Affiliation:
1. School of Aircraft Engineering Nanchang Hangkong University Nanchang China
2. Air Force Armament Division Equipment Department of China PLA Air Force Beijing China
3. Engineering Research Center of Aero‐engine Technology for General Aviation Ministry of Education Nanchang China
Abstract
AbstractIn this paper, the thickness debit and stress concentration effects of a nickel‐based directionally solidified superalloy were investigated through strain‐controlled low cycle fatigue (LCF) and creep–fatigue interaction (CFI) experiments. Compared to the fatigue lives of solid specimens provided in the existing literature, the results of this paper indicate that when the wall thickness of the specimen is reduced from 5 to 1.125 mm, the fatigue life with different strain amplitudes decreases by about 45%. When film‐cooling holes (FCHs) are introduced into the hollow specimens, the fatigue life is further reduced by about 25%. Based on the observation of the scanning electron microscope (SEM), the formation mechanisms of the thickness debit and stress concentration effects under LCF and CFI loads were revealed. Subsequently, two parameters, the “wall‐thickness coefficient” and “hole coefficient,” were proposed to establish a new fatigue life prediction method.
Funder
National Science and Technology Major Project