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首页> 外文期刊>International Journal of Fatigue >Localized cyclic deformation and corresponding dislocation arrangements of polycrystalline Ni-base superalloys and pure Nickel in the VHCF regime
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Localized cyclic deformation and corresponding dislocation arrangements of polycrystalline Ni-base superalloys and pure Nickel in the VHCF regime

机译:VHCF态下多晶镍基高温合金和纯镍的局部循环形变及相应的位错排列

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摘要

Knowledge about the fatigue behaviour of metallic materials in the range of very high cycle fatigue (VHCF, N > 10~7) is a key factor to improve the safety against failure of component parts. Even in the conventional field of application of nickel-base alloys (e.g. turbine blades) superimposed high frequency loading requires a safe life at very high number of cycles. Thus, the fatigue behaviour of structural materials in the very high cycle regime has become an important and active subject of research. In this paper, polycrystalline nickel-base alloys (Nimonic 80A and Nimonic 75) and pure Nickel (wavy slip character) were investigated in the VHCF regime by varying the precipitation conditions (peak-aged, overaged and precipitation-free), dislocation slip behaviour and test frequency. In addition, mechanisms of fatigue failure in the VHCF regime were compared to conventional damage evolution (in the LCF and HCF region) on the basis of load-controlled low frequency tests. Surprisingly the overaged condition of Nimonic 80A shows a slightly higher fatigue strength in the VHCF regime as compared to the peak-aged condition. The results obtained document that fatigue failure can still occur beyond 107 cycles. Transmission electron microscopy (TEM) was carried out, in order to characterize the influence of microstructure, the resulting dislocation slip behaviour and the relevant dislocation particle interaction mechanism. Studies of the development of slip markings on surface grains were performed mainly using scanning electron microscopy (SEM).
机译:了解金属材料在极高周期疲劳(VHCF,N> 10〜7)范围内的疲劳行为,是提高零件失效安全性的关键因素。即使在镍基合金(例如涡轮叶片)的常规应用领域中,叠加的高频负载也需要在非常高的循环次数下的安全寿命。因此,结构材料在非常高的循环状态下的疲劳行为已成为重要而活跃的研究课题。在本文中,通过改变沉淀条件(峰时,过时效和无沉淀),位错滑移行为,研究了VHCF态的多晶镍基合金(Nimonic 80A和Nimonic 75)和纯镍(波浪滑移特性)。和测试频率。此外,在负载控制的低频测试的基础上,将VHCF方案中的疲劳失效机制与常规损伤演变(在LCF和HCF区域)进行了比较。令人惊讶的是,与峰值时效相比,VHCF方案中Nimonic 80A的时效过高显示出稍高的疲劳强度。所获得的结果证明,疲劳失效仍然可能发生超过107个循环。为了表征微观结构,所产生的位错滑移行为和相关的位错粒子相互作用机理,进行了透射电子显微镜(TEM)。主要使用扫描电子显微镜(SEM)进行了表面晶粒上滑痕的发展研究。

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