按标准EN 45545中规定的危险等级对航空复合材料进行火灾风险评估

S. Szabo, I. Vajdová, E. Jenčová, D. Blasko, R. Rozenberg, B. Mikula
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引用次数: 0

摘要

如今,复合材料不仅在航空工业中经常被用作建筑材料。一般来说,复合材料是指技术材料。虽然它们在结构上是异质的,但它们被认为是同质的。复合材料是由至少两种化学上和物理上不同的材料组成的。本文论述了航空工业中常用的复合材料的耐火性能。可燃性测试是作为“模拟航空事故干预”项目的一部分进行的,其中测试了用于飞机结构和内饰的几种材料。本文以最大平均放热率(kW/m2)评价复合材料的耐火性能。所研究的样品既有有芯夹层结构,也有无芯夹层结构。对样品的两面(光滑和粗糙)进行可燃性测试。耐火测试是根据EN 45545进行的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fire Risk Assessment of Composite Materials in Aviation by Hazard Levels Characterized in Standard EN 45545
Nowadays, composite materials are often used as construction materials  not only in the aviation industry. In general, composite materials mean  technical material. Although, they are  heterogeneous in their  structure, they are  understood to be homogeneous. Composites are formed by a composition of at least two chemically and physically different materials. This  article deals with fire resistance of composite materials, regularly  used in aviation industry. The flammability tests were performed as a part of the project "Simulation of Intervention in Air Accidents," where several materials used in aircraft constructions and interiors were tested. The fire resistance of composite materials is evaluated in the article based on the Maximum Average Rate of Heat Emission (kW/m2). The investigated samples are both of core and core-free sandwich structures. The flammability test was performed on both sides of the sample (smooth and rough). The fire resistance test  was performed on the basis of EN 45545.
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