Development of a Thrust Measurement Device System for Micro-Gas Turbine

Abstract

This study focuses on developing a specialized system model for thrust measurement in micro-gas turbines, addressing the need to modify conventional techniques to accommodate their unique design, size, and operational characteristics. The primary objective of this paper is to develop and design a reliable and practical thrust measurement device system that accurately simulates the forces exerted by a micro-gas turbine on a specific material, with a focus on ensuring trustworthiness and usability. By completing a thorough literature review and using an appropriate methodology, this project intends to construct a thrust measurement system, design a related model, and successfully implement and integrate the simulation results. As a result, a reliable and practical device system model for measuring micro gas turbines was developed and designed, and through Solidworks CAD simulation tests, we found that malleable cast iron is the most ideal material due to its ideal results among applied materials. The research not only contributes to the field of aeronautical engineering by developing new avenues for micro-gas turbine technology research, and innovation, but also highlights the need for further advancements, including the integration of high-quality weighing sensors, robust mounts and suspensions, reliable signal conditioning, comprehensive calibration and validation procedures, robust data acquisition systems, and prioritization of safety considerations throughout the design process.