航空学报 > 2026, Vol. 47 Issue (4): 432129-432129   doi: 10.7527/S1000-6893.2025.32129

表面硬度与表面残余应力对FGH99微动磨损特性的影响

邱颖博, 孔维瑜, 何湘萍, 白倩()   

  1. 大连理工大学 高性能精密制造全国重点实验室,大连 116024
  • 收稿日期:2025-04-15 修回日期:2025-05-09 接受日期:2025-06-09 出版日期:2025-07-23 发布日期:2025-07-15
  • 通讯作者: 白倩 E-mail:baiqian@dlut.edu.cn
  • 基金资助:
    国家级项目

Effect of surface hardness and surface residual stress on fretting wear characteristics of FGH99

Yingbo QIU, Weiyu KONG, Xiangping HE, Qian BAI()   

  1. State Key Laboratory of High-Performance Precision Manufacturing,Dalian University of Technology,Dalian 116024,China
  • Received:2025-04-15 Revised:2025-05-09 Accepted:2025-06-09 Online:2025-07-23 Published:2025-07-15
  • Contact: Qian BAI E-mail:baiqian@dlut.edu.cn
  • Supported by:
    National- Level Project

摘要:

以镍基粉末高温合金FGH99为研究对象,研究了铣削径向切深对加工表面完整性参数及其微动磨损性能的影响。通过控制表面粗糙度一致,分析了表面硬度与表面残余应力对FGH99微动磨损行为的协同作用。研究结果表明:径向切深的增加引起了切削热和切削力的升高,从而导致表面完整性参数发生变化。随着径向切深从0.06 mm增加到0.30 mm,表面硬度从476.8 HV提升至589.2 HV,表面残余拉应力从100.8 MPa增加至661.3 MPa。微动磨损实验表明,在低表面硬度/低表面残余拉应力状态下,磨损主要表现为塑性变形和氧化磨损;而在高表面硬度/高表面残余拉应力条件下,表面残余拉应力对磨损的加剧作用超越了表面硬度提升的抑制作用,形成氧化-磨粒-疲劳复合磨损机制。当径向切深在0.12~0.18 mm范围时,表面硬度和表面残余拉应力达到最佳平衡,此时FGH99铣削表面表现出最佳的抗微动磨损性能。

关键词: 粉末高温合金, 铣削, 表面硬度, 表面残余应力, 微动磨损

Abstract:

This study investigated the effect of the radial depth of cut during milling on the machining-induced surface integrity parameters and the subsequent fretting wear performance of FGH99. By maintaining a consistent surface roughness, the synergistic effects of surface hardness and surface residual stress on the fretting wear behavior of FGH99 were analyzed. The results indicate that an increase in radial depth of cut leads to elevated cutting temperatures and cutting forces, consequently altering the surface integrity parameters. As the radial depth of cut increased from 0.06 mm to 0.30 mm, the surface hardness rose from 476.8 HV to 589.2 HV, and the surface residual tensile stress increased from 100.8 MPa to 661.3 MPa. Fretting wear tests revealed that under conditions of low surface hardness and low surface residual tensile stress, wear primarily manifested as plastic deformation and oxidative wear. Conversely, under high surface hardness and high surface residual tensile stress conditions, the detrimental effect of surface residual tensile stress on wear outweighed the beneficial effect of increased surface hardness, leading to a composite wear mechanism involving oxidation, abrasion and fatigue. When the radial depth of cut is in the range of 0.12 to 0.18 mm, an optimal balance between surface hardness and surface residual tensile stress was achieved, leading to the best fretting wear resistance of the milled FGH99 surface

Key words: powder metallurgy superalloy, milling, surface hardness, surface residual stress, fretting wear

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