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

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...

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Main Authors: Angadi Vijet, Patil Arun Y., Mathad Shridhar N., Patil Mallikarjunagouda B.
Format: Article
Language:English
Published: Faculty of Technology, Novi Sad 2022-01-01
Series:Acta Periodica Technologica
Subjects:
Online Access:http://www.doiserbia.nb.rs/img/doi/1450-7188/2022/1450-71882253176A.pdf
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author Angadi Vijet
Patil Arun Y.
Mathad Shridhar N.
Patil Mallikarjunagouda B.
author_facet Angadi Vijet
Patil Arun Y.
Mathad Shridhar N.
Patil Mallikarjunagouda B.
author_sort Angadi Vijet
collection DOAJ
description 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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spelling doaj.art-a1ad340d63df4bf5b334a0063c016eb52022-12-22T04:39:55ZengFaculty of Technology, Novi SadActa Periodica Technologica1450-71882406-095X2022-01-0120225317618710.2298/APT2253176A1450-71882253176AThermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor bladeAngadi Vijet0Patil Arun Y.1Mathad Shridhar N.2Patil Mallikarjunagouda B.3School of Mechanical Engineering, KLE Technological University, Hubballi, IndiaSchool of Mechanical Engineering, KLE Technological University, Hubballi, IndiaKLE institute of Technology, Hubballi, Karnataka, IndiaBharat Ratna Prof. CNR Rao Research Centre, Basaveshwar Science College, Bagalkot, IndiaThis 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.http://www.doiserbia.nb.rs/img/doi/1450-7188/2022/1450-71882253176A.pdfbig sheep horndeccanithermal propertysimulationhigh temperature application
spellingShingle Angadi Vijet
Patil Arun Y.
Mathad Shridhar N.
Patil Mallikarjunagouda B.
Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
Acta Periodica Technologica
big sheep horn
deccani
thermal property
simulation
high temperature application
title Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
title_full Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
title_fullStr Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
title_full_unstemmed Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
title_short Thermal studies of big sheep horn as thermal barrier coating (TBC) material for gas turbine compressor blade
title_sort thermal studies of big sheep horn as thermal barrier coating tbc material for gas turbine compressor blade
topic big sheep horn
deccani
thermal property
simulation
high temperature application
url http://www.doiserbia.nb.rs/img/doi/1450-7188/2022/1450-71882253176A.pdf
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AT mathadshridharn thermalstudiesofbigsheephornasthermalbarriercoatingtbcmaterialforgasturbinecompressorblade
AT patilmallikarjunagoudab thermalstudiesofbigsheephornasthermalbarriercoatingtbcmaterialforgasturbinecompressorblade