UCL Discovery
UCL home » Library Services » Electronic resources » UCL Discovery

Investigation of Ammonia/Hydrogen Mixtures and Pilot-Split Strategies in a Laboratory-Scale Radial Swirl Combustor

Rizza, R; Talibi, M; Cosway, B; Kenny, L; Beita, J; Ducci, A; Sadasivuni, S; (2024) Investigation of Ammonia/Hydrogen Mixtures and Pilot-Split Strategies in a Laboratory-Scale Radial Swirl Combustor. In: Proceedings of the ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition. Volume 2: Ceramics and Ceramic Composites; Coal, Biomass, Hydrogen, and Alternative Fuels. ASME: London, UK.

[thumbnail of GT2024-129167.pdf] Text
GT2024-129167.pdf - Accepted Version
Access restricted to UCL open access staff

Download (7MB)

Abstract

The transition to a decarbonised energy future relies on identifying the most suitable alternative fuels that can meet the needs of various energy sectors. While both ammonia and hydrogen are zero-carbon energy vectors, their physical properties and burning characteristics sit on either side of that of natural gas. Hence, mixtures of ammonia and hydrogen are being increasingly looked at as having the potential to fuel current energy systems without requiring significant combustor redesign. However, the combustion characteristics and operation limits for different ammonia/hydrogen mixtures still need to be evaluated. For GT applications in particular, the effect of ammonia/hydrogen mixture composition and operating condition on flame behaviour and stability is not well understood. The current work was carried out in a laboratory scale, radial swirl-stabilised turbulent combustor. A systematic study of two ammonia/hydrogen blend ratios (70:30 and 80:20 by volume) and a range of equivalence ratios were tested for different pilot-split ratios, to understand the effect on flame shape, stability and dynamics. Time-resolved pressure and integrated heat release fluctuations were measured to evaluate combustor dynamics, and NH2* chemiluminescence flame images were captured to understand spatial differences in flame structure. When comparing blend ratios, differences were observed in flame macro-structures and combustor dynamics, which could be largely attributed to the considerable difference in the laminar flame speeds of the blends. The addition of pilot generally improved the stability and lean operation for both blend ratios.

Type: Proceedings paper
Title: Investigation of Ammonia/Hydrogen Mixtures and Pilot-Split Strategies in a Laboratory-Scale Radial Swirl Combustor
Event: ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition
Location: ENGLAND, London
Dates: 24 Jun 2024 - 28 Jun 2024
ISBN-13: 978-0-7918-8793-6
DOI: 10.1115/GT2024-129167
Publisher version: https://doi.org/10.1115/GT2024-129167
Language: English
Additional information: This version is the author accepted manuscript. For information on re-use, please refer to the publisher’s terms and conditions.
Keywords: Ammonia, hydrogen, radial swirl combustor, gas turbines, pilot split, combustor dynamics
UCL classification: UCL
UCL > Provost and Vice Provost Offices > UCL BEAMS
UCL > Provost and Vice Provost Offices > UCL BEAMS > Faculty of Engineering Science > Dept of Mechanical Engineering
URI: https://discovery.ucl.ac.uk/id/eprint/10199845
Downloads since deposit
1Download
Download activity - last month
Download activity - last 12 months
Downloads by country - last 12 months

Archive Staff Only

View Item View Item