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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2003, Vol. 24 ›› Issue (4): 377-381.

• 论文 • Previous Articles     Next Articles

Recrystallization and Fatigue Failure of Blades Made of a Directionally Solidified Alloy

ZHANG Wei-fang1, GAO Wei1, ZHAO Ai-guo1, TAO Chun-hu1, TIAN Ji-feng2, YAO Ge2   

  1. 1. Beijing Institute of Aeronautical Materials; Beijing 100095; China;2. Metal Institute of Academic; Shenyang 110035; China
  • Received:2002-09-05 Revised:2003-01-12 Online:2003-08-25 Published:2003-08-25

Abstract: The crack and fracture of blades made of a directionally solidified superalloy were analyzed. The failuremode and cause were studied in virtue of fracture observation and metallographic structure analysis. The results showthat the crack and fracture on the superalloy blades have the same failure mode resulting from surface recrystallization. Owing to the plastic deformation at the blade surface, recrystallization formed during the solid solution heattreatment . Before blade application, the recrystallization zone is already exist on its two sides and surface.

Key words: directionally solidified superalloy, blade, recrystallization, fatigue failure

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