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22184

Binary Brayton Cycle with Isothermal Concept

Article

Last updated: 04 Jan 2025

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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.

DOI

10.21608/asat.2013.22184

Keywords

Isothermal combustion, Isothermal heating, Binary cycle, Brayton cycle, Gas turbine

Authors

First Name

R.

Last Name

Abd El-Maksoud

MiddleName

M.

Affiliation

Assistant professor, Faculty of Eng., Mataria, Helwan University, Cairo, Egypt.

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Volume

15

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013

Related Issue

4183

Issue Date

2013-05-01

Receive Date

2018-12-18

Publish Date

2013-05-01

Page Start

1

Page End

11

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_22184.html

Detail API

https://asat.journals.ekb.eg/service?article_code=22184

Order

75

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Binary Brayton Cycle with Isothermal Concept

Details

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Article

Created At

22 Jan 2023