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  • 标题:人工海水中における造船用鋼板の長寿命腐食疲労強度の検討
  • 本地全文:下载
  • 作者:小林 佑規 ; 田中 義久 ; 後藤 英信
  • 期刊名称:日本造船学会論文集
  • 印刷版ISSN:0514-8499
  • 电子版ISSN:1884-2070
  • 出版年度:1998
  • 卷号:1998
  • 期号:183
  • 页码:383-390
  • DOI:10.2534/jjasnaoe1968.1998.383
  • 出版社:The Japan Society of Naval Architects and Ocean Engineers
  • 摘要:

    In order to evaluate precisely the life and residual-life time of ship structures, it is essential to examine the S/N relationships of their fatigue strengths. The long term corrosion fatigue behaviors, however, have not been fully investigated yet. In the present study, we have measured the corrosion rates and the fatigue crack growth rates of a 500 MPa class steel plate in synthetic seawater, and discussed the long term corrosion fatigue strength obtained under a cyclic frequency of 0.17 Hz within stress ranges less than the fatigue limit tested in air. The results obtained are as follows. (1) The corrosion rate, Rc , in an immersion test was 0.07 and 0.09mm/year for a polished and shotblasted surfaces of the plate, respectively. The effect of the stress increase in corrosion wastage cannot be neglect in the corrosion fatigue tests exceeding five years under the cyclic frequency of 0.17 Hz. (2) The crack growth rate measured in seawater was two to three times larger than that in air in the range where Paris equation may hold. The effect of the environment on a crack growth rate is significant in the range where the crack intensity factor is relatively low. (3) The range of the threshold stress intensity factor, Δ Kth , is 2.5 and 1.2 MPa m1/2 in air and in seawater, respectively. (4) The long term corrosion fatigue strength can be calculated roughly from the empirical equation.Δ K = f ( Rc , y ) CcNnc , where f ( Rc , y ) is the corrosion wastage rate estimated from the corrosion rate of material and year, Nc is crack initiation life, n is the index given by crack growth rate, and Cc is a constant obtained from the corrosion fatigue tests of about 106 cycles. (5) For the long term corrosion fatigue, according to the results of Komai and coauthor, no fatigue cracks initiate from the corrosion pits after 14 to 24 years in the plate specimen area of 320 mm2 with Rc =0.09 mm/year, and the pits move to the progression of corrosion wastage in corrosion fatigues less than Δ KCF . (6) In order to decide the f ( Rc , y ) during corrosion fatigue, the tests through five years are necessary.

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