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Analysis of isothermal forging process and mechanical properties of complex aluminum forging for aviation 被引量:2
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作者 胡建良 易幼平 黄始全 《Journal of Central South University》 SCIE EI CAS 2014年第7期2612-2616,共5页
Large complex 7A85 aluminum wing-body joint was forged employing isothermal forging process and its mechanical properties were studied.The tensile strength after forging is up to 587.5 MPa in longitudinal direction,15... Large complex 7A85 aluminum wing-body joint was forged employing isothermal forging process and its mechanical properties were studied.The tensile strength after forging is up to 587.5 MPa in longitudinal direction,15% higher than that using free forging.Moreover,the tensile strength of the forging is almost the same in three directions.Isothermal forging also performs well on overall fracture toughness,with a maximum value of 39.8 MPa·m1/2,and that of short transverse direction all reaches 36 MPa·m1/2 and above,with a maximum relative error of only 3.6%.The results indicate that the isothermal forging leads to better performance as well as higher uniformity in mechanical properties. 展开更多
关键词 aviation forging isothermal forging process UNIFORMITY fracture toughness
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