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SiC纤维增强Ti3Al复合材料螺纹区域残余应力分析

王金鹏 齐金磊 王宁 高明钦 王龙鹏 王敏涓 黄浩 黎克楠 文懋

材料工程2026,Vol.54Issue(4):47-54,8.
材料工程2026,Vol.54Issue(4):47-54,8.DOI:10.11868/j.issn.1001-4381.2025.000485

SiC纤维增强Ti3Al复合材料螺纹区域残余应力分析

Analysis of residual stress in threaded regions of SiC fiber-reinforced Ti3Al composite

王金鹏 1齐金磊 1王宁 1高明钦 1王龙鹏 1王敏涓 2黄浩 2黎克楠 3文懋1

作者信息

  • 1. 吉林大学材料科学与工程学院,长春 130012
  • 2. 中国航发北京航空材料研究院先进钛合金航空科技重点实验室,北京 100095
  • 3. 郑州磨料磨具磨削研究所有限公司高性能工具全国重点实验室,郑州 450001
  • 折叠

摘要

Abstract

Continuous SiC fiber-reinforced Ti3Al(SiCf/Ti3Al)composite combines the advantages of high damage tolerance and ease of forming for Ti3Al matrix and high-strength for SiC fibers.It is an ideal candidate material for lightweight,high-strength,and high-temperature resistant fasteners in the aerospace field.However,complex residual stresses are inevitably introduced during the thread machining process of SiCf/Ti3Al composites.Therefore,analyzing the residual stresses in the threaded regions of SiCf/Ti3Al composites is of great significance for enhancing the service safety and reliability of fasteners.Given the complex geometric structures of the threaded regions in turned SiCf/Ti3Al composites and the close relationship between their stress distribution and core diameter,the characterization and analysis of stress are challenged by the intricate thread profile and limited dimensions.Residual stress measurements and analyses are conducted on the thread crest and radial cross-sections of the threads using side-inclined X-ray diffraction and nanoindentation method,respectively.The results show that the thread crest is in a state of compressive stress after turning.When the core diameter increases from 3.0 mm to 4.0 mm,the compressive stress increases from 387.6 MPa to 540.6 MPa.The radial cross-sections of the thread are also under compressive stress.As the core diameter increases from 3.0 mm to 4.0 mm,the compressive stress at the same location 100 μm from the thread crest increases from 326.9 MPa to 430.8 MPa.Furthermore,the compressive stress decreases with increasing distance from the thread crest.

关键词

SiCf/Ti3Al复合材料/紧固件螺纹/X射线衍射法/纳米压痕法/残余应力

Key words

SiCf/Ti3Al composite/fastener thread/XRD method/nanoindentation method/residual stress

分类

通用工业技术

引用本文复制引用

王金鹏,齐金磊,王宁,高明钦,王龙鹏,王敏涓,黄浩,黎克楠,文懋..SiC纤维增强Ti3Al复合材料螺纹区域残余应力分析[J].材料工程,2026,54(4):47-54,8.

基金项目

稳定支持项目资助(2023-2) (2023-2)

材料工程

1001-4381

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