现代制造工程 ›› 2026, Vol. 549 ›› Issue (6): 99-109.doi: 10.16731/j.cnki.1671-3133.2026.06.011

• 车辆工程制造技术 • 上一篇    下一篇

FGH96材料拉削表面完整性研究

冯博1,2, 张莹1,2, 吴宝海1,2, 王琳叶1,2   

  1. 1 西北工业大学航空发动机先进制造技术教育部工程研究中心,西安 710072;
    2 西北工业大学航空发动机高性能制造工业与信息化部重点试验室,西安 710072
  • 收稿日期:2025-06-21 出版日期:2026-06-18 发布日期:2026-07-02
  • 通讯作者: 张莹,博士,副研究员,主要研究方向为CAD/CAM、多轴数控加工、自适应加工及智能加工。E-mail:2159620944@qq.com
  • 作者简介:冯博,硕士研究生,主要研究方向为拉削加工表面完整性控制。

A study on surface integrity of FGH96 material for broaching

FENG Bo1,2, ZHANG Ying1,2, WU Baohai1,2, WANG Linye1,2   

  1. 1 Engineering Research Center of Advanced Manufacturing Technology for Aero Engine, Ministry of Education,Northwestern Polytechnical University,Xi’an 710072,China;
    2 Key Laboratory of High Performance Manufacturing for Aero Engine,Ministry of Industry and Information Technology,Northwestern Polytechnical University,Xi’an 710072,China
  • Received:2025-06-21 Online:2026-06-18 Published:2026-07-02

摘要: FGH96是一种广泛应用于高温环境的粉末冶金材料,拉削作为FGH96涡轮盘榫槽等关键特征的加工方法,其工艺参数选择直接影响最终零件的服役性能与寿命。研究了FGH96材料的拉削表面完整性,分析了不同工艺参数对表面粗糙度、表面形貌、残余应力和显微硬度的影响。试验结果表明,表面粗糙度随前角增大而减小,随齿升量、拉削速度增大而增大;表面形貌状态随前角增大变优,随齿升量和速度增大而迅速恶化;表面残余应力在拉削方向呈现为压应力,在垂直拉削方向为拉应力;表面维氏硬度随着拉刀前角和速度的增大而减小,随着齿升量的增大而增大。深入理解并研究FGH96拉削表面完整性,对于提升涡轮盘等关键部件的抗疲劳性能、可靠性和极端环境下的安全性具有至关重要的意义。

关键词: FGH96, 拉削, 表面粗糙度, 残余应力, 表面形貌, 维氏硬度

Abstract: FGH96 is a powder metallurgy material widely used in high-temperature environments. As a machining method for key features such as FGH96 turbine disk tongue and groove,the selection of broaching process parameters directly affects the serviceability and life of the final part. The surface integrity of broached FGH96 material is investigated,and the effects of different process parameters on surface roughness,surface morphology,residual stress and microhardness are analyzed. The result shows that surface roughness is reduced with the increase of the front angle,and is increased with the increase of tooth rise and broaching speed;surface morphology is improved with the increase of the front angle,and is deteriorated rapidly with the increase of the tooth rise and the speed;the residual stress on the surface in the direction of broaching is manifested as compressive stress,and in the direction of perpendicular broaching,it is manifested as tensile stress;the Vickers hardness on the surface is reduced with the increase of the front angle of the broach and the increase of the speed,and is reduced with the increase of tooth rise. In-depth understanding and study of the FGH96 broaching surface integrity is of vital significance for improving the fatigue resistance,reliability and safety in extreme environments of key components such as turbine disks.

Key words: FGH96, broaching, surface roughness, residual stress, surface morphology, Vickers hardness

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