A review on computational studies on hydrogen combustion for gas turbine applications

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Shankar A., Parammasivam K.M., Subramanian Surya Narayanan
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Abstract

Purpose

The purpose of this paper is to provide an overview of the computational progress in the development of hydrogen-fired gas turbines. This review aims to identify suitable combustion models, appropriate NOx chemistry mechanisms and NOx emission levels for effective utilization of hydrogen as an alternative fuel in gas turbines.

Design/methodology/approach

Hydrogen is recognized as a potential alternative fuel for achieving exceptionally low emissions in gas turbines. The developments in conventional, trapped vortex combustor and micromix combustors are discussed, along with various computational models aimed at accurately predicting combustion and emission characteristics. The results of numerical simulations were then discussed with emphasis on their role in optimizing the combustor geometry.

Findings

Computational studies that were used to optimize the combustor geometry to reduce NOx emissions and the flashback phenomenon are discussed. To retrofit existing gas turbines for hydrogen fuel, minor modifications that are required were discussed by analyzing extensive literature. The influence of key design and geometrical parameters on NOx emissions and the appropriate selection of combustion models for numerical simulations in optimizing various combustion systems are elaborated.

Originality/value

The review emphasizes the computational studies in the progress of hydrogen-fired gas turbine developments. The previous reviews were primarily focused on the combustion technologies for hydrogen-fired gas turbines. This comprehensive review focuses on the key design parameters, flame structure, selection of combustion models, combustion efficiency improvement and impact of parametric studies on NOx formation of various combustion systems, in particular hydrogen combustion for gas turbine applications.

燃气轮机应用中的氢气燃烧计算研究综述
本文旨在概述氢燃气轮机开发过程中的计算进展。本综述旨在确定合适的燃烧模型、适当的氮氧化物化学机制和氮氧化物排放水平,以便在燃气轮机中有效利用氢气作为替代燃料。本文讨论了传统、捕集涡流燃烧器和微混合燃烧器的发展,以及旨在准确预测燃烧和排放特性的各种计算模型。研究结果讨论了用于优化燃烧器几何形状以减少氮氧化物排放和回火现象的计算研究。通过分析大量文献,讨论了对现有燃气轮机进行氢燃料改造所需的小改动。详细阐述了关键设计和几何参数对氮氧化物排放的影响,以及在优化各种燃烧系统的数值模拟中燃烧模型的适当选择。以往的综述主要关注氢燃气轮机的燃烧技术。本综述重点关注各种燃烧系统的关键设计参数、火焰结构、燃烧模型的选择、燃烧效率的提高以及参数研究对氮氧化物形成的影响,尤其是燃气轮机应用中的氢燃烧。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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