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    Compressive Thermal Yielding Leading to Hydrogen Cracking in a Fired Cannon

    Source: Journal of Pressure Vessel Technology:;1999:;volume( 121 ):;issue: 001::page 116
    Author:
    J. H. Underwood
    ,
    A. P. Parker
    ,
    P. J. Cote
    ,
    S. Sopok
    DOI: 10.1115/1.2883658
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Investigation of environmental cracking of a 1100-MPa yield strength A723 steel cannon tube subjected to prototype firings is described. Metallographic results show cracking of the steel beneath a 0.12-mm protective layer of chromium. Cracks undermine and remove sections of chromium and lead to localized erosion that ruins the cannon. Key features of the firing thermal damage and cracking are: (i ) recrystalization of the chromium to a depth of up to 0.08 mm; (ii ) steel transformation to 0.19 mm below the chrome surface; (iii ) two different periodic arrays of cracks normal to the hoop and axial directions, with mean depths of 0.23 and 0.46 mm, respectively. Time-temperature-depth profiles for the firing cycle were derived via bi-material finite difference analysis of a semi-infinite solid which incorporated cannon combustion gas temperatures and material properties that vary as a function of temperature. The temperature and depth associated with the steel transformation were used to solve iteratively for the convective heat transfer coefficient. This value was further confirmed by the depths of chromium recrystalization and of the crack arrays in the two orientations. A profile of maximum temperature versus depth is used to determine the near-bore applied and residual stress distributions within the tube. The measured volume change of steel transformation is used to determine an upper limit on applied and residual stresses. These stresses are used to determine crack-tip stress intensity factors for the observed crack arrays, and hence provide some explanation for the differential depths of cracking. The near-bore temperature and residual stress distributions are used to help determine the cause of hydrogen cracking and measures to prevent cracking. Compressive yielding due to thermal loading produces near-bore tensile residual stresses, and thereby causes hydrogen cracking. Prevention of cracking is discussed in relationship to hydrogen crack growth rate tests of alternative alloys and coatings.
    keyword(s): Fracture (Process) , Hydrogen , Artillery , Temperature , Fracture (Materials) , Steel , Stress , Residual stresses , Firing (materials) , Yield strength , Engineering prototypes , Cycles , Combustion gases , Coatings , Alloys , Materials properties , Convection AND Erosion ,
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      Compressive Thermal Yielding Leading to Hydrogen Cracking in a Fired Cannon

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    http://yetl.yabesh.ir/yetl1/handle/yetl/122767
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    • Journal of Pressure Vessel Technology

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    contributor authorJ. H. Underwood
    contributor authorA. P. Parker
    contributor authorP. J. Cote
    contributor authorS. Sopok
    date accessioned2017-05-09T00:00:45Z
    date available2017-05-09T00:00:45Z
    date copyrightFebruary, 1999
    date issued1999
    identifier issn0094-9930
    identifier otherJPVTAS-28389#116_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122767
    description abstractInvestigation of environmental cracking of a 1100-MPa yield strength A723 steel cannon tube subjected to prototype firings is described. Metallographic results show cracking of the steel beneath a 0.12-mm protective layer of chromium. Cracks undermine and remove sections of chromium and lead to localized erosion that ruins the cannon. Key features of the firing thermal damage and cracking are: (i ) recrystalization of the chromium to a depth of up to 0.08 mm; (ii ) steel transformation to 0.19 mm below the chrome surface; (iii ) two different periodic arrays of cracks normal to the hoop and axial directions, with mean depths of 0.23 and 0.46 mm, respectively. Time-temperature-depth profiles for the firing cycle were derived via bi-material finite difference analysis of a semi-infinite solid which incorporated cannon combustion gas temperatures and material properties that vary as a function of temperature. The temperature and depth associated with the steel transformation were used to solve iteratively for the convective heat transfer coefficient. This value was further confirmed by the depths of chromium recrystalization and of the crack arrays in the two orientations. A profile of maximum temperature versus depth is used to determine the near-bore applied and residual stress distributions within the tube. The measured volume change of steel transformation is used to determine an upper limit on applied and residual stresses. These stresses are used to determine crack-tip stress intensity factors for the observed crack arrays, and hence provide some explanation for the differential depths of cracking. The near-bore temperature and residual stress distributions are used to help determine the cause of hydrogen cracking and measures to prevent cracking. Compressive yielding due to thermal loading produces near-bore tensile residual stresses, and thereby causes hydrogen cracking. Prevention of cracking is discussed in relationship to hydrogen crack growth rate tests of alternative alloys and coatings.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCompressive Thermal Yielding Leading to Hydrogen Cracking in a Fired Cannon
    typeJournal Paper
    journal volume121
    journal issue1
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.2883658
    journal fristpage116
    journal lastpage120
    identifier eissn1528-8978
    keywordsFracture (Process)
    keywordsHydrogen
    keywordsArtillery
    keywordsTemperature
    keywordsFracture (Materials)
    keywordsSteel
    keywordsStress
    keywordsResidual stresses
    keywordsFiring (materials)
    keywordsYield strength
    keywordsEngineering prototypes
    keywordsCycles
    keywordsCombustion gases
    keywordsCoatings
    keywordsAlloys
    keywordsMaterials properties
    keywordsConvection AND Erosion
    treeJournal of Pressure Vessel Technology:;1999:;volume( 121 ):;issue: 001
    contenttypeFulltext
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