Binary Brayton Cycle with Isothermal Concept | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 75, Volume 15, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013, May 2013, Page 1-11 PDF (341.35 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2013.22184 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| R. M. Abd El-Maksoud | ||||
| Assistant professor, Faculty of Eng., Mataria, Helwan University, Cairo, Egypt. | ||||
| Abstract | ||||
| The literature introduced binary Brayton cycle and the isothermal concept as two promising methods used to enhance the performance of the gas turbine. Consequently, this work presents a cycle based on the blending of the two methods. This cycle is composed of gas turbine topping cycle with isothermal combustion and air turbine bottoming cycle with isothermal heating. Different parameters affecting the cycle performance have been studied. Simulations demonstrate that the present cycle achieves drastic enhancement in performance. The cycle merits justify its potential utilization for future power generation. | ||||
| Keywords | ||||
| Isothermal combustion; Isothermal heating; Binary cycle; Brayton cycle; Gas turbine | ||||
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