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Thermal Fatigue Behavior of Ni_3Al Based Superalloy IC6E
作者姓名:JI Lei*  LI Shu-suo  HAN Ya-fang  JIANG Li-wu School of Materials Science and Engineering  Beijing University of Aeronautics and Astronautics  Beijing  China
作者单位:JI Lei*,LI Shu-suo,HAN Ya-fang,JIANG Li-wu School of Materials Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China
摘    要:The thermal fatigue behavior of Ni3Al based superalloy IC6E during the cycles between 900 ℃/1 000 ℃ and the room tempera-ture was investigated. The experimental results indicate that the primary and secondary thermal fatigue cracks initiate inside or round the borides and then spread away along grain boundaries and/or in interdendritic areas. The fracture of borides and their separation from the matrix at interfaces are mainly responsible for the crack initiation and its spreading. At temperatures higher than 1 000 ℃, the grain boundary oxidation combined with cyclic stresses accelerates the crack growth.


Thermal Fatigue Behavior of Ni3Al Based Superalloy IC6E
JI Lei*,LI Shu-suo,HAN Ya-fang,JIANG Li-wu School of Materials Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing ,China.Thermal Fatigue Behavior of Ni_3Al Based Superalloy IC6E[J].Chinese Journal of Aeronautics,2006,19(Z1).
Authors:JI Lei  LI Shu-suo  HAN Ya-fang  JIANG Li-wu
Abstract:The thermal fatigue behavior of Ni3Al based superalloy IC6E during the cycles between 900 ℃/1 000 ℃ and the room temperature was investigated. The experimental results indicate that the primary and secondary thermal fatigue cracks initiate inside or round the borides and then spread away along grain boundaries and/or in interdendritic areas. The fracture of borides and their separation from the matrix at interfaces are mainly responsible for the crack initiation and its spreading. At temperatures higher than 1 000 ℃, the grain boundary oxidation combined with cyclic stresses accelerates the crack growth.
Keywords:Ni3Al  thermal fatigue  cast superalloy
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