THERMAL STUDIES OF BIG SHEEP HORN AS THERMAL BARRIER COATING (TBC) MATERIAL FOR GAS TURBINE COMPRESSOR BLADE

Vijet Angadi; Arun Y. Patil; Shridhar N. Mathad; Mallikarjunagouda B. Patil

doi:10.2298/APT2253176A

THERMAL STUDIES OF BIG SHEEP HORN AS THERMAL BARRIER COATING (TBC) MATERIAL FOR GAS TURBINE COMPRESSOR BLADE

Vijet Angadi
, Arun Y. Patil^*
, Shridhar N. Mathad
, Mallikarjunagouda B. Patil

^*Corresponding author for this work

Department of Mechanical and Industrial Engineering, Manipal Institute of Technology, Bengaluru

Research output: Contribution to journal › Article › peer-review

1 Citation (Scopus)

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.

Original language	English
Pages (from-to)	176-187
Number of pages	12
Journal	Acta Periodica Technologica
Issue number	53
DOIs	https://doi.org/10.2298/APT2253176A
Publication status	Published - 2022

All Science Journal Classification (ASJC) codes

General Engineering

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10.2298/APT2253176A

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AB - 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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THERMAL STUDIES OF BIG SHEEP HORN AS THERMAL BARRIER COATING (TBC) MATERIAL FOR GAS TURBINE COMPRESSOR BLADE

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