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Daily Archives: January 1, 2026

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Transformer Health Monitoring System Using Iot

Authors: Dr. Chetana Reddy, Divya K, Madhumitha B, Maithra K, Melisha K Sunny

Abstract: Power transformers must work well and be reliable to keep the flow of electricity stable and uninterrupted. Standard periodic maintenance often does not find problems in their early stages, which can lead to insulation breakdown, oil breakdown, thermal stress, overloading, and unexpected outages. This paper proposes an IoT-based Transformer Health Monitoring System to address these limitations. The system can continuously and in real time monitor important operating parameters. The system uses sensors for temperature, oil level, load current, and input voltage that are connected to a microcontroller. The microcontroller processes the data and sends it to a cloud-based monitoring platform. The data analyzed by the IOT platform ensures early fault detection for maintenance planning. To support predictive maintenance, the suggested framework provides threshold-based alert notifications, historical logging, real-time data visualization, and remote access. The system creates automated alerts to stop overheating, insulation failure, and possible transformer failures when anomalous conditions are identified. This system monitors multiple transformers at different distributed substation. This IoT- enabled strategy prolongs transformer lifespan, lowers maintenance costs, minimizes downtime, and improves operational safety. The solution offers a scalable architecture for intelligent monitoring across substations and distribution networks and is in line with efforts to modernize smart grids.

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Vibration Analysis of Aircraft Wing

Authors: Abhishek Rawat, Basant Agarwal

Abstract: In recent years, extensive research has been conducted on vibrations in air-craft. Vibration can cause some serious failure in the structure. The increase in disquisition in vibration has led to taking design considerations in the bod-ies. This paper specifically focuses on the vibration in bodies causing defor-mation in aircraft wing. Modal analysis of two different wing is done using Fi-nite Element Analysis. Three different material namely: Aluminium Alloy, Copper Alloy and Titanium Alloy have been incorporated to describe the ef-fects of free vibration on different wings.

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