Modelling of NOx Emissions from Gas Turbine Combustors

Master Thesis (2022)
Author(s)

M.A. Maćkowiak (TU Delft - Mechanical Engineering)

Contributor(s)

Sikke A. Klein – Mentor (TU Delft - Energy Technology)

Michael Huth – Graduation committee member (Siemens Energy)

Juergen Meisl – Graduation committee member (Siemens Energy)

Faculty
Mechanical Engineering
Copyright
© 2022 Marlena Maćkowiak
More Info
expand_more
Publication Year
2022
Language
English
Copyright
© 2022 Marlena Maćkowiak
Graduation Date
11-11-2022
Awarding Institution
Delft University of Technology
Programme
Mechanical Engineering | Energy, Flow and Process Technology
Faculty
Mechanical Engineering
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The detrimental influence of nitric oxides (NOx) on humans and the environment has been widely discussed by researchers.
The dominant part of nitic oxides emissions comes from combustion - majority of NOx is being produced by reaction of nitrogen and oxygen at high temperatures.

This thesis project is carried out in cooperation with Siemens Energy, one of the gas turbines manufacturers.
The gas turbine combustor design requires extensive work in many fields: in addition to temperature distribution and flow field prediction, modelling of acoustics and emissions is necessary. As NOx are influenced by many variables, detailed sensitivity analyses of design features is required. Since that gas turbine producers are developing their own tools for emissions predictions.

The aim of this study is improvement and assessment of the existing tool used by Siemens Energy to predict NOx emissions by simulating the combustor system (both the flow and chemical kinetics).
As NOx emissions depend on the air-fuel mixing quality, the tool is equipped with a Monte Carlo-based turbulent mixing model. The combustor flow is divided into small parts - particles, that react and exchange properties between each other according to the Curl's turbulent mixing model.

The tool was improved by adding useful features (such as prescribed unmixedness in the flame front). After that, the Siemens Energy axially staged combustor was modelled (with different equivalence ratios, pressure levels and pilot fuel flows). In the end the tool was validated - the simulation results were compared to the experimental ones.

Files

License info not available