飞机隐蔽区域的火灾点燃和蔓延:一种用于火焰蔓延调查的新型受限火灾装置(CFA)

IF 3 3区 农林科学 Q2 ECOLOGY Fire-Switzerland Pub Date : 2023-07-31 DOI:10.3390/fire6080292
V. Papadogianni, A. Romeos, A. Giannadakis, K. Perrakis, T. Panidis
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引用次数: 0

摘要

本研究调查了飞机受压段隐藏区域的潜在火灾隐患。目的是建立一种实验室规模的可燃性测试方法,以预测真实火灾条件下的火灾传播行为。设计和建造了一个密闭消防装置,并进行了几次测试,以更好地了解相关机制及其后果,并估计隐藏区域火灾中的火焰传播。介绍并讨论了涉及隐性火灾的典型材料,特别是天花板的实验装置和火焰传播结果。实验设施由一个狭窄的通道组成,在那里,使用燃烧器对暴露于受控热通量的样品点火。实验是在没有强制气流的情况下进行的。火焰蔓延是通过对火灾发展的视觉监测或样本中特定位置的温度测量来估计的。两种方法都产生了相似的结果。与施加的热通量相关的火焰传播速度,可用于估计传播q*sp,cr〃和点火q*ig,cr〃的临界热通量;相应的温度Ts、min和Tig;以及火焰蔓延参数Φ。
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Fire Ignition and Propagation in Hidden Zones of Aircrafts: A Novel Confined Fire Apparatus (CFA) for Flame Spreading Investigation
This research investigated potential fire hazards originating in hidden areas of pressurized sections of aircrafts. The objective was to establish a laboratory-scale flammability test method to predict the behavior of fire propagation under real fire conditions. A confined fire apparatus (CFA) was designed and constructed, and several tests were conducted to better understand the involved mechanisms and their consequences and to estimate flame spreading in hidden-zone fires. The experimental facility and flame-spreading results obtained for a typical material involved in hidden fires, specifically a ceiling panel, were presented and discussed. The experimental facility consisted of a narrow passage where a fire was initiated using a burner on a specimen exposed to a controlled heat flux. Experiments were conducted in the absence of forced airflow. Flame spreading was estimated through visual monitoring of fire development or temperature measurements at specific locations in the specimen. Both methods yielded similar results. The flame spread velocity in relation to the imposed heat flux allowed for the estimation of the critical heat flux for spreading q˙sp,cr″ and for ignition q˙ig,cr″; the corresponding temperatures, Ts,min and Tig; and the flame spread parameter Φ.
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来源期刊
Fire-Switzerland
Fire-Switzerland Multiple-
CiteScore
3.10
自引率
15.60%
发文量
182
审稿时长
11 weeks
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