Design and Performance Optimization of a Radial Turbine Using Hydrogen Combustion Products

The combustion of hydrogen increases the water content of the combustion products, affecting the aerodynamic performance of turbines using hydrogen as a fuel. This study aims to design a radial turbine using the differential evolution (DE) algorithm to improve its characteristics and optimize its aerodynamic performance through an orthogonal experiment and analysis of means (ANOM). The effects of varying water content in combustion products, ranging from 12% to 22%, on the performance of the radial turbine are also investigated. After optimization, the total–static efficiency of the radial turbine increased to 89.12%, which was 1.59% higher than the preliminary design. The study found that flow loss in the impeller primarily occurred at the leading edge, trailing edge, and the inlet of the suction surface tip and outlet. With a 10% increase in water content, the enthalpy dropped, Mach number increased, and turbine power increased by 4.64%, 1.71%, and 2.41%, respectively. However, the total static efficiency and mass flow rate decreased by 0.71% and 2.13%, respectively. These findings indicate that higher water content in hydrogen combustion products enhances the turbine’s output power while reducing the combustion products’ mass flow rate.

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Publication Details

Journal
Aerospace
Published
2024-12-23
DOI
https://doi.org/10.3390/aerospace11121051
Primary Topic
Turbomachinery Performance and Optimization
Type
article
Field-Weighted Citation Impact
0.00

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article

Design and Performance Optimization of a Radial Turbine Using Hydrogen Combustion Products

Abdalazeem Adam, Pengfei Su, Omer Musa, Chen Wang et al.
Aerospace
Turbomachinery Performance and Optimization
article

Design and Performance Optimization of a Radial Turbine Using Hydrogen Combustion Products

Abdalazeem Adam, Pengfei Su, Omer Musa, Chen Wang, Zhichao Lou, Weifeng He
article en

Abstract

The combustion of hydrogen increases the water content of the combustion products, affecting the aerodynamic performance of turbines using hydrogen as a fuel. This study aims to design a radial turbine using the differential evolution (DE) algorithm to improve its characteristics and optimize its aerodynamic performance through an orthogonal experiment and analysis of means (ANOM). The effects of varying water content in combustion products, ranging from 12% to 22%, on the performance of the radial turbine are also investigated. After optimization, the total–static efficiency of the radial turbine increased to 89.12%, which was 1.59% higher than the preliminary design. The study found that flow loss in the impeller primarily occurred at the leading edge, trailing edge, and the inlet of the suction surface tip and outlet. With a 10% increase in water content, the enthalpy dropped, Mach number increased, and turbine power increased by 4.64%, 1.71%, and 2.41%, respectively. However, the total static efficiency and mass flow rate decreased by 0.71% and 2.13%, respectively. These findings indicate that higher water content in hydrogen combustion products enhances the turbine’s output power while reducing the combustion products’ mass flow rate.

AerospaceVol. 11(12)
Dongfang Electric Corporation (China) (CN), Karary University (SD), Nanjing University of Aeronautics and Astronautics (CN)
State Key Laboratory of Long-life High Temperature Materials, National Natural Science Foundation of China, Government of Jiangsu Province, Nanjing University of Aeronautics and Astronautics, Nanjing University
Affordable and clean energy
Openalex Percentile: Top 61%
Turbomachinery Performance and Optimization
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