Composite thermal protective system and method
一种体系、组合物的技术,应用在防火涂料、运输和包装、薄料处理等方向,能够解决防护体系防喷射火焰不是非常有效的、难以安装等问题
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Embodiment 1
[0035] Prepare an upper layer composition for ablation, which contains 35%-65wt% of flexible polymer resin (modified epoxy resin, especially epoxy polysulfide resin can be exemplified), 5%-30% of synthetic Air agent (such as polyol foaming agent, amine blowing agent and phosphate acid generator) and about 10% to about 40% refractory filler. An exemplary composition is a two-part modified epoxy resin having the nominal formula as described below:
[0036] Table 1
[0037] Wt%
[0038] Melamine 5
[0039] Ammonium polyphosphate 10
[0040] Pentaerythritol 5
[0041] Epoxy resin (bisphenol A) 25
[0042] Polysulfide and Amine Curing Agents 25
[0043] Fiberglass (chopped) 5
[0044] Ceramic particles 25
Embodiment 2
[0046] Prepare the lower layer active thermal protection composition, it contains 30%-70wt% polymer resin (exemplary modified epoxy resin, especially epoxy polysulfide resin) and 20-50wt% air forming agent (exemplary polyol foaming agents, amine blowing agents and phosphate acid generators). The compositions used in the tests described below are two-component epoxy-based heat-activated coatings that, when exposed to fire or thermal extremes, volatilize at a fixed temperature to exhibit a small amount of volume through the formation of an open-celled substrate Increases (greater than 2 times the starting volume), and absorbs and blocks heat to protect the substrate. Composition comprising polyol, 1,3,5-triazine-2,4,6-triamine, epoxy resin and polymer of bis(ethyleneoxy)methane, containing disulfide bonds and curable terminal Thiol groups (polysulfides).
[0047] An exemplary composition is a two-part modified epoxy resin having the nominal formula as described below:
[0048...
Embodiment 3
[0060] Test articles prepared according to Example 2 were exposed to jet flames according to the test procedure outlined in OTI 95634, 1996. The test showed that the composite structure provided about 60 minutes of protection under the test conditions.
[0061] Smaller scale tests have shown that the protection provided by the composite system is much greater than that provided by individual upper or lower layers of thickness equal to the total thickness of the composite. The following summarizes those test results:
[0062] table 3
[0063] Small-Scale Jet Flame Simulation
[0064] Temperature about 1100℃
[0065] Heat flux about 300kw / m 2
[0066] Coating composition: A = lower coat, B = upper coat
[0067] Test product coating composition Time to 400°C
[0068] flat
[0069] 6”×6”×1 / 4” 3mmA and 3mmB 44 minutes
[0070] 6”×6”×1 / 4” 6mmA 27 minutes
[0071] pipeline
[0072] Diameter - 4” 5mmB 10 minutes
[0073] Diameter - 4" 3mmA, 3mmB 26 minutes ...
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