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Review of domestic designs in the field of protecting carbonaceous materials against gas corrosion and erosion in high-speed plasma fluxes

机译:在保护碳质材料免受高速等离子通量中的气体腐蚀和侵蚀方面的国内设计综述

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摘要

The article is a continuation of the publication cycle of the authors the on the theme "Multifunctional Protective Coatings for Especially Thermally Loaded Elements of Constructions of Hypersonic Systems." Modern domestic approaches to the formation of single-layer and multilayered high-temperature protective coatings of various classes such as glass-ceramics ones obtained by various methods, coatings based on oxide ceramics, oxygen-free reaction-coupled coatings, and microcomposition coatings of the synergetic type are analyzed. Attention is paid to the fact that the scientific-and-applied investigation directed at the development of the structural and physicochemical models of the coating architecture and substantiation of their functioning with high-speed gas streams are almost absent. The selection of the chemical composition of coatings and production procedures of their formation is performed mainly based on the empirical basis. A series of coatings claimed as workable in conditions in a medium of tranquil or weakly perturbed air up to temperatures of 1600-2000A degrees C is presented; however, their protective ability in conditions of the effect of high-enthalpy supersonic and hypersonic gas streams cannot be judged because of the insufficiency or absence of required data. Microcompositional coatings of the synergetic type based on the Si-TiSi2-MoSi2-B-Y system, which were developed in terms of an original conceptual approach to the formation of a multilevel system of heat protection of thermally stressed constructional elements made of heat-resistant materials of hypersonic aircrafts and their propulsion systems, are especially emphasized. A detailed analysis of their functioning in the composition of a unique construction wall with protected carbonaceous materials will make it possible to determine the tendencies and directions of subsequent investigations by the authors with the purpose of improving the developments.
机译:本文是作者发表周期的延续,主题是“高超声速系统结构的特别是热负载元件的多功能保护涂层”。形成各种类型的单层和多层高温保护涂层的现代国内方法,例如通过各种方法获得的玻璃陶瓷涂层,基于氧化物陶瓷的涂层,无氧反应耦合涂层以及该涂层的微组成涂层协同类型进行了分析。需要注意的是,几乎没有针对涂层结构的结构和物理化学模型的开发以及其在高速气流下的功能证实的科学和应用研究。涂料化学成分的选择和形成过程的选择主要基于经验基础。提出了一系列声称可在温度高达1600-2000A的宁静或微扰空气中工作的涂料;然而,由于所需数据不足或缺乏,因此无法判断它们在高焓超音速和高音速气流影响下的保护能力。基于Si-TiSi2-MoSi2-BY系统的增效型微复合涂料,是根据原始概念方法开发的,用于形成由耐热材料制成的热应力结构元件的多层热保护体系特别强调了高超音速飞机及其推进系统。对它们在含碳质保护材料的独特建筑墙体中的功能进行的详细分析,将有可能确定作者随后进行研究的趋势和方向,以改善开发情况。

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