航空学报 > 1989, Vol. 10 Issue (9): 517-520

FGH95粉末高温合金应力时效的组织和相分析

臧鑫士, 郭淑平, 李晓欣   

  1. 北京航空航天大学
  • 收稿日期:1988-11-03 修回日期:1900-01-01 出版日期:1989-09-25 发布日期:1989-09-25

THE STRUCTURE AND PHASE ANALYSIS OF P/M SUPERALLOY FGH 95 DURING STRESS AGEING

Zang Xinshi, Guo Shuping, Li Xiaoxin   

  1. Beijing University of Aeronautics and Astronautics
  • Received:1988-11-03 Revised:1900-01-01 Online:1989-09-25 Published:1989-09-25

摘要:

FGH95合金用于制造飞机发动机涡轮盘。曾有人对该合金长期时效的组织变化进行过研究,考虑到涡轮盘受温度和应力的双重作用,研究该合金长期应力时效过程中的相变规律和组织稳定性更有实际意义。

关键词: 热等静压, 相变, 应力时效

Abstract:

The phase transformation behavior and microstructural stability of P/M superalloy FGH95 in the long time stress ageing have been studied. It has been found that the hot-isostatically pressed FGH 95 alloy, which is in solution and ageing state and is subsequently subjected to long time stress ageing at 650℃ and lower temperatures consists of γ, γ',MC, M23C6 and M3B2 phases. A certain amount of secondary γ' coarsened, while some dissolved during the stress ageing. The γ' and minor phases contents showed a tendency to increase and grain boundary precipitation also increase as the stress ageing time increased. This alloy exhibits a relatively good structural stability.

Key words: hot-isostatical press (HIP), phase transformation, stress ageing