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Investigation on high temperature strengthening and toughening of iron-base superalloy

Investigation on high temperature strengthening and toughening of iron-base superalloy
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摘要 A new modified A-286 (15Cr-28Ni-1.5Mo-lW-2Ti-Nb-Al) (mass fraction) designated as GH871 is characterized by high strengths but low ductility at 650℃ stress rupture and also high crack propagation rates at 650℃ creep and creep/fatigue interaction conditions. For improvement of ductility and crack propagation behaviour, a primary vacuum induction melting and followed electro-slag refining process (VIM+ESR) has been adopted instead of air melting and electro-slag refining process (AIM+ESR). Vacuum melted GH871 (VIM+ESR) can keep the high strength level of this alloy and improve the ductility and also decrease crack propagation rates by this alloy purification. It is a good combination of strengthening and toughening for the alloy improvement and development. A new modified A-286 (15Cr-28Ni-1.5Mo-lW-2Ti-Nb-Al) (mass fraction) designated as GH871 is characterized by high strengths but low ductility at 650℃ stress rupture and also high crack propagation rates at 650℃ creep and creep/fatigue interaction conditions. For improvement of ductility and crack propagation behaviour, a primary vacuum induction melting and followed electro-slag refining process (VIM+ESR) has been adopted instead of air melting and electro-slag refining process (AIM+ESR). Vacuum melted GH871 (VIM+ESR) can keep the high strength level of this alloy and improve the ductility and also decrease crack propagation rates by this alloy purification. It is a good combination of strengthening and toughening for the alloy improvement and development.
出处 《Journal of University of Science and Technology Beijing》 CSCD 2003年第1期44-48,共5页 北京科技大学学报(英文版)
关键词 SUPERALLOY modified A-286 stress rupture low cycle fatigue(LCF) crack propagation superalloy modified A-286 stress rupture low cycle fatigue(LCF) crack propagation
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参考文献8

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