首页|缺口取向及温度对第三代单晶高温合金DD33热疲劳行为的影响

缺口取向及温度对第三代单晶高温合金DD33热疲劳行为的影响

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使用OM、SEM和EDS等手段,研究了第三代镍基单晶高温合金DD33不同V型缺口取向([100]、[210]和[110])片状试样从室温到不同上限温度(1000℃、1100℃和1200℃)的热疲劳过程中裂纹的萌生和扩展行为.结果表明,在三种上限温度,DD33合金的热疲劳性能均出现明显的各向异性.在三个上限温度[100]取向试样均表现出最好的热疲劳性能;上限温度为1000℃和1200℃[110]取向试样的热疲劳性能最差,上限温度为1100℃[210]取向试样的热疲劳性能最差.不同取向试样的热疲劳裂纹的萌生和扩展行为,均呈现出一定的晶体学取向规律.热应力、氧化以及滑移系的开动,导致不同取向试样裂纹的扩展速率不同.
Effect of Notch Orientation and Temperature on Thermal Fatigue Behavior of a Third-Generation Single Crystal Superalloy DD33
The crack initiation and propagation behavior of a third-generation single crystal superal-loy DD33 with V-notches of different orientations([100],[210]and[110])during thermal fatigue tests:sam-ples were hold at different high-temperatures(1000℃,1100℃ and 1200℃ respectively)for 60 s and then quick quenching into water as one cycle,was investigated by OM,SEM and EDS.The results show that the thermal fatigue properties of DD33 show obvious anisotropy tested at different high-temperatures.The initiation and propagation behavior of thermal fatigue cracks in samples with different notch orienta-tions show the dependence of crystallographic orientation.At 1000℃/1100℃/1200℃,the[100]orientated specimens exhibit the best thermal fatigue performance.The thermal fatigue performance of the[210]ori-ented sample is the worst at 1100℃,while the thermal fatigue performance of the[110]oriented sample is the worst at 1000℃ and 1200℃.The thermal stress,oxidation,and the operation of slip systems result in the difference in crack growth rate of samples with different notch orientations.

metallic materialssingle crystal superalloynotch orientationthermal fatigueanisotropyoxidation

郑明瑞、李亚微、刘静、王莉、郑伟、董加胜、张健、楼琅洪

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中国科学院金属研究所 沈阳 110016

中国科学技术大学材料科学与工程学院 沈阳 110016

金属材料 单晶高温合金 缺口取向 热疲劳 各向异性 氧化

航空发动机及燃气轮机基础科学中心项目国家科技重大专项

P2021-AB-Ⅳ-001-0022017-Ⅵ-0019-0091

2024

材料研究学报
国家自然科学基金委员会 中国材料研究学会

材料研究学报

CSTPCD北大核心
影响因子:0.605
ISSN:1005-3093
年,卷(期):2024.38(2)
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