4.6 Article

Cutting force model and damage formation mechanism in milling of 70wt% Si/Al composite

Journal

CHINESE JOURNAL OF AERONAUTICS
Volume 36, Issue 7, Pages 114-128

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2022.07.018

Keywords

Cutting force analytical model; Cutting-edge radius; Surface quality; Damage formation mechanism

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High-mass fraction silicon aluminium composite (Si/Al composite) has unique properties and wide applications, while its machining process is often hindered by rapid tool wear and damaged surfaces. This work investigates the mechanisms of milling-induced damages of 70wt% Si/Al composites and provides guidance for tool selection and damage inhibition in high-efficiency and high-precision machining.
High-mass fraction silicon aluminium composite (Si/Al composite) has unique properties of high specific strength, low thermal expansion coefficient, excellent wear resistance and weldability. It has attracted many applications in terms of radar communication, aerospace and automobile industry. However, rapid tool wear resulted from high cutting force and hard abrasion, and damaged machined surfaces are the main problem in machining Si/Al composite. This work aims to reveal the mechanisms of milling-induced damages of 70wt% Si/Al composites. A cutting force analytical model considering the characteristics of both the primary silicon particles and the cutting-edge radius was established. Milling experiments were conducted to verify the validity of the model. The results show that the analytical model exhibits a good consistency with the experimental results, and the error is about 10%. The cutting-edge radius has significant effects on the cutting force, surface roughness and damage formation. With the increase in the cutting-edge radius, both the cutting force and the surface roughness decrease firstly and then increase. When the cutting-edge radius is 27 lm, the surface roughness (Sa) reaches the minimum of 2.3 lm. Milling-induced surface damages mainly contain cracks, pits, scratches, matrix coating and burrs. The damage formation is dominated by the failure mode of primary silicon particles, which includes compressive breakage, intragranular fracture, particle pull-out, and interface debonding. In addition, the high ductility of aluminium matrix leads to matrix coating. This work provides guidance for tool selection and damage inhibition in high-efficiency and high-precision machining of high & COPY; 2022 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).

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