Ultra high molecular weight polyethylene multifilament yarn
Multifilament yarn containing n filaments are provided, wherein the filaments are obtained by spinning an ultra-high molecular weight polyethylene (UHMWPE), said yarn having a tenacity (Ten) as expressed in cN/dtex of Ten(cN/dtex)=f×n −0.05 ×dpf −0.15 , wherein Ten is at least 39 cN/dtex, n is at least 25, f is a factor of at least 58 and dpf is the dtex per filament.
1. A panel comprising a plurality of sheets, wherein each sheet comprises at least 2 monolayers, wherein each of the monolayers comprises unidirectionally aligned yarn spun from an ultra-high molecular weight polyethylene (UHMWPE), wherein the yarn has a tenacity (Ten) as expressed in cN/dtex according to Formula 1:
Ten(cN/dtex)= f×n −0.05 ×dpf −0.15 (Formula 1)
wherein Ten is at least 39 cN/dtex, n is at least 50, f is a factor of at least 62.0 and dpf is the dtex per filament.
2. The panel according to claim 1 , wherein each sheet comprises at least 4 monolayers.
3. The panel according to claim 1 , wherein each sheet comprises at most 8 monolayers.
4. The panel according to claim 1 , wherein the factor f is at least 64.0.
5. The panel according to claim 1 , wherein the factor f is at least 67.0.
6. The panel according to claim 1 , wherein the sheets and/or the monolayers comprise a matrix material in an amount of at most 25 mass %, based on the total weight of the panel.
7. The panel according to claim 1 , wherein the sheets and/or the monolayers comprise a matrix material in an amount of at least 5 mass %, based on the total weight of the panel.
8. The panel according to claim 1 , wherein each of the sheets comprises a stack of the monolayers and a pair of polymeric films which sandwich the stack of monolayer.
9. The panel according to claim 8 , wherein the polymeric films are polyethylene films.
10. The panel according to claim 9 , wherein the polymeric films are low density polyethylene (LDPE) films.
11. A rigid panel comprising:
a stack of sheets, wherein
each of the sheets comprises at least 2 monolayers, wherein
each of the monolayers comprises unidirectionally aligned yarn spun from an ultra-high molecular weight polyethylene (UHMWPE), wherein the yarn has a tenacity (Ten) as expressed in cN/dtex according to Formula 1:
Ten(cN/dtex)= f×n −0.05 ×dpf −0.15 (Formula 1)
wherein Ten is at least 39 cN/dtex, n is at least 50, f is a factor of at least 62 and dpf is the dtex per filament, and wherein
the rigid panel has (i) a flexural strength of at least 10 MPa as measured before impact and (ii) an Eabs (J/[kg/m 2 ]) of at least 170 against an AK47 FMJ MSC projectile as determined for an areal density of the panel of about 15.5 kg/m 2 .
12. A method of making the ridged panel according to claim 11 , wherein the method comprises compressing the stack of the sheets to a pressure of at least 50 bars and to a temperature below a melting temperature of the yarns.
13. A flexible panel comprising:
a stack of uncompressed sheets, wherein
each of the sheets comprises at least 2 monolayers, wherein
each of the monolayers comprises unidirectionally aligned yarn spun from an ultra-high molecular weight polyethylene (UHMWPE), wherein the yarn has a tenacity (Ten) as expressed in cN/dtex according to Formula 1:
Ten(cN/dtex)= f×n −0.05 ×dpf −0.15 (Formula 1)
wherein Ten is at least 39 cN/dtex, n is at least 50, f is a factor of at least 62 and dpf is the dtex per filament.
14. The flexible panel according to claim 13 , wherein the sheets are stitched or glued together.
15. The flexible panel according to claim 14 , wherein the sheets are spot-glued together.
16. The flexible panel according to claim 13 , which comprises a bag containing the stack of sheets for holding the stack of sheets together.
17. The flexible panel according to claim 13 , wherein the flexible panel has an Eabs (J/[kg/m 2 ]) of at least 370 against a 0.357 Magnum JSP projectile as determined for an areal density of the panel of about 3.1 Kg/m 2 .
18. The flexible panel according to claim 13 , wherein the flexible panel has an Eabs (J/[kg/m 2 ]) against an 9 mm FMJ Parabellum projectile of at least 220 as determined for a flexible panel having an areal density of about 3.1 Kg/m 2 .
19. The flexible panel according to claim 13 , wherein the flexible panel has an Eabs (J/[kg/m 2 ]) against a 17 grain FSP projectile of at least 35 as determined for an areal density of the panel of about 3.1 Kg/m 2 .