SPUNBOND NONWOVEN WEB FOR AN ACQUISITION/DISTRIBUTION LAYER

Abstract

A spunbond nonwoven web for an acquisition/distribution layer, the web comprising a first layer (1) of filaments, wherein the first layer (1) consists of continuous crimped bi-component filaments of an eccentric core/sheath structure, the filaments having a diameter in the range of 15 to 35 microns and exhibiting at least 3 crimps/cm, a second filament layer (2) arranged in direct contact on the first layer (1), wherein the second layer (2) of filaments comprises continuous crimped bi-component filaments of an eccentric core/sheath structure, the filaments having a diameter, which is smaller than the diameter of the filaments in the first layer (1) and which is in the range of to 20 microns and exhibiting at least 3 crimps/cm.

Claims

1-10. (canceled)

11. An acquisition/distribution layer comprising: a spunbond nonwoven web comprising: a first layer comprising continuous crimped bi-component filaments of an eccentric core/sheath structure, the filaments having a diameter in the range of 15 to 35 microns and exhibiting at least 3 crimps/cm, a second layer arranged in direct contact on the first layer, the second layer comprising continuous crimped bi-component filaments of an eccentric core/sheath structure, the filaments having a diameter, which is smaller than the diameter of the filaments in the first layer and which is in the range of 10 to 20 microns, and exhibiting at least 3 crimps/cm.

12. The acquisition/distribution layer of claim 11, wherein at least some of the filaments of the second layer are mutually thermally bonded via their sheath components and at least some of the filaments of the first and the second layer are mutually thermally bonded together via their sheath components.

13. The acquisition/distribution layer of claim 11, wherein the core of the filaments of at least one of the first layer or the second layer comprises polyethylene terephthalate (PET) or polylactic acid (PLA) or PET copolymer and extends over at least 50% of the filament cross section.

14. The acquisition/distribution layer of claim 11, wherein the sheath of at least one of the filaments of the first layer or of the second layer comprises polyethylene homopolymer or polyethylene copolymer or polypropylene copolymer.

15. The acquisition/distribution layer of claim 11, wherein the first layer has a lower bulk density than the second layer.

16. The acquisition/distribution layer of claim 15, wherein the first layer has a lower bulk density than the second layer by an amount of 5 to 80 kg/m.sup.3.

17. The acquisition/distribution layer of claim 15, wherein the first layer has a lower bulk density than the second layer by an amount of 40 to 60 kg/m.sup.3.

18. The acquisition/distribution layer of claim 11, wherein the degree of bonding at an outer surface of the second layer decreases continually through the nonwoven web in a direction towards an outer surface of the first layer.

19. The acquisition/distribution layer of claim 11, wherein at least one of the first layer or the second layer comprises continuous crimped bi-component filaments having a diameter of 20 to 30 microns, and comprises 5-15 crimps/cm.

20. The acquisition/distribution layer of claim 11, wherein the second layer is shrunken relative to an original size of the second layer after bonding of the first layer to the second layer.

21. The acquisition/distribution layer of claim 11, wherein a the first layer comprises wrinkles at its outer surface.

22. The acquisition/distribution layer of claim 21, wherein at least 30% of the wrinkles form with a machine direction an angle which is in the range of 5 and 20 .

23. Absorbent article comprising an acquisition/distribution layer according to claim 11, wherein the absorbent article further comprises: a liquid pervious topsheet; a liquid impervious backsheet joined to the topsheet; and an absorbent core positioned between the topsheet and the backsheet, wherein the acquisition/distribution layer is positioned between the topsheet and the absorbent core.

24. The absorbent article of claim 23, wherein the acquisition/distribution layer has a length and a width, the filaments of the first and second layers extend substantially along the length direction and have a length which is at least 120% of the length of the acquisition/distribution layer.

25. The absorbent article of claim 24, wherein the filaments of the first and second layers have a length which is at least 150% of the length of the acquisition/distribution layer.

26. The absorbent article of claim 24, wherein the filaments of the first and second layers have a length which is at least 180% of the length of the acquisition/distribution layer.

Description

FIGURES

[0038] FIG. 1: Material according to the invention: the web comprising at least a first layer of thicker crimped filaments and a second layer of thinner crimped filaments

[0039] FIG. 2: Material according to the invention: the wrinkles forming angles with machine direction

[0040] FIGS. 3-1 to 3-3: Examples of crimp counting on fibres in bonded fabric.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

EXAMPLE 1

eC/S PET/PE Homopolymer 70/30

[0041] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylenelene homopolymer (Aspun 6834 from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 16 m and with filament composition core/sheet are produced with filament speed 3000 m/min and subsequently collected on a conveyor belt continuously moving by speed 190 m/min. The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 130 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 35 gsm and the bulk density about 105 kg/m.sup.3.

EXAMPLE 2

eC/S PET/PE Homopolymer 70/30

[0042] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylenelene homopolymer (Aspun 6834from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 20 m and with filament composition core/sheet are produced with filament speed 2000 m/min and subsequently collected on a conveyor belt continuously moving by speed 190 m/min.The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 140 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 35 gsm and the bulk density about 56 kg/m.sup.3.

EXAMPLE 3

eC/S PET/PE Homopolymer 70/30

[0043] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylene homopolymer (Aspun 6834 from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 15 m and with filament composition core/sheet are produced with filament speed 3000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min .The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 140 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm, the bulk density is about 107 kg/m.sup.3.

EXAMPLE 4

eC/S PET/PE Homopolymer 70/30

[0044] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylene homopolymer (Aspun 6834 from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 21 m and with filament composition core/sheet are produced with filament speed 2000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min. The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 140 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm, the bulk density is about 60 kg/m.sup.3.

EXAMPLE 5

eC/S PET/PE Homopolymer 70/30

[0045] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylene homopolymer (Aspun 6834 from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 12 m and with filament composition core/sheet are produced with filament speed 5000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min. The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 140 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm, the bulk density is about 110 kg/m.sup.3.

EXAMPLE 6

eC/S PET/PE Homopolymer 70/30

[0046] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 70% by weight of a polyethylene terephthalate homopolymer (5520 from Invista), 30% by weight of polyethylene homopolymer (Aspun 6834 from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is between between 270-300 C. for PET and 230-235 C. for PE. Melt spun bicomponent filaments with diameter of 16 m and with filament composition core/sheet are produced with filament speed 3000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min .The cross section of the filament comprises a core, which consists of a polyethylene terephthalate homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section. Filaments are conveyed through continuous narrow flow of air with temperature 140 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm, the bulk density is about 115 kg/m.sup.3.

EXAMPLE 7

eC/S PLA/PE Homopolymer 50/50

[0047] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 50% by weight of a polylactic acid homopolymer (6302D from Nature Works), 50% by weight of polyethylene homopolymer (Aspun 6834from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is about 230 C. for PLA and about 230 C. for PE. Melt spun bicomponent filaments with diameter of 15 m and with filament composition core/sheet are produced with filament speed 3000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min. The cross section of the filament comprises a core, which consists of a polylactic acid homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section.

[0048] Filaments are conveyed through continuous narrow flow of air with temperature 107 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm and bulk density about 102 kg/m.sup.3.

EXAMPLE 8

eC/S PLA/PE Homopolymer 50/50

[0049] A spunbond type nonwoven web is produced via a continuous process using two beams. Each of the beams is fed a composition that consists essentially of about 50% by weight of a polylactic acid homopolymer (6302D from Nature Works), 50% by weight of polyethylene homopolymer (Aspun 6834from DOW). For both beams the temperature of polymeric composition measured after the extruder zone is about 230 C. for PLA and about 230 C. for PE . Melt spun bicomponent filaments with diameter of 20 m and with filament composition core/sheet are produced with filament speed 2000 m/min and subsequently collected on a conveyor belt continuously moving by speed 267 m/min. The cross section of the filament comprises a core, which consists of a polylactic acid homopolymer, and a sheath which surrounds the core and consists of a polyethylene homopolymer, the core being arranged eccentrically with respect to the outer surface of the sheath, i.e. the center of gravity of the core is offset from the center of gravity of the filament cross section.

[0050] Filaments are conveyed through continuous narrow flow of air with temperature 107 C. to enhance and/or set their crimp. The basis weight of the nonwoven layer thus formed is 25 gsm and bulk density about 55 kg/m.sup.3.

EXAMPLE 9

eC/S PET/PE Copolymer 70/30

[0051] Spunbond nonwoven textile has been produced in the same way as Example 3, except that polyethylene copolymer has been used in the sheath instead of polyethylene homopolymer.

EXAMPLE 10

eC/S PET/PE Copolymer 70/30

[0052] Spunbond nonwoven textile has been produced in the same way as Example 4, except that polyethylene copolymer has been used in the sheath instead of polyethylene homopolymer.

EXAMPLE 11

eC/S PET/PP Copolymer 70/30

[0053] Spunbond nonwoven textile has been produced in the same way as Example 3, except that polypropylene copolymer has been used in the sheath instead of polyethylene homopolymer.

EXAMPLE 12

eC/S PET/PP Copolymer 70/30

[0054] Spunbond nonwoven textile has been produced in the same way as Example 4, except that polypropylene copolymer has been used in the sheath instead of polyethylene homopolymer.

[0055] According to the invention the spubond nonwoven comprises two layers 1, 2 one arranged in direct contact on the other. Superimposing one layer on the other may be done in various ways.

[0056] According to one embodiment a layer 2 (e.g. Example 1) is directly deposited onto another layer 1 (e.g. Example 2) within an in-line production process and subsequently the composite is bonded or at least consolidated by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blows hot-air at the upper surface of the composite andif requiredconcurrently or subsequently at the lower surface of the composite. The sheath components of the filaments partially melt during the process, so that they bond the filaments together at the points where they contact each other.

[0057] According to another embodiment, at least one of the layers 1, 2, preferably both layers 1, 2 are at least partially pre-bonded to facilitate handling. Then, the pre-bonded layers 1, 2 are superimposed and consolidated by means of the above mentioned hot air bonding unit.

[0058] According to a preferred embodiment, a first layer 1 of crimped bi-component filaments having an eccentric core/sheath structure and a diameter of about 15 to 35 microns is provided and a second layer 2 of crimped bi-component filaments is deposited onto the first layer 1, the second layer filaments having an eccentric core/sheath structure, and a diameter lower than the filaments of the first layer 1 and in the range of about 10 to 20 microns. The second layer 2 has a density higher than the first layer 1. The composite is exposed to a hot air knife or hot air diffuser such that the hot air impacts the second filament layer 2, the temperature of the hot air impacting the second filament layer 2 being slightly above the melting point of the sheath component of the filaments of the second layer 2. As the hot air impacts the outer surface of the second filament layer 2 and then passes through the composite, the sheath component of the filaments get tacky or melt and the filaments are fused at the points of their cross-section. The whole composite is thermally bonded in such a manner that the farther from the outer surface of the second layer 2, the lower degree of bonding. Without intending to be bound by theory, it is believed that this is due to i) the decrease of temperature of the hot air as the air travels from the point of impact through the composite towards the outer surface of the first layer 1, and ii) higher surface to mass ratio of the filaments of the second filament layer 2, because of the ilaments having lower diameter than the filaments of the first filament layer 1.

[0059] Thus the resulting composite or laminate comprises the first layer 2 of coarser filaments having a lower density and the second layer 2 of finer filaments having a higher density, while the degree of bonding (and the number of bonding points) decreases from the outer surface of the second layer 2 towards the contact surface between the first layer 1 and the second layer 2 and therefrom towards the outer surface of the first layer 1. The total volume of voids within the nonwoven decreases significantly in the opposite direction.

[0060] According to the invention, the first layer 1 of crimped bi-component filaments has an eccentric core/sheath structure and a diameter of more than about 15 microns.

[0061] According to the invention, the first layer 1 of crimped bi-component filaments has an eccentric core/sheath structure and a diameter of less than about 35 microns, preferably less than about 30 microns, preferably less than about 28 microns, preferably less than about 26 microns, most preferably less than about 24 microns.

[0062] According to the invention, the second layer 2 of crimped bi-component filaments has an eccentric core/sheath structure and a diameter of more than about 10 microns, preferably more than about 11 microns, most preferably more than about 12 microns.

[0063] According to the invention, the second layer 2 of crimped bi-component filaments has an eccentric core/sheath structure and a diameter of less than about 20 microns, preferably less than about 18 microns, most preferably less than about 16 microns.

[0064] Preferably, the difference in fiber diameter between first layer 1 and the second layer 2 is more than 2 microns, preferably more than 3 microns, preferably more than 4 microns.

[0065] Preferably, the difference in fiber diameter between the first layer 1 and the second layer 2 is less than 20 microns, preferably less than 16 microns, preferably less than 13 microns, preferably less than 10 microns.

[0066] According to the invention, the first layer 1 consists of fibers showing at least 3 crimps/cm, preferably at least 4 crimps/cm, more preferably at least 5 crimps/cm, most preferably at least 6 crimps/cm.

[0067] Preferably, the first layer 1 consists of fibers showing max. 30 crimps/cm, preferably max. 25 crimps/cm, more preferably max 20 crimps/cm, most preferably max 15 crimps/cm. According to the invention, the second layer 2 consist of fibers showing at least 3 crimps/cm, preferably at least 4 crimps/cm, more preferably at least 5 crimps/cm, more preferably at least 6 crimps/cm, more preferably at least 8 crimps/cm, most preferably at least 10 crimps/cm.

[0068] Preferably, the second layer 2 consists of fibers showing max. 30 crimps/cm, preferably max. 25 crimps/cm, more preferably max. 20 crimps/cm, most preferably max. 15 crimps/cm. In another advantageous embodiment, the second layer 2 consists of fibers showing 5-15 crimps/cm and the first layer 1 consists of fibers showing 5-15 crimps/cm. In another embodiment it can be preferred, when the level of crimping in the first layer 1 is lower than the level of crimping in the second layer 2.

[0069] In another embodiment it can be preferred, when the level of crimping in the first and second layer 1, 2 is more or less the same. A person skilled in the art will know that due to various technological issues it can occur during the production process that some individual fibers are not crimped in the desired way. Not to be bound by theory, we expect to achieve an inventive product that behaves in the described way with at least 90% of the fibers crimped according to the description. Additionally, the second layer 2 of filaments may shrink due to the application of heat from the hot air knife or diffuser. The first layer 1, which has not shrunk or which has shrunken less than the second layer 2, becomes more lofty then. This is because the second layer 2 has been bonded to the first layer 1 by the heat, however, as the heat was not enough to initiate shrinking of the first layer 1, the first layer 1 wrinkled as the second layer 2 shrunk. The wrinkles 3 and their directions are neither strictly regularly distributed nor oriented, they form channels extending mostly about in the machine direction 5, but at least 30%, preferably at least 40% of the wrinkles 3 forms an angle 4 with the machine direction 5, the angle 4 being in the range of 5 to 20. The resulting nonwoven textile has a wrinkled first surface provided by the first layer 1 and a substantially even second surface provided by the second layer 2. This effect may also appear when both layers 1, 2 shrink, but with a different level of shrinkage for each of the layer.

[0070] When such a composite is used as an acquisition/distribution layer within an absorbent article, the wrinkles 3 and their varying direction at the surface of the ADL enhance the ability of the ADL to distribute liquid in various parts of the core of the absorbent article. According to the invention, the spunbond nonwoven layers 1, 2 comprise crimped fibers. The formation of such crimped fibers resulting from a significant difference in the properties of the individual subsections, commonly expressed using the so-called contractibility of individual subsections is well known in the industry. Fibers produced in this way are known under the name of chemically formed fibers. A person skilled in the art will appreciate that the term subsection contractibility describes primarily the volume during the transition from the liquid to the solid state, which is affected by the various properties of the polymers. A person skilled in the art will also appreciate that the difference in crystallinity can also be a crimping engine. The growth rate of crystals and the level of crystalinity can cause so-called secondary crimping when the fiber is in the solid state. Crimping can be also activated or supported by added energy (for. example heating, mechanical force, etc.). A person skilled in the art will appreciate that crimping theories are described in literature and the above mentioned cases are examples of possible principles.

[0071] According to the invention, the nonwoven can comprise bicomponent eccentric C/S fibers, wherein the core comprises polyesters including both artificial ones (as for example Polyethylene Terephthalate PET) and bio-based ones (such as for example Polylactic AcidPLA) or their copolymers. In some embodiments, it may be preferred to have the same core material in both the first and the second layer 1, 2. In other embodiments it may be preferred to combine the core materials in the final producte.g. to have PLA as a core material in the first layer 1 with thicker fibers and PET as a core material in the second layer 2 with thinner fibers. A person skilled in the art can appreciate that different core polymers can lead to different final properties of the layer surface (for example stiffness). The final product can be designed according to specific needs. According to the invention, the nonwoven can comprise bicomponent eccentric C/S fibers, where the sheath comprises polymers with a lower melt temperature than the core polymer. With advantage the polymers can be chosen from a group of polyolefins (e.g. polypropylenePP or polyethylenePE) or their copolymers (e.g. polypropylene copolymercoPP, polyethylene copolymercoPE). With advantage, polymers can also be chosen from a group of polyester copolymers (e.g. polyethylene teraphtalate copolymercoPET).

[0072] A person skilled in the art can also appreciate the advantage of the use of polymer blends from above mentioned groups or of adding suitable additives.

[0073] In some embodiments, it can be advantageous to have the same sheath material in both the first and the second layer 1, 2. In other embodiments it can be preferred to combine the sheath material in the final materiale.g. to have the PP sheath in the first layer and the coPP sheath in the second layer. The sheath material in the first and the second layer 1, 2 shall show very good mutual miscibility. A person skilled in the art will appreciate, for example, the different level of adhesion on the outer surface of the first and the second layer 1, 2 that can be used with advantage, for example, in its positioning in a hygiene absorbent product. According to the invention, the nonwoven can be with advantage used as a part of a hygiene disposable product, as a diaper, feminine care product, adult incontinence product, absorbent pad or other types of absorbent products, where an acquisition distribution function is desired. Modern absorbent products are constructed as multilayer structures, where the neighboring functional layers may with advantage be so perfectly adjacent to one another that they seem to associate. The nonwoven according to the invention shall be generally placed between the topsheet and the absorbent core. The topsheet can be designed, for example, from a single layer to create a multilayer soft bulky structure with pleasant touch characteristics. The absorbent core can be constructed in different ways, for example, from a fluffy core with a low amount of superabsorbent or no superabsorbent to a so called fluffless core with a high amount of superabsorbent. The absorbent core can be also covered in so-called corewrap. A person skilled in the art will appreciate that the nonwoven according to the invention can be used as an ADL functional layer or as a part of an ADL functional layer, being combined, for example, with some other layer according to the absorbent product designer's intention.

Specific Examples of Spunbond Nonwoven Web According to the Invention

EXAMPLE 13

[0074] Examples 1 and 2 were combined laminating Example 2 onto Example 1 to form a double layer nonwoven structure, wherein the layer consisting of Example 1 formed the second layer 2 and consisted of filaments having a diameter of about 16 microns and crimping degree about 13 crimps/cm and bulk density about 105 kg/m.sup.3 and the layer consisting of Example 2 formed the first layer 1 and consisted of filaments having a diameter of about 20 microns and crimping degree about 7 crimps/cm and bulk density about 56 kg/m.sup.3. Thus a composite is provided, having a total basis weight of 70 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer 2, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted 2.5 seconds in hot air dryerSize. 1/2600AB 4800 (FLEISSNER GmbH) with air circulation set on 90% and air exhaust set on 100%. During such bonding of the layers 1, 2, the hot air (e.g. from omega Fleissner dryer) impacts the outer surface of the second layer 2 and penetrates through the layers 1, 2 and the temperature of the air drops down gradually from the point of impact, such that the temperature of the air acting upon the first layer 1 is lower than the temperature of the air acting upon the second layer 2. Thus, an effect of different shrinkage of the two individual layers 1, 2 may be generated. The layer, which has shrunken less, can generate a channels-wrinkles like 3D structure and this positively improves bulkiness of the nonwoven web and also its liquid storage capacity and liquid distribution ability.

EXAMPLE 14

[0075] Examples 3 and 4 were combined laminating Example 4 onto Example 3 to form a double layer nonwoven structure, wherein the layer consisting of Example 3 formed the second layer 2 and consisted of filaments having a diameter of about 15 microns and crimping degree about 14 crimps/cm and bulk density about 107 kg/m.sup.3 and the layer consisting of Example 4 formed the first layer 1 and consisted of filaments having a diameter of about 21 microns and crimping degree about 8 crimps/cm and bulk density about 60 kg/m.sup.3. Thus a composite is provided, having a total basis weight of 50 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer 2, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted about 2 seconds in hot air dryerSize. 1/2600AB 4800 (FLEISSNER GmbH) with air circulation set on 90% and air exhaust set on 100%. Again, during such bonding of the layers 1, 2, the hot air (e.g. from omega Fleissner dryer) impacts the outer surface of the second layer 2 and penetrates through the layers 1, 2 and the temperature of the air drops down gradually from the point of impact, such that the temperature of the air acting upon the first layer 1 is lower than the temperature of the air acting upon the second layer 2. Thus, an effect of different shrinkage of the two individual layers 1, 2 may be generated. The layer, which has shrunken less, can generate a channels-wrinkles like 3D structure and this positively improves bulkiness of the nonwoven web and also its liquid storage capacity and liquid distribution ability.

EXAMPLE 15

[0076] Examples 5 and 6 were combined laminating Example 6 onto Example 5 to form a double layer nonwoven structure, wherein the layer consisting of Example 5 formed the second layer 2 and consisted of filaments having a diameter of about 12 microns and crimping degree about 4 crimps/cm and bulk density about 110 kg/m.sup.3 and the layer consisting of Example 6 formed the first layer 1 and consisted of filaments having a diameter of about 16 microns and crimping degree about 6 crimps/cm and bulk density about 115 kg/m.sup.3. Thus a composite is provided, having a total basis weight of 50 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer 2, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted 1.5 seconds.

EXAMPLE 16

[0077] Examples 7 and 8 were combined laminating Example 8 onto Example 7 to form a double layer nonwoven structure, wherein the layer consisting of Example 7 formed the second layer 2 and consisted of filaments having a diameter of about 15 microns and crimping degree about 13 crimps/cm and bulk density about 1021 g/m.sup.3 and the layer consisting of Example 8 formed the first layer 1 and consisted of filaments having a diameter of about 20 microns and crimping degree about 7 crimps/cm and bulk density about 551 g/m.sup.3. Thus a composite is provided, having a total basis weight of 50 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted 2.5 seconds in hot air dryerSize. 1/2600AB 4800 (FLEISSNER GmbH) with air circulation set on 90% and air exhaust set on 100%. Again, during such bonding of the layers, different shrinkage of the individual layers may be achieved, as described in respect of Example 13 and 14.

EXAMPLE 17

[0078] Examples 9 and 10 were combined laminating said Example 10 onto said Example 9 to form a double layer nonwoven structure, wherein the layer consisting of said Example 9 formed the second layer 2 and consisted of filaments having a diameter of about 15 microns and crimping degree about 12crimps/cm and bulk density about 108 kg/m.sup.3 and the layer consisting of said Example 10 formed the first layer 1 and consisted of filaments having a diameter of about 21 microns and crimping degree about 6 crimps/cm and bulk density about 59 kg/m.sup.3. Thus a composite is provided, having a total basis weight of 50 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer 2, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted 2 seconds in hot air dryerSize. 1/2600AB 4800 (FLEISSNER GmbH) with air circulation set on 90% and air exhaust set on 100%. Again, during such bonding of the layers, different shrinkage of the individual layers may be achieved, as described in respect of Example 13 and 14.

EXAMPLE 18

[0079] Examples 11 and 12 were combined laminating laminating said Example 12 onto said Example 11 to form a double layer nonwoven structure, wherein the layer consisting of said Example 11 formed the second layer 2 and consisted of filaments having a diameter of about 16 microns and crimping degree about 13 crimps/cm and bulk density about 106 kg/m.sup.3 and the layer consisting of said Example 12 formed the first layer 1 and consisted of filaments having a diameter of about 20 microns and crimping degree about 6 crimps/cm and bulk density about 58 kg/m.sup.3. Thus a composite is provided, having a total basis weight of 50 gsm and thickness of about 1 mm. The layers 1, 2 have been bonded together by leading the composite through a hot air bonding unit (hot-air knife or hot air diffuser), which blew hot-air at the outer surface of the second layer 2, the hot-air having a temperature of about 125-130 C. at impacting the second layer 2. The duration of impact and the velocity/pressure of the hot air were such that the sheaths of the filaments at the outer surface of the second layer 2 have been melted enough to provide strong bonding, while the filaments at the outer surface of the first layer 1 remained substantially unbonded. In this specific embodiment, the hot-air impact at a specific point lasted 2 seconds in hot air dryerSize. 1/2600AB 4800 (FLEISSNER GmbH) with air circulation set on 90% and air exhaust set on 100%. Again, during such bonding of the layers, different shrinkage of the individual layers may be achieved, as described in respect of Example 13 and 14.

Test Methods:

[0080] The Basis weight of a nonwoven web is measured according to the European standard test EN ISO 9073-1:1989 (conforms to WSP 130.1). There are 10 nonwoven web layers used for measurement, Example size 1010 cm2.

[0081] The Caliper or Thickness of the nonwoven material is measured according to the European standard test EN ISO 9073-2:1995 (conforms to WSP 120,6) with following modification: [0082] 1. the material shall be measured on an Example taken from production without being exposed to higher strength forces or spending more than a day under pressure (for. example on a product roll), otherwise before measurement the material has to lie freely on a surface for at least 24 hours. [0083] 2. the overall weight of upper arm of the machine including added weight is 130 g.

[0084] The degree of crimping is measured according to ASTM D-3937-82 with following modification: [0085] 1. as unit of measurement is used crimps/cm

[0086] Setting the degree of crimping in a bonded layer is an issue since single fibres are bonded to each other and it is not possible to remove one of them from the composition (without the danger of affecting the original crimp level) and to measure the crimp value and the fiber length. For the purpose of this invention, the following estimation may be used: [0087] 1) A picture of the assessed layer is provided in such a magnification that the fibers can be well seen [0088] 2) One single fiber is chosen and its path through the picture or at least part of the picture is marked [0089] 3) The length of the marked fiber in the picture is measured [0090] 4) The number of crimps in the measured length is counted [0091] In contrast to the measurement of individual fibers, it is not possible to place the fiber in such a way that all the crimps can be seen clearly and then counted in a repeating sequence. In a bonded structure, some parts can be masked in the z direction, some parts may be masked by other fibers; some parts may be masked by bonding. Each fiber turn shall be counted as half a crimp. Also, a change from sharp to blurry on one fiber shall be counted as half a crimpsee the examples at FIGS. 3-1 to 3-3, where the half-crimps 1A+1B form one crimp (the same applies to 2A+2B, and 3A+3B) [0092] 5) The number of crimps/cm is calculated
It needs to be kept in mind that the value is calculated from a 2D picture of a 3D object and that the length of the fiber in the z direction is not covered. The real length of the fiber would probably be higher. Also, the 2D picture can mask certain crimps on the fiber, especially in the vicinity of a bonding point. Nevertheless, it is expected that the described estimation can provide a relevant picture of fiber crimping.

[0093] The length of the filament to the length of the fabric ratio can be measured in two different ways: [0094] a) the length of the filaments is measured by stretching them out so that they extend along a line without exhibiting the crimps [0095] b) in a fabric bonded to a given level, it is not possible to use method a) to measure the length of the filaments, so that the following estimation may be used: [0096] a. A picture of the assessed layer is provided in such a magnification that the fibers can be well seen [0097] b. One single fiber is chosen and its path through the picture or at least through part of the picture is marked [0098] c. The length of fiber marked on the picture is measured [0099] d. The length of the fabric, where the fiber is marked is measured [0100] c) The length of the filament to the length of the fabric ratio (percentage) is calculated

[0101] The resilience of a nonwoven is measured according to the European standard test EN ISO 964-1 with following modification: [0102] 1. on the sample of a nonwoven is appplied preload force 1.06N. [0103] 2. on the sample of a nonwoven is appplied force 5 N with loading speed 5 mm/min. [0104] Resilience is than calculated by following equation:

[00001]$C\left[\%\right]=\frac{T_1\left[\mathrm{mm}\right]}{T_0\left[\mathrm{mm}\right]}.Math.100.Math.\%$ [0105] C=resilience [%] [0106] T.sub.1=distance between clamps under the load 5N [mm] [0107] T.sub.0=thickness (acc. EN ISO 9073-2:1995) [mm]

[0108] The Bulk density of the nonwoven material is calculated by following equation:

[00002]${}_b\left[\mathrm{kg}/m^3\right]=\frac{\mathrm{BW}\left[g/m^2\right]}{T\left[\mathrm{mm}\right]}$ [0109] .sub.b=bulk density [kg/m.sup.3] [0110] BW=basis weight (acc. EN ISO 9073-1.sup..1989) [g/m.sup.2] [0111] T=thickness (acc. EN ISO 9073-2:1995) [mm] The bulk density of one layer in a composite:

[0112] 1) The thickness of a single layer using the optical method from the cross section of a nonwoven is measured. The number of samples shall be at least 10 and the number shall be set so that the corrected sample standard deviation s shall be smaller than 30% of the average value (v is below 30%)

[0113] 2) The basis weight is measured [0114] a. The production value is taken [0115] b. To obtain an approximate value, it is possible to do the following: [0116] i. A sample of a known surface area is taken [0117] ii. The layers are carefully separated from each other, or the fibers from the layers are separated out, [0118] iii. The weight of the separated layers and the fibers from them are measured. [0119] iv. The basis weight is calculated from the known surface area and the weight of layer. [0120] v. The number of samples shall be at least 10 and the number shall be set so that the corrected sample standard deviation s shall be smaller than 20% of the average value (v is below 20%) [0121] The corrected sample standard deviation shall be calculated using following formula:

[00003]$a=\sqrt{\frac{1}{N-1}.Math.\underset{i=1}{\overset{N}{.Math.}}.Math.{\left(x_i-\stackrel{\_}{x}\right)}^2}..Math.v=\frac{s}{x}.Math.100.Math..Math.\left(\%\right)$ [0122] Where: [0123] Nnumber of samples [0124] xisingle measured value [0125] xaverage measured value