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    Revisiting the Inhibition of Vanadium-Induced Hot Corrosion in Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003::page 664
    Author:
    E. Rocca
    ,
    M. Moliere
    ,
    P. Steinmetz
    DOI: 10.1115/1.1456095
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Since the 1970s, nothing substantially new has been published in the gas turbine community about the hot corrosion by vanadium and its inhibition, after the “inhibition orthodoxy” based on the formation of magnesium vanadate, was established. However, the experience acquired since the late 1980s with heavy-duty gas turbines burning ash-forming fuels in southern China, shows that the combustion of very contaminated fuels does not entail corrosion nor abundant ash-deposit on gas turbines buckets. Analyses of deposits collected from gas turbines fired with these crude oils showed that the ash-deposit contains a large amount of nickel. These new facts led to revisit the role played by nickel and envisage its possible inhibiting action against the vanadium-induced hot corrosion. A thorough review of the literature on the vanadium-induced corrosion have been carried out, and the study of the nickel effects with respect to magnesium effects on the ash deposit have been performed. Results show that nickel presents an interesting way to substitute magnesium for the inhibition of vanadium-induced hot corrosion. The advantages of nickel with respect to magnesium are to be efficient at alow Ni/V ratio, to produce less abundant, less adherent ash and to act, to some extent, as a self-cleaning agent for the blades of the turbine.
    keyword(s): Nickel , Corrosion , Gas turbines , Magnesium AND Combustion ,
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      Revisiting the Inhibition of Vanadium-Induced Hot Corrosion in Gas Turbines

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    contributor authorE. Rocca
    contributor authorM. Moliere
    contributor authorP. Steinmetz
    date accessioned2017-05-09T00:10:07Z
    date available2017-05-09T00:10:07Z
    date copyrightJuly, 2003
    date issued2003
    identifier issn1528-8919
    identifier otherJETPEZ-26823#664_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128344
    description abstractSince the 1970s, nothing substantially new has been published in the gas turbine community about the hot corrosion by vanadium and its inhibition, after the “inhibition orthodoxy” based on the formation of magnesium vanadate, was established. However, the experience acquired since the late 1980s with heavy-duty gas turbines burning ash-forming fuels in southern China, shows that the combustion of very contaminated fuels does not entail corrosion nor abundant ash-deposit on gas turbines buckets. Analyses of deposits collected from gas turbines fired with these crude oils showed that the ash-deposit contains a large amount of nickel. These new facts led to revisit the role played by nickel and envisage its possible inhibiting action against the vanadium-induced hot corrosion. A thorough review of the literature on the vanadium-induced corrosion have been carried out, and the study of the nickel effects with respect to magnesium effects on the ash deposit have been performed. Results show that nickel presents an interesting way to substitute magnesium for the inhibition of vanadium-induced hot corrosion. The advantages of nickel with respect to magnesium are to be efficient at alow Ni/V ratio, to produce less abundant, less adherent ash and to act, to some extent, as a self-cleaning agent for the blades of the turbine.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRevisiting the Inhibition of Vanadium-Induced Hot Corrosion in Gas Turbines
    typeJournal Paper
    journal volume125
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1456095
    journal fristpage664
    journal lastpage669
    identifier eissn0742-4795
    keywordsNickel
    keywordsCorrosion
    keywordsGas turbines
    keywordsMagnesium AND Combustion
    treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003
    contenttypeFulltext
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