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Effect of Severe Shot Peening on the Very-High Cycle\nNotch Fatigue of an AW 7075 Alloy

  1. 1.
    SYSNO ASEP0532360
    Document TypeJ - Journal Article
    R&D Document TypeJournal Article
    Subsidiary JČlánek ve WOS
    TitleEffect of Severe Shot Peening on the Very-High Cycle
    Notch Fatigue of an AW 7075 Alloy
    Author(s) Jambor, Michal (UFM-A) ORCID, RID
    Trško, L. (SK)
    Klusák, Jan (UFM-A) RID, ORCID
    Fintová, Stanislava (UFM-A) ORCID
    Kajánek, D. (SK)
    Nový, F. (SK)
    Bokůvka, O. (SK)
    Number of authors7
    Article number1262
    Source TitleMetals. - : MDPI
    Roč. 10, č. 9 (2020)
    Number of pages18 s.
    Languageeng - English
    CountryCH - Switzerland
    Keywordsultrasonic fatigue testing ; severe shot peening ; notched fatigue ; surface crack initiation ; AW7075 aluminum alloy
    Subject RIVJG - Metallurgy
    OECD categoryMaterials engineering
    R&D ProjectsLQ1601 GA MŠMT - Ministry of Education, Youth and Sports (MEYS)
    Method of publishingOpen access
    Institutional supportUFM-A - RVO:68081723
    UT WOS000580166200001
    EID SCOPUS85091095126
    DOI10.3390/met10091262
    AnnotationThe severe shot peening process was applied to the notched specimens from an AW7075
    alloy with the aim to improve fatigue endurance in the very-high cycle fatigue region. To reveal the
    stress state in the notch vicinity, finite element analysis was performed, simulating the conditions
    of the used 20 kHz ultrasonic fatigue loading. Modified surface characteristics by the severe shot
    peening process were analyzed in terms of residual stress distribution measured by X-ray di raction
    methods and near-surface microstructural observations by scanning electron microscopy. The applied
    severe shot peening increased the fatigue limit by 11%, however, the positive e ect was recorded
    only for the loading amplitudes corresponding to the fatigue lifetimes in the range 107–109 cycles.
    At higher loading amplitudes, the fatigue properties tended to decrease, most likely due to accelerated
    fatigue crack initiation on the surface damage features created by the peening process and also by
    rapid residual stress relaxation.
    WorkplaceInstitute of Physics of Materials
    ContactYvonna Šrámková, sramkova@ipm.cz, Tel.: 532 290 485
    Year of Publishing2021
    Electronic addresshttps://www.mdpi.com/2075-4701/10/9/1262
Number of the records: 1  

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