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阳极化对航空铝合金疲劳性能的影响 被引量:22

Effect of Anodizing on Fatigue Performance of Aeronautic Aluminum Alloys
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摘要 采用S-N曲线研究硫酸阳极化、铬酸阳极化和硼酸硫酸阳极化对航空铝合金疲劳极限的影响。结果表明,对包铝的铝合金,不同阳极化试样的疲劳极限差别很小,对于铝合金基材,硫酸阳极化明显降低材料的疲劳极限,铬酸阳极化使材料的疲劳极限下降,而硼酸-硫酸阳极化不降低材料的疲劳极限。并对造成上述现象的原因进行了讨论。 The effect of sulfuric acid, chromate acid and boric/sulfuric acid anodizing on fatigue performance of aeronautic aluminum alloys was studied by using S-N curve. The results illustrated that, different anodized cladding aluminum alloys had almost same fatigue limits ; however, suffutrie acid anodizing greatly decreased fatigue limits of aluminum alloys, chromate acid also decreased fatigue limits of materials; boric/sulfuric acid anodizing did not decrease fatigue limits of aluminum alloys. The reason of above results was discussed.
出处 《航空材料学报》 EI CAS CSCD 2007年第2期25-28,共4页 Journal of Aeronautical Materials
关键词 铝合金 阳极化 疲劳极限 硼酸-硫酸阳极化 S-N曲线 aluminum alloy anodizing fatigue limit boric/sulfuric acid anodizing S-N curve
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参考文献4

  • 1ZHANG L,THOMPSON G E,SMITH C J E,et al.Boric/sulphuric acid anodizing of 2024 and 7075 aluminum alloys:film growth and corrosion resistance[J].Corrosion,1999,55:1052-1061.
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  • 3BAC 5884D,Anodizing of aluminum alloys[S].1995.
  • 4HB5287-96.金属材料轴向加载疲劳试验方法[S].[S].,..

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