This study investigates the fretting wear and fatigue behavior of aluminum alloy–steel connections fastened using type II ring groove rivets under tension loading. It includes fatigue testing, fretting wear and fatigue analysis, and subsequent fatigue strength prediction. Experimental results reveal that fatigue cracks initiate at the edge of the prefabricated hole in the aluminum alloy plate, accompanied by severe fretting wear at the interface between the rivet and the aluminum alloy plate. A finite element model was developed to analyze the contact status and stress distribution within the riveted structure. The actual clamping force was determined by comparing the contact status of the clamped plates observed experimentally and in simulations. Results indicate that the clamping force significantly decreases from its initial value during the test, leading to a reduction in the fatigue strength of the riveted structure. Additionally, the fatigue crack initiation location shifts from the length to the width direction of the aluminum plate, and from a location distant from the prefabricated hole to the hole edge. As tensile stresses govern the crack initiation, the SWT criterion, when accounting for clamping force loss, accurately identifies fatigue crack initiation sites in riveted connection, with a fatigue strength prediction error of 15 %.
扫码关注我们
求助内容:
应助结果提醒方式:
