Flammability of Aircraft Structure Materials

S. Szabo, I. Vajdová, E. Jenčová, B. Mikula, D. Blasko, A. Tobisová, Lucia Balejčíková
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Abstract

This study deals with airplane construction material flammability and is focused on aircraft with MTOW of 2500 kg or less. All combustibility tests were examined by a conic calorimeter that matching with a norm of ISO 5660-1: 2002. By individual testing of all exterior building and interior furnishing materials, an airplane is made of; we achieve results as the basis for further composing of safety recommendations for fire and rescue services while assisting at air disasters. Also, the study very briefly deals with fundamental sources for fire-resistant materials used in the aviation industry and their testing as well. Besides this, the study describes basic construction materials and a variety of other ones used for building aircraft with MTOW of 2500 kg or less.
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飞机结构材料的可燃性
本研究涉及飞机结构材料的可燃性,主要针对最大起飞重量为2500公斤或以下的飞机。所有可燃性试验均采用符合ISO 5660- 1:20 02标准的锥形量热计进行检测。通过对所有外部建筑和内部装饰材料的单独测试,飞机是由;我们取得的结果,作为进一步编制消防和救援服务安全建议的基础,同时协助处理空难。此外,该研究非常简单地处理了航空工业中使用的耐火材料的基本来源及其测试。除此之外,该研究还描述了用于建造最大重量为2500公斤或以下的飞机的基本建筑材料和各种其他材料。
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