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CFRP二次切削加工表面的形成机理及试验研究

李纯杰 苏飞 刘广涛 陈冰 郑雷

宇航材料工艺2024,Vol.54Issue(4):93-102,10.
宇航材料工艺2024,Vol.54Issue(4):93-102,10.DOI:10.12044/j.issn.1007-2330.2024.04.014

CFRP二次切削加工表面的形成机理及试验研究

Formation Mechanism and Experimental Study of CFRP Secondary Cutting Surface

李纯杰 1苏飞 1刘广涛 1陈冰 1郑雷2

作者信息

  • 1. 湖南科技大学机电工程学院难加工材料高效精密加工湖南省重点实验室,湘潭 411201
  • 2. 盐城工学院机械工程学院,盐城 224051
  • 折叠

摘要

Abstract

In the actual processing procedure,multi-step processing was commonly used to optimize the hole-making quality of carbon fiber-reinforced plastic(CFRP).However,there was still a lack of detailed analysis on the formation mechanism of the cutting surface in multi-step processing.To address this issue,this paper constructed a secondary cutting simulation model for four typical fiber orientations(θ=0°,45°,90°,135°),and explored the formation mechanism of the cutting surface and the evolution pattern of cutting damage during the secondary cutting process.The results show that with the increase of the spindle speed n,the secondary cutting force exhibits a significant downward trend;while an increase in the feed rate Vf leads to a significant rise in the secondary cutting force.Further analysis reveals that when the fiber orientation θ is 0°,the influence of the cutting surface damage from the first cutting on the second cutting is relatively small.However,when the fiber orientation θ is 45°,90°or 135°,under the condition that the second cutting thickness is less than the depth of the fiber damage layer caused by the first cutting,the second cutting can effectively remove the damage layer generated by the first cutting without causing new fiber damage,thus significantly improving the quality of the cutting surface.

关键词

碳纤维增强复合材料(CFRP)/多工序/损伤演变/切削力/有限元仿真

Key words

CFRP(Carbon fiber reinforced plastic)/Multi-process/Damage evolution/Cutting force/Finite element simulation

分类

化学工程

引用本文复制引用

李纯杰,苏飞,刘广涛,陈冰,郑雷..CFRP二次切削加工表面的形成机理及试验研究[J].宇航材料工艺,2024,54(4):93-102,10.

基金项目

国家自然科学基金(52175400 ()

51805164) ()

湖南省自然科学基金(2021JJ30263) (2021JJ30263)

江苏省自然科学基金(BK20201474) (BK20201474)

湖南省教育厅资助科研项目(18A182) (18A182)

宇航材料工艺

OA北大核心CSTPCD

1007-2330

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