航空用超高强度钢疲劳裂纹表面长度与内部长度之间的关系

王苗苗;曾燕屏;王习术;谢锡善

航空材料学报 ›› 2009, Vol. 29 ›› Issue (3) : 102-106.

PDF(1932 KB)
PDF(1932 KB)
航空材料学报 ›› 2009, Vol. 29 ›› Issue (3) : 102-106.
论文

航空用超高强度钢疲劳裂纹表面长度与内部长度之间的关系

  • 王苗苗;曾燕屏;王习术;谢锡善
作者信息 +

Relationship between Surface Length and Inside Length of Fatigue Crack in Ultra-high Strength Steel

  • WANG Miao-miao;ZENG Yan-ping;WANG Xi-shu;XIE Xi-shan
Author information +
文章历史 +

摘要

采用扫描电镜原位观测的方法,跟踪观察了低周疲劳载荷作用下超高强度钢中AlN夹杂导致裂纹萌生与扩展的微观行为,得到了材料疲劳裂纹表面长度与内部长度之间的关系,可以根据实际检测到的材料或者结构疲劳裂纹表面长度计算其内部长度,并估算其剩余寿命.

Abstract

Ultra-high strength steel makes advancement incessantly with development of aeronautical industry.However,its sensitivity to the flaw increases with increasing in strength level.Non-metallic inclusion as one of the inevitable flaws must influence the performance,especially fatigue performance,of ultra-high strength steel.In-situ fatigue tests with special designed SEM have been conducted to trace the whole process of crack initiation and propagation induced by AlN inclusion in ultra-high strength steel under low-cycle fatigue load.The strong linear between the surface length and the inside length of fatigue crack was gained.The inside length can be calculated based on the surface length of fatigue crack detected in material or structure and the residual life can be estimated.

关键词

超高强度钢 / 低周疲劳 / 夹杂物 / 裂纹萌生与扩展 / 原位观测

Key words

ultra-high strength / low-cycle fatigue / inclusions / crack initiation and / In-situ observation

引用本文

导出引用
王苗苗;曾燕屏;王习术;谢锡善. 航空用超高强度钢疲劳裂纹表面长度与内部长度之间的关系[J]. 航空材料学报, 2009, 29(3): 102-106
WANG Miao-miao;ZENG Yan-ping;WANG Xi-shu;XIE Xi-shan. Relationship between Surface Length and Inside Length of Fatigue Crack in Ultra-high Strength Steel[J]. Journal of Aeronautical Materials, 2009, 29(3): 102-106

参考文献

王习术,梁锋,曾燕屏,等.夹杂物对超高强度钢低周疲劳裂纹萌生及扩展影响的原位观测[J].金属学报,2005,12:1272-1276.
YUKITAKA Murakami.Metal fatigue:effects of small defects and nonmetallic inclusions[M].Amsterdam Elservier,2002.
曾燕屏,董建新,张麦仓,等.拉伸载荷下镍基粉末高温合金中夹杂物行为[J].科技大学学报,2005,27(2):202-204.
李守新.夹杂对高强钢疲劳性能影响的研究[J].中国基础科学,2005,7(4):14-15.
WANG Xi-shu,ZHANG Lina,ZENG Yan-ping,et al.SEM in-situ investigation on fatigue cracking behavior of P/M Rene95 alloy with surface inclusions[J].Journal of University of Science and Technology Beijing,2006,13(3):244-249.
冯西桥,何树延.表面裂纹疲劳扩展的一种损伤力学方法[J].清华大学学报(自然科学版),1997,37(5):78-82.
赵勇铭,宋迎东.夹杂对粉末高温合金裂纹扩展寿命的影响[J].航空动力学报,2005,20(5):772-777.
PDF(1932 KB)

14

Accesses

0

Citation

Detail

段落导航
相关文章

/