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Fatigue properties of B1914 superalloy at high temperatures

机译:B1914高温合金的高温疲劳性能

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B1914 is a nickel-based superalloy with an increased amount of B (boron) and C (carbon) to reach an adequate amount of borides and carbides in the cast structure ensuring improved creep properties. However, the influence of the structure on the material high-cycle fatigue properties is not sufficiently described. The present study brings the experimental results on the high-cycle fatigue properties of a cast polycrystalline nickel-based boron-rich B1914 superalloy, obtained at temperatures of 800, 900 and 950°C. The cast superalloy was processed by hot isostatic pressing (HIP) to diminish the casting defects. The fatigue tests were performed in symmetrical loading in laboratory air. The fracture surfaces of the specimens were studied by scanning electron microscopy in order to describe the influence of temperature on the fatigue crack initiation and propagation. Change of the primary fatigue crack propagation mechanism from the crystallographic to the non-crystallographic mechanism was observed with increasing temperature. Decrease of a material lifetime and decrease of the fatigue endurance limit due to the increasing testing temperature was observed.
机译:B1914是一种镍基高温合金,其B(硼)和C(碳)含量增加,以在铸造结构中达到足够数量的硼化物和碳化物,确保改善蠕变性能。然而,结构对材料高周疲劳性能的影响尚未充分描述。本研究提供了在800、900和950°C温度下获得的铸造多晶镍基富硼B1914高温合金高周疲劳性能的实验结果。铸造高温合金通过热等静压(HIP)处理,以减少铸造缺陷。疲劳试验在实验室空气中的对称载荷下进行。为了描述温度对疲劳裂纹萌生和扩展的影响,用扫描电子显微镜研究了试样的断口。随着温度的升高,主要的疲劳裂纹扩展机制从晶体学机制转变为非晶体学机制。观察到由于试验温度升高,材料寿命降低,疲劳极限降低。

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