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    Low-Pressure Plasma-Spray Coatings for Hot-Corrosion Resistance

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 001::page 146
    Author:
    R. W. Smith
    ,
    W. F. Schilling
    ,
    H. M. Fox
    DOI: 10.1115/1.3230687
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The hot corrosion of low-pressure plasma-sprayed coating, GT-29 (Co-29Cr-6Al-1Y) on a γ′ -strengthened nickel base superalloy, IN-738, was characterized at both 871 °C and 983 °C in a simulated gas turbine environment. The test results show that at 871 °C the dense, defect-free, low-pressure, plasma-sprayed GT-29 coatings provide good corrosion protection up to 8000 hr. The mechanism of protection was the formation of a dense, adherent Al2 O3 scale underneath a mixed oxide scale; scale was maintained by a uniformly dispersed Al rich β(CoAl) reservoir. At 982 °C, the coating corrosion protection exceeded 5000 hours and also utilized a protective Al2 O3 scale. Due to the higher test temperature, interdiffusion of O, S, Al, Co, and Cr was higher and internal sulfidation/oxidation of the coating occurred; however, the rates were much lower than uncoated IN-738. Field tests were run (13051 and 19842 hr) to evaluate the low-pressure, plasma-sprayed GT-29 coatings’ corrosion resistance on turbine buckets. Metallographic inspection of the field-tested coatings verified the simulated burner-rig test results and demonstrated that the low-pressure plasma process provides an attractive alternative to other coating processes for producing hot-corrosion resistant coatings.
    keyword(s): Coatings , Pressure , Electrical resistance , Plasmas (Ionized gases) , Sprays , Corrosion , Coating processes , Gas turbines , Turbines , Corrosion resistance , oxidation , Mechanisms , Coal , Temperature , Nickel , Inspection , Superalloys AND Reservoirs ,
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      Low-Pressure Plasma-Spray Coatings for Hot-Corrosion Resistance

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/94572
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. W. Smith
    contributor authorW. F. Schilling
    contributor authorH. M. Fox
    date accessioned2017-05-08T23:11:11Z
    date available2017-05-08T23:11:11Z
    date copyrightJanuary, 1981
    date issued1981
    identifier issn1528-8919
    identifier otherJETPEZ-26763#146_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94572
    description abstractThe hot corrosion of low-pressure plasma-sprayed coating, GT-29 (Co-29Cr-6Al-1Y) on a γ′ -strengthened nickel base superalloy, IN-738, was characterized at both 871 °C and 983 °C in a simulated gas turbine environment. The test results show that at 871 °C the dense, defect-free, low-pressure, plasma-sprayed GT-29 coatings provide good corrosion protection up to 8000 hr. The mechanism of protection was the formation of a dense, adherent Al2 O3 scale underneath a mixed oxide scale; scale was maintained by a uniformly dispersed Al rich β(CoAl) reservoir. At 982 °C, the coating corrosion protection exceeded 5000 hours and also utilized a protective Al2 O3 scale. Due to the higher test temperature, interdiffusion of O, S, Al, Co, and Cr was higher and internal sulfidation/oxidation of the coating occurred; however, the rates were much lower than uncoated IN-738. Field tests were run (13051 and 19842 hr) to evaluate the low-pressure, plasma-sprayed GT-29 coatings’ corrosion resistance on turbine buckets. Metallographic inspection of the field-tested coatings verified the simulated burner-rig test results and demonstrated that the low-pressure plasma process provides an attractive alternative to other coating processes for producing hot-corrosion resistant coatings.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLow-Pressure Plasma-Spray Coatings for Hot-Corrosion Resistance
    typeJournal Paper
    journal volume103
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230687
    journal fristpage146
    journal lastpage153
    identifier eissn0742-4795
    keywordsCoatings
    keywordsPressure
    keywordsElectrical resistance
    keywordsPlasmas (Ionized gases)
    keywordsSprays
    keywordsCorrosion
    keywordsCoating processes
    keywordsGas turbines
    keywordsTurbines
    keywordsCorrosion resistance
    keywordsoxidation
    keywordsMechanisms
    keywordsCoal
    keywordsTemperature
    keywordsNickel
    keywordsInspection
    keywordsSuperalloys AND Reservoirs
    treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 001
    contenttypeFulltext
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