LAMINATE AND METHOD OF MAKING SAME
20170203539 ยท 2017-07-20
Inventors
- Sebastian Sommer (Troisdorf, DE)
- Michael Maas (Roesrath, DE)
- Claudio Cinquemani (Koeln, DE)
- Markus Jansen (Duesseldorf, DE)
- Nicolas Quick (Winterberg, DE)
Cpc classification
D01D5/088
TEXTILES; PAPER
B32B2262/12
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/08
PERFORMING OPERATIONS; TRANSPORTING
D04H5/06
TEXTILES; PAPER
B32B37/06
PERFORMING OPERATIONS; TRANSPORTING
B32B3/263
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/54
PERFORMING OPERATIONS; TRANSPORTING
B32B37/144
PERFORMING OPERATIONS; TRANSPORTING
D04H3/16
TEXTILES; PAPER
D04H1/4374
TEXTILES; PAPER
B32B2250/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/145
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/0284
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/14
PERFORMING OPERATIONS; TRANSPORTING
B32B37/14
PERFORMING OPERATIONS; TRANSPORTING
B32B37/06
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B38/00
PERFORMING OPERATIONS; TRANSPORTING
D04H5/06
TEXTILES; PAPER
D01D5/088
TEXTILES; PAPER
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A laminate is made by first making by melt-blowing or spunbonding of multicomponent, thermoplastic, and endless filaments a first nonwoven layer lying generally in a plane and having a predetermined shrinkage capacity or potential parallel to the plane and making of thermoplastic and endless filaments a second nonwoven layer also lying generally in a respective plane and having a shrinkage capacity or potential that is smaller than that of the first nonwoven layer. The two layers are directly juxtaposed flatly on each other, and the directly juxtaposed first and second layer are bonded together only at bonded regions while leaving an array of unbonded regions distributed over a surface of the two bonded-together nonwoven layers. Then only the first nonwoven layer is shrunk so that the second layer bunches in the unbonded regions and is there raised transverse to a plane of the bonded-together layers.
Claims
1. A method of making a laminate, the method comprising the steps of: making by melt-blowing or spunbonding of multicomponent, thermoplastic, and endless filaments a first nonwoven layer lying generally in a plane and having a predetermined shrinkage capacity or potential parallel to the plane; making of thermoplastic and endless filaments a second nonwoven layer also lying generally in a respective plane and having a shrinkage capacity or potential that is smaller than that of the first nonwoven layer; directly juxtaposing one of the first and second layers flatly on the other of the first and second layers; bonding the directly juxtaposed first and second layer together only at bonded regions while leaving an array of unbonded regions distributed over a surface of the two bonded-together nonwoven layers; and thereafter shrinking the first nonwoven layer so that the second layer bunches in the unbonded regions and is there raised transverse to a plane of the bonded-together layers.
2. The laminate-making method defined in claim 1, herein the different shrinkage capacities or potentials of the first and second nonwoven layers are set by using different raw materials for the filaments of the first and second nonwoven layers or by different method conditions during manufacture of the filaments for the first and second nonwoven layers or by different filament cross sections of the monofilaments of the first and second nonwoven layers or by different orientations of the monofilaments in the first and second nonwoven layers.
3. The laminate-making method defined in claim 1, wherein a shrinkage capacity of the first nonwoven layer in a machine direction is different from a shrinkage capacity in a crosswise direction and forms therewith a ratio of 1:1 to 3:1.
4. The laminate-making method defined in claim 1, wherein the first layer of nonwoven is made from bicomponent filaments having a core-sheath configuration.
5. The laminate-making method defined in claim 1, wherein the second nonwoven layer is made from bicomponent filaments having a core-sheath configuration or a side-to-side configuration.
6. The laminate-making method defined in claim 1, wherein the bonding of the two juxtaposed nonwoven layers is a thermal bonding during which filaments of the first nonwoven layer are fused to filaments of the second nonwoven layer.
7. The laminate-making method defined in claim 1, wherein the bonding of the two joined and juxtaposed nonwoven layers is done out with at least one calender.
8. The laminate-making method defined in claim 1, wherein the shrinking of the first nonwoven layer is effected thermally activated by exposure to a hot fluid or by contact with a hot surface.
9. The laminate-making method defined in claim 1, wherein making of the layers, bonding of the juxtaposed layers, and shrinking of the first nonwoven layer are carried out inline.
10. A laminate made according to the method of claim 1.
11. A laminate having at least two juxtaposed nonwoven layers made of monofilaments, in particular made from a thermoplastic synthetic resin, preferably made by a method according to any one of claims 1 to 9, wherein a first nonwoven layer is formed as a spunbond layer or as melt-blown layer of multicomponent filaments, in particular bicomponent filaments, a second nonwoven layer provided on the first nonwoven layer comprises multicomponent filaments, in particular bicomponent filaments and/or monocomponent filaments, the first nonwoven layer is designed to shrink because of thermal shrinkage in the direction of its plane and because of this shrinkage regions of the second nonwoven layer are displaced and/or raised transversely to, in particular at a right angle to a plane of the two joined and juxtaposed nonwoven layers.
12. The laminate defined in claim 11, wherein at least one synthetic component on an outer surface of the filaments of the first nonwoven layer corresponds to a synthetic component on the outer surface of the monofilaments of the second nonwoven layer, and a synthetic component on the outer surface of the monofilaments of the first nonwoven layer and the second nonwoven layer is a polyethylene or polypropylene.
13. The laminate defined in claim 11, wherein a melting point of a synthetic-resin component of the filaments of the first nonwoven layer is higher on an outer surface of the monofilaments of the first nonwoven layer than the temperature at which shrinkage of the first nonwoven layer can be activated, the monofilaments of the first nonwoven layer have a core-sheath configuration, and the melting point of the sheaths of these continuous monofilaments is higher than the temperature at which the shrinkage of the first nonwoven layer can be activated.
15. The laminate defined in claim 11, wherein the temperature at which the shrinkage of the first nonwoven layer can be activated is to at least 5 C., below a melting point of a synthetic component of two joined and juxtaposed nonwoven layers that melts at the lowest temperature or of the nonwoven layer laminate exposed to the shrink activation.
15. The laminate defined in claim 11, wherein an average minimum spacing between the two bonded regions of two joined and juxtaposed nonwoven layers is more than 1 mm.
16. The laminate defined in claim 11, wherein a thickness of two joined and juxtaposed nonwoven layers is less than 2 mm.
17. The laminate defined in claim 11, wherein a ratio of the maximum tensile strength of the laminate in a machine direction to the maximum tensile strength of the laminate crosswise to the machine direction amounts to 2.5:1 to 1.2:1.
18. The laminate defined in claim 11, wherein the laminate has at least three nonwoven layers including the first nonwoven layer with a higher shrinkage capacity or potential in the direction of its plane than the second and a third nonwoven layer or a first nonwoven layer has a lower shrinkage capacity or melting potential in the direction of its plane than the second and a third nonwoven layer.
19. The laminate defined in claim 11, wherein the laminate has two outer more strongly shrinking nonwoven layers as well as an average non-shrinking or less shrinking nonwoven layer therebetween.
20. The laminate defined in claim 11, wherein the laminate has two outer non-shrinking or less shrinking nonwoven layers and a middle more strongly shrinking nonwoven layer.
Description
BRIEF DESCRIPTION OF THE DRAWING
[0038] The above and other objects, features, and advantages will become more readily apparent from the following description, it being understood that any feature described with reference to one embodiment of the invention can be used where possible with any other embodiment and that reference numerals or letters not specifically mentioned with reference to one figure but identical to those of another refer to structure that is functionally if not structurally identical. In the accompanying drawing:
[0039]
[0040]
[0041]
[0042]
SPECIFIC DESCRIPTION OF THE INVENTION
[0043] As seen in
[0044] According to one highly recommended embodiment and in this embodiment, the laminate of the cooler 4 and the stretcher 6 and/or the assembly of the cooler 4, the intermediate passage 5 and the stretcher 6 is designed as a closed system. Except for the supply of cooling air in the cooler 4, there is no additional air supply from the outside into this closed assembly.
[0045] In the embodiment according to
[0046] The nonwoven layers 1 and 2 deposited on the deposition screen belt 9 illustrated in
[0047]
[0048]
[0049]