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涡轮盘用新型GH4975合金拉伸变形机制与温度的关联性
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1.中国科学院金属研究所 师昌绪先进材料创新中心高温结构材料研究部;2.中国航发沈阳黎明航空发动机有限责任公司

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辽宁省科技重大专项 (No. 2024JH1/11700037), 国家科技重大专项项目 (No. J2019-VI-0006-0120), 中科院先导C类专项 (No. XDC0140000), 中国科学院青年创新促进会会员资助项目 (No. 2023202), 辽宁省自然科学基金面上项目 (No. 2023-MS-024), 新材料专项 (No. 2024ZD0600600).辽宁省中国科学院金属研究所创新No.2023-PY08.


Temperature dependence of tensile deformation mechanism of GH4975 alloy for turbine disk
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Major Science and Technology Projects of Liaoning Province (No. 2024JH1/11700037), National Science and Technology Major Special Project (No. J2019-VI-0006-0120), Chinese Academy of Sciences Pilot C Special Project (No. XDC0140000), China Academy of Sciences Youth Innovation Promotion Association Member Support Project (No. 2023202), Liaoning Province Natural Science Foundation General Project (No. 2023-MS-024), New Materials Special Project (No. 2024 ZD0600600), the Innovation Program of Institute of Metal Research, Chinese Academy of Sciences (No. 2023-PY08).

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    摘要:

    采用了光学显微镜(OM)、扫描电子显微镜(SEM)、透射电子显微镜(TEM)等手段研究了GH4975合金从室温到1100℃之间的拉伸性能、变形机制及断裂行为。结果表明,该合金的变形机制由低温下的强耦合位错对剪切,转变至中温时的层错、微孪晶共同作用,当温度高于850℃后,位错绕过机制开始启动并随温度的升高逐渐主导位错运动。温度较低时碳化物裂纹主导了合金的开裂,随温度升高,晶界强度降低,晶界率先开裂成为裂纹源。晶界强度的降低和位错绕过机制的启动是合金高于800℃后强度迅速下降的主要原因。

    Abstract:

    The tensile properties, deformation mechanism, and fracture behavior of the GH4975 superalloy, were investigated using optical microscopy (OM), scanning electron microscopy (SEM), electron backscatter diffraction (EBSD), transmission electron microscopy (TEM), and other advanced characterization techniques. The results show that the deformation mechanism of the alloy transitions from strong coupling dislocation shear at low temperatures to stacking fault and microtwin formation at intermediate temperatures. At temperatures higher than 850 °C, the dislocation bypass mechanism is activated and gradually dominates the dislocation movement with increasing temperature. Carbide cracking dominates the failure of the alloy at low temperatures. As the temperature increases, the grain boundary strength decreases, leading to grain boundary cracks becoming the primary crack sources. At temperatures above 800 °C, the reduction in grain boundary strength and the activation of the dislocation bypass mechanism are the primary reasons for the rapid decline in alloy strength.

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邰文彬,张瑞,伍晶晶,周子荐,崔传勇,周亦胄,孙晓峰.涡轮盘用新型GH4975合金拉伸变形机制与温度的关联性[J].稀有金属材料与工程,,().[TaiWenbin, ZhangRui, WuJingjing, ZhouZijian, CuiChuanyong, ZhouYizhou, SunXiaofeng. Temperature dependence of tensile deformation mechanism of GH4975 alloy for turbine disk[J]. Rare Metal Materials and Engineering,,().]
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  • 收稿日期:2025-01-19
  • 最后修改日期:2025-04-08
  • 录用日期:2025-04-21
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