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contributor authorS. J. Markowski
contributor authorR. P. Lohmann
contributor authorR. S. Reilly
date accessioned2017-05-08T23:00:40Z
date available2017-05-08T23:00:40Z
date copyrightJanuary, 1976
date issued1976
identifier issn1528-8919
identifier otherJETPEZ-26723#123_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88623
description abstractThe vorbix burner (acronym for Vortex Burning and Mixing) represents a new approach to a practical gas turbine combustor design. The concept exploits the Rayleigh instability of swirling flows to enhance the mixing and combustion rates. The combination of a two-stage fuel system with a piloted combustor leads to a unique high rate technique for fuel prevaporization within the combustor proper. This paper presents the fundamental concepts in the definition of the vorbix combustor and the results of exploratory tests conducted on can (tubular) and annular vorbix combustors. The results indicate that this type of combustor has unique performance characteristics that include excellent stability and high combustion efficiency over wide excursions in operating fuel air ratios in addition to substantially reduced emission levels during high power operation.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Vorbix Burner—A New Approach to Gas Turbine Combustors
typeJournal Paper
journal volume98
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446102
journal fristpage123
journal lastpage129
identifier eissn0742-4795
keywordsCombustion chambers
keywordsGas turbines
keywordsCombustion
keywordsFuels
keywordsFuel systems
keywordsDesign
keywordsVortices
keywordsSwirling flow
keywordsEmissions
keywordsPerformance characterization AND Stability
treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 001
contenttypeFulltext


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