Session: 03-02 Ammonia as Fuel and Hydrogen Carrier – Combustion, Storage, and Safety II
Submission Number: 176916
Fuel-Lean Ammonia-Hydrogen Combustion in a Jet-Stirred Reactor: NO and H2O Speciation in RQL Stage 2 Conditions
The need for more sustainable fuel alternatives in the modern aircraft industry is growing. The acceleration of climate change has catalyzed the search for alternative fuels. Carbon dioxide (CO2) is 80% of US greenhouse gas emissions. Transportation contributes to 28.5% of those CO2 emissions, and 10% of transportation CO2 emissions are due to aviation (U.S. Environmental Protection Agency, 2024). It is imperative that all sectors that use fossil fuels decarbonize. SAF is the current sustainable jet fuel in use but still produces harmful carbon emissions. A promising alternative to SAF is hydrogen, which produces zero carbon emissions. Hydrogen (H2) has been identified as a prime fuel candidate for decarbonization (Otto et al., 2022; Valera-Medina et al., 2021). However, with its low liquefaction temperature and high flammability, storage and transportation are complex and costly. Instead, ammonia can be used as a hydrogen carrier, which minimizes both the engineering difficulties and cost of using pure hydrogen (Valera-Medina et al., 2021). Liquid ammonia contains more hydrogen than an equal volume of liquid hydrogen and stays as a liquid at higher temperatures and over a wider range than hydrogen (Otto et al., 2023). By decomposing ammonia (NH3) into its constituents of N2 and H2 using a chemical catalyst, a hydrogen-ammonia fuel mix is created. H2/NH3 mixtures still have the desired characteristic of burning without carbon emissions but are less reactive than pure hydrogen. Additionally, ammonia is a widely used compound, so infrastructure already exists for production, transportation, and storage. One drawback of burning ammonia-hydrogen fuels is the combustion byproduct, nitrogen oxide (NOx), and unburned NH3. These emissions are both poisonous to humans and harmful to the environment.
This work focuses on the measurement of total emissions from an NH3/H2 combustor in a rich-burn, quick-quench, lean-burn (RQL) combustor, this paper will focus on the results from the lean-burn stage (Lefebvre et al., 2010). Combustion experiments will be performed in a toroidal jet stirred reactor at atmospheric pressure. A sensor using laser absorption spectroscopy (LAS) is designed and developed to measure combustion byproducts: NO, NH3, and H2O, as well as temperature, using two infrared lasers. H2O will be measured at 1936.21 cm-1 using fixed-wavelength LAS. NO and H2O will be measured at 1937.02 cm-1 and 1937.94 cm-1 respectively, using scanned-wavelength LAS. NH3 will be measured at 962.16 cm-1 using fixed-wavelength LAS. Equivalence ratios will range from 0.4-0.8. Fuel fraction of NH3/H2 will range from 0-1. NO, NH3 and H2O will be measured at each testing parameter. This study will look at pure ammonia as well as cracked ammonia as a fuel, which can be simulated with a mixture of ammonia/hydrogen. The results from this research will be used to validate NH3 chemical kinetic mechanisms for their applicability in fuel lean combustion relevant to RQL stage 2. Experimental results will be compared to model predictions using three different chemical kinetic mechanisms, Glarborg (2023), Zhang et al. (2021), and Stagni et al. (2020). The results presented here will help in the design and development of ammonia combustors operating on RQL configurations.
Presenting Author: Marzuqa Ahmed University of Central Florida
Presenting Author Biography: Marzuqa is a graduate student at the University of Central Florida studying alternative fuels for aviation, with a focus on ammonia.
Authors:
Marzuqa Ahmed University of Central FloridaAmanda Maia University of Central Florida
Guillermo Barrios Cadenas University of Central Florida
Oli Marquez Valenzuela University of Central Florida
Avril Elmer-Santiago University of Central Florida
Ashley Thornton University of Central Florida
Ramees K. Rahman University of Central Florida
Farhan Arafin University of Central Florida
Justin Urso University of Central Florida
Subith Vasu University of Central Florida
Fuel-Lean Ammonia-Hydrogen Combustion in a Jet-Stirred Reactor: NO and H2O Speciation in RQL Stage 2 Conditions
Paper Type
Technical Paper Publication