• Title/Summary/Keyword: Dewpoint Corrosion

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A Study on Stress Corrosion Cracking Evaluation with Material Degradation of High Temperature Components (고온부재의 재질열화에 따른 응력부식균열 평가에 관한 연구)

  • Park, Jong-Jin;Yu, Ho-Seon;Jeong, Se-Hui
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.20 no.4
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    • pp.1123-1132
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    • 1996
  • It has been reported that high temperature structural components represent the phenomenon of material degradation according to a long term service under high temperature and pressure. Especially, fossile power plant components using the fossil fuel and heavy oil are affected by dewpoint corrosion of $H_2SO_4$produced during a combustion. Therefore, the service materials subjected to high temperature and pressure may occur the stress corrosion cracking. The object of this paper is to investigate SCC susceptibility according to the material degradation of the high temperature structural materials in dewpoint corrosive environment-$H_2SO_4$.The obtained results are summarized as follows : 1) In case of secondary superheater tube, the fractograph of dimple is observed at the concentration of $H_2SO_4$-5%. When the concentration of $H_2SO_4$ is above 10%, the fracture mode is shifted from a transgranular fracture to an quasi-intergranular fracture according to the increment of concentration. 2) In the relationship between [$\Delta$DBTT]$_sp$ and SCC susceptibility, it is confirmed that the greater material degradation degree is, the higher SCC susceptibility is. In addition, it can be known that SP test is useful test method to evaluate SCC susceptibility for high temperature structural components. 3) When [$\Delta$DBTT]$_sp$ is above 17$17^{\circ}C$ the SCC fracture behavior is definitely observed with SCC susceptibility of above 0.4.

A mechanical proprties and fatigue life of aluminum alloy sheets for autobodies (자동차 차체용 알루미늄 합금 판재의 기계적특성과 부식피로수명)

  • 박인덕;윤옥남;남기우
    • Journal of Ocean Engineering and Technology
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    • v.11 no.2
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    • pp.57-69
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    • 1997
  • The objetive of this study is to compare the mechanical proprties of 6000 series Al-Mg-Si aluminum alloy (AC120) with 5000 series Al-Mg aluminum alloy (TG25), and to investigate the influence of corrosion solution for fatigue life. Comparing of TG25 and AC120 alloy sheets, TG25 alloy sheets showing higher plastic ratio and total elongation have better formability than AC120 alloy sheets. The hardness of nugget area was a little higher than that of base metal area. Also, grain coarsening was observed in HAZ(Heat Affected Zone). In a corrosion fatigue experiment, the fatigue life decreased as concentration increased, when a dipping time was constant. The life decreased as dippling time increased, when a concentration was constant.

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