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Investigation on Nickel base superalloy steam turbine bolts fractured at high temperatures, a case history

机译:镍基高温合金汽轮机螺栓在高温下断裂的案例研究

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Ni-base superalloys have been often used as material for bolts of the steam turbine valvesrnand of the steam admission areas of the turbine casings, thanks to their high-temperaturernresistance properties. In order to withstand high creep and fatigue loading these alloys arernstrengthened by u0001’ and/or u0001” precipitates.rnAmong them, the most used are Incoloy 901, Refractalloy 26, Inconel X750, Nimonic 80Arnand Nimonic 90 (PER 2 B). Although these alloys are designed specifically for employingrnin high temperature applications (up to 600 ℃) some brittle intergranular cracking havernbeen observed to be a consequence of high temperature exposure and high tensile loads.rnIn the present paper a case study on some fractured Refractalloy 26 bolts, after aboutrn31.000 h service at 600℃ has been reported.rnMechanical and microstructural analysis have been performed on fractured, as-receivedrnand serviced (not fractured) bolts. Fractographic analysis have shown an intergranularrnbrittle fracture in all the fracture surface. SEM observations of secondary cracks havernrevealed an oxides penetration at grain boundary without evidence of impurities from thernenvironment other than oxygen. A moderate microstructural degradation of used andrnfractured bolts have been highlighted by the presence of “eta” phase. Nevertheless, thisrnkind of microstructural degradation seems not to be responsible of the observed fracturernboth because the tensile tests on as-received and exercised samples have not shownrnsignificant differences and because the eta phase has not been observed in the regionrnclose to the cracks.rnMoreover, no creep-induced microstructural damages (such as grain boundariesrnmicrovoids) have been observed in failured and serviced samples.rnFrom all the experimental evidence, the most probable governing failure mechanism is thernStress Accelerated Grain Boundary Oxidation (SAGBO), the only one compatible with thernintergranular brittle appearance of fracture surface and the presence of oxygen penetrationrnat grain boundaries in regions close to the fracture surface.
机译:镍基高温合金由于其耐高温性能,经常被用作汽轮机阀门螺栓和汽轮机壳体蒸汽入口区域的材料。为了承受高蠕变和疲劳载荷,这些合金通过u0001'和/或u0001“沉淀物进行强化。其中,最常用的是Incoloy 901,Refractalloy 26,Inconel X750,Nimonic 80Arn和Nimonic 90(PER 2 B)。尽管这些合金是专为在高温(高达600℃)中使用而设计的,但观察到一些脆性的晶间开裂是由于暴露于高温和高拉伸载荷引起的。在本文中,我们对一些断裂的Refractalloy 26螺栓进行了案例研究,据报道在600℃下约31.000 h服役后。rn对断裂,按接收和使用(未断裂)的螺栓进行了机械和微观结构分析。分形分析表明,在所有断裂面均存在晶间脆性断裂。 SEM观察到的二次裂纹已揭示出氧化物在晶界的渗透,没有证据表明环境中的杂质不是氧。 “ eta”相的存在突出了使用过的和未断裂的螺栓的适度微观结构退化。然而,这种微观结构的退化似乎与观察到的断裂无关,这是因为在接受和运动的样品上进行的拉伸试验没有显示出显着的差异,并且因为在靠近裂纹的区域内未观察到η相。在失效和维修后的样品中观察到了由金属引起的微结构损伤(例如晶界或微孔)。从所有实验证据来看,最可能的控制失效机理是应力加速晶粒边界氧化(SAGBO),它是唯一与晶界脆性相兼容的材料。断裂面和在靠近断裂面的区域存在氧渗透性晶界。

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