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Corrosion Fatigue Crack Propagation Behaviour of a High Strength Low Alloy Steel in a Synthetic Sea Water Environment.

机译:高强度低合金钢在合成海水环境中的腐蚀疲劳裂纹扩展行为。

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摘要

The corrosion fatigue crack propagation behaviour of a highstrength low alloy steel, N-A-XTRA 70, in a synthetic seawater solution was tested using S. E. N. specimens subjectedto a loading frequency of 0.1 Hz and a load ratio of 0.6.In order to simulate the conditions encountered by a thumbnailtype crack several specimens from each of themicrostructural types tested, namely parent plate, heataffected zone and heat treated material, had their cracksides covered by transparent plastic covers. Severe overprotectionand slight underprotection conditions wereproduced using cathodic protection potentials of -1400,-1300, -1200 and -700 mV (S. C. E. ).The Paris relationship da/dN = CLKm was found to be a usefultool in describing the crack propagation rate data. Resultsobtained, presented in the form of plots of log da/dN againstlog AK, show that for parent plate, H. A. Z. and heat treatedmaterial, covering the crack sides of specimens producesenhanced corrosion fatigue crack propagation rates, atcathodic protection potentials of -1400 and -1300 mV (S. C. E. ),when compared to non covered specimens. This trend was alsotrue for H. A. Z. specimens at a potential of -700 mV (S. C. E. ).For parent plate specimens, however, covering the crack sidesat a potential of -700 mV (S. C. E. ) produced reduced crackpropagation rates over non covered specimens. It is believedrestriced oxygen access may account for these results.Plots of the Paris exponent m and constant C for the threemicrostructures tested produced three lines of the formm= alnC +b where a and b were found to be dependent uponmaterial parameters.Comparison of results with BS 4360: 50D revealed that N-A-XTRA70 exhibited superior fatigue performance when tested in airbut behaved worse under conditions of free corrosion.
机译:使用SEN样品测试了高强度低合金钢NA-XTRA 70在合成海水溶液中的腐蚀疲劳裂纹扩展行为,其载荷频率为0.1 Hz,载荷比为0.6。缩略图状裂缝,来自每个测试的微观结构类型的几个样本,即母板,热影响区和热处理材料,其裂缝的一面被透明塑料盖覆盖。使用-1400,-1300,-1200和-700 mV(S.C.E.)的阴极保护电位会产生严重的过度保护和轻微的欠保护条件。巴黎关系da / dN = CLKm是描述裂纹扩展速率数据的有用工具。以log da / dN对log AK的曲线图形式获得的结果表明,对于母板,热影响区和热处理材料,覆盖样品的裂纹面会产生增强的腐蚀疲劳裂纹扩展速率,阴极保护电位为-1400和-1300 mV (SCE),与未覆盖的标本相比。对于H.A.Z.试样在-700 mV(S.C. E.)的电位也是如此,但是对于母板试样,在-700 mV(S.C. E.)的电位下覆盖裂纹面会导致未覆盖试样的裂纹扩展速率降低。相信限制的氧气进入可能是这些结果的原因。测试的三个微观结构的巴黎指数m和常数C的图产生了三条式,即formm = alnC + b,其中a和b取决于材料参数。 BS 4360:50D揭示了NA-XTRA70在空气中测试时表现出优异的疲劳性能,但在自由腐蚀条件下表现更差。

著录项

  • 作者

    Millar Peter G.;

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  • 年度 1986
  • 总页数
  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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