航空学报 > 1989, Vol. 10 Issue (7): 404-408

第二相对GH33A疲劳和蠕变交互作用机制的影响

刘江南, 田长生   

  1. 西北工业大学
  • 收稿日期:1988-09-26 修回日期:1900-01-01 出版日期:1989-07-25 发布日期:1989-07-25

INFLUENCE OF SECOND PHASE ON THE MECHANISM OF INTERACTION BETWEEN FATIGUE AND CREEP FOR GH33A

Liu Jiangnan, Tian Changsheng   

  1. Northwestern Polytechic University
  • Received:1988-09-26 Revised:1900-01-01 Online:1989-07-25 Published:1989-07-25

摘要:

借助扫描电镜、透射电镜对试样的断口及剖面进行了金相观察,分析研究了第二相对GH33A合金在700℃下的晶界损伤方式及疲劳和蠕变交互作用的影响。

关键词: 第二相, 晶界损伤, R型空洞, 疲劳, 蠕变

Abstract:

In this paper, the influence of second phase on the behavior of interaction between fatigue and creep for a Nickel-based superalloy GH33A at 700℃ is investigated. Preliminary experimental results showed that the characteristics of intergranular damage and the interaction mechanism vary with the size ot second phase particles and the distance between them. The finely linked second phases at grain boundary cause W type intergranular creep damages its microscopic mechanism is that fatigue crack joins with W type microcrack. On the other hand, the thinly scattered coarse second phases at grain boundary cause R type void intergranular creep damage.

Key words: Second phase, intergranutar damage, R type void.fatigue, creep