Composite sheet and cargo container comprising same

Patent metadata

Field	Value
Publication number	US-9302845-B2
Application number	US-201414160850-A
Country	US
Kind code	B2
Filing date	Jan 22, 2014
Priority date	Feb 5, 2013
Publication date	Apr 5, 2016
Grant date	Apr 5, 2016

Abstract

This invention is directed to a non-rigid composite sheet comprising in order a first component having an areal density of from 102 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, a second component having an areal density of from 10 to 170 gsm comprising a flame resistant inorganic refractory layer adjacent to at least one protective polymeric layers, and a third component having an areal density of from 102 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 refractory layer of the second component.

First claim

What is claimed is:

1. A non-rigid composite sheet comprising in order
(i) a first component having an areal density of from 102 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 40 to 170 gsm comprising an inorganic refractory layer adjacent to at least one polymeric layer, and
(iii) a third component having an areal density of from 102 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 polymer of the protective polymeric layer of the second component is a polyketone, polyimide, polysulfone, polyarylene sulfide, fluoropolymer, liquid crystal polymer or polycarbonate,
(d) the first polymeric layer of the first component blocks at least 95% of UV rays,
(e) the first and second fabrics individually have an areal weight of from 84-508 gsm,
(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 degrees C. for 5 minutes without burn-through penetration when tested according to FAA test method 14 CFR 25.855 Appx. F Part III.

4. The composite sheet of claim 1 , wherein the composite sheet can withstand a flame temperature of 927 degrees C. for 5 minutes 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 Appx. 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 refractory layer comprises vermiculite.

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

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

10. The polymer of claim 1 wherein the ionomer is ethylenemethacrylicacid copolymer.

11. The composite sheet of claim 1 wherein the protective polymeric layer of the second component is capable of withstanding a temperature of at least 200 degrees C. for at least 10 min.

12. The composite sheet of claim 1 wherein the second component further comprises an adhesive layer having an areal weight of from 2 to 40 gsm, the adhesive being capable of activation at a temperature of from 75 to 200 degrees C.

13. The composite sheet of claim 12 wherein the adhesive bond between the refractory layer and the protective polymeric layer is at least 43 N/m.

Assignees

• Du Pont

Inventors

• Kawka Dariusz Wlodzimierz
• Chang Karl K

Classifications

• B32B2307/3065

  Flame resistant or retardant, fire resistant or retardant · CPC title

• B32B27/32

  comprising polyolefins {(comprising vinyl (co)polymers or acrylic (co)polymers B32B27/30)} · CPC title

• B32B7/05

  the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection (using interposed adhesives or bonding materials applied in spaced arrangements B32B7/14) · CPC title

• B32B7/12

  using interposed adhesives or interposed materials with bonding properties · CPC title

• B32B27/286

  comprising polysulphones; polysulfides · CPC title