Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor
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Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor
Vol. 24, Issue 9, (2009)
作者机构:
北京航空航天大学, 能源与动力工程学院 航空发动机气动热力重点实验室,北京,100191
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
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ZHANG Chi, WANG Jian-chen, QIN Qing-qin, et al. Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor[J]. 2009, 24(9).
DOI:
ZHANG Chi, WANG Jian-chen, QIN Qing-qin, et al. Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor[J]. 2009, 24(9).DOI:
Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor
An experimental investigation was conducted on the combustor of micro gas turbine burning ethanol as a renewable biomass fuel
including 4 kinds of fuel supply modes.The ignition and lean blowout performance characteristics of this combustor under atmospheric pressure and temperature inlet condition were obtained.The research results indicate that
at atmospheric pressure and temperature
the equivalence ratios of lean ignition and lean blowout for the ethanol combustor with swirl-cup decrease with the increasing airflow rate
and the swirl-cup combustor has better ignition and lean blowout performance than the premixed prevaporized combustor.
Starting technical scheme of a micro gas turbine adapting to plateau
Influence of air split of a radial swirler on ignition and extinction characteristics
Influence of oxygen addition in multi-swirl pilot zone on atmospheric pressure ignition characteristics
Influences of the swirl cup flares design on the small combustor ignition performances
Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve
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Related Institution
中国航空发动机集团 湖南动力机械研究所
中国兵器工业集团有限公司 西北机电工程研究所
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Department of Scientific Research Project, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
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