[1]曹自洋,潘杰,倪家伟,等.CFRP/Ti叠层材料制孔技术研究现状及进展[J].中国材料进展,2025,44(10):893-902.[doi:10.7502/j.issn.1674-3962.202208022]
CAO Ziyang,PAN Jie,NI Jiawei,et al.Research Status and Progress of Hole Making Technology for CFRP/Ti Laminated Materials[J].MATERIALS CHINA,2025,44(10):893-902.[doi:10.7502/j.issn.1674-3962.202208022]
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CFRP/Ti叠层材料制孔技术研究现状及进展(
)
中国材料进展[ISSN:1674-3962/CN:61-1473/TG]
- 卷:
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44
- 期数:
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2025年10
- 页码:
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893-902
- 栏目:
-
- 出版日期:
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2025-10-30
文章信息/Info
- Title:
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Research Status and Progress of Hole Making Technology for CFRP/Ti Laminated Materials
- 文章编号:
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1674-3962(2025)10-0893-10
- 作者:
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曹自洋; 潘杰; 倪家伟; 许威; 朱译文
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1. 苏州科技大学机械工程学院,江苏 苏州 215009
2. 苏州市高效与精密加工技术重点实验室,江苏 苏州 215009
- Author(s):
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CAO Ziyang; PAN Jie; NI Jiawei; XU Wei; ZHU Yiwen
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1. School of Mechanical Engineering, Suzhou University of Science and Technology,Suzhou 215009, China
2. Suzhou Key Laboratory of Precision and Efficient Machining Technology, Suzhou 215009, China
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- 关键词:
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碳纤维增强复合材料/钛合金(CFRP/Ti)叠层材料; 钻削; 螺旋铣削; 微量润滑(MQL); 振动辅助加工
- Keywords:
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carbon fiber reinforced composite/titanium alloy (CFRP/Ti) laminated materials; drilling; helical milling; micro-lubrication (MQL); vibrationassisted machining
- 分类号:
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TG506;TH161
- DOI:
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10.7502/j.issn.1674-3962.202208022
- 文献标志码:
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A
- 摘要:
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碳纤维增强复合材料/钛合金(CFRP/Ti)叠层材料因其优异的综合性能在航空航天领域被大量使用。在制造过程中,叠层材料通常以螺栓连接的方式组成所需的装配结构,连接孔的加工质量直接影响着叠层材料的力学性能等质量指标,因此如何提高其制孔质量及其制孔寿命被广泛关注。总结了近年来CFRP/Ti叠层材料制孔技术的研究进展,从钻削制孔和螺旋铣孔2个方面重点阐述了CFRP/Ti叠层材料的制孔过程、制孔缺陷及其形成机理以及制孔质量的影响因素;介绍了振动辅助加工技术和微量润滑(MQL)冷却方式在CFRP/Ti叠层材料制孔过程中减小切削力、降低切削温度等方面的加工优势,并对未来CFRP/Ti叠层材料制孔技术的发展方向进行了展望。
- Abstract:
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Carbon fiber reinforced composite/titanium alloy (CFRP/Ti) laminated materials are widely used in the aerospace sector due to their exceptional qualities. The laminated material is typically bolted together during the manufacturing process to create the necessary assembly structure. Improvements in holemaking quality and hole-making life are of great concern because they directly impact the mechanical properties of the laminated material and other quality indicators. In this paper, the development of hole-making technology for CFRP/Ti composites is reviewed both domestically and internationally. The process of making holes in CFRP/Ti laminated materials, the defects and their formation mechanism as well as the factors influencing the quality of hole making are highlighted from two aspects: drilling hole making and helical milling. The benefits of vibrationassisted machining and the minimum quantity lubrication (MQL) cooling technique are discussed, along with the potential future development path for CFRP/Ti laminated material holemaking technology.
备注/Memo
- 备注/Memo:
-
收稿日期:2022-08-17修回日期:2022-10-17
基金项目:国家自然科学基金项目(51905363);江苏省中外合作办学平台联合科研项目(2019-21);江苏省研究生科
研与实践创新计划项目(KYCX22_3263)
第一作者:曹自洋,男,1979年生,教授,硕士生导师,
Email: dukeczy@nuaa.edu.cn
更新日期/Last Update:
2025-11-14