Composite sheet and cargo container comprising same
This invention is directed to a non-rigid composite sheet comprising in order (i) a first component having an areal weight of from 88 to 678 gsm comprising a first fabric of filamentary yarns having a tenacity of at least 11 g/dtex and a UV and weather impervious first polymeric layer. (ii) a second component having an areal weight of from 120 to 430 gsm comprising a flame resistant paper and (iii) a third component having an areal weight of from 88 to 678 gsm comprising a second fabric of filamentary yarns having a tenacity of at least 11 g/dtex and an impact and scratch resistant second polymeric layer, the second fabric of the third component being adjacent to the paper of the second component.
1. A non-rigid composite sheet comprising in order
(i) a first component having an areal weight of from 88 to 678 gsm comprising a first woven fabric having an areal weight of from 70 to 508 gsm, the fabric comprising continuous filament yarns having a tenacity of at least 11 g/dtex and a first polymeric layer
(ii) a second component having an areal weight of from 120 to 430 gsm comprising a paper positioned adjacent to the first fabric of the first component and the second fabric of the third component, the paper further comprising aramid fibers, a polymeric binder and mica, and
(iii) a third component having an areal weight of from 88 to 678 gsm comprising a second woven fabric having an areal weight of from 70 to 508 gsm, the fabric comprising continuous filament yarns having a tenacity of at least 11 g/dtex and a second polymeric layer, the second fabric of the third component being adjacent to the paper of the second component,
wherein
(a) the yarns of the first and second fabrics comprise aromatic polyamide, aromatic copolyamide, glass fiber or carbon fiber, and
(b) the polymer of the first polymeric layer of the first component and second polymeric layer of the third component is polyurethane, polyethylene, polypropylene, polyethylenenaphthalate, polyacrylonitrile, fluoropolymer, polyimide, polketone, polyimide, polysulfone, polyarylene sulfide, liquid crystal polymer, polycarbonate or an ionomer,
wherein the polymeric binder of the paper is present in an amount of from 45-60 weight percent based on the combined weight of aramid fiber plus binder present in the paper.
2. The composite sheet of claim 1 , wherein the composite has a break strength of at least 350 N/cm.
3. The composite sheet of claim 1 , wherein the composite sheet can withstand a flame temperature of 927° C. for 5 minutes without burn-through penetration when tested according to FAA test method 14 CFR 25.855 Appendix F Part III.
4. The composite sheet of claim 1 , wherein the composite sheet can withstand a flame temperature of 927° C. for 5 min without burn-through penetration and the temperature 101 mm away from the side of the sheet remote from the flame does not exceed 204° C. when tested according to FAA test method 14 CFR 25.855 Appendix F Part III.
5. The composite sheet of claim 1 , wherein the first fabric has an areal weight from 101 to 170 gsm.
6. The composite sheet of claim 1 , wherein the second fabric has an areal weight from 170 to 270 gsm.
7. The composite sheet of claim 1 , wherein the filamentary yarns of the first and/or second fabrics comprise have a linear density of from 333 to 2222 dtex.
8. The composite sheet of claim 1 wherein the paper has a dry areal weight of from 195 to 255 gsm.
9. The composite sheet of claim 1 wherein the paper has a moisture content of no greater than 10%.
10. The polymer of claim 1 wherein the ionomer is ethylenemethacrylicacid copolymer.
11. A cargo container comprising a frame assembly, a plurality of side walls, a ceiling and a floor wherein the sidewalls and ceiling comprise the non-rigid composite sheet of claim 1 .
12. A fire-resistant cover, separator, blanket or liner comprising the non-rigid composite sheet of claim 1 .