A Review of Low Cycle Mechanical Fatigue Life Models for Nickel-based Single Crystal Superalloy
LI Piao1, YAO Weixing1,2
1 Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China 2 State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract: The turbine blades of advanced power propulsion systems such as aeroengines have long been serving in high temperature, high pressure and high centrifugal force working environment, which requires high performance of blade materials. Common polycrystalline alloys have grain boundaries, which are relatively fragile. Cracks tend to grow at and propagate along grain boundaries. The nickel-based single crystal alloys, developed with directional solidification process, have been used as turbine blade materials for a long time with their elevated temperature strength, good creep and fatigue resistance and excellent thermal stability resulted from the elimination of grain boundary. Fatigue damage of nic-kel-based single crystal material is an important factor that directly affects the service life of blades. The assessment of fatigue damage depends on reasonable and effective fatigue life models. The research of fatigue model of nickel-based single crystal materials concerns a wide range of studies. On the one hand, the working environment of nickel-based single crystal material is complex. The fatigue problems occurring during service include mechanical fatigue, thermal fatigue, thermomechanical fatigue and creep fatigue. On the other hand, the anisotropy of the single crystal material itself leads to the anisotropy of fatigue properties. The orientation deviation caused in casting determines that the actual orientation of the single crystal material is not the preferred orientation of material properties. At present, researchers mainly study the fatigue life models by focusing on the complex fatigue states caused by complex environment and the anisotropy of crystal itself. In view of the complex fatigue states, the current fatigue models extend basic mechanical fatigue to various fatigue research directions. There is no widely applicable model with clear fatigue mechanism. The research of mechanical fatigue model still plays an important role. In the research of material anisotropy, scholars have proposed different ways to deal with the anisotropic fatigue properties, such as the widely recognized orientation parameter models based on single crystal modulus anisotropy. This kind of model is suitable for engineering application because of its simplicity, meanwhile the evaluation of their predictive ability is still absent. Since the complex fatigue states cover a wide range, this paper focuses only on low cycle mechanical fatigue. The basic low-cycle mechanical fatigue models of nickel-based single crystal superalloys are sorted and classified into two categories: macroscopic damage parameter model and micro-damage parameter model according to the definition of fatigue damage parameters. The modeling mechanisms of various models are discussed. 11 sets of fatigue test data of five kinds of nickel-based single crystal materials were collected to evaluate the typical models, looking forward to providing insights in further study of the fatigue life model of nickel-based single crystals.
李飘, 姚卫星. 镍基单晶合金低周机械疲劳寿命模型评述[J]. 材料导报, 2020, 34(9): 9124-9131.
LI Piao, YAO Weixing. A Review of Low Cycle Mechanical Fatigue Life Models for Nickel-based Single Crystal Superalloy. Materials Reports, 2020, 34(9): 9124-9131.
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2020, Vol. 34 
