首页|Ti-22Al-25Nb合金双板条组织的高温疲劳性能

Ti-22Al-25Nb合金双板条组织的高温疲劳性能

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研究了 Ti-22Al-25Nb合金双板条组织在300、500和700 ℃下的轴向高周疲劳行为,并对疲劳试样的断口与组织形貌进行了表征.结果发现:3种温度下Ti-22Al-25Nb合金双板条组织的条件疲劳极限分别为510、338和356 MPa.300 ℃试样的裂纹既有表面形核也有内部形核,500和700 ℃试样的裂纹均起源于试样表面.300 ℃的疲劳条纹呈现脆性条带特征,500 ℃呈现间断与连续的过渡条纹,而700 ℃则表现为塑性条纹.细小针状O相板条区域容易产生裂纹,而粗大片状板条在裂纹扩展路径上起到阻碍作用,有利于提高材料的疲劳寿命.
High temperature fatigue properties of Ti-22Al-25Nb alloy double slats
The axial high-cycle fatigue behavior of Ti-22Al-25Nb alloy multi-scale double slats at 300,500 and 700℃ was studied,and the fracture and structure morphology of fatigue samples were characterized.The results showed that the fatigue limits were 510,338 and 356 MPa,respectively.The cracks of 300 ℃ samples have both surface and internal nucleation,and the cracks of 500 and 700 ℃ samples originated from the surface of the sam-ples.The fatigue striations at 300 ℃ show the characteristics of brittle bands,the intermittent and continuous tran-sition striations at 500 ℃,and the plastic striations at 700 ℃.Small acicular O-phase slats are prone to crack,while large sheet slats hinder the crack propagation path,which is conducive to improving the fatigue life of the ma-terial.

Ti-22Al-25Nb alloydouble lath structurehigh cycle fatiguefracture morphology

孙玉鑫、马雄、梁晓波、韩潮雨、史晓强、赵洪泽

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烟台大学精准材料高等研究院,山东烟台 264005

北京钢研高纳科技股份有限公司,北京 100081

钢铁研究总院有限公司,北京 100081

Ti-22Al-25Nb合金 双板条组织 高周疲劳 断口形貌

国家科技重大专项经费资助

2017-VI-0004-0074

2024

金属功能材料
中国钢研科技集团有限公司 中国金属学会功能材料分会

金属功能材料

CSTPCD
影响因子:0.527
ISSN:1005-8192
年,卷(期):2024.31(5)