1007 further includes a spin head 1017, preferably in the form of a spinning bracket, or cylinder 1017 and the like.
  • the spin cylinder 1017 is configured to hold an "end section" of the continuous strand WW of elastic and move it about a generally vertical plane XX in a reciprocal or repetitive pattern (relative to the conveyor assembly 1009).
  • This plane XX is defined by the area within the spinning perimeter of the cylinder 1017 and which is traced by the outer most bracket or eye 1017b securing the strand of elastic WW to the spin cylinder 1017.
  • the paths of the spinning head 1017 and the section of elastic strand retained thereby are provided on the plane XX.
  • nonwoven inputs 1003a and 1003b are fed, utilizing a series of rollers, into the conveyor assembly 1009. Before the two nonwoven webs are fed into the conveyor assembly 1009, the webs are directed through the folding guides or plates 1039.
  • the folding guides 1039 serve to effectively reduce the overall width of the nonwoven web by folding the lateral or side edges along a pre-determined, longitudinally-extending side fold line YY.
  • the first folding guide 1039a initiates the first 90° turn while the second folding guide 1039b initiates a second 90° turn.
  • the roller 1039 disposed in between the guide 1039a, 1039b facilitates the folding process.
  • the two folding guides 1039 and roller 1369 may be referred together as a folding guide assembly.
  • FIG. 6 illustrates yet another typical folding guide assembly.
  • the folding assembly 1639 includes folding plates 1639 and a roller 1669 upstream of the folding plates 1639.
  • a web 1603 is passed around the narrow roller 1669, whereby the width of roller 1669 helps determine the width of the web 1603 between the folded flaps VV (i.e., the width of exposed outward surface 1689 defined between the fold lines YY).
  • the width of the roller 1669 is substantially less than the width of the nonwoven web 1603.
  • the flat plates 1639 then helps to complete the fold and hold the folded sides down.
  • Another folding guide (not shown) may be provided in a position upstream of the folding roller 1669 to help guide or initiate the folding process.
  • the inward surface 1679 is the surface or side of the web 1603 toward which the folded flaps VV are turned.
  • the exposed outward surface 1689 is the surface opposite of the inward surface 1679.
  • the conveyor assembly 1009 is set up so as to guide these two nonwoven webs 1003a and 1003b through the center of the assembly 1009 towards and eventually inside the elastic spin cylinder 1007 (into the spinning path).
  • the conveyor assembly 1009 delivers the nonwoven webs to each outside,, upper and lower faces (outward faces) of the conveyor assembly 1009.
  • the direction of travel of the nonwoven webs are reversed and the webs are directed out of the spin cylinder 1007.
  • an elastic strand WW is wrapped around the entire conveyor assembly 1009, and as it contacts the upper and lower face of the web platforms it comes into contact with the nonwoven web.
  • the elastic strand WW is applied crosswise or laterally on the web, and transverse to the direction of the moving web.
  • the friction between the tensioned elastic strand and the nonwoven webs on the upper and lower faces of the conveyor assembly draws the "wrapped" elastic strand out of the spin cylinder 1017 and towards contact with two further nonwoven webs 1003c and 1003d.
  • the nonwoven webs 1003c and 1003d are operatively positioned upstream of an adhesive applicator 1013. Utilizing a system of rollers in conjunction therewith, the non- woven inputs 1003c, 1003d and adhesive applicators 1013 apply a web of pre-glued non- woven material onto the conveyor assembly 1009 and onto the elastic strand "wrapped" around the nonwoven webs 1003a and 1003b.
  • the system 1001 employs a standard elastic input source, e.g., a bobbin of elastic yarn, that feeds elastic strands or fibers WW onto a tensioning/speed controlling unit 1037 and then to the spin cylinder or the spinning head 1017, so as to apply the strands WW onto the conveyor assembly 1009 and the non-woven material webs conveyed therethrough.
  • Elastic is taken off the bobbin, box or positive drive system and fed through a tension and speed controlling motor towards the spin cylinder 1017.
  • the elastic WW is delivered through a hollow shaft in the motor controlling the spin cylinder 1017.
  • the elastic WW then passes into the spin cylinder 1017 and is guided by rollers, eyes or any other suitable mechanism around the inside face of the spin cylinder 1017.
  • FIGS. 6 and 7 provide alternate views of the spinning head assembly 1007 and conveyor assembly 1009.
  • the conveyor assembly 1009 receives four separate webs of non-woven materials and outputs two webs 1031 of elastic composite.
  • FIGS. 8 and 9 are provided to further illustrate the process of making the elastic composite. These figures, more particularly FIG. 8, illustrates the paths taken by the non-woven web materials to and from the conveyor assembly 1009.
  • Non-woven raw material webs are fed into the process at stage A. These webs provide four separate non- woven web inputs into the process.
  • Non-woven webs 1 and 3 are combined to make an elastic composite output 1 (i.e., referred to in the Figures as the WRAP output).
  • Non-wovens 2 and 4 which are both on the downside of the spinning head assembly 1007 and conveyor assembly 1009, combine to make a second elastic composite output 2 (i.e., WRAP 2).
  • non-woven webs 1 and 2 are folded prior to being directed to the conveyor assembly 1009.
  • a predetermined width of non- woven is folded over each side of the web to make two folded flaps VV.
  • the width of the flap VV determines the width of the dead zone or non-elasticized region described previously, while the width of the non- woven, after folding, determines the width of the elasticized region.
  • the non-woven webs 1 and 2 are fed into the conveyor assembly 1009, in particular into the middle or inside of the conveyor assembly 1009 with the folded side of each web facing the outside of or away from the conveyor assembly 1009. It should be noted that at this stage C, non- woven webs 1 and 2 are not bonded together.
  • the conveyor 1009 then feeds the non-woven webs 1 and 2 towards the spinning head assembly 1007.
  • the non-woven webs 1 and 2 have traveled almost the length of the conveyor assembly 1009 and progresses into the spinning path of spinning head assembly 1007 and intersecting the "spinning" vertical plane XX of the elastic strand WW.
  • the webs 1 and 2 are directed away from each other and onto the outside of the conveyor 1009 and away from the spinning head 1007.
  • Non-woven web 1 turns up on the upper side of the conveyor assembly 1009, while non- woven web 2 travels along the lower side of the conveyor assembly 1009.
  • an elastic strand WW is wound around the folded non-woven webs 1 and 2, as these webs pass through the spinning head and the vertical plane XX.
  • the elastic strand WW is applied to the moving webs 1 and 2 cross-directionally to the direction of the moving web.
  • the movements of the webs 1 and 2 away from within the spin cylinder 1017 draws the "wrapped" elastic strand out of the spin cylinder 1017.
  • non-woven webs 3 and 4 these webs are provided to the conveyor assembly 1009 with adhesive applied on one side (i.e., applied by the adhesive applicator 1013).
  • the non- woven webs 3 and 4 are brought into contact with webs 1 and 2, respectively, and the elastic strands WW.
  • the webs 1 and 3 sandwich elastic strands WW on the upper side of the conveyor assembly 1009
  • non- woven webs 2 and 4 sandwich elastic strands WW on the under side of the conveyor assembly 1009.
  • the elastic strands WW run between the two non-woven elastic non-woven composite (cross- direction), but is then cut by a knife (see knife 1410 in FIG. 9, as described below), thereby separating the two wrapped composites.
  • the composites 1 and 2 are fed away from the conveyor assembly 1009 and the folded flaps on webs 1 and 2 become unfolded, with guiding, to form a flat non-woven composite. Subsequently, the composites are guided from the spinning head assembly 1007 and conveyor assembly 1009 and into further processes. As shown in FIG. 5, the elastic output webs arrives via a system of rollers onto an elastic composite output reel 1005.
  • the conveyor assembly 1009 preferably includes two web moving platforms 1412 which are juxtapositioned so as to provide an interface therebetween.
  • Each web moving platform 1412 includes a continuous belt 1414 supported about a plurality of rollers 1416 so as to be capable of reciprocal motion.
  • the spinning head assembly 1007 is positioned about and in the vicinity of one end of the conveyor assembly 1009. In operation, the spinning head 1017 spins about the vertical plane XX which intersects the ends of the web moving platforms 1412 so as to deliver the elastic strands WW around and about both web moving platforms 1412.
  • the first and second non-woven move along the outside or exposed surfaces or sides of the web moving platforms 1412 and receives the elastic strands WW delivered by the spinning head 1017.
  • the moving web draws the continuous elastic strand WW from the spinning head 1017.
  • the above-described process provides an elastic composite with cross directional stretch properties.
  • the process also provides non-elasticized regions on either latitudinal side of the central elasticized zone of the composite.
  • non-woven is used to describe the principal material used in the construction of the elastic composite.
  • this invention is not limited to non-woven materials but may be applied to any material that is available in the form of a continuous sheet.
  • Other materials suitable for this application include PE film, PE film/non-woven laminates and tissue.
  • FIG. 10 illustrates an alternative conveyor assembly 1509 and an alternative elastic element applicator in the form of a spinning head assembly 1507.
  • the spinning head assembly 1507 is operated to convey or transmit elastic strands onto a web moving platform 1512 of the conveyor assembly 1509.
  • the conveyor assembly 1509 preferably employs two web moving platforms 1512, which are juxtapositioned so as to provide an interface therebetween.
  • the conveyor assembly 1509 is similar to that illustrated in FIGS. 5 and 6.
  • the conveyor assembly 1509 is operated differently in that more than one elastic strand WW is applied onto and about the web moving platforms 1512 at one time.
  • the spinning head assembly 1507 includes a spinning head in the form of a spin bracket 1517 having a plurality of arms 1517a.
  • the spin bracket 1517 receives elastic strands 1553 from a shaft 1551a of a motor 1551.
  • the motor 1551 feeds the two lines of elastic strands 1553 to the spin bracket 1517, and the two feeds of elastic strands 1553 are guided together through the spinning head assembly 1517 (where the two lines twist together). As shown in FIG.
  • the two strands 1533 are moved about a v vertical plane then delivered, together, onto a nonwoven web 1544 moving horizontally on the web moving platform 1512.
  • both lines of elastic strand 1553 are fed onto the same arm 1517a of the spinning bracket assembly 1517 (rather than on opposite sides). In this way, the separate feeds or lines of elastic strands 1553 are prevented from twisting together and possibly breaking.
  • the speed of the manufacturing process is increased. Specifically, the speed at which the composite is manufactured may be increased by up to 100%, without increasing the speed at which the spinning head assembly is spinning and without changing the overall number of elastic strands in the final composite.
  • Table 1 below provides two examples of the result of a process of applying the elastic strands WW onto a nonwoven web.
  • the spinning head assembly 1517 operates at the same rotational speed in both processes. However, the pitch (i.e., the separation between elastic strands WW) is doubled for the alternative process (wherein a pair of elastic strands are applied to the nonwoven web).
  • the total machine output is also doubled (i.e., from 40m/min of composite to 80m/min).
  • the overall amount or length of elastic strands WW utilized or applied to the composite is generally the same. Consequently, the final composite produced by both subprocesses have the same, or at least, similar tensile characteristics. Table 1
  • the elastic strands may be separated inside the spin head and directed independently to opposite sides of the nonwoven web.
  • the assembly 1507 that includes the elastic bobbins/reel and tensioners and guides the elastic strands into the motor 1551 (or more appropriately, the motor shaft 1551a), is rotated at the same speed and in the same direction as the spin head 1517. In this way, the risk of twisting of the strands together inside the spin head 1517 is minimized.
  • FIGS. 12A-14B are provided to illustrate aspects and embodiments of a present invention.
  • FIGS. 12B and 13B depict alternative elastic composites according to the invention.
  • FIGS. 14A and 14B illustrate an exemplary system that is operable to implement a method of making the elastic composite also according to the invention.
  • the exemplary system may be used with or integrated into the system(s) previously described in respect, for example, to FIG. 5.
  • the invention, and its various aspects and embodiments, shall be understood in view of FIGS. 12A-14B and/or the accompanying descriptions, as well as the previous illustrations and accompanying descriptions.
  • FIGS. 1-11, and accompanying descriptions demonstrate application of a tensioned elastic strand across a moving web of nonwoven sheet.
  • the elastic strand was affixed to the nonwoven sheet so as to provide a composite having, among other attributes, cross- directional elasticity.
  • the elastic strand, or a group of elastic strands were fed via a single path and then applied to a moving web of nonwoven sheet by operation of a spin head.
  • the elastic strand or group of elastic strands are distributed onto the web at the rate of one strand per single revolution of spinhead.
  • a method is now described whereby multiple strands, e.g., two strands or two separate group of strands, are applied to a moving web of nonwoven sheet.
  • the strands or collection of strands travel by two separate paths and are distributed onto the web of nonwoven sheet at the rate of two strands per single revolution of the spinhead.
  • the two strands may be applied simultaneously to different portions of a conveyor assembly conveying one or more webs.
  • This variation of the invention provides advantages in efficiency as the output of the machine is increased by at least 100%. Alternatively, the machine speed may be reduced by as much as 50%, providing a reduction in running costs due to wear and tear and energy consumption.
  • the present inventive method maintains, however, the same output and volume as the single path processes previously described.
  • SSSP single strand, single path method
  • the term “multiple strands, single path method (MSSP)” refers to a method of manufacture whereby multiple strands of elastic element are grouped together and distributed via a single path or mode of travel through the spinhead. In this method, the elastic strands are distributed on the web of nonwoven sheet at the rate of one collection of strands per revolution of the spinhead. An example of this method was described in respect to FIG. 15. [0089] Furthermore, the term “single strand, dual path method (SSDP)” refers to a method of manufacture whereby two strands of elastic element enters the spinhead and are distributed onto the web of nonwoven sheet via two separate paths or modes of travel, in accordance with the present invention.
  • SSDP single strand, dual path method
  • the elastic elements are distributed on the moving web of nonwoven sheet at the rate of two strands per revolution of the spinhead.
  • MSDP multiple strands, dual path method
  • a substantially long feed of elastic may be referred to as a "continuous strand” even though it is understood that the strand is not infinitely long.
  • the elastic strand is, for practical purposes, continuous.
  • the term “continuous”, as applied to "strand”, shall indicate a length that will not be consumed in less than a few revolutions of the spinhead.
  • strand is used to refer to the feed or continuous length of elastic whereas the section or segments applied to the elastic composite may be referred to as “elastic elements.”
  • a “section” of elastic is referred to herein as the length (i.e., the end length) outside of, fed by, the arms or eyelets of the spinhead and is spun by the spinhead.
  • FIG. 12A reproduces, in an alternative view, the elastic composite 210 depicted in FIGS. 2A, 2B 5 and 3.
  • the elastic composite 210 has a fixed width DD in the lateral direction and a predetermined cut length EE along the longitudinal direction.
  • a continuous web of the elastic composite 210 is delivered as output, having continuous longitudinally directed side edges 210a, 210b and a central elasticized region 214 in which an elastic construction is situated.
  • Extending laterally from the elasticized region 214 are non-elasticized regions 216 and 218 (also referred to herein as "dead zones").
  • the elastic composite 210 includes atop layer 218, a bottom layer 220, and a plurality of elastic elements 322 sandwiched therebetween.
  • the top and bottom layers 218, 220 provided in most, if not all, of the examples in these descriptions are preferably nonwoven. It is contemplated, however, that other materials may also be used, including a variety of textile materials, fabrics, and the like.
  • the elastic element 322 extends generally along a direction generally perpendicular to the longitudinal or machine direction and are spaced apart from one another by a generally fixed distance n or pitch.
  • FIG. 12B depicts an exemplary sheet of elastic composite 1710 according to the present the invention.
  • the elastic composite 1710 has been manufactured in accordance with a single strand dual path method.
  • the elastic composite 1710 includes sections and components that are identical to those of the elastic composite 210 in FIG. 17 A, with the exception of a central elasticized region 1714.
  • Sandwiched between a top layer 1718 and a bottom layer 1720 are a plurality of spaced-apart, laterally extending elastic elements 1722.
  • the distribution of elastic elements 1722 is alternately provided by a first elastic element 1722a and a second elastic element 1722b.
  • the first and second elastic elements 1722a, 1722b differ in that one is fed from a source different from the source of the other.
  • the sources are preferably a first continuous elastic strand and a second distinct, continuous, elastic strand.
  • the two continuous elastic strands are of the same material type and have the same material properties, but may be varied, in further embodiments, to impart specifically targeted elastic properties to the elastic composite 1710.
  • the two elastic strands may also differ in thickness (see e.g., FIG. 29B as described below), as well as or in lieu of varying elasticity.
  • One of the elastic strands may even be a type of activated elastomer (e.g., heat activated).
  • the two elastic strands may have a different color to achieve a specific aesthetic design, for example.
  • the method according to the present invention provides some flexibility in the functional and aesthetic design of the elastic composite.
  • the elasticized region 1714 includes an arrangement consisting of alternating first and second elements 1722a, 1722b that are spaced apart by a generally fixed distance or pitch n'. This pitch n' is reduced from the pitch n in the previous elastic composite 210 (see FIG. 17A), thereby providing for a greater elastic density across the elasticized region 1714.
  • the two elastic elements 1722a, 1722b are distributed onto the web or nonwoven substrate preferably from opposing sides of the spinhead. For every revolution of the spinhead, two strands of elastic elements 1722a, 1722b are delivered onto the web.
  • FIG. 24B depicts an exemplary web substrate 2960 whereon a plurality of first elastic elements 2922a and second elastic elements 2922b are applied on a moving first input web Wl .
  • the distribution of elastic elements provides an alternating sequence of first elastic element — second elastic element — first elastic element on the web substrate 2960.
  • the first and second elastic elements 2922a, 2922b are provided by, and are discrete, severed portions of, different elastic strands.
  • the first elastic element 2922a has a greater thickness than the second elastic element 2922b.
  • the distribution of elastic elements provides for different or alternating pitch between successive elastic elements in the sequence.
  • the elastic elements 2922a, 2922b are alternately separated by a pitch of nl and a pitch of n2.
  • the larger pitch n2 is three times greater than the pitch nl .
  • this alternating pitch sequence may be achieved by providing a spinhead 2917 such as the spinhead 2917 illustrated in FIG. 24A.
  • the spinhead 2917 has a pair of eyelets 2917b, 2917b' for distributing a first continuous strand W and a second continuous strand W respectively.
  • FIG. 25 provides a front view of a spinhead 3017 wherein a pair of strand dispenser eyelets 3017b, 3017b' are diametrically opposed and thus, separated by 180° (spin phase revolution).
  • the eyelets 3017b, 3017b' are therefore equidistantly spaced from each other in either direction. Operation of this spinhead 3017 generates a web output 3060 whereon each successive pair of elastic elements 3022a, 3022b are ultimately separated by a pitch n, as discussed previously.
  • FIG. 13 A depicts an elastic composite 210' manufactured in accordance with the method previously described in respect to the system of FIG. 15.
  • the elastic composite 210' is manufactured by an MSSP method.
  • the elastic composite 210' includes sections and components that are generally identical to those of the elastic composite 210 in FIG. 12A 5 with the exception of the elasticized region 214'.
  • the elasticized region 214' is composed of discrete groups 322' of multiple elastic elements that extend generally in the lateral direction.
  • the center of the groups 322' of elastic elements are spaced apart from one another in generally parallel relation by the same fixed distance n (from Fig. 17) (a center-to- center distance).
  • n from Fig. 17
  • a center-to- center distance In accordance with the method previously described in respect to the system of FIG. 15, a group 322' of elastic strands is delivered to the web upon each revolution of the spin head.
  • the groups 322' consist of two adjacent elastic elements.
  • FIG. 13B depicts an exemplary elastic composite 1810 according to a further embodiment of the present invention.
  • the elastic composite is manufactured by an MSDP method, in accordance with an alternative embodiment of the present invention.
  • the elastic composite 1810 includes sections and components that are generally identical to those of the three previously described elastic composites 210, 1710 and 210', with the exception of the elasticized region 1814.
  • two different groups of elastic strands 1822a, 1822b are delivered onto the web upon each revolution of the spinhead.
  • the lateral centerlines of the groups 1822a, 1822b are spaced apart by the smaller pitch n' — as with the elasticized region 1714 in FIG. 12B.
  • the resulting elasticized region 1814 in this embodiment imparts a greater degree of elasticity to the elastic composite 1810 than any of the other arrangements.
  • a higher elastic density is achieved by both providing for a smaller fixed distance, n', between the individual elastic elements or groups and providing for more elastic elements at application by the spin head.
  • the speed of the operation is increased from the operation associated with each of the elastic composites in FIGS. 12A and 13A.
  • each of the two groups 1822a, 1822b may be varied or may be of one type. Further, the constituents of the other two groups may be different or identical.
  • the elastic elements are directed generally perpendicular to the longitudinal or machine direction. Further, the elastic elements are structurally independent of each other, although in some embodiments may be of (i.e., severed sections) one or more elastic strand. In FIG. 12A, for example, all of the elastic elements are elastic elements of a single, continuous strand, although, in the composite, the elastic elements are structurally independent. Furthermore, each elastic element generally does not have a vertical (or longitudinal) component. As a result, a certain uniformity in horizontal elasticity is achieved. In some embodiments, this characteristic provides an elongated elastic composite that does not tend to twist or kink when at rest, and at rest, is more uniform and aesthetically pleasing.
  • Table 2 summarizes some of the benefits and advantages attained by the different manufacturing methods discussed above. To facilitate the comparisons, the number of elastic elements per unit of linear length provided by the four methods is the same. Thus, the tensile and elastic properties of the output elastic composites are similar. TABLE 2
  • Output (m/min) spinhead speed (rpm) x no. of elastic elements applied per revolution x pitch x 2.
  • Table 2 illustrates the design and operational flexibility attainable through employment of the various methods previously described. As will become apparent to one skilled in the art provided with the present disclosure, certain methods may prove more useful than others depending on the particular design and operational requirements. In this regard, attention is now directed to the systems available to implement these manufacturing methods.
  • FIGS. 14A and 14B depict a system 1901 and system components, and illustrate a method of making an elastic composite (e.g., elastic composite 1710 or 1810) according to the present embodiment.
  • the system and its components are substantially similar to those previously described.
  • the differences between the previously described systems and the system 1901 of FIGS. 14A, 14B represent improvements provided by the present invention. These differences will be the focus of the following description.
  • the system 1909 includes the same components provided, for example, in the system depicted in FIGS. 5-11.
  • the system 1901 includes a conveyor assembly 1909 for receiving, manipulating, and conveying each of the two nonwoven web inputs.
  • the conveyor assembly 1909 is positioned next to, and operatively associated with, an elastic element applicator in the form of a spinning head assembly 1907.
  • the spinning head assembly 1907 is operable to apply elastic fibers or strands upon, onto, and/or integrally with an input web of nonwoven conveyed by the conveyor assembly 1909.
  • the spinning head assembly 1907 further includes a spinhead 1917, preferably in the form of a spinning bracket or cylinder 1917 (spinhead).
  • the spinhead 1917 is configured to hold an "end section" of the continuous strand WW of elastic element and move it about a generally vertical plane XX in a reciprocal or repetitive manner (relative to the conveyor assembly 1909).
  • this plane XX is defined by the area within the spinning perimeter of the cylinder 1917 that is traced by the outer-most bracket or eye 1917b securing the continuous strand WW to the spin cylinder 1917.
  • the vertical plane XX need not be at 90° to the web platforms U, L (and thus, to the web plane moving direction), but it is generally preferred.
  • the path of the spinning head 1917 and the section of elastic strand retained thereby are provided on the plane XX.
  • the section of strand WW between the eyelet 1917b and the platform U is indicative of a linear portion of the plane XX.
  • the conveyor assembly 1909 includes an upper conveyor or web moving platform U (web platform U) provided by a movable, continuous belt Ul and a series of rollers supporting the belt Ul .
  • the conveyor assembly 1909 further includes a lower conveyor or web moving platform L (web platform L) also provided by a movable, continuous belt Ll and a series of rollers supporting the belt Ll .
  • the lower belt Ll is positioned in generally parallel relation with the upper belt Ul and vertically spaced therefrom by a distance or gap HH.
  • the belts Ul 5 Ll are designed for reciprocal motion during system operation, the belts Ul 5 Ll may be described as having a planar outside deck or surface Sl, S3 and a planar inside deck or surface S2, S3 at any fixed point in time (for purposes of the present description).
  • the use of "inside” and “outside” references are made in view of the relative locations of the surfaces (i.e., facing outside of the assembly 1909 or facing inside the assembly 1909). This use of such references is provided to facilitate the description only, and should not be construed as a limitation on the inventive system and method.
  • each of first and second primary inputs webs Wl, W2 provide a web of nonwoven utlizing a series of rollers and guides.
  • the two webs Wl, W2 are first directed through folding guides or plates, which serve to effectively reduce the overall width of the nonwoven web by folding the ends or side edges along a predetermined, longitudinally extending side fold line.
  • the input webs Wl, W2 are directed centrally into the gap HH between the upper and lower web platforms U, L, along a first web plane moving direction, MM and toward the spinhead 1917.
  • This first web plane moving direction MM also corresponds to a direction from right to left in the side view of FIG. 14B.
  • This first web plane moving direction MM also directs the nonwoven inputs 1903a, 1903b toward the center of the spinhead 1907.
  • the conveyor assembly 1909 reverses the direction of travel of the input webs Wl, W2 (a turn of 180 degrees), from the first web plane moving direction MM to the oppositely directed second web plane moving direction NN.
  • the second web plane moving direction NN is identical (orientation) to the first web moving plane moving direction MM, except that the directions are reversed.
  • a first elastic strand WW is wrapped around the entire conveyor assembly 1909 and contacts the outside surfaces Sl, S3 of the belts Ul, Ll 5 respectively.
  • the first elastic strand WW also comes into contact with the moving webs Wl, W2.
  • the elastic strand WW is applied crosswise or laterally on the web, and transverse to the second web plane moving direction NN. As explained previously, this transverse direction is also the cross-machine direction. Friction between the elastic strand WW and the input webs Wl, W2 on the belt surfaces Sl, S3, helps to draw the "wrapped" elastic strand WW out of the spinhead 1917.
  • the system 1901 positions a first elastic input source El on the left side of the system 1901 (in the views of FIG. 14 A, 14B).
  • the input source may be in the form of a spool of elastic.
  • the continuous first elastic strand WW is delivered through a hollow shaft in a motor that controls the spinhead 1917.
  • the elastic strand WW then passes into the spinhead 1917 and is guided by rollers, eyes, or other suitable means, around the inside of the cylinder of the spinhead 1917.
  • the system 1909 further employs a second elastic input source E2 that is, in the views of FIGS. 14A, 14B, positioned on the right side of the system 1901.
  • a second continuous elastic strand WW' may be delivered via any suitable system of rollers and eyes, centrally along the gap HH and into the open end of the spinhead 1917. Upon exiting the gap HH, the second continuous elastic strand WW' is directed across the center of the spinhead 1917 and to the back of the spinhead 1917.
  • the second continuous elastic strand WW' is then guided by rollers, eyes, or other suitable means, around the inside face of the cylinder, to an eyelet 1917b' positioned diametrically opposite (180°) of the eyelet 1917b of the first continuous elastic strand WW.
  • the first and second elastic strands WW, WW' are separated by 180°, within the spin cylinder.
  • the elastic strands WW, WW' are preferably tensioned by passing the continuous strand through any suitable tensioning unit prior to being received by the spinhead 1917.
  • the spinhead 1917 As the spinhead 1917 is spun around the upper and lower platforms U, L, sections of the first and second elastic strands WW, WW' are applied simultaneously about the two web moving platforms U 5 L.
  • the eyelet 1917b' for the second elastic strand WW is shown at a position slightly forward of the eyelet 1917b of the first elastic strand WW.
  • the eyelets 1719a, 1719b are not separated as such, but aligned so as to provide a common vertical plane XX.
  • the mis-alignment depicted in FIGS. 14 A, 14B are provided primarily to best show the distribution of elastic strands WW, WW' about the conveyor assembly 1909.
  • the generally vertical plane XX about which the first elastic strand WW is spun, is slightly left of a second generally vertical plane XX' (not shown), about which the second elastic strand WW' is spun.
  • the two vertical planes XX, XX" are disposed in mutual parallel relation and both intersect the upper and lower platforms U, L.
  • the elastic elements WW, WW' are applied onto the moving webs at these linear intersections of the vertical planes XX, XX' with the belt surfaces Sl, S3 (i.e., along the web path of the nonwoven webs).
  • the positions of the eyelets 1917b, 1917b' may be adjusted to achieve the desired pitch n' discussed above.
  • FIGS. 24A, 24B depict an alternative system 2001 (to the system 1901 of
  • FIGS. 14A and 14B for making the elastic composite according to the invention (wherein like reference numerals are used to indicate like elements).
  • a bracket system 2090 of tensioning rollers is provided proximate the end of the web platforms U, L and the end of the gap HH.
  • the bracket system 2090 directs the second continuous elastic strand WW away from the center line AA of the spinhead momentarily to avoid front rollers 2084.
  • the bracket system 2090 may be supported or suspended between the upper and lower web platforms U, L, and in between the input webs Wl, W2, by any suitable means. [00116] Returning to FIGS.
  • FIGS. 16A-16D provide cross-sectional views through the system 1901 depicted in FIG. 14. These simplified views are provided to illustrate certain points in the process of applying elastic elements onto the nonwoven webs.
  • a first cross-sectional view also is presented proximate the ends of the two web platforms U, L. The view reveals cross-sections of the two continuous belts Ul, Ll. This view includes cross sections showing outside belt surfaces Sl, S3, and inside belt surfaces S2, S4. As viewed in FIG.
  • the two inside belt surfaces S2, S4 move out from the page along the first web plane moving direction MM and convey the input webs Wl, W2 into the spinhead 1917.
  • the two outside surfaces Sl, S3 move into the page along the second web plane moving direction NN and convey the webs Wl, W2 away from the spinhead 1917.
  • the input webs Wl, W2 of nonwoven are shown on the belts Ul, Ll with their ends already folded.
  • the term "web plane path" shall mean the path (including direction) taken by the input webs Wl, W2 as conveyed by the conveyor assembly 1909.
  • the "web plane path” includes the path along the inside surface S2 of the continuous belt Ul directed along the first web plane moving direction MM and the path along the outside surface Sl of the same belt Ul directed along the second web plane moving direction NN.
  • the web plane path of the other input web is different from the first web plane path, although it is also directed, in certain segments of the path, in the same web plane moving directions MM or NN.
  • the vertical plane XX, XX' intersects the web plane path on the outside belt surface Sl and along a transverse line common with the web plane path.
  • the spinhead 1917 has applied several sections of the first and second continuous elastic strands WW, WW' about the conveyor assembly 1909, and more specifically, over the input webs Wl, W2. In doing so, the spinhead 1917 has applied the continuous elastic strands WW, WW' transversely in respect to the second web plane moving direction NN.
  • FIG. 16C a cross-sectional view is provided across a section downstream of the rollers for the third and fourth input webs W3, W4 of nonwoven.
  • the rollers facilitate the application of a second web layer upon each substrate that now includes the elastic elements and a first nonwoven web.
  • a moving web of elastic composite is produced consisting of a top layer of nonwoven sheet, a base layer of nonwoven sheet, and elastic elements sandwiched therebetween.
  • the ends of the input webs Wl, W2 are still folded around the ends of the belt surfaces Sl, S3.
  • the view of FIG. 21C also indicates the locations of knife mechanisms KK where the elastic strands WW, WW' are cut immediately downstream of the cross-sectional view. As discussed previously, the cuts may be provided by knife structures located adjacent the web platforms Ul, Ll.
  • the cross-sectional view of FlG. 16D represents a point further downstream in the process.
  • the continuous elastic strand WW, WW' has been cut to provide a distribution of segmented elastic elements 1722 within the web substrate. Every other segmented elastic element 1722 in the distribution is characterized as having originated from the same first or second continuous elastic strand. Further, each pair of adjacent or sequential elastic element 1722 are characterized as having originated from a different continuous elastic strand.
  • This view also reveals that the first and second input webs 1903 have been unfolded, in a manner described previously.
  • FIG. 16D depicts, therefore, a cross- section of web outputs Ol , O2 of the system and method of manufacture, according to the invention.
  • FIG. 17 provides a simplified flow chart of the basic steps of a method of making an elastic composite, in accordance with the present invention.
  • the flow chart 2210 also provides a summary of the process described in respect to FIGS. 19-21.
  • the basic steps of the method are preferably performed through operation of a system such as the exemplary systems 1901, 2101 of FIGS. 14 and 15.
  • a first web of material e.g., a nonwoven layer
  • the web plane path is simply a path along which a web having an expanse (i.e., width and substantial length) may be conveyed.
  • the web plane path is preferably controlled by a fixed system to provide a consistent path for a moving, continuous web, directed along a predetermined web direction (which is planar).
  • the web plane path is generally predetermined, in the preferred embodiment, by the web platforms of a conveyor assembly and the conveying step 2210 is implemented through operation of the web platforms.
  • a section of a first continuous elastic strand is then applied onto the first web and generally transversely to the web plane path (Step 2214). Further, a section of a second elastic strand is applied onto the second web and generally transversely to the web plane path (Step 2218).
  • steps 2214, 2218 are preferably performed through operation of a single spinhead that spins the two strands about the first web being conveyed and about a plane(s) that intersects the moving web.
  • a plurality of sections of the first and second elastic elements is arranged on the first web in generally parallel relation (Step 2222).
  • this plurality of elastic elements distributed longitudinally along the web and in mutual parallel relation provides an elasticized region in the web output and in each individual, finished elastic composite product, according to the present invention.
  • FIGS. 13-17 depict a system and system components, and illustrate a method of making an elastic composite according to another embodiment of the invention.
  • FIG. 18 provides a plan view of the inventive system 2301.
  • FIG. 19 provides a perspective, isometric view that reveals several of the components of the inventive system.
  • Directional arrows are provided throughout FIG. 19 to indicate the movement of conveyors, web of materials or elastic composites, the spinhead assembly, and the like.
  • a system provides and a method is implemented for making an elastic composite, whereby a continuous strand of elastic is applied onto a first and a second web along a direction generally transverse to a web plane moving direction.
  • the first and second input webs are conveyed along the web plane moving direction.
  • a plane may be extended from (and including) one web into (and including) the other web, and the two webs move along that plane in the same direction (i.e., parallel directional vectors, such as 90 degrees horizontally and vertically of the vertical plane XX).
  • the two moving webs are, therefore, generally coplanar about the locations or sections whereupon a ' section of the elastic strand is applied to both webs.
  • the section of elastic strands is applied generally "linearly" onto both the first and second webs.
  • this reference to the section of strand being applied “generally linearly” means that the applied section generally provides a linear segment that extends across the planes of both the first and second webs and includes a shorter linear segment on each of the first and second webs.
  • a system 2301 is provided to implement the inventive method and produce a web output Ol of inventive elastic composite and preferably a second web output O2.
  • a conveyor assembly 2309 is provided having a web platform U and preferably a second web platform L (for outputting second web output O2).
  • an upper web platform U is positioned above, and generally aligned with, a lower web platform L.
  • Each web platform U, L is referred to as having a pair of conveyors in the form of movable continuous belts.
  • a left continuous belt Ul of the upper platform U is spaced laterally from a second continuous belt U2.
  • Lower web platform L also has similarly positioned left continuous belt Ll and right continuous belt L2.
  • the continuous belts Ul and U2 are referred to as having, at any given point in time, an inside deck or surface S3, S4 that is moving toward the spinhead 2317 (in the web plane moving direction MM) and an outside deck or surface Sl, S2 that is moving away from the spinhead 2317 (in the web plane moving direction NN).
  • the outside surfaces S3, S4 are generally co-planar or at least corresponding sections of the surfaces S3, S4 are, such that sections of input webs supported on the corresponding sections are co-planar and positioned to receive a section of elastic strand that extends lineealry across the two webs.
  • continuous belts Ll, L2 have inside surfaces S7, S8, which are moving toward the spinhead 2317, and outside surfaces S5, S6, which are moving away from the spinhead.
  • the pair of inside surfaces for each web platform may be referred to as being generally disposed on the same imaginary, extended plane and the pair of outside surfaces may be referred to as being generally disposed on another imaginary, extended plane.
  • the two imaginary, extended planes are spaced vertically apart and generally disposed in parallel relation.
  • Sl and S2 are generally on the plane, as are S3 and S4, S7, and S8, and S5 and S6.
  • the pairs of continuous belts are, therefore, operable to convey a pair of input webs along a predetermined web plane path, first along a first web plane moving direction toward the spinhead and a second, reversed, web plane moving direction away from the spinhead. It is preferred, of course, to convey the pair of input webs at the same time.
  • An elastic applicator assembly 2307, including a spinhead 2317, in this embodiment, has a construction that is consistent with that previously described in respect to FIGS. 5-8.
  • a single input source El of a continuous elastic strand WW is provided and received by a motor operatively associated with the spinhead described before.
  • the spinhead 2317 includes arms as described previously, and a series of rollers and eyelets for routing and applying the continuous elastic strand WW about the conveyor assembly 2309 and about the generally vertical plane XX.
  • this exemplary system is provided with four independent sources of a primary input web of nonwoven: a first input web Wl arriving from an upper part of the system; a second input web W2 lower web arriving also from an upper part of the system; a third input web W3 generally below the first input web Wl ; and a fourth input web W4 generally below the second input web W2.
  • Each of the four primary input webs W1-W4 is preferably processed through a folding mechanism, as described previously.
  • the four input webs are then moved along a first web plane moving direction MM and in between the upper and lower web platforms Ul, LL Movement of the input webs is, of course, driven by the four continuous belts Ul, U2, Ll, L2.
  • the exemplary system is further provided with an upper secondary input web W5 of nonwoven positioned above the conveyor assembly 2309 for applying a base layer simultaneously to a pair of elasticated substrates as will be described below.
  • a lower secondary input web W6 is provided for applying a base layer, as will also be discussed below.
  • a pair of large rollers 2342, 2344 is positioned downstream of the conveyor assembly 2309. Each roller serves to output a web Ol or O2 of elastic composite from the system. For this exemplary system and process, that web output Ol , O2 will provide a dual-elasticized elastic composite 2322 according to the invention.
  • FIGS. 20A-20C provides a cross-sectional view through various points in the process and through sections of the system depicted in FIG. 23.
  • the cross- sectional view of FIG. 25 A is placed to highlight the two web platforms U, L, the four continuous belts Ul, U2, Ll, L2, and the four input webs W1-W4 conveyed thereon.
  • the four webs W1-W4 are conveyed in a direction coming out of the page and toward the spinhead (i.e., first web plane moving direction MM).
  • the ends of the input webs W1-W4 enter the spinhead 2317 in a folded configuration.
  • an elastic strand WW is applied continuously about the conveyor assembly 2309 and upon each of the four primary webs W1-W4 of nonwoven. Friction between the input webs Wl -W4 and the applied elastic strand WW helps draw the continuous strand WW from the spinhead 2317.
  • FIG. 2OC the cross-sectional view is moved further downstream in the process. Specifically, the cross-section is provided at a point in the process after application of the secondary web inputs W5, W6.
  • one secondary input web is used in conjunction with the two primary input webs to creat the elastic composite.
  • a secondary nonwoven is shown applied upon the substrate combination of elastic elements and adjacent pair of input webs (Wl and W2; W3 and W4).
  • the application of the secondary input web W5, W6 of nonwoven provides, therefore, an elastic composite.
  • FIG. 2OC also illustrates the use of central folded section Fl, F2 in each secondary input webs W5, W6.
  • the secondary input web W5, W6 is folded so as to later reveal a central dead zone between two elasticized regions of the elastic composite. This feature of the inventive elastic composite is discussed in further detail below.
  • FIG. 2OC also indicates the location of a knife mechanism KK downstream of the cross-section as discussed previously.
  • the knife mechanisms cut elastic strand WW, thereby severing elastic elements from the continuous strands.
  • the cuts also separates the process into an upper process and a lower process. More specifically, the cuts separates the upper, moving substrate consisting of input webs Wl, W2, secondary input web W5 and elastic elements therebetween, from a similarly constituted lower, moving substrate.
  • another pair of knife mechanisms KK' is positioned at locations downstream of the cross-sectional view and, above, and below, the centers of the web platforms U, L. The knife mechanisms KK' are located to purposefully coincide with the middle of the central folded sections Fl, F2.
  • FIG. 21 provides a cross-sectional view of a finished web output of the system and process. Two identical web outputs Ol, O2 of elastic composites are provided.
  • a first nonwoven layer is provided by the pair of primary input webs Wl 5 W2
  • a second nonwoven layer is provided by the single secondary input web W5
  • a pair of elasticized regions 2614 therebetween make up the finished elastic composite web.
  • the elasticized regions 2614 are provided by a distribution of elastic elements 2622 that are in generally parallel relation and extend laterally.
  • the elastic elements also provide, as a result, elasticity in the lateral direction and without a vertical component.
  • the two elasticized regions 2614 are laterally spaced from one another to provide a dead zone 2650 therebetween. As discussed above, the dead zone results from cutting the elastic strand WW or elastic element using the knife mechanisms KK' and the unfolding of the folded sections Fl, F2.
  • Dead zones are also provided between the side edges of the nonwovens and each of the elasticized regions.
  • the side dead zones result partly from the unfolding of the folded ends of the primary input webs Wl -W4. These unfolding steps may be performed immediately downstream of the two knife mechanisms in a manner previously described in this disclosure.
  • the width of the central non-elasticized region or dead zone 2650 may be controlled by controlling the lateral separation between the pairs of belts in each web platform (e.g., the space between Ul and U2 and the space between Ll and L2). It may also be controlled by specifying the width of the excess fold in the center of the secondary web. This fold is configured to retain some of the material away from the composite during the process and is typically opened up downstream to reveal the central non-elasticized region or dead zone.
  • the system 2301 and method are modified to produce four web outputs and four separate elastic composites, according to the present invention.
  • the knife mechanisms KK' may be modified to also sever the secondary input webs W5,W6 (in addition to the elastic strand WW). In this way, each of the two web substrates is divided to produce an independent elastic composite to the left and also to the right of the knife mechanisms KK'.
  • Each elastic composite has a single central elasticized region and two side dead zones.
  • the width of the folded sections Fl, F2 may be provided to correspond with the folded ends of the primary input webs.
  • four independent secondary input webs are used instead of two.
  • FIG. 22 provides a simplified flow chart of the basic steps of a method of making an elastic composite, in accordance with this embodiment of the present invention.
  • the flow chart 2700 also summarizes the process described above in respect to FIGS. 23-25.
  • the basic steps of the method are preferably performed through operation of a system such as the exemplary system 2301 in FIGS. 18 and 19.
  • initial steps 2710, 2714 a first web of material is conveyed along a web plane moving direction and a second web of material is conveyed along the web plane moving direction.
  • the web plane moving direction is predetermined by the web platforms of a conveyor assembly and the conveying steps 2710, 2714 are implemented through operation of the web platforms.
  • a section of a first continuous elastic strand is then applied generally linearly onto both the first and second webs along a direction generally transverse to the web plane moving direction (Step 2718).
  • the applying step 2718 is preferably performed through operation of a spinhead that spins the elastic strand about the first and second webs as these webs are conveyed along the web plane moving direction.
  • the applying step 2718 is performed while performing the conveying steps 2710, 2714 such that a plurality of sections of the first and second elastic elements are arranged on each of the first web and the second web in generally parallel relation.
  • the elastic elements are distributed longitudinally along the web and in mutual parallel relation, so as to provide, in the finished elastic composite, an elasticized region.
  • the first and second webs provide a top or base layer and the first and second arrangements of elastic elements provide the pair of elasticized regions.
  • FIGS. 23A-23C illustrates an elastic composite 2810 containing a pair of elasticized regions 2814 and three non-elasticized zones or dead zones, including a central dead zone 2850 extending longitudinally between the two elasticized regions 2814 and side dead zones 2816, 2818 on the other side of each elasticized region 2850.
  • the elastic composite 2810 may be referred to herein as a dual-elasticized elastic composite.
  • the elastic composite 2810 shown is formed from two discrete composite sections Cl, C2.
  • Each composite section Cl, C2 is manufactured independently as a discrete elastic composite having a single elasticized region. Any one of the three methods described herein may be employed to make the singly elasticized composite section.
  • two of the singly elasticized composite sections are joined together by overlapping one side edge of one composite section over a side edge of the other composite section.
  • a suitable adhesive or adhesive means may be used to maintain bonding at the overlap.
  • the overlap creates a multi-layer bonding portion B as shown in FIG. 28A, which also serves as a portion of the central dead zone.
  • the bonding portion B consists of atop nonwoven layer 2818 and a base layer 2820 of each composite section. Accordingly, the thickness of the bonding portion B and the central dead zone 2850 may be significantly, or at least observably, greater than the thickness of the rest of dual-elasticized elastic composite. For each composite section Cl, C2, the top nonwoven layer 2818 and the base nonwoven layer 2820 have the same width and the side edges are aligned.
  • FIG. 23B a second dual-elasticized elastic composite 2810' is shown again consisting of two adjoined singly elasticized, composite sections Cl ', C2'.
  • C2 For each composite section Cl', C2 ⁇ one of a top layer 2818' and a bottom layer 2820' is wider than the other.
  • the right composite section C2 has a bottom layer 2820' that extends laterally farther than the top layer 2818', thereby forming a step.
  • the top layer 2818' extends laterally farther than the bottom layer 2820% thereby forming a ledge.
  • a suitable construction joint is provided between the two composite sections Cl', C2'.
  • An overlapping bonding portion B' (and central dead zone 2850') is also provided that consists of a single top layer 2818' and a single base layer 2820' and is characterized by a thickness generally consistent with the other portions of the dual elasticized elastic composite 2810'.
  • a suitable adhesive or adhesive means may be employed to facilitate and maintain bonding between the layers of the bonding portion.
  • FIG. 23C illustrates an improved dual elasticized elastic composite 2810" that may be manufactured in accordance with the method described in respect to FIGS. 18-21, in accordance with the present invention.
  • the elastic composite also has two side dead zones 2816" and a central dead zone 2850" situated between the elasticized regions 2814".
  • the thickness of the dead zone 2850" is provided by a single top layer 2818" and a single base layer 2820" and is, therefore, consistent with the thickness of other portions of the dual elasticized elastic composite 2810".
  • the dual elasticized elastic composite 2810" provides a single composite structure.
  • the base layer 2820" of the elastic composite 2810" is provided by a seamless sheet of nonwoven (or other material).
  • the elastic composite 2810" does not require joining of two discrete elastic composite sections. Rather, a web of the dual elasticized elastic composite 2810" is generated linearly as output of the method described in respect to FIGS. 18-22.
  • a seamless composite structure, the dual elasticized composite 2810 eliminates the bonding region required of the elastic composites in FIGS. 23A and 23B and thus, avoids the potential for leakage generally associated with these bonding regions B, B'.
  • the seamless composite structure is also more structurally sound than the other composites and has a higher tensile strength (laterally and longitudinally).
  • the term "seamless composite structure” shall refer to a structure that does not have a seam at which two or more originally independent sections are joined as one to form the present structure.
  • the top layer 2818" of the elastic composite 2810 in FIG. 23C may provide a single seam S" along the central dead zone 2850" and thus, may not be referred to as “seamless.”
  • This seam S" of the top layers 2818" is not, however, a seam of the elastic composite 2810" as that seam S" does not extend through the thickness of the dead zone 2850" and the multi-layer composite 2810", and is not required to join two independent sections of the elastic composite 2810".
  • the dual elasticized elastic composite 2810" is generally easier to manufacture than the other composites in that it does not require the joining and bonding steps required described previously. It also does not require the machines or manpower to implement these steps. Furthermore, the seamlessness of the elastic composite 2810" is generally more aesthetically pleasing than the bonding regions B, B'. By eliminating or reducing the use of adhesives, the central dead zone of the present elastic composite is also generally cleaner. Further advantages and benefits of the dual elasticized composite according to the invention, or of the method of making same, will be apparent to one generally skilled in the art.

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  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biomedical Technology (AREA)
  • Heart & Thoracic Surgery (AREA)
  • Vascular Medicine (AREA)
  • Epidemiology (AREA)
  • Animal Behavior & Ethology (AREA)
  • General Health & Medical Sciences (AREA)
  • Public Health (AREA)
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  • Textile Engineering (AREA)
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  • Absorbent Articles And Supports Therefor (AREA)

Abstract

L'invention concerne, dans un aspect, un procédé de fabrication d'un composite élastique destiné à être incorporé dans un vêtement absorbant jetable, une structure textile ou de tissu et analogue. Le procédé comprend les étapes consistant à : transporter une première bande de matériau le long d'un premier trajet de déplacement plan de bande ; transporter une seconde bande de matériau le long d'un second trajet de déplacement plan de bande généralement parallèle à la première direction de déplacement plan de bande et appliquer un tronçon constitué d'une bande continue d'élément élastique sur à la fois la première bande et la seconde bande le long d'une direction généralement transversale par rapport aux trajets de déplacement plan de bande.
PCT/US2007/018576 2007-08-22 2007-08-22 Composite élastique, et système et procédé pour fabriquer le composite élastique WO2009025643A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CA2697023A CA2697023C (fr) 2007-08-22 2007-08-22 Composite elastique, et systeme et procede pour fabriquer le composite elastique
PCT/US2007/018576 WO2009025643A1 (fr) 2007-08-22 2007-08-22 Composite élastique, et système et procédé pour fabriquer le composite élastique
MX2010002055A MX337926B (es) 2007-08-22 2007-08-22 Material compuesto elastico y sistema y metodo para elaborar el material compuesto elastico.

Applications Claiming Priority (1)

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PCT/US2007/018576 WO2009025643A1 (fr) 2007-08-22 2007-08-22 Composite élastique, et système et procédé pour fabriquer le composite élastique

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3663331A (en) * 1969-10-08 1972-05-16 Erik Solbeck Method and apparatus for manufacturing net material and other non-woven fabrics
US5338382A (en) * 1992-08-10 1994-08-16 Ultrafab Inc. Fabrication of pile weatherstripping having fins
US20030089454A1 (en) * 2001-11-14 2003-05-15 The Procter & Gamble Company Method of manufacturing an elasticized composite material
US20040026011A1 (en) * 2000-04-17 2004-02-12 Edwards Mark Stephen Method and apparatus for making bristle subassemblies
US20050139311A1 (en) * 2003-12-24 2005-06-30 Dsg Technology Holdings Ltd Elastic composite for a disposable absorbent garment, and a system and process for making the elastic composite and a garment having the elastic composite

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3663331A (en) * 1969-10-08 1972-05-16 Erik Solbeck Method and apparatus for manufacturing net material and other non-woven fabrics
US5338382A (en) * 1992-08-10 1994-08-16 Ultrafab Inc. Fabrication of pile weatherstripping having fins
US20040026011A1 (en) * 2000-04-17 2004-02-12 Edwards Mark Stephen Method and apparatus for making bristle subassemblies
US20030089454A1 (en) * 2001-11-14 2003-05-15 The Procter & Gamble Company Method of manufacturing an elasticized composite material
US20050139311A1 (en) * 2003-12-24 2005-06-30 Dsg Technology Holdings Ltd Elastic composite for a disposable absorbent garment, and a system and process for making the elastic composite and a garment having the elastic composite

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CA2697023A1 (fr) 2009-02-26
CA2697023C (fr) 2014-07-08
MX2010002055A (es) 2010-03-25

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