Ning Haifeng, Zheng Hualin, Wang Guixin
School of Mechatronic Engineering, Southwest Petroleum University, Chengdu 610000, China.
Materials (Basel). 2022 Mar 14;15(6):2127. doi: 10.3390/ma15062127.
Carbon fiber-reinforced composite material (CFRP) has been widely applied in the aerospace industry, which places demanding requirements on the accuracy and quality of its processing. However, there remains a lack of clarity on the microscopic material removal process of CFRP, despite substantial relevant research. This paper aims to reveal the mechanism of material removal in the CFRP cutting process at different fiber cutting angles and to establish an analytical model for CFRP cutting force by considering the radius of the edge circle. Furthermore, the CFRP cutting force analytical model was established by considering the radius of the edge circle on the basis of the CFRP representative volume unit (RVE). According to the model, the cutting process was divided into three regions, the cutting slip zone, fiber fracture zone, and spring back zone, with consideration given to the effect of residual fibers on the cutter teeth. The CFRP cutting finite element model was defined using the software Abaqus, while the chip removal and single-fiber deformation processes were analyzed using the finite element model. As indicated by the experimental results, the analytical model is reliable and capable of providing cutting force values within a 15% deviation.
碳纤维增强复合材料(CFRP)已在航空航天工业中广泛应用,该行业对其加工精度和质量有严格要求。然而,尽管有大量相关研究,但CFRP微观材料去除过程仍不明确。本文旨在揭示不同纤维切割角度下CFRP切割过程中的材料去除机理,并通过考虑刃口圆角半径建立CFRP切削力分析模型。此外,在CFRP代表性体积单元(RVE)的基础上,考虑刃口圆角半径建立了CFRP切削力分析模型。根据该模型,切削过程分为三个区域,即切削滑移区、纤维断裂区和回弹区,同时考虑了残余纤维对刀具齿的影响。使用Abaqus软件定义了CFRP切削有限元模型,并使用该有限元模型分析了切屑去除和单纤维变形过程。实验结果表明,该分析模型可靠,能够提供偏差在15%以内的切削力值。