航空学报 > 1987, Vol. 8 Issue (10): 504-512

GH33A疲劳/蠕变交互作用下裂纹扩展特性研究

王荣, 田长生   

  1. 西北工业大学
  • 收稿日期:1986-10-20 修回日期:1900-01-01 出版日期:1987-10-25 发布日期:1987-10-25

INVESTIGATION OF CRACK GROWTH PROPERTY UNDER FATIGUE-CREEP INTERACTIONS IN ALLOY GH33A

Wang RongTian Changsheng   

  1. Northwestern Polytechnical University
  • Received:1986-10-20 Revised:1900-01-01 Online:1987-10-25 Published:1987-10-25

摘要: 本文采用交流电位法研究了镍基高温合金GH33A在700℃、疲劳/蠕变交互作用下的裂纹扩展特性。用光学显微镜和扫描电镜对断裂特征进行了分析。结果表明:疲劳/蠕变交互作用加速裂纹扩展,且dα/dN和⊿K在双对数坐标上呈折线规律变化,实验证明:弹塑性断裂力学参数C作为疲劳/蠕变交互作用下裂纹扩展判据是可行的,并建立了经验关系式。疲劳/蠕变交互作用促进裂纹沿晶扩展。主裂纹与W型微裂纹的连接和沿滑移面剪切型扩展是疲劳/蠕变交互作用的两种主要微观断裂机理。

Abstract: The crack growth property under fatigue-creep interactions in nickel-base superalloy GH33A at 700 C is investigated with the alternate electric potential technique.The fracture feature is analyzed with optical microscopes and SEM. It is shown that the fatigue-creep interactions accelerate the crack prowth, and log(da/dN) varies with log( K)in accordance with the broken line rule. As indicated by experiwents, it is possible to use the elastic -plastic fracture mechanics parameter C*as the criterion of the crack growth under fatigue-creep interaction.The equation of crack growth rate is (da/dN) = 6.00×10-2C*0.78Fatigue-creep interactions cause intergranular growth to appear, and both the link of main crack with W type micro-crack and the shearing fracture along the sliping plane are two main micro-mechanisms of fatigue-creep interactions.