CFRP/Ti 叠层钻削力热行为与切屑成形分析

王贤锋; 周磊; 安庆龙; 陈明

doi:10.16080/j.issn1671–833x.2018.23/24.096

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CFRP/Ti 叠层钻削力热行为与切屑成形分析

研究论文 | 更新时间：2025-10-30

- CFRP/Ti 叠层钻削力热行为与切屑成形分析
- 航空制造技术 2018年61卷第23/24期
- 作者机构：
  
  1. 上海飞机制造有限公司,上海,201324
  2. 上海交通大学机械与动力工程学院,上海,200240
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671–833x.2018.23/24.096
  中图分类号：
- 纸质出版：2018
- 稿件说明：
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王贤锋，周磊，安庆龙，陈明. CFRP/Ti 叠层钻削力热行为与切屑成形分析[J]. 航空制造技术, 2018, 61(23/24): 96-101. WANG Xianfeng1, ZHOU Lei2, AN Qinglong2, CHEN Ming2. Analysis on Force-Thermal Behaviors and Chip Forming of CFRP/Ti Stacks Drilling[J]. Aeronautical Manufacturing Technology, 2018, 61(23/24): 96-101.

WANG Xianfeng, ZHOU Lei, AN Qinglong, et al. Analysis on Force-Thermal Behaviors and Chip Forming of CFRP/Ti Stacks Drilling[J]. Aeronautical Manufacturing Technology, 2018, 61(23/24).
王贤锋，周磊，安庆龙，陈明. CFRP/Ti 叠层钻削力热行为与切屑成形分析[J]. 航空制造技术, 2018, 61(23/24): 96-101. WANG Xianfeng1, ZHOU Lei2, AN Qinglong2, CHEN Ming2. Analysis on Force-Thermal Behaviors and Chip Forming of CFRP/Ti Stacks Drilling[J]. Aeronautical Manufacturing Technology, 2018, 61(23/24): 96-101. DOI： 10.16080/j.issn1671–833x.2018.23/24.096.

WANG Xianfeng, ZHOU Lei, AN Qinglong, et al. Analysis on Force-Thermal Behaviors and Chip Forming of CFRP/Ti Stacks Drilling[J]. Aeronautical Manufacturing Technology, 2018, 61(23/24). DOI： 10.16080/j.issn1671–833x.2018.23/24.096.

摘要

碳纤维增强复合材料(CFRP) 是一种以环氧树脂作为基体材料、碳纤维作为增强材料的复合材料，具有高强度、高比强度以及耐腐蚀性的特点。CFRP 与钛合金是航空航天领域广泛使用的两种轻质的材料，经常作为叠层结构出现在大型客机的关键部位，使大型客机制造装配过程中需要对CFRP/Ti叠层进行大量的制孔。而CFRP/Ti叠层钻削过程中的力热变化与切屑形态会直接影响刀具的切削状态。在此基础之上，对CFRP/Ti 叠层钻削过程中的力热行为与切屑成形进行研究，这对于CFRP-Ti 叠层实际钻削过程具有重要的指导意义。

Abstract

Carbon fiber reinforced polymer (CFRP) is a kind of material with epoxy resin as matrix material and carbon fiber as reinforced material

which has the characteristics of high strength

high specific strength and corrosion resistance. CFRPs and titanium alloys are two kinds of lightweight materials widely used in aerospace fields. CFRPs and titanium alloys often appear as laminated structures in the key areas of large passenger aircraft

which leads to a large number of hole-making of CFRP/Ti stacks in the manufacturing and assembly processes of large passenger aircraft. The variation of heat and force as well as chip shape in the CFRP/Ti stacks drilling process will directly affect the cutting state of the tool.Therefore

the study of force-thermal behavior and chip forming in the CFRP/Ti stacks drilling process was carried out in this paper

which has important guiding significance for the actual drilling process of CFRP-Ti stack.

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