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Fire safety in space – Investigating flame spread interaction over wires

机译:太空火灾安全 - 研究火线在火线上的相互作用

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摘要

A new rig for microgravity experiments was used for the study flame spread of parallel polyethylene-coated wires in concurrent and opposed airflow. The parabolic flight experiments were conducted at small length- and time scales, i.e. typically over 10 cm long samples for up to 20 s. For the first time, the influence of neighboring spread on the mass burning rate was assessed in microgravity. The observations are contrasted with the influence characterized in normal gravity. The experimental results are expected to deliver meaningful guidelines for future, planned experiments at a larger scale.Arising from the current results, the issue of the potential interaction among spreading flames also needs to be carefully investigated as this interaction plays a major role in realistic fire scenarios, and therefore on the design of the strategies that would allow the control of such a fire. Once buoyancy has been removed, the characteristic length and time scales of the different modes of heat and mass transfer are modified. For this reason, interaction among spreading flames may be revealed in microgravity, while it would not at normal gravity, or vice versa. Furthermore, the interaction may lead to an enhanced spread rate when mutual preheating dominates or, conversely, a reduced spread rate when oxidizer flow vitiation is predominant.In more general terms, the current study supports both the SAFFIRE and the FLARE projects, which are large projects with international scientific teams. First, material samples will be tested in a series of flight experiments (SAFFIRE 1-3) conducted in Cygnus vehicles after they have undocked from the ISS. These experiments will allow the study of ignition and possible flame spread in real spacecraft conditions, i.e. over real length scale samples within real time scales. Second, concomitant research conducted within the FLARE project is dedicated to the assessment of new standard tests for materials that a spacecraft can be composed of. Finally, these tests aim to define the ambient conditions that will mitigate and potentially prohibit the flame spread in microgravity over the material studied.
机译:一种用于微重力实验的新装置用于研究平行和平行气流在平行和相反气流下的火焰蔓延。抛物线飞行实验是在较小的长度和时间尺度上进行的,即通常在10厘米长的样本上进行长达20 s的时间。首次以微重力评估了邻近扩散对质量燃烧速率的影响。观测结果与法向重力的影响形成对比。预期实验结果将为将来的大规模计划实验提供有意义的指导。从目前的结果来看,蔓延火焰之间潜在相互作用的问题也需要仔细研究,因为这种相互作用在现实火灾中起着重要作用场景,因此在策略设计上将可以控制此类火灾。一旦消除浮力,就可以改变不同的传热和传质模式的特征长度和时标。因此,火焰传播会在微重力中显示出来,而在正常重力下则不会,反之亦然。此外,当相互预热占主导时,这种相互作用可能导致扩散率提高,反之,当氧化剂流偏向占主导地位时,相互作用可能导致扩散率降低。与国际科学团队合作的项目。首先,将材料样品从ISS上卸下后,将在天鹅座飞行器中进行一系列飞行实验(SAFFIRE 1-3)。这些实验将允许研究在实际航天器条件下,即在实时范围内的真实长度范围内的样本中的点火和可能的火焰传播。其次,在FLARE项目中进行的伴随研究致力于评估可组成航天器的材料的新标准测试。最后,这些测试旨在确定可减轻并有可能阻止火焰在微重力中散布在所研究材料上的环境条件。

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