Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments

In the present work, a water-cooled, modular, atmospheric pressure Trapped Vortex Combustor (TVC) test rig is designed and fabricated for reacting and non-reacting flow experiments. The unique features of this rig consist of a continuously variable length-to-depth ratio (L/D) of the cavity and optic...

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Main Authors: Atul Singhal, R. V. Ravikrishna
Format: Article
Language:English
Published: SAGE Publishing 2011-03-01
Series:International Journal of Spray and Combustion Dynamics
Online Access:https://doi.org/10.1260/1756-8277.3.1.23
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spelling doaj-4e199cfd4a4c4a70a95fbcc3cb6ea25a2020-11-25T03:45:17ZengSAGE PublishingInternational Journal of Spray and Combustion Dynamics1756-82771756-82852011-03-01310.1260/1756-8277.3.1.2310.1260_1756-8277.3.1.23Single Cavity Trapped Vortex Combustor Dynamics – Part-1: ExperimentsAtul SinghalR. V. RavikrishnaIn the present work, a water-cooled, modular, atmospheric pressure Trapped Vortex Combustor (TVC) test rig is designed and fabricated for reacting and non-reacting flow experiments. The unique features of this rig consist of a continuously variable length-to-depth ratio (L/D) of the cavity and optical access through quartz plates provided on three sides for visualization. Flame stabilization in the single cavity TVC was successfully achieved with methane as fuel and the range of flow conditions for stable operation were identified. From these, a few cases were selected for detailed experimentation. Reacting flow experiments for the selected cases indicated that reducing L/D ratio and increasing cavity-air velocity favour stable combustion. The pressure drop across the single cavity TVC is observed to be lower as compared to conventional combustors. Temperatures are measured at the exit using thermocouples and corrected for radiative losses. Species concentrations are measured at the exit using an exhaust gas analyzer. The combustion efficiency is observed to be around 97-99 % and the pattern factor is observed to be in the range of 0.08 to 0.13. High-speed imaging made possible by the optical access indicates that the overall combustion is fairly steady, and there is no vortex shedding downstream.https://doi.org/10.1260/1756-8277.3.1.23
collection DOAJ
language English
format Article
sources DOAJ
author Atul Singhal
R. V. Ravikrishna
spellingShingle Atul Singhal
R. V. Ravikrishna
Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
International Journal of Spray and Combustion Dynamics
author_facet Atul Singhal
R. V. Ravikrishna
author_sort Atul Singhal
title Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
title_short Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
title_full Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
title_fullStr Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
title_full_unstemmed Single Cavity Trapped Vortex Combustor Dynamics – Part-1: Experiments
title_sort single cavity trapped vortex combustor dynamics – part-1: experiments
publisher SAGE Publishing
series International Journal of Spray and Combustion Dynamics
issn 1756-8277
1756-8285
publishDate 2011-03-01
description In the present work, a water-cooled, modular, atmospheric pressure Trapped Vortex Combustor (TVC) test rig is designed and fabricated for reacting and non-reacting flow experiments. The unique features of this rig consist of a continuously variable length-to-depth ratio (L/D) of the cavity and optical access through quartz plates provided on three sides for visualization. Flame stabilization in the single cavity TVC was successfully achieved with methane as fuel and the range of flow conditions for stable operation were identified. From these, a few cases were selected for detailed experimentation. Reacting flow experiments for the selected cases indicated that reducing L/D ratio and increasing cavity-air velocity favour stable combustion. The pressure drop across the single cavity TVC is observed to be lower as compared to conventional combustors. Temperatures are measured at the exit using thermocouples and corrected for radiative losses. Species concentrations are measured at the exit using an exhaust gas analyzer. The combustion efficiency is observed to be around 97-99 % and the pattern factor is observed to be in the range of 0.08 to 0.13. High-speed imaging made possible by the optical access indicates that the overall combustion is fairly steady, and there is no vortex shedding downstream.
url https://doi.org/10.1260/1756-8277.3.1.23
work_keys_str_mv AT atulsinghal singlecavitytrappedvortexcombustordynamicspart1experiments
AT rvravikrishna singlecavitytrappedvortexcombustordynamicspart1experiments
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