Experimental analysis of swirl number and nozzle design for scale-up of partially cracked ammonia flames

• Stable flames achieved at different thermal powers with various nozzles and swirlers • High thermal power requires wide flame brush to prevent jet-like flames pinching off • Wider flame brush can be achieved by varying swirl number or nozzle design • Too wide a flame brush can impinge on confinement, reducing combustion efficiency. • Both swirl number and nozzle design affect emissions of NOx and NH 3 Due to its ease of storage and existing global distribution network, interest in the use of renewably produced ammonia for decarbonising energy systems is growing. Partially cracking ammonia can overcome the flame stability challenges of this fuel, but demonstrations of high-power ammonia-based swirl flames with acceptable emissions have yet to be realised. Therefore, the present study examines the effects of varying swirl number and nozzle design on the static stability and emissions from 20% (vol.) cracked ammonia swirl flames for a wide range of equivalence ratios (0.3 < Φ < 2.2) and thermal powers of 5, 10 and 15kW. Additionally, a reference case of 100kW thermal power at stoichiometric conditions was tested. Stable flames were shown across a broad range of equivalence ratios, swirl numbers and nozzle geometries although flame morphologies varied greatly. Of note was a geometric swirl number of 1.75 paired with a long nozzle, which enabled the transition to a flat, Coanda jet flow flame at equivalence ratios of 0.6 and 0.7. For a geometric swirl number of 1.45, shortening the nozzle resulted in significantly shorter, wider V-shape flames with greatly improved rich blowoff limits. This was found to be a desirable characteristic for reaching high thermal power with a constant nozzle throat diameter – i.e. dump plane velocity – as a widened flame brush prevents jet-like flames, which are susceptible to pinching off. This can also be achieved by increasing the swirl number, although to a lesser extent. However, with a widened flame brush, careful consideration must be given to confinement diameter to avoid flame impingement which has potential to increase local heat loss and hence reduce combustion efficiency, resulting in an increase in unburned NH 3 emissions. With the same geometric swirl number of 1.45, the shorter nozzle configuration resulted in higher NO emissions, potentially due to the shorter nozzle forming shorter, wider flames, meaning there was less residence time for NH 2 to consume NO in the flame zone. This difference was less noticeable at rich conditions, with all configurations reaching negligible NO emissions by Φ = 1.15

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Publication Details

Journal
Applications in Energy and Combustion Science
Published
2025-05-20
DOI
https://doi.org/10.1016/j.jaecs.2025.100338
Citations
3
Primary Topic
Combustion and flame dynamics
Type
article
Field-Weighted Citation Impact
4.00

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article

Experimental analysis of swirl number and nozzle design for scale-up of partially cracked ammonia flames

Agustín Valera-Medina, Syed Mashruk, J. Davies, Daisuke Sato
3 citations
Applications in Energy and Combustion Science
Combustion and flame dynamics
4.00
article

Experimental analysis of swirl number and nozzle design for scale-up of partially cracked ammonia flames

Agustín Valera-Medina, Syed Mashruk, J. Davies, Daisuke Sato
article en
3 citations

Abstract

• Stable flames achieved at different thermal powers with various nozzles and swirlers • High thermal power requires wide flame brush to prevent jet-like flames pinching off • Wider flame brush can be achieved by varying swirl number or nozzle design • Too wide a flame brush can impinge on confinement, reducing combustion efficiency. • Both swirl number and nozzle design affect emissions of NOx and NH 3 Due to its ease of storage and existing global distribution network, interest in the use of renewably produced ammonia for decarbonising energy systems is growing. Partially cracking ammonia can overcome the flame stability challenges of this fuel, but demonstrations of high-power ammonia-based swirl flames with acceptable emissions have yet to be realised. Therefore, the present study examines the effects of varying swirl number and nozzle design on the static stability and emissions from 20% (vol.) cracked ammonia swirl flames for a wide range of equivalence ratios (0.3 < Φ < 2.2) and thermal powers of 5, 10 and 15kW. Additionally, a reference case of 100kW thermal power at stoichiometric conditions was tested. Stable flames were shown across a broad range of equivalence ratios, swirl numbers and nozzle geometries although flame morphologies varied greatly. Of note was a geometric swirl number of 1.75 paired with a long nozzle, which enabled the transition to a flat, Coanda jet flow flame at equivalence ratios of 0.6 and 0.7. For a geometric swirl number of 1.45, shortening the nozzle resulted in significantly shorter, wider V-shape flames with greatly improved rich blowoff limits. This was found to be a desirable characteristic for reaching high thermal power with a constant nozzle throat diameter – i.e. dump plane velocity – as a widened flame brush prevents jet-like flames, which are susceptible to pinching off. This can also be achieved by increasing the swirl number, although to a lesser extent. However, with a widened flame brush, careful consideration must be given to confinement diameter to avoid flame impingement which has potential to increase local heat loss and hence reduce combustion efficiency, resulting in an increase in unburned NH 3 emissions. With the same geometric swirl number of 1.45, the shorter nozzle configuration resulted in higher NO emissions, potentially due to the shorter nozzle forming shorter, wider flames, meaning there was less residence time for NH 2 to consume NO in the flame zone. This difference was less noticeable at rich conditions, with all configurations reaching negligible NO emissions by Φ = 1.15

Applications in Energy and Combustion ScienceVol. 22
Kyoto University (JP), Kyoto Katsura Hospital (JP), Cardiff University (GB)
Cardiff University, Engineering and Physical Sciences Research Council
Openalex Percentile: Top 7%
Combustion and flame dynamics
4.00
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