METHOD OF MAKING A NONWOVEN LAMINATE
20200307146 ยท 2020-10-01
Inventors
Cpc classification
B32B37/0076
PERFORMING OPERATIONS; TRANSPORTING
B32B37/156
PERFORMING OPERATIONS; TRANSPORTING
B32B2305/20
PERFORMING OPERATIONS; TRANSPORTING
D04H3/16
TEXTILES; PAPER
B32B2250/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/242
PERFORMING OPERATIONS; TRANSPORTING
D04H3/14
TEXTILES; PAPER
D01D5/22
TEXTILES; PAPER
B32B37/06
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/00
PERFORMING OPERATIONS; TRANSPORTING
B32B37/06
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A nonwoven laminate having at least two nonwoven layers is made by first spinning, cooling, and stretching, first crimped multicomponent filaments to form a first nonwoven web that is deposited on a deposition device. Then second continuous continuous filaments including an elastomer based on polypropylene are spun, cooled, and stretched to form a second nonwoven web that is deposited on the first nonwoven web and thereby forming the nonwoven laminate that it then consolidated.
Claims
1. A method of making a nonwoven laminate having at least two nonwoven layers, the method comprising the steps of: spinning, cooling, and stretching first crimped multicomponent filaments to form a first nonwoven web; depositing the first nonwoven web on a deposition device; and spinning, cooling, and stretching, second continuous filaments including an elastomer based on polypropylene to form a second nonwoven web; and depositing the second nonwoven web on the first nonwoven web and thereby forming the nonwoven laminate.
2. The method according to claim 1, wherein the second filaments are monocomponent filaments.
3. The method according to claim 1, further comprising the step of: spinning, cooling, stretching, third crimped multicomponent filaments to form a third nonwoven web; and depositing the third nonwoven web on the second nonwoven web, whereby the laminate has three layers.
4. The method according to claim 3, further comprising the step of: spinning, cooling, and stretching, second such second continuous filaments including an elastomer based on polypropylene to form a second such second nonwoven web; and depositing both of the second nonwoven webs atop the first nonwoven web such that the third nonwoven web can be deposited atop them.
5. The method according to claim 3, wherein the crimped filaments of the first spunbonded web or the third spunbonded web are formed as crimped filaments with side-by-side configuration or with a core-sleeve configuration.
6. The method according to claim 3, wherein the crimped filaments of the first spunbonded web or the third spunbonded web have at least one component based on polypropylene.
7. The method according to claim 3, wherein the crimped filaments of the first spunbonded web or the third spunbonded web have two components on polypropylene that differ in their melt-flow rate such the melt-flow rate of one component is preferably at least 1.2 times greater than the melt-flow rate of the other component.
8. The method according to claim 3, wherein the crimped filaments of the first spunbonded web or the third spunbonded web have a degree of crimp of more than 2.5 loops per cm of their length.
9. The method according to claim 2, wherein the continuous filaments of the second spunbonded woven web consist substantially of a copolymer of propylene and ethylene having a melting point between 50 C. and 170.
10. The method according to claim 1, wherein the polypropylene of the elastomer of the second filaments of the second spunbonded web has a mesopentad fraction of more than 70%.
11. The method according to claim 1, wherein the continuous second filaments of the second spunbonded web are manufactured with a titer of 10 m to 50 m.
12. The method according to claim 1, further comprising the step of: calendering the laminate formed by the first spunbonded web and the second spunbonded web with a pressing surface portion or welding surface portion of the calender of 8% to 15%.
13. The method according to claim 12, wherein the calendering is effected by a calender with a figure density of 10 to 50 figures/cm.sup.2.
14. The method according to claim 12, wherein the calendering is effected by a calender whose surface temperature is 60 C. to 90 C.
15. The method according to claim 1, further comprising the step of: stretching the laminate in a machine direction.
16. A nonwoven laminate comprising: a first spunbonded nonwoven web formed by crimped multicomponent filaments having a degree of crimp of more than 2.5 loops per cm of their length; and a second spunbonded nonwoven web formed by continuous filaments having an elastomer based on polypropylene with a mesopentad fraction of more than 70%.
17. The laminate according to claim 16, further comprising: a third spunbonded nonwoven web formed by crimped multicomponent filaments or crimped bicomponent filaments in turn having a degree of crimp of more than 2.5 loops per cm of their length, the second spunbonded nonwoven layer being between the first and second webs.
18. The laminate according to claim 17, wherein a titer of the continuous filaments of the first spunbonded web or the third spunbonded web is 1.0 to 2.0.
Description
BRIEF DESCRIPTION OF THE DRAWING
[0047] The above and other objects, features, and advantages will become more readily apparent from the following description, reference being made to the accompanying drawing in which:
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SPECIFIC DESCRIPTION OF THE INVENTION
[0057] As seen in
[0058] According to the invention, a diffuser 17 is downstream of the stretcher 14 in the flow direction F. Expediently, the continuous filaments 5 are deposited downstream of the diffuser 17 on a deposition device designed as a moving screen belt 7 for the spunbonded layers 2, 3, 4. Preferably, air inlet gaps 18 are formed between the stretcher 14 or the stretching passage 16 and the diffuser 17, through which air inlet gaps 18 air or secondary air is introduced into the diffuser 17.
[0059] According to a preferred embodiment, the deposition device of the spinning system S is designed as an air-permeable sieve belt 7. Preferably, suction air is drawn downward through the moving screen belt 7 from the underside of the moving screen belt 7 facing away from the spunbonded layer 2. For this purpose, at least one aspirator or suction device 19 is below the moving screen belt 7. The spunbonded layer 2 is preferably preconsolidated after it has been deposited, preferably by a preconsolidation calender 20 having two preconsolidation rolls 21. The spunbonded layer 2 is then conveyed further in the machine direction MD with the aid of the moving screen belt 7.
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[0061] In the machine direction MD, the first left-hand spinning system S.1 is followed by a middle spinning system S.2 that advantageously produces continuous filaments in the form of monocomponent filaments 5.2 that are deposited as the second spunbonded layer 3. According to the invention, these monocomponent filaments 5.2 of the second spunbonded nonwoven have an elastomer based on polypropylene. The monocomponent filaments 5.2 expediently consist of this elastomer or substantially of this elastomer. It is preferably an elastomer in the form of a copolymer of propylene and ethylene. It is recommended that this copolymer have a melting point between 50 C. and 160 C. The monocomponent filaments 5.2 are expediently uncrimped continuous filaments 5. A particularly preferred embodiment of the invention is characterized in that the polypropylene of the elastomer or the copolymer of the monocomponent filaments 5.2 has a mesopentad fraction (mmmm) of more than 90%. The monocomponent filaments 5.2 of the second spunbonded layer 3 preferably and, in this embodiment, have a titer of 25 m to 40 m. It is within the scope of the invention that the second spunbonded layer 3 is not preconsolidated. The partial laminate from the first spunbonded fabric layer 2 and the second spunbonded fabric layer 3 disposed thereon is then conveyed further in the embodiment with the moving screen belt 7 in the machine direction MD and specifically to the third spinning system S to the right in
[0062] The third spinning system S.3 preferably makes continuous filaments 5 in the form of bicomponent filaments 5.3 and deposits them as a third spunbonded layer 4 on the second spunbonded layer 3 of the partial laminate. The bicomponent filaments 5.3 are preferably identical to the filaments 5.1, that is they are crimped bicomponent filaments 5.2 preferably having a degree of crimp of more than 2.5 loops per cm of their length, in particular of more than 3 loops per cm of their length. Preferably, the bicomponent filaments 5.3 have a side-by-side configuration and the two components of the bicomponent filaments 5.3 expediently consist of polypropylene, in particular homopolypropylene or substantially polypropylene, in particular substantially homopolypropylene. The two components of the bicomponent filaments 5.3 of the third spunbonded layer 4 expediently differ in their melt-flow rate (MFR). The melt-flow rate of one component is preferably at least 1.2 times, in particular at least 1.3 times greater than the melt-flow rate of the other component. After being deposited, the third spunbonded layer 4 is preferably s preconsolidated by a preconsolidation calender 20.3 with preconsolidation rolls 21. A middle consolidator 20.2 is shown, but with its rollers separated since it is not in use, being optional.
[0063] According to a particularly preferred embodiment, the laminate 1 comprising the first spunbonded layer 2, the second spunbonded layer 3 and the third spunbonded layer 4 is then calendered or finally consolidated by a calender 8 with rollers 9. The calender preferably and, in this embodiment, has a press area proportion of 8% to 15%. It is recommended that the laminate be calendered by a calender 8 with a figure density of 15 to 30 figures/cm.sup.2. It has been proven that the surface temperature of at least one calender roll 9 of the calender 8 is 65 C. to 85 C. Following the calendering or final consolidation, the nonwoven laminate 1 is stretched according to a particularly preferred embodiment by a stretcher 22. According to one embodiment, the stretching by the stretcher 22 can take place immediately (inline) downstream of where the nonwoven laminate 1 is formed. However, it is also within the scope of the invention that the nonwoven laminate 1 is stretch (offline) in particular at a different location or in a different system. For this purpose, the nonwoven laminate 1 is expediently wound up after it has been made and later stretched in particular at another location with at least one stretcher 22.
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[0065] The stretcher 22 shown in
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Embodiment
[0069] The invention is explained in more detail below with reference to an embodiment. According to a preferred embodiment, a nonwoven laminate 1 according to the invention has a first spunbonded layer 2, a second spunbonded layer 3 thereon and a third spunbonded layer 4 again thereon. The first and third spunbonded layers 2, 4 thus form outer layers or high-loft outer layers for the second spunbonded layer 3 as an elastic core layer. Appropriately, the continuous filaments 5 of the first spunbonded layer 2 and the third spunbonded layer 4 consist of bicomponent filaments 5.1, 5.3 with a side-by-side arrangement, and the continuous filaments 5 of the second spunbonded layer 3 preferably consist consist of monocomponent filaments 5.2. The bicomponent filaments 5.1 and 5.3 of the first spunbonded layer 2 and the third spunbonded layer 4 are crimped. As recommended, both the bicomponent filaments 5.1 of the first spunbonded layer 2 and the bicomponent filaments 5.3 of the third spunbonded layer 4 have a degree of crimp of more than 3 loops per cm of length.
[0070] As recommended, both the first component of the bicomponent filaments 5.1 of the first spunbonded layer 2 and the first component of the bicomponent filaments 5.3 of the third spunbonded layer 4 essentially consist of a homopolypropylene, preferably at least 95% by weight of this homopolypropylene. According to a particularly preferred embodiment variant, the first component of the bicomponent filaments 5.1 and 5.3 has 97 to 99% by weight of a homopolypropylene and 1 to 3% by weight of a lubricant, preferably a fatty-acid amide and particularly preferably 2% eurucic-acid amide. It is recommended that the melt-flow rate (MFR) of the first component of the bicomponent filaments 5.1 and the bicomponent filaments 5.3 is between 28 g/10 min and 42 g/10 min and preferably between 30 g/10 min and 40 g/10 min. Advantageously, the second component of the bicomponent filaments 5.1 of the first spunbonded layer 2 and the bicomponent filaments 5.3 of the third spunbonded layer 4 consists of a mixture of homopolypropylenes or substantially a mixture of homopolypropylenes. One homopolypropylene of this mixture preferably has a higher melt-flow rate (MFR) than the second homopolypropylene of this mixture. The mass ratio of the two homopolypropylenes in the mixture of the second component of the bicomponent filaments 5.1 and 5.3 is preferably 60:40 to 70:30, with the homopolypropylene with the higher mass proportion also preferably having the higher melt-flow rate (MFR). The second component of the bicomponent filaments 5.1 and the bicomponent filaments 5.3 expediently contains at least one additive, preferably in the form of a lubricant. Preferably 1% to 3% by weight of this additive or lubricant is present in the second component. The lubricant is preferably a fatty-acid amide and in particular an eurucic-acid amide. The mass ratio of the first component to the second component of the bicomponent filaments 5.1 and the bicomponent filaments 5.3 is preferably 60:40 to 80:20, preferably 65:35 to 75:25 and for example 70:30.
[0071] The monocomponent filaments 5.2 of the second spunbonded layer 3 expediently consist of a polypropylene-based elastomer. It is recommended that a copolymer of propylene and ethylene is used for the monocomponent filaments 5.2 of the second spunbonded layer 3, the propylene content preferably being more than 70% by weight and preferably more than 80% by weight. The elastomer of the monocomponent filaments 5.2 is particularly preferably a low-crystalline isotactic copolymer with a propylene or polypropylene component, the polypropylene having a mesopentad fraction (mmmm) of more than 90%.
[0072] Table 1 below shows parameters for a particularly preferred embodiment for making a nonwoven laminate 1 according to the invention. The nonwoven laminate 1 consists of three spunbonded layers 2, 3, 4. The bicomponent filaments 5.1 and 5.3 of the first spunbonded layer 2 and the third spunbonded layer 4 each have a first component in the form of a homopolypropylene 1. This first component can expediently have 2% by weight of eurucic-acid amide added as a lubricant. According to a preferred embodiment of the invention, the homopolypropylene 1 has a melt-flow rate of 36 g/10 min. The second component X2 of the bicomponent filaments 5.1 and the bicomponent filaments 5.3 of the first spunbonded layer 2 and the third spunbonded layer 4 consists of a mixture of the homopolypropylene 1 and a homopolypropylene 2. A component of the mixture therefore corresponds to homopolypropylene 1 of the first component X1. The mass ratio of homopolypropylene 1 to homopolypropylene 2 in the mixture may be 65:35. A lubricant in the form of eurucic-acid amide, for example in an amount of 2% by weight, can be added to the second component. The homopolypropylene 2 expediently has a melt-flow rate of 13 g/min. The mass ratio of the first component X1 to the second component X2 of the bicomponent filaments 5.1 and the bicomponent filaments 5.3 of the first spunbonded layer 2 and the third spunbonded layer 4 is 70:30. Monocomponent filaments made of an elastomer in the form of a copolymer of propylene and ethylene are used for the second spunbonded nonwoven layer 3. The proportion of propylene is expediently more than 80% by weight. The mesopentad fraction (mmmm) of polypropylene is more than 90%. In the last two columns of Table 1, particularly preferred values for the throughput in the spinneret 6 of the respective spinning system S are given, as well as the preferred cabin pressure in the respective spinning system S.
TABLE-US-00001 TABLE 1 Mass Throughput Cabin Spunbond ratio [g/hole/ Pressure layer 1st Component 2d Component X1/x2 min} Pa First Homopolypropylene 1 Homopolypropylene 1 + 70:30 0.32 3800 Homopolypropylene 2 Second Elastomer 0.75 2800 Third Homopolypropylene 1 Homopolypropylene 1 + 70:30 0.32 3800 Homopolypropylene 2