Abstract
Carbon fiber-reinforced plastic (CFRP) is used widely in aerospace. The cutting mechanism of CFRP is markedly different from that of metals due to anisotropic and non-homogeneous material structure. The cutting mechanisms are highly dependent on the fiber orientation. The quality of the machined surface can be affected by the fiber fracture models. In this paper, based on the elastic foundation beam theory and the Hertzian contact theory, the cutting mechanics are established. And the cutting model is simulated by the three-dimensional micro-scale numerical model. Then, the continuous varying cutting mechanism and the sub-damage are deeply studied in detail by combining the cutting mechanics model and the simulation model. The results indicate that the fiber orientation θ = 80° and θ = 150° is the transition critical point of the fracture form. When θ = 0°, the fiber failure mode is buckling dominated. When 0° < θ < 80° and 150° < θ < 180°, the fiber failure mode is dominated by contact fracture. When 80° < θ < 150°, the fiber failure mode is bending-dominated. The cutting mechanics model and finite element model can effectively reflect the evolution law of CFRP-machined surface.
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Abbreviations
- E 1 :
-
Equivalent elastic modulus in 1 direction (viz., the fiber axial direction)
- E 2 :
-
Equivalent elastic modulus in 2 direction (viz., vertical the fiber axial direction)
- E 3 :
-
Equivalent elastic modulus in 3 direction (viz., vertical the fiber axial direction)
- E f :
-
Young’s elastic modulus of the fiber
- E m :
-
Young’s elastic modulus of the matrix
- ν f :
-
Fiber Poisson’s ratio
- G 12 :
-
In-plane shear modulus
- ν 12 :
-
Equivalent Poisson’s ratio for the deformation in 2-direction causing by the stress in 1 direction
- ν 21 :
-
Equivalent Poisson’s ratio for the deformation in 1-direction causing by the stress in 2 direction
- θ :
-
Fiber orientation
- X t :
-
Ultimate tensile strength
- X c :
-
Ultimate compressive strength
- t0 n:
-
Represents the nominal stress normal-only mode
- t0 s:
-
Represents the nominal stress first direction
- t0 t:
-
Represents the nominal stress first direction
- Gc n:
-
Represents the normal fracture energy
- Gs c:
-
Represents the shear fracture energy
- Gc t:
-
Represents the shear fracture energy
- K nn :
-
Represents the rigidity normal direction
- K ss :
-
Represents the rigidity shear direction
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Funding
This work was financially supported by the National Science Foundation of China (No.52175400, No.51805164, No.52075127), the Natural Science Foundation of Hunan Province (No. 2021JJ30263), and the Natural Science Foundation of Jiangsu Province (No.BK20201474).
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Fei Su: conceptualization, formal analysis, resources, writing-review and editing, supervision, project administration, and funding acquisition. Chunjie Li: methodology, validation, investigation, data curation, and writing original draft. Guojun Dong: modeling analysis, test operation, writing-review, and editing (Sects. 2.1 and 2.2). Lei Zhen: data curation, writing-review, and editing (Sect. 2.3). Bing Chen: test operation and Matlab programming.
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Su, F., Li, C., Dong, G. et al. Study on the formation mechanism of cutting surface of carbon fiber-reinforced composites. Int J Adv Manuf Technol 121, 2049–2062 (2022). https://doi.org/10.1007/s00170-022-09478-5
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DOI: https://doi.org/10.1007/s00170-022-09478-5