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新型航空发动机用Ni-cBN主动切削涂层性能

王帅 郭睿 黄凌峰 刘建明

理化检验-物理分册2024,Vol.60Issue(5):20-23,27,5.
理化检验-物理分册2024,Vol.60Issue(5):20-23,27,5.DOI:10.11973/lhjy-wl202405005

新型航空发动机用Ni-cBN主动切削涂层性能

Performance of Ni-cBN active cutting coating for new aviation engines

王帅 1郭睿 1黄凌峰 1刘建明1

作者信息

  • 1. 矿冶科技集团有限公司,北京 100160||北京市工业部件表面强化与修复工程技术研究中心,北京 102206||特种涂层材料与技术北京市重点实验室,北京 102206
  • 折叠

摘要

Abstract

Composite electrodeposition technology was used to prepare nickel-cubic boron nitride(Ni-cBN)active cutting coatings on the surface of grate teeth,and Ni-cBN coatings were prepared on FGH95 nickel based high-temperature alloy matrix.The microstructure,bonding strength and thermal shock performance of the coatings were analyzed,and the influence of the coatings on the mechanical properties of the matrix was studied.The results show that the coating was tightly bonded to the substrate,the abrasive distribution was relatively uniform,and the bonding strength of Ni-cBN coating was greater than 160 MPa.After 1 200 thermal shocks at 600℃,the coating was not damaged and the bonding performance between the coating and the substrate was good.

关键词

复合电沉积/Ni-cBN涂层/篦齿封严/显微组织/结合强度/抗热震性能

Key words

composite electrodeposition/Ni-cBN coating/labyrinth gas seal/microstructure/bond strength/thermal shock resistance

引用本文复制引用

王帅,郭睿,黄凌峰,刘建明..新型航空发动机用Ni-cBN主动切削涂层性能[J].理化检验-物理分册,2024,60(5):20-23,27,5.

基金项目

国家重点研发计划项目(2023YFB3408200) (2023YFB3408200)

理化检验-物理分册

1001-4012

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