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The influence of air distribution on homogeneity and pollutant formation in the primary zone of a tubular combustorThis paper summarizes the work undertaken by the Defense Research Agency (DRA Pyestock) for the BRITE/EURAM Low Emissions Combustor Technology Project No 1019. The work was jointly funded by the CEC (DGXIIH), the UK DTI (CARAD - ATF4) and the UK MOD (DCSA). The gas turbine emissions problem is summarized and the design philosophy of the experimental program is described. The principal objective was to demonstrate a simultaneous reduction of NO(x) and smoke emissions together with acceptable idling emissions and stability in an unstaged combustor. A secondary objective was to demonstrate the extent to which NO(x) and smoke could be reduced if the combustor was to be used as the main stage of a staged combustor where a poorer idling performance could be accepted. The work consisted of a parametric investigation of the principal factors controlling the emissions produced in the combustor primary zone. Particular emphasis was placed on the influence of the distribution, number, and size of air entry holes and of residence time on pollutant formation. The results from the complete experimental program are summarized. These suggest that NO(x) reductions of about 30-40 percent should be possible together with excellent smoke and idling performance. The results suggest that NO(x) was formed very close to stoichiometric flame temperatures even at very weak combustor mixture strengths and under well mixed conditions. The reductions that were achieved were largely as a result of reductions of residence time.
Document ID
19940024771
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
J R Tilston
(Defence Research Agency Farnborough, Hampshire, United Kingdom)
M I Wedlock
(Defence Research Agency Farnborough, Hampshire, United Kingdom)
A D Marchment
(Defence Research Agency Farnborough, Hampshire, United Kingdom)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: AGARD, Fuels and Combustion Technology for Advanced Aircraft Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0719-3
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AGARD-CP-536
AD-A275679
Meeting Information
Meeting: The Propulsion and Energetics Panel 81st Symposium
Location: Fiuggi
Country: IT
Start Date: May 10, 1993
End Date: May 14, 1993
Sponsors: North Atlantic Treaty Organization
Accession Number
94N29274
Funding Number(s)
CONTRACT_GRANT: BRITE/EURAM-1019
Distribution Limits
Public
Copyright
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