Abstract
The article deals with the problem of creating a t-protective coating for information-measuring devices and systems for various purposes exposed to external high-temperature exposure in emergency situations related to fire. As a solution to the problem, it is proposed to use thermal-protective materials containing active additives that provide a thermal-protective effect that promotes the refraction of heat flows aimed at heating the protected object. The heat-shielding effect is provided by an endothermic reaction that occurs in the material when the decomposition temperature of the selected component is reached. It should be noted that the temperature at which the reaction with heat absorption should occur should be lower than the temperature of the lesion of the protected object. In this case, the heat flows passing through the layer of heat-shielding material will be refracted, since heat will be spent on the decomposition of the endothermic filler. The heating of the material will be carried out due to the matrix of the material and decomposition products. Based on the tasks that require the use of a heat-protective material, the amount of endothermic filler is determined. Accordingly, with an increase in the time interval during which it is necessary to eliminate the fire, the content of endothermic filler also increases. The use of thermal-protective material is relevant for emergency flight data recorders, since in the event of a plane crash, a fire is likely to occur, which can lead to the loss of information necessary to determine the causes of an emergency.
Publisher
Samara State Technical University
Reference17 articles.
1. Okhapkin A.S. Study of the heat-transfer characteristics of a thermally protective composite materials, Journal of Engineering Physics and Thermophysics. Vol. 49, 6(1985). 1469–1473.
2. Alifanov O.M., Cherepanov V.V. Identification of models and prediction of physical properties of highly porous heat-shielding materials, Journal of Engineering Physics and Thermophysics. Vol. 83 (2010). 770-782.
3. Alifanov O.M., Budnik S.A., Nenarokomov A.V., Netelev A.V., Titov D.M. Destructive Materials Thermal properties determination with application for spacecraft structures testing. The 61th International Astronautical Congress (IAC-10) (Prague, Czech Republic) (2010) 10.
4. Dec J.A., Braun R.D., Lamb B. Ablative thermal response analysis using the finite element method, Journal of Thermophysics and Heat Transfer. Vol. 26, 2 (2012). 201–212.
5. Reznik S.V., Prosuntsov P.V., Mikhailovskii K.V. Prediction of Thermophysical and Thermo-mechanical Characteristics of Porous Carbon-Ceramic Composite Materials of the Heat Shield of Aerospace Craft, Journal of Engineering Physics and Thermophysics. Vol. 88, 3 (2015). 594–601.