Affiliation:
1. Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran
Abstract
In this article, an attempt is made to utilize the exhaust gases of a small gas turbine to augment power output through the employment of a thermoacoustic system. A simple gas turbine cycle is selected as the base cycle and it is assumed that the thermoacoustic system is powered only by the waste heat of the base gas turbine. A comprehensive cycle analysis of the integrated gas turbine thermoacoustic engine (IGTTE) is carried out from an energy and exergy point of view. Exergy efficiency and internal exergy efficiency are calculated for the different components of the base gas turbine engine as well as the IGTTE. Value and exergy flow diagrams are used to investigate the possible improvements. Furthermore, a sensitivity analysis is performed by considering different conditions for the thermoacoustic system. The results clearly indicate some improvements with respect to exergetic efficiency from a simple thermodynamic point of view.
Subject
Mechanical Engineering,Energy Engineering and Power Technology
Cited by
9 articles.
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