The blow-off and transient characteristics of co-firing ammonia/methane fuels in a swirl combustor

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Abstract

Recent studies have demonstrated that ammonia could be one of the most promising hydrogen carrier candidates which can be used in large-scale power plants. However, it is challenging to burn ammonia in gas turbines due to its narrow flame stabilization limits. In this study, the blow-off characteristics and flame macrostructure transition behavior of ammonia/air flame (NH3 flame) and ammonia/methane/air flame (50%NH3 flame) in a swirl combustor were investigated. Flame structures and flow fields near the blow-off limit were analyzed. Methane/air flame (CH4 flame) was also examined for comparative purposes. The flow field and instantaneous OH profile were measured with PIV and OH-PLIF technique, respectively. Large eddy simulation (LES) was conducted to extend the understanding of the experimental findings. Results revealed that the NH3 flame possesses a poor lean flame stability limit which can be largely extended by adding CH4 in the fuel. Changing swirl number (S) had no apparent effect on the lean blow-off limit (Φb) for the NH3 flame. On the contrary, a clear extension on Φb was found for the 50%NH3 flame when increasing S. Four flame macrostructure modes were identified when decreasing equivalence ratio (Φ). The transition from flame II to flame III ((Φtdescribes the transition equivalence ratio) can be considered as the early warning of blow-off for a swirl stabilized flame. For the NH3 flame, there was no clear flame macrostructure transition at small inlet velocities (U < 3.8 m/sec), i.e., Φb ≈ Φt. The difference between Φb and (Φtwas observed as the inlet velocity increased. However, for the 50%NH3 and CH4 flames, a clear flame macrostructure transition from flame II to flame III was observed even for a lower inlet velocity. The LES results demonstrated that the NH3 flame has a faster blow-off process compared to the CH4 flame, which is mainly attributed to the excessive stretch causing local extinction during the blow-off process.

Original languageEnglish
Pages (from-to)5859-5868
Number of pages10
JournalProceedings of the Combustion Institute
Volume38
Issue number4
DOIs
StatePublished - 2021
Event38th International Symposium on Combustion, 2021 - Adelaide, Australia
Duration: 24 Jan 202129 Jan 2021

Keywords

  • Ammonia
  • Carbon-free fuel
  • Hydrogen carrier
  • Lean blow-off
  • Swirl combustor

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