摘要
为了给700℃超超临界机组选材提供技术参考,研究了2种固溶强化型镍基合金(617和625)经时效处理(时效)后的析出行为。结果表明:2种镍基合金760℃时效后,均析出M23C6、M6C碳化物和γ′相;M23C6、M6C碳化物分布于晶界和晶内,γ′相分布于晶内;γ″相在625合金晶界、层错处析出并向晶内生长。617合金时效3 000 h,晶界析出相不连续分布;时效5 000 h后晶界析出相聚集且连续分布,晶内析出相的尺寸基本稳定。625合金时效3 000 h的晶内析出相尺寸无明显变化,晶界M23C6颗粒聚集长大;时效5 000 h后M23C6转变为M6C碳化物。617合金和625合金时效后的冲击吸收能量均明显下降,时效后的625合金脆化程度较时效后的617合金严重。
Aging preeipilation hehavior of the two solid-solution strengthened Ni-based alloys (617 and 625) Ires been invesligated. The resuhs revealed thal the M23C6, and M6C, carbide particles precipitated both at the grain boundaries anti inside grains, and the γ phase particles were situated at intragranular sites in the process of aging al 760 ℃ for two alloys. In addition, γ phase precipitated at grain houndaries arid stacking faults in the aged alloy 625. The carbide partieles discontinuously dispersed at grain boundaries after aging for up to 3 000 h for alloy 617: however, the 5 000 h aging induced the coalescence of the tar'hide particles. After aging up to 5 000 h, the size of precipihltes inside grains remained basieally stable for alloy 617. The carbides preeipitates dispersed continuously al inter-granular site were observed in the alloy 625 aged for 3 000 h and an incre, ase of aging lime resulted in the growth of carbide partitcles. The size of inlragranular parlieles kept almost unchanged after aging for up to 3 000 h for alloy 625; however, the presence of a nnmher of M6C partieles was visible for alloy 625 after 5 000 h. The impact absorbed energy obviously declined for two alloys after aging. Aging cmhrilllement of the alloy 625 is grealer than that hi'the alloy 617.
出处
《中国电力》
CSCD
北大核心
2013年第9期34-38,共5页
Electric Power
基金
2010年度中国电机工程学会电力青年科技创新资助项目