The high-cycle fatigue fracture mechanism and fatigue strength prediction of compacted graphite iron

The tensile properties, high-cycle fatigue (HCF) properties and corresponding fatigue fracture mechanism of compacted graphite iron (CGI) were investigated. It is found that the tensile strength, yield strength and fatigue strength of CGI decrease as the temperature increases. At 25 degrees C, the fatigue cracks of CGI are mainly caused by local cleavage fracture at ferrite around the tip of vermicular graphite. At 400 degrees C and 500 degrees C, the gradual occurrence of grain boundary softening and oxidation may reduce the difficulty of fatigue crack propagation. Similar to temperature, the change of microstructure content also has a significant effect on the fatigue properties of CGI. By analyzing the damage characteristics of fatigue fracture morphology, it is shown that the fatigue crack initiation of CGI is mainly dependent on the damage localization caused by the ferrite and vermicular graphite inside the graphite cluster and the pearlite and spheroidal graphite outside the graphite cluster under cyclic loading. Based on those results, a fatigue strength prediction model associated with tensile strength, yield strength and microstructure area percentage was proposed. This model can provide a reasonable prediction of HCF strength of CGI at different temperatures.

Automated summary

This study investigated the tensile properties, high-cycle fatigue (HCF) properties, and corresponding fatigue fracture mechanism of compacted graphite iron (CGI). It was found that the tensile strength, yield strength, and fatigue strength of CGI decrease with increasing temperature. Fatigue cracks in CGI at 25 degrees C primarily result from local cleavage fracture in the ferrite around the tip of the vermicular graphite. At 400 degrees C and 500 degrees C, the gradual occurrence of grain boundary softening and oxidation may reduce the difficulty of fatigue crack propagation. The change in microstructure content also significantly affects the fatigue properties of CGI. Based on the analysis of fatigue fracture morphology, fatigue crack initiation in CGI mainly depends on damage localization caused by ferrite and vermicular graphite within the graphite cluster, as well as pearlite and spheroidal graphite outside the graphite cluster under cyclic loading. A fatigue strength prediction model associating tensile strength, yield strength, and microstructure area percentage was proposed, which provides a reasonable prediction of HCF strength of CGI at different temperatures.