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    Evaluation of Heat-Resistant Alloys for Marine Gas Turbine Applications

    Source: Journal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 001::page 23
    Author:
    L. J. Fiedler
    ,
    R. M. N. Pelloux
    DOI: 10.1115/1.3616602
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Materials for the turbine and combustor sections of gas turbine engines were evaluated for their resistance to sulfidation corrosion. The basic evaluation was conducted in a test facility by exposing the materials to a combustion gas atmosphere which simulates conditions of gas composition, corrosive combustion residue, gas velocity, and temperature that are encountered while operating a gas turbine engine in a marine environment. The influence of alloy composition, protective coatings, salt ingestion rates, and fuel sulfur content is discussed in relation to the degree of sulfidation corrosion. The mechanism of sulfidation corrosion attack, as determined by electron microprobe analyses and X-ray diffraction studies of corroded materials, is also discussed.
    keyword(s): Heat , Alloys , Marine gas turbines , Corrosion , Gas turbines , Turbines , Protective coatings , Sulfur , Test facilities , Mechanisms , X-ray diffraction , Fuels , Electrical resistance , Combustion gases , Microprobe analysis , Combustion chambers , Temperature , Electrons AND Combustion ,
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      Evaluation of Heat-Resistant Alloys for Marine Gas Turbine Applications

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/118911
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorL. J. Fiedler
    contributor authorR. M. N. Pelloux
    date accessioned2017-05-08T23:53:52Z
    date available2017-05-08T23:53:52Z
    date copyrightJanuary, 1967
    date issued1967
    identifier issn1528-8919
    identifier otherJETPEZ-26658#23_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118911
    description abstractMaterials for the turbine and combustor sections of gas turbine engines were evaluated for their resistance to sulfidation corrosion. The basic evaluation was conducted in a test facility by exposing the materials to a combustion gas atmosphere which simulates conditions of gas composition, corrosive combustion residue, gas velocity, and temperature that are encountered while operating a gas turbine engine in a marine environment. The influence of alloy composition, protective coatings, salt ingestion rates, and fuel sulfur content is discussed in relation to the degree of sulfidation corrosion. The mechanism of sulfidation corrosion attack, as determined by electron microprobe analyses and X-ray diffraction studies of corroded materials, is also discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEvaluation of Heat-Resistant Alloys for Marine Gas Turbine Applications
    typeJournal Paper
    journal volume89
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3616602
    journal fristpage23
    journal lastpage27
    identifier eissn0742-4795
    keywordsHeat
    keywordsAlloys
    keywordsMarine gas turbines
    keywordsCorrosion
    keywordsGas turbines
    keywordsTurbines
    keywordsProtective coatings
    keywordsSulfur
    keywordsTest facilities
    keywordsMechanisms
    keywordsX-ray diffraction
    keywordsFuels
    keywordsElectrical resistance
    keywordsCombustion gases
    keywordsMicroprobe analysis
    keywordsCombustion chambers
    keywordsTemperature
    keywordsElectrons AND Combustion
    treeJournal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 001
    contenttypeFulltext
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