ИССЛЕДОВАНИЕ ВЫСОКОТЕМПЕРАТУРНОЙ ТЕРМОСТОЙКОСТИ АНТИОКИСЛИТЕЛЬНОГО ПОКРЫТИЯ ДЛЯ КЕРАМИЧЕСКОГО КОМПОЗИЦИОННОГО МАТЕРИАЛА С МНОГОСЛОЙНОЙ СТРУКТУРОЙ

Abstract

The article covers the performance of thermal shock resistance experiments of a ceramic composite with two types of anti-oxidation coatings. A thermal shock burner rig was used to carry out the experiments similar to those expected in a combustor of a turbojet engine. SEM and х-ray diffraction analyses were used to examine the antioxidation coatings. It was deter-mined that the coating based on the refractory compounds possesses high thermal shock resistance when exposed to the fuel gas flow from a burner rig.