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다양한 절삭이송속도로 가공한 A1 7075-T6 소재의 쇼트피닝 전후 피로수명에 관한 연구
김형태,이재헌,신기훈,노승남,서성원 서울産業大學校 2005 논문집 Vol.54 No.1
Aluminum alloy 7075-T6 is ideally used for highly stressed parts such as aircraft components because of its excellent strength to weight ratio. This paper presents a study on the effect of feedrate changes on the fatigue life of A1 7075-T6 specimens before and after shotpeening. For this purpose, five groups of specimens, each of which consists of eight specimens, were first machined at five different feedrates (0.05, 0.10, 0.15, 0.20 0.25mm/rev). Half of eight specimens in each group were then peened and the others remained un-peened. Finally, the fatigue life of each specimen was measured by using 4-point rotatry bending machine. In this paper, comparison of fatigue life among ten sets of specimens is presented. One observation is that the fatigue life of unpeened specimens are inversely proportional to the feedrates. On the other hand, the fatigue life of peened specimens are similarly improved regardless of feedrates except 0.05. Based on the results, it is concluded that shotpeening may improve the fatigue life of Aluminium alloy regardless of feedrates. Therefore, machining productivity may also be increased by choosing higher feedrates for structural conponents that need to be strain-hardened by shotpeening after machining