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Opposed-Flow Flame Spread in a Narrow Channel Apparatus over Thin PMMA Sheets

机译:在薄PMMA板上的窄沟道设备中的相反流动火焰蔓延

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Flame spread tests have been conducted over polymethylmethacrylate (PMMA) samples in San Diego State University's Narrow Channel Apparatus (SDSU NCA). The Narrow Channel Apparatus (NCA) has the ability to suppress buoyant flow in horizontally spreading flames, and is currently being investigated as a possible replacement or complement to NASA's current material flammability test standard for non-metallic solids, NASA-STD-(I)-6001B Test 1. The buoyant suppression achieved with a NCA allows for tests to be conducted in a simulated microgravity atmosphere-a characteristic that Test 1 lacks since flames present in Test 1 are buoyantly driven. The SDSU NCA allows for flame spread tests to be conducted with varying opposed flow oxidizer velocities, oxygen percent by volume, and total pressure. Also, since the test sample is placed symmetrically between two confining plates so that there is a gap above and below the sample, this gap can be adjusted. This gap height adjustment allows for a compromise between heat loss from the flame to the confining boundaries and buoyancy suppression achieved by those boundaries. This article explores the effect gap height has on the flame spread rate for 75 μm thick PMMA at 1 atm pressure and 21% oxygen concentration by volume in the SDSU NCA. Flame spread results from the SDSU NCA for thin cellulose fuels have previously been compared to results from tests in actual microgravity at various test conditions with the same sample materials and were found to be in good agreement. This article also presents results from the SDSU NCA for PMMA at 1 atm pressure, opposed oxidizer velocity ranging from 3 to 35 cm/s, oxygen concentration by volume at 21%, 30%, and 50% and fuel thicknesses of 50 and 75 μm. These results are compared to results obtained in actual microgravity for PMMA obtained at the 4.5s drop tower of MGLAB in Gifu, Japan, and the 5.2s drop tower at NASA's Zero-Gravity Research Facility in Cleveland, OH. This comparison confirms that at 1 atm pressure, the SDSU NCA successfully simulates microgravity for not only thin cellulose fuels, but also for thin PMMA sheets as well. This further supports the idea that the NCA is a viable option to complement or replace NASA's Test 1 for material flammability testing. Tests with thick fuels will be conducted in the future to further characterize the SDSU NCA.
机译:火焰蔓延测试已经在聚进行(PMMA)在圣地亚哥州立大学的窄通道设备(SDSU NCA)的样品。窄通道装置(NCA)具有抑制在水平方向扩展的火焰浮力流的能力,以及目前正在研究作为一个可能的替代或补充,NASA的当前材料燃烧性试验标准为非金属固体,NASA-STD-(I) -6001B测试1.用NCA实现的浮力抑制允许在一个模拟失重气氛 - 这一试验1缺乏由于火焰存在于试验1被浮力驱动的特性进行测试。所述SDSU NCA允许被具有不同逆流氧化剂速度,氧%(体积),以及总压力下进行火焰蔓延试验。另外,由于试验样品在两个围板之间对称地放置,以便有上方和下方样本的间隙,该间隙可以被调整。该间隙的高度调节允许从火焰的热量损失到围边界和由这些边界达到浮力抑制之间的折衷。本文探讨效果间隙高度对火焰蔓延速度为75微米厚的聚甲基丙烯酸甲酯在1点大气压的压力和21%的氧浓度通过在SDSU NCA体积。从SDSU NCA火焰蔓延结果薄纤维素燃料先前已与在用相同的样品材料的各种试验条件,从测试的结果在实际的微重力和被认为是较好的一致性。本文还从SDSU NCA为PMMA呈现结果在1点大气压的压力,相对的氧化剂速度范围从3到35厘米/秒,氧浓度按体积计在21%,30%,和50和75微米50层%和燃料厚度。这些结果相比,PMMA在日本岐阜县的MGLAB的4.5S落塔获得实际的微重力获得的结果,以及5.2s在克利夫兰在NASA的零重力研究设施落塔,OH。这种比较证实,在1个大气压的压力,SDSU NCA成功模拟的微重力,不仅薄纤维素燃料,而且对于薄PMMA板为好。这进一步支持了国家版权局是一个可行的选择来补充或替换美国宇航局的试验1材料可燃性测试。厚厚的燃料测试将在未来进行进一步表征SDSU NCA。

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