MUMBAI, India, July 24 -- Intellectual Property India has published a patent application (202641068296 A) filed by Kalasalingam Academy Of Research And Education on June 01, 2026, for Design And Development Of An Integrated Thrust Measurement And Electrical Performance Analysis System For Uav Propulsion Systems.
Inventors include Dr. J Rjessy Michla; Dr. P. Ramkumar; Kavinkumar S; and Sakthipriyan L S.
The application for the patent was published on July 17, 2026, under issue no. 29/2026.
Abstract: Title: DESIGN AND DEVELOPMENT OF AN INTEGRATED THRUST MEASUREMENT AND ELECTRICAL PERFORMANCE ANALYSIS SYSTEM FOR UAV PROPULSION SYSTEMS 10 15 20 The titled invention discloses a compact and integrated thrust measurement and electrical performance analysis system for evaluating UAV propulsion systems under controlled conditions. The system comprises a load-cell-based thrust measurement unit (3), an ESP32 microcontroller (4) for data processing and control, and a wattmeter (5) for real-time measurement of voltage, current, and power consumption. A motorpropeller assembly including a propeller (1) and motor (2) is mounted on a rigid frame to ensure accurate thrust sensing, supporting propellers up to 16-inch diameter and compatibility with BLDC motors including 5010 360 KV and similar configurations. The system operates with battery input through a battery connector (9) and main power switch (8), and features a modular design enabling interchangeability of propulsion components, A user interface comprising control buttons (11), tare/power button (6), thrust display (7), throttle and time display (12), and electrical parameter display (10) provides real-time monitoring and control. The invention enables synchronized analysis of thrust and electrical parameters, improving accuracy and efficiency.
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