Feasibility study of ultra-low NOx Gas turbine combustor using the RML combustion concept
Volume: 30, Issue: 12, Pages: 5749 - 5757
Published: Dec 1, 2016
Abstract
A new combustion concept, the so called RML, was investigated to validate its application as a gas turbine combustor for combustor outlet temperatures over 1973 K. The feasibility study of the RML combustor was conducted with zero dimensional combustion calculations. The emission characteristics of RQL, LEAN, EGR and RML combustors were compared. The calculation results showed that the RQL combustor has lower NOx emissions than the LEAN at high...
Paper Details
Title
Feasibility study of ultra-low NOx Gas turbine combustor using the RML combustion concept
Published Date
Dec 1, 2016
Volume
30
Issue
12
Pages
5749 - 5757
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