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    Vortex Generators in Lean-Premix Combustion

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 001::page 41
    Author:
    A. Eroglu
    ,
    F. Joos
    ,
    P. Brunner
    ,
    K. Döbbeling
    DOI: 10.1115/1.1335481
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A novel fuel-air mixing technique on the basis of vortex generators has been developed and successfully implemented in the worlds first lean-premix reheat combustor of ABB’s GT24/GT26 series industrial gas turbines. This technique uses a special arrangement of delta-wing type vortex generators to achieve rapid mixing through longitudinal vortices, which produce low pressure drop and no recirculation zones along the mixing section. In this paper, after a short introduction to the topic, the motivation for utilizing vortex generators and the main considerations in their design are explained. A detailed analysis of the flow field, pressure drop and the strength of the vortices generated by a single vortex generator are presented as one of the three main geometrical parameters is varied. The results obtained through water model tests indicate that an optimum vortex generator geometry exists, which produces the maximum circulation at a relatively low pressure drop price. Moreover, the axial velocity distribution along the mixing section stays uniform enough to assure flash-back free operation despite the elevated inlet temperatures encountered in a reheat combustor. After selecting this optimized geometry, the process of the arrangement of multiple vortex generators in an annular combustor segment is described. The optimum arrangement presented here is suitable both for gaseous and liquid fuel injection, since it requires only one injection location per combustor segment.
    keyword(s): Vortices , Generators AND Fuels ,
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      Vortex Generators in Lean-Premix Combustion

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    http://yetl.yabesh.ir/yetl1/handle/yetl/125235
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. Eroglu
    contributor authorF. Joos
    contributor authorP. Brunner
    contributor authorK. Döbbeling
    date accessioned2017-05-09T00:04:54Z
    date available2017-05-09T00:04:54Z
    date copyrightJanuary, 2001
    date issued2001
    identifier issn1528-8919
    identifier otherJETPEZ-26802#41_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125235
    description abstractA novel fuel-air mixing technique on the basis of vortex generators has been developed and successfully implemented in the worlds first lean-premix reheat combustor of ABB’s GT24/GT26 series industrial gas turbines. This technique uses a special arrangement of delta-wing type vortex generators to achieve rapid mixing through longitudinal vortices, which produce low pressure drop and no recirculation zones along the mixing section. In this paper, after a short introduction to the topic, the motivation for utilizing vortex generators and the main considerations in their design are explained. A detailed analysis of the flow field, pressure drop and the strength of the vortices generated by a single vortex generator are presented as one of the three main geometrical parameters is varied. The results obtained through water model tests indicate that an optimum vortex generator geometry exists, which produces the maximum circulation at a relatively low pressure drop price. Moreover, the axial velocity distribution along the mixing section stays uniform enough to assure flash-back free operation despite the elevated inlet temperatures encountered in a reheat combustor. After selecting this optimized geometry, the process of the arrangement of multiple vortex generators in an annular combustor segment is described. The optimum arrangement presented here is suitable both for gaseous and liquid fuel injection, since it requires only one injection location per combustor segment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVortex Generators in Lean-Premix Combustion
    typeJournal Paper
    journal volume123
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1335481
    journal fristpage41
    journal lastpage49
    identifier eissn0742-4795
    keywordsVortices
    keywordsGenerators AND Fuels
    treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 001
    contenttypeFulltext
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