CONCEPTUAL DEVELOPMENT OF A PULVERIZED COAL COMBUSTOR RIG (PCCR) FOR TESTING CO-FIRING PULVERIZED COAL AND AMMONIA FUEL

Authors

  • Mohd Khairul Hafiz Md Lias Universiti Teknologi Malaysia, Malaysia
  • Mazlan Abdul Wahid Universiti Teknologi Malaysia, Malaysia
  • Norazila Othman Universiti Teknologi Malaysia, Malaysia

Keywords:

green fuel, pulverized coal, ammonia, co-firing, swirl nozzle

Abstract

In Malaysia, the National Energy Policy 2022 - 2040 is focusing on achieving global net-zero greenhouse gas (GHG) emissions by 2050. To accelerate the energy transition plan, the National Energy Transition Roadmap (NETR) has been developed, which also includes the development of hydrogen, H2 and ammonia, NH3 co-firing for power generation. The ammonia co-firing with coal has a significant effect on reducing carbon dioxide, CO2 emissions but it also increases the nitrogen oxide, NOx content due to the high nitrogen content in its molecules. Additionally, the flame characteristic of the ammonia combustion has a narrow flammable range and slow flame propagation. Therefore, by introducing the ammonia injection swirl nozzle in the co-firing combustion, it enables a higher flammable range and increase flame propagation to achieve a higher temperature at the burner tip. The objective of this study is to conceptually develop a new test rig for co-firing pulverized coal and ammonia fuel with ammonia injection axial swirl nozzle. The significance of this development is to further improve GHG reduction for CO2 and NOX emissions. The conceptual test rig is designed for conducting experiments with the variation of axial swirl nozzle angle between 30⁰ to 60⁰ and also swirl number, Sn between 0.50 to 1.48. The test rig design concept is also expected to be able to test up to 100% ammonia firing.

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Published

30.04.2024

How to Cite

Md Lias, Mohd Khairul Hafiz, Mazlan Abdul Wahid, and Norazila Othman. 2024. “CONCEPTUAL DEVELOPMENT OF A PULVERIZED COAL COMBUSTOR RIG (PCCR) FOR TESTING CO-FIRING PULVERIZED COAL AND AMMONIA FUEL”. Journal of Aerospace Society Malaysia 2 (1):10-18. https://www.aerosmalaysia.my/aeros_journal/index.php/journal/article/view/22.

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