Perspective Heat-Resistant Coating for Protection of Cf/SiC Composites in Air Plasma Hypersonic Flow

被引：15

作者：

Astapov, A. N. ^{[1
]}

Lifanov, I. P. ^{[1
]}

Rabinskiy, L. N. ^{[1
]}

机构：

[1] Natl Res Univ, Moscow Aviat Inst, Moscow 125993, Russia

来源：

HIGH TEMPERATURE | 2019年 / 57卷 / 05期

基金：

俄罗斯科学基金会;

关键词：

OXIDATION;

D O I：

10.1134/S0018151X19050018

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The investigation results on development and testing of heat-resistant coating with experimental composition of Si-TiSi2-MoSi2-TiB2-CaSi2 for protection of C-f/SiC composites from oxidation and high-speed erosion in high-speed gas flows are presented. This coating was formed by slip firing technology out of slip compositions with filler based on heterophase powder of the system of interest. The results of fire bench tests of samples with coating under conditions of flow-around and off balance heating by air plasma streams with M = 5.5-6.0 and enthalpy of 40-45 MJ/kg. The effectiveness of the protective action of coating at surface temperature T-w = 1810-1820 degrees C is kept not less than 920-930 s, at T-w >= 1850-1860 degrees C-not less than 420-430 s. It was found that the effectiveness of coating is provided by structural-phase state of the base coating and formation of heterogeneous oxide film on its surface formed by borosilicate glass with titanium and calcium segregation heterogeneity and TiO2 reinforce micro-needles in the form of rutile. The decrease in saturated steam pressure level in oxide film-coating system induced by increase in the level of external layer heterogeneity was experimentally confirmed.

引用

页码：744 / 752

页数：9

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