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P对定向凝固高温合金DZ125组织和性能的影响

宋尽霞 姜驰航 康永旺 肖程波 蒋立武 李明 戴圣龙

航空材料学报2025,Vol.45Issue(5):142-149,8.
航空材料学报2025,Vol.45Issue(5):142-149,8.DOI:10.11868/j.issn.1005-5053.2025.000116

P对定向凝固高温合金DZ125组织和性能的影响

Effects of P on microstructures and properties of directionally solidified superalloy DZ125

宋尽霞 1姜驰航 2康永旺 1肖程波 1蒋立武 2李明 1戴圣龙1

作者信息

  • 1. 中国航发北京航空材料研究院先进高温结构材料重点实验室,北京 100095
  • 2. 北京科技大学国家材料服役安全中心,北京 100083
  • 折叠

摘要

Abstract

The directionally solidified superalloy DZ125 is widely used as turbine blades in aero-engines.This work investigates the influence of phosphorus(P)on the microstructure,mechanical properties and crack susceptibility of DZ125 alloy.The results indicate that P primarily segregates at grain boundaries in DZ125 alloy and has little effect on γ′phases,γ+γ′eutectic and carbides in the alloy.When P content reaches 0.008%(mass fraction,the same below)P-rich phases form in the interdendritic regions during casting,which subsequently dissolve back into the matrix during heat treatment.When the P content is no more than 0.0039%,P shows no obvious effects on the room-temperature tensile properties or the stress rupture life at 980℃/235 MPa.However,it has a significant impact on the stress rupture life at 760℃/805 MPa:the alloy with 0.0039%P exhibits a 37%decrease in stress rupture life at 760℃/805 MPa compared to the alloy with 0.0013%P,due to the segregation of P at grain boundaries weakens the grain boundaries.When the P content reaches 0.011%,the intergranular cracks appear in the DZ125 alloy hollow turbine blades during directionally solidified process.The main reason for the increase of crack susceptibility is excessive enrichment of P at grain boundaries and precipitation of P-rich phases nearby grain boundaries,which leads to grain boundary weakening and crack initiation.

关键词

P元素/DZ125合金/微观组织/力学性能/裂纹倾向性

Key words

P element/DZ125 alloy/microstructure/mechanical property/crack susceptibility

分类

矿业与冶金

引用本文复制引用

宋尽霞,姜驰航,康永旺,肖程波,蒋立武,李明,戴圣龙..P对定向凝固高温合金DZ125组织和性能的影响[J].航空材料学报,2025,45(5):142-149,8.

基金项目

国家重点研发计划项目(2022YFB3705004) (2022YFB3705004)

航空材料学报

OA北大核心

1005-5053

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