TY - JOUR
T1 - Carbon fiber reinforced polymer in drilling
T2 - From damage mechanisms to suppression
AU - Gao, Teng
AU - Li, Changhe
AU - Wang, Yiqi
AU - Liu, Xueshu
AU - An, Qinglong
AU - Li, Hao Nan
AU - Zhang, Yanbin
AU - Cao, Huajun
AU - Liu, Bo
AU - Wang, Dazhong
AU - Said, Zafar
AU - Debnath, Sujan
AU - Jamil, Muhammad
AU - Ali, Hafiz Muhammad
AU - Sharma, Shubham
N1 - Publisher Copyright:
© 2022 Elsevier Ltd
PY - 2022/4/15
Y1 - 2022/4/15
N2 - Realizing the integrated manufacturing of components with high specific strength and stiffness is easy using carbon fiber reinforced polymer (CFRP), which has become the preferred material for weight reduction and efficiency enhancement in the aerospace field. Massive connection holes are machined in assembly. However, CFRP is a multiphase material comprising fiber, resin, and interface at the mesoscopic level. Macroscopically, CFRP has the characteristics of heterogeneity, anisotropy, and heat sensitivity, thus easily causing delamination and burr, which limits its application. Only a few systematic analyses and reviews from the aspects of drilling systems, machining conditions, and tools are currently available. This paper presents a systematic scheme of drilling damage suppression from the overall drilling system. First, the formation mechanism of damage at different hole positions, including exit push-out delamination, entrance peel-up delamination, and burr and fiber pull-out, is analyzed. Second, the suppression strategies are systematically reviewed from the following four aspects: drilling techniques and methods, drilling conditions, tool design, and multi-techniques integration. The damage evaluation methods are then summarized from qualitative detection and quantitative characterization, covering destructive and nondestructive testing and delamination factors in different dimensions. Finally, the unique advantages of various suppression strategies are determined, and the research gaps and future popular research directions are prospected.
AB - Realizing the integrated manufacturing of components with high specific strength and stiffness is easy using carbon fiber reinforced polymer (CFRP), which has become the preferred material for weight reduction and efficiency enhancement in the aerospace field. Massive connection holes are machined in assembly. However, CFRP is a multiphase material comprising fiber, resin, and interface at the mesoscopic level. Macroscopically, CFRP has the characteristics of heterogeneity, anisotropy, and heat sensitivity, thus easily causing delamination and burr, which limits its application. Only a few systematic analyses and reviews from the aspects of drilling systems, machining conditions, and tools are currently available. This paper presents a systematic scheme of drilling damage suppression from the overall drilling system. First, the formation mechanism of damage at different hole positions, including exit push-out delamination, entrance peel-up delamination, and burr and fiber pull-out, is analyzed. Second, the suppression strategies are systematically reviewed from the following four aspects: drilling techniques and methods, drilling conditions, tool design, and multi-techniques integration. The damage evaluation methods are then summarized from qualitative detection and quantitative characterization, covering destructive and nondestructive testing and delamination factors in different dimensions. Finally, the unique advantages of various suppression strategies are determined, and the research gaps and future popular research directions are prospected.
KW - Carbon fiber reinforced polymer
KW - Damage formation
KW - Delamination
KW - Drilling
KW - Suppression strategies
UR - http://www.scopus.com/inward/record.url?scp=85123688126&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2022.115232
DO - 10.1016/j.compstruct.2022.115232
M3 - Article
AN - SCOPUS:85123688126
SN - 0263-8223
VL - 286
JO - Composite Structures
JF - Composite Structures
M1 - 115232
ER -