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ArticlePeer ReviewedOpen AccessPlagiarism Passed
Paper ID:IJSREM61454

AIRCRAFT BRAKE TEMPERATURE MONITORING AND ALERTING SYSTEM

Stream/Area:

-

Subject:

-

Paper ID:

IJSREM61454

Volume:

10 |

4 |

April 2026

Pages:

Publication Frequency:

Monthly (12 issues per year)

DOI
Digital Object Identifier
10.55041/ijsrem61454

License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.

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Authors

MN

Mallampalli Natasha

SR

S. Ramasubramanian

VV

Vigneshwaran V

AG

Abirami Govindaraj

AVK

Anto Vibin K.R

KS

Khushi Singh

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Abstract

Aircraft carbon brakes generate extreme thermal loads exceeding 450°C during high-energy landings, posing significant safety risks. This research develops a 6-sensor Brake Temperature Monitoring System (BTMS) prototype utilizing an Arduino Uno microcontroller and MAX6675 thermocouple module sensors. The system provides real-time 1Hz monitoring with ATmega328P processing, displaying data on a 16×2 LCD with color-coded LED alerts following FAA TSO-C163 thresholds. Testing validates complete alert progression reaching 465°C peak temperatures. The 180g prototype demonstrates production readiness for general aviation, enabling predictive maintenance and enhanced safety .

KEYWORDS

BTMS Arduino Uno MAX6675 thermocouple module sensors Carbon Brakes TSO-C163 Aircraft Safety

Cite This Article

Mallampalli Natasha, S. Ramasubramanian, Vigneshwaran V, Abirami Govindaraj, Anto Vibin K.R, Khushi Singh, "AIRCRAFT BRAKE TEMPERATURE MONITORING AND ALERTING SYSTEM," International Journal of Scientific Research in Engineering and Management, vol. 10, no. 4, April 2026. https://doi.org/10.55041/ijsrem61454

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Publication Date

4/26/2026

Peer Review Type

Double-Blind Peer Review

Review Rounds: 2

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The authors declare no conflict of interest related to this research work.

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