Fatigue crack propagation of the gradient surface-modified layer of high-strength steel

A gradient modified layer can be produced on the high-strength steel surface by carburizing heat treatment. In this study, microstructure characterization and fatigue crack propagation test were carried out on the gradient surface-modified layer of the 18CrNiMo7-6 high-strength steel. With increasing depth of the surface-modified layer, the yield strength and the kernel average misorientation value decrease, and the equivalent grain size of the slatted martensite structure and the number of the large-angle boundaries increase. The orientation difference angle of the point to point pre-and post-fatigue at the crack of the transition layer and the matrix layer increases from less than 2 degrees to approximately 10 degrees and about 4 degrees, respectively. With the increase of the depth of the surface-modified layer, the degree of deformation inside the martensitic packet decreases, while the extent of macroscopic deformation of the material increases. Deformation occurs inside the martensitic packet at the main crack, and there is essentially no deformation inside the martensite packets away from the main crack. On both sides of the main crack, a large number of extrusions parallel to the martensitic lath appear. The large-angle boundaries of the original austenite grain boundary and martensite boundary hinder the propagation of the fatigue crack.

Automated summary

A gradient modified layer can be produced on the high-strength steel surface by carburizing heat treatment. Increasing the depth of the surface-modified layer leads to a decrease in yield strength and kernel average misorientation value, as well as an increase in equivalent grain size and the number of large-angle boundaries. Deformation occurs inside the martensitic packet, while the large-angle boundaries hinder the propagation of the fatigue crack.