摘要
测试了2124铝合金TL与LT取向疲劳裂纹扩展门槛值,提出了用疲劳裂纹失稳扩展阶段最后十个循环中的最大值来估算2124铝合金TL与LT取向的断裂韧度K′C的方法,并将其与Forman公式预测的断裂韧度Kc值进行对比。结果表明:K′C与Kc值结果相近,误差分散度小;将K′C值代入全范围疲劳裂纹扩展速率表达式中,对2124铝合金TL和LT取向试验数据进行计算,预测结果与试验结果较好吻合。
Fatigue crack growth threshold values of 2124 aluminum alloy in TL and LT directions were tested.A method was proposed to estimate fracture toughness K′Cof 2124 aluminum alloy in TL and LT directions by the maximum load in last 10 cycles in the instable expansion stage of fatigue cracks.The estimated K′C were compared with fracture toughness KCpredicted using forman formula.The results show that the values of K′C were close to the values of KC,and the error dispersion was small.Fracture toughness K′Cvalues were brought into the full range fatigue crack growth rate expression to calculate the experiment data of 2124 Al alloy in TL and LT directions,and predicted results were fitted well to the experimental results.
出处
《机械工程材料》
CAS
CSCD
北大核心
2014年第12期105-108,共4页
Materials For Mechanical Engineering
关键词
断裂韧度
裂纹扩展
估算方法
fracture toughness
crack growth
estimation method
