Composite sheet and cargo container comprising same

1. A non-rigid composite sheet comprising in order

(i) a first component having an areal density of from 88 to 678 gsm comprising a first woven fabric of continuous filament yarns, the yarns having a tenacity of at least 11 g/dtex and a first polymeric layer,

(ii) a second component having an areal density of from 30 to 237 gsm comprising a substrate and an inorganic refractory layer, and

(iii) a third component having an areal density of from 88 to 678 gsm comprising a second woven fabric of continuous filament yarns, the 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 refractory layer of the second component, wherein

(a) the yarns of the first and second fabrics comprise aromatic polyamide, aromatic copolyamide, glass fiber or carbon fiber,

(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, polyketone, polyimide, polysulfone, polyarlene sulfide, liquid crystal polymer, polycarbonate or an ionomer,

(c) the substrate of the second component is a nonwoven fibrous sheet comprising fibers wherein the fibers are glass, aramid, crystalline ceramic oxide, silicon nitride, silicon carbide, oxidized polyacrylonitrile, carbon, and combinations thereof, or a paper comprising from 40 to 70 weight percent of aramid fibers and from 30 to 60 weight percent of polymeric binder,

(d) the first polymeric layer blocks at least 95% of UV rays,

(e) the first and second fabrics individually have an areal weight of from 70-508 qsm,

(f) the inorganic refractory layer of (ii) comprises platelets, and

(g) the composite sheet is either a sidewall or a ceiling of a cargo container or both.

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 refractory layer comprises vermiculite.

9. The composite sheet of claim 1 wherein the refractory layer has a dry areal weight of from 15 to 50 gsm.

10. The composite sheet of claim 1 wherein the inorganic refractory layer has a moisture content of no greater than 10%.

11. The polymer of claim 1 wherein the ionomer is ethylenemethacrylic acid copolymer.