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对GC-4(40CrMnSiMoVA)钢在空气与3.5%NaCl中性溶液中腐蚀疲劳裂纹扩展(CFCG)的单次超载与周期超载效应进行了试验性研究.结果表明,CFCG超载迟滞效应由快速撕裂过程,迟滞过程和恢复过程组成.对于周期超载,当两次超载周次之间裂纹扩展长度ad远小于超载塑性区尺寸rpOL与恒载塑性区尺寸rpCLA之差,即ad<<rpOL-rpCLA时,CFCG会发生比空气疲劳时还强烈的超载迟滞效应.而当ad>rpOL-rpCLA时,会发生超载加速效应.断口分析表明,当ad<<rpOL-rpCLA时,CFCG不会发生超载撕裂,而当ad>rpOL-rpCLA时,会发生显著的超载撕裂.上述试验的宏观规律与断口特征均验证了前文所建立的CFCG超载效应的定量描述模型.

Experimental studies were conducted on the effects of single and periodic overloading oh corrosion fatigue crack growth (CFCG) in the two commonly used environments, air and 3.5% NaCl neutral solution,for GC-4 (40CrMnSiMoVA) steel. Test results show that the whole process of the effect of overloading on CFCG involves three phases in time sequence: the fast tearing, the retardation, and the recovery. For periodic overloading tests, if the crack length, ad, grown during the interval of two overloading cycles were far smaller than the difference between the overloading plastic region size, rpOL, and the constant plastic region size rpCLA, i.e. ad <

参考文献

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[4] 路民旭,郑修麟.中国腐蚀与防护学报,1994,14(2)2路民旭,刘晓坤,王建军,郑修麟.航空学报,1990,11(12):B617-B6213王建军.刘晓坤,路民旭.航空学报,1988,9(13):S140-S1434ZuidemaJ
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