Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade

Q3 Engineering Acta Periodica Technologica Pub Date : 2022-01-01 DOI:10.2298/apt2253176a
Vijet Angadi, A. Patil, S. Mathad, Mallikarjunagouda B. Patil
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Abstract

This research focuses on the decomposition temperature of a large sheep horn from Haveri District, Karnataka, India, which is 302.9?C. It also demonstrates the possible use of large sheep horn in the aerospace industry. It can be utilised as a Thermal Barrier Coating (TBC) in high-pressure compressor blades of jet engines. Because of its poor thermal conductivity and specific heat capacity, it is a superb insulator, and temperatures throughout the TBC take around 10 minutes to match.
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大羊角作为燃气轮机压气机叶片热障涂层材料的热学研究
本研究以印度卡纳塔克邦Haveri地区一只大羊角的分解温度为302.9℃为研究对象。它还展示了大羊角在航空航天工业中的可能用途。它可以用作喷气发动机高压压气机叶片的热障涂层(TBC)。由于其导热性和比热容差,它是一种极好的绝缘体,整个TBC的温度需要大约10分钟才能匹配。
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来源期刊
Acta Periodica Technologica
Acta Periodica Technologica Engineering-Engineering (all)
CiteScore
0.60
自引率
0.00%
发文量
0
审稿时长
8 weeks
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