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定向凝固合金DZ17G室温疲劳裂纹扩展行为的研究
引用本文:廖鄂斌,郭建亭,王淑荷.定向凝固合金DZ17G室温疲劳裂纹扩展行为的研究[J].航空材料学报,1999,19(1):39-44.
作者姓名:廖鄂斌  郭建亭  王淑荷
作者单位:中国科学院金属研究所,沈阳,110015
摘    要:Fatigue crack growth behavior of DZ17G at room temperature is studied at different testing conditions of loading direction and loading frequency.The results indicate that the fatigue crack growth rate(FCGR) is the largest on the specimen with loading angle 90°,smaller on that with loading angle 0°,and the smallest on that with loading angle 45° due to crack deflection effect.The influence of loading frequency upon FCGR is related to the range of stress intensity factor ΔK.The dimension of precipitate γ′ has influence upon the dislocation arrangement.Microcracks propagate along the γ channel.

关 键 词:定向凝固高温合金  加载取向  加载频率  疲劳裂纹扩展速率
文章编号:1005-5053(1999)01-0039-06
修稿时间:1998-12-22

Research on fatigue crack growth behavior of DZ17G at room temperature
LIAO E-bin,GUO Jian-ting,WANG Shu-he.Research on fatigue crack growth behavior of DZ17G at room temperature[J].Journal of Aeronautical Materials,1999,19(1):39-44.
Authors:LIAO E-bin  GUO Jian-ting  WANG Shu-he
Abstract:
Keywords:DS superalloy  loading direction  loading frequency  fatigue crack growth rate
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