AIRCRAFT BRAKE TEMPERATURE MONITORING AND ALERTING SYSTEM

Ramasubramanian, S. and Vigneshwaran, V and Abirami, Govindaraj and Anto Vibin, K.R and Khushi, Singh and Mallampalli, Natasha (2026) AIRCRAFT BRAKE TEMPERATURE MONITORING AND ALERTING SYSTEM. International Journal of Scientific Research in Engineering and Management (IJSREM), 10 (4): 1. pp. 1-5. ISSN 2582-3930

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Official URL: https://ijsrem.com/?utm_source=chatgpt.com

Abstract

Aircraft carbon brakes generate extreme
thermal loads exceeding 450°C during highenergy
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 colorcoded
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 .

Item Type:	Article
Subjects:	Automobile Engineering > Auto Electrical and Electronics
Domains:	Automobile Engineering
Depositing User:	Mr IR Admin
Date Deposited:	16 May 2026 12:30
Last Modified:	19 May 2026 08:57
URI:	https://ir.vistas.ac.in/id/eprint/19883

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