BALLISTIC LAMINATE COMPRISING UNIDIRECTIONAL LAYERS JOINED TOGETHER
20220228840 · 2022-07-21
Inventors
Cpc classification
B32B7/09
PERFORMING OPERATIONS; TRANSPORTING
B32B2571/02
PERFORMING OPERATIONS; TRANSPORTING
F41H5/0478
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/265
PERFORMING OPERATIONS; TRANSPORTING
F41H5/0485
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B5/08
PERFORMING OPERATIONS; TRANSPORTING
B32B5/262
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/14
PERFORMING OPERATIONS; TRANSPORTING
B32B2270/00
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/718
PERFORMING OPERATIONS; TRANSPORTING
B32B5/073
PERFORMING OPERATIONS; TRANSPORTING
B32B3/266
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/028
PERFORMING OPERATIONS; TRANSPORTING
B32B2260/048
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/106
PERFORMING OPERATIONS; TRANSPORTING
B32B5/142
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/724
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
F41H5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B5/06
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present invention relates to a structure for producing ballistic protection which combines high levels of performance in terms of stopping bullets and reducing trauma with great flexibility and breathability. A ballistic laminate comprising joined together unidirectional layers is produced. The ballistic laminate provided by the present invention is preferably produced by superposing at least two layers of ballistic yarns 101 and 103, arranged unidirectionally according to directions inclined relative to one another by approximately 90° (+/−10°). Each layer comprises a plurality of fibres arranged unidirectionally according to a substantially mutually parallel direction (+/−10°).
Claims
1. Ballistic laminate for ballistic protection comprising at least one first unidirectional textile element and at least one second unidirectional textile element, the first textile element comprising a first plurality of ballistic fibers arranged substantially according to a first direction, the second textile element comprising a second plurality of ballistic fibers arranged substantially according to a second direction, the first and the second direction forming a relative angle of 90°+/−10°, the laminate being covered by a first protective layer external to the first unidirectional textile element and by a second protective layer external to the second unidirectional textile element, the laminate being characterized in that it comprises a plurality of through holes having a diameter comprised between 0.02 mm and 3 mm, the through holes passing through the first and second protective layer and the at least first and the at least second unidirectional textile element, wherein the density of the through holes is between 0.1 and 10 per cm.sup.2.
2. Ballistic laminate according to claim 1, in which the density of the through holes is between 0.5 and 10 per cm.sup.2.
3. Ballistic laminate according to claim 1 in which the ballistic fibers are made of one or more of the following materials: aramidic, polyamide, polyethylene with a very high molecular weight called UHMWPE, copoliaramidic, polybenzoxazole, polybenzothiazole, liquid crystals, carbon, glass.
4. Ballistic laminate according to claim 1 in which the first and second protective layer and the at least first and the at least second unidirectional textile element are joined together by pressing.
5. Ballistic laminate according to claim 4 in which the through holes are made after the pressing step.
6. Ballistic laminate according to claim 1 in which the first and second protective layers and the at least first and the at least second unidirectional textile element are joined together by sewing and at least a part of the through holes is made during the step of sewing.
7. Ballistic laminate as claimed in claim 6, wherein the seam is made by means of needles having a diameter at least 20% greater than the diameter of the yarn used for sewing.
8. Ballistic laminate as claimed in claim 5, wherein the through holes are made by means of a rotating device provided with a plurality of points adapted to create the holes during the rolling of the device on the laminate.
9. Ballistic laminate according to claim 1, in which the first and second protective layers comprise one or more of the following materials: polyurethane, polyester, polyamide, polyethylene, polypropylene, in the form of a film or other structure, such as nets, felts or woven/non-woven fabric.
10. Ballistic laminate according to claim 1, in which the weight of each textile element is between 10 g/m.sup.2 and 500 g/m.sup.2.
11. Process of manufacture of the ballistic laminate of claim 1, comprising the steps of: arranging at least one first unidirectional textile element and at least one second unidirectional textile element in contact with each other, the first textile element comprising a first plurality of ballistic fibers arranged substantially according to a first direction, the second textile element comprising a second plurality of ballistic fibers arranged substantially according to a second direction, the first and the second directions forming a relative angle of 90°+/−10°; joining the at least first textile element and the at least second textile element together by pressure; arranging a first external protective layer on the first unidirectional textile element and a second external protective layer on the second unidirectional textile element; joining the at least first and the at least second textile element and the first and second protective layer together with a pressure of between 1 and 200 bar; making a plurality of through holes with a diameter between 0.02 mm and 3 mm, in which the through holes pass through the first and second protective layers and the at least one and the at least second unidirectional textile element, the density of the through holes being between 0.5 and 10 per cm.sup.2.
12. Ballistic protection comprising at least one ballistic laminate layer of claim 1.
Description
BRIEF DESCRIPTION OF THE FIGURES
[0015] These and further advantages, objects and features of the present invention will become more apparent to a skilled person from the following description and appended drawings which relate to embodiments of an exemplary but not in any way limiting nature, in which:
[0016]
[0017]
[0018]
DETAILED DESCRIPTION
[0019] The ballistic laminate provided by the present invention is preferably produced by superposing at least two layers of ballistic yarns 101 and 103, arranged unidirectionally according to directions inclined relative to one another by approx. 90° (+/−10°). Each layer (in the example of
[0020] As an alternative to yarns, which are generally composed of numerous filaments, it is possible to use tapes or monofilaments. The linear densities of such yarns (tapes, monofilaments) are advantageously between 20 and 6500 dtex, tenacity values are greater than 10 g per dtex, modulus values are greater than 400 GPa and tensile elongation values are between 1% and 10%; these classes include, for example, aramid yarns produced by Teijin®, DuPont®, Kolon or Hyundai® respectively having the trade names Twaron®, Kevlar®, Heracron® or Alkex®.
[0021] In addition to aramid yarns, it is also possible to use ultra-high molecular weight polyethylene yarns produced by Honeywell® or DSM®, having the respective trade names Spectra® and Dyneema®, or also in the form of known tapes having the trade names Tensylon® or Endumax®. Copolyaramid yarns under the name Ruslan®, Rusar®, Autx manufactured by Kamenksvolokno® have recently been introduced. These yarns are characterised by dynamic tensile strength which is at least twice the static strength and so enable elevated ballistic performance. Such dynamic strength values are measured using a procedure developed by Purdue University in the USA, as for example described in the document: [0022] MECHANICAL PROPERTIES OF A265 SINGLE FIBER, Jaeyoung Lima and Weinong W Chena, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Ind. 47907-2045.
[0023] For the purposes of the present invention, as shown in
[0024] Films which are useful for this purpose are based on essentially thermoplastic polymers, such as for example polyethylene, polypropylene, polyester or polyamide polymers. Since the protection film does not contribute to the ballistic characteristics, it is appropriate for its thickness to be as thin as is possible and compatible with the desired protection. Typical thicknesses are between 6 microns and 20 microns. The resulting structure is subject to the action of pressure and temperature. Pressures are advantageously between 2 and 200 bar and more advantageously between 20 and 40 bar. Pressing temperatures are between 50° and 200° C. and more advantageously between 80° and 140° C. A pressing operation is optionally also carried out before deposition of the protective films. Application of the pressure/temperature combination proceeds in accordance with processes known to those skilled in the art and may proceed both continuously and discontinuously. The resulting laminate is subjected to a further process step which involves producing discontinuities through the entire structure of the laminate.
[0025]
[0026] Producing through-holes in the unidirectional laminate structure which pass through the entire structure brings about waviness and hence deflections (or discontinuities) in the rectilinear course of the ballistic threads, as shown in
[0027] In a preferred solution, the various layers of the laminate are stitched together and it is the stitching operation which creates the through-holes.
[0028] It is preferable for the diameter of the stitching thread to be less than 20% to 90% of the diameter of the through-hole created by the needle or hook which produces such stitching. Such stitching thread is selected on the basis of the structure and the weight of laminate which is to be produced. The linear density of the stitching thread is between 20 dtex and 300 dtex. Yarns based on organic polymers such as for example polyester, polyamides, polyethylene, polypropylene, or inorganic yarns such as for example basalt, carbon or glass are used. The type of stitching does not determine the performance of the laminate. In some cases when the diameter of the joining thread is very much smaller than the diameter of the hole/channel created and especially with certain types of joining, the thread is not locked in place and may thus be easily “undone”, so ceasing to perform its function. In this case, stitching is performed using a bicomponent monofilament, the external part of which is readily fusible, unlike the internal part which has a very much higher melting temperature and thus remains intact during the pressing step in the presence of heat. In a preferred embodiment, the needles (e.g. crochet) are supplied with non-ballistic threads which pass perpendicularly through all the layers of the laminate, so increasing cohesion between the various layers of the laminate once they have been appropriately knotted for example by a tricot or chain stitch.
[0029] The length of the joining stitch is advantageously between 1 and 20 mm and the distance between the various stitching threads in the lengthwise direction is advantageously between 1 and 20 mm.
[0030] Stitching may be performed using known, optionally appropriately modified, devices and machinery which are familiar to a person skilled in the art, such as for example quilting machines or multi-head stitching machines.
[0031] As stated, stitching of the structure is optional. The essential feature according to the present invention is the presence of the through-holes which, in the absence of the stitching operation, may be obtained by alternative methods. One of the alternative methods for producing the through-holes and the associated discontinuities in the rectilinear direction of the fibres involves subjecting the laminate to the action of a series of punches arranged on a rotating cylinder under appropriate load to exert the pressure necessary to perforate the laminate in such a manner as to cause said punches to penetrate through the entire thickness of the laminate.
[0032] It is also possible, in an optional embodiment of the present invention, for the two techniques to coexist, i.e. both stitching and punching (or another technique capable of producing the through-holes) are performed: in this case, some holes will have the stitching thread inside while others will not.
[0033] In order to elucidate the content of the present invention,
[0034] In a preferred embodiment, the number of layers in an individual laminate is 2 layers, but may also be greater, for example 2, 4, 6, 8 (preferably a multiple of 2). In a preferred embodiment, such layers are then covered with continuous films capable of providing the required abrasion resistance.
[0035] A ballistic protection produced with the laminate of the present invention may comprise a variable number of above-described laminated structures, preferably between a minimum of 1 and a maximum of 50.