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© 2022 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.

Abstract

The composite-material laminate structure will inevitably encounter connection problems in use. Among them, mechanical connections are widely used in aerospace, automotive and other fields because of their high connection efficiency and reliable connection performance. Milling parameters are important for the opening quality. In this paper, continuous-glass-fiber-reinforced-polypropylene (GFRPP) laminates were chosen to investigate the effects of different cutters and process parameters on the hole quality. The delamination factor and burr area were taken as the index to characterize the opening quality. After determining the optimal milling tool, the process window was obtained according to the appearance of the milling hole. In the selected process parameter, the maximum temperature did not reach the PP melting temperature. The best hole quality was achieved when the spindle speed was 18,000 r/min and the feed speed was 1500 mm/min with the corn milling cutter.

Details

Title
Milling Parameter Optimization of Continuous-Glass-Fiber-Reinforced-Polypropylene Laminate
Author
Hu, Hanjie 1 ; Du, Bing 2 ; Conggang Ning 3 ; Zhang, Xiaodong 3 ; Wang, Zhuo 3 ; Xiong, Yangyang 3 ; Zeng, Xianjun 4 ; Chen, Liming 5 

 School of Aeronautics, Chongqing Jiaotong University, Chongqing 400074, China; [email protected]; The Green Aerotechnics Research Institute of CQJTU, Chongqing 401120, China; [email protected] 
 Chongqing Key Laboratory of Nano–Micro Composite Materials and Devices, School of Metallurgy and Materials Engineering, Chongqing University of Science and Technology, Chongqing 401331, China; [email protected] (C.N.); [email protected] (X.Z.); [email protected] (Z.W.); [email protected] (Y.X.); College of Aerospace Engineering, Chongqing University, Chongqing 400030, China 
 Chongqing Key Laboratory of Nano–Micro Composite Materials and Devices, School of Metallurgy and Materials Engineering, Chongqing University of Science and Technology, Chongqing 401331, China; [email protected] (C.N.); [email protected] (X.Z.); [email protected] (Z.W.); [email protected] (Y.X.) 
 The Green Aerotechnics Research Institute of CQJTU, Chongqing 401120, China; [email protected] 
 College of Aerospace Engineering, Chongqing University, Chongqing 400030, China 
First page
2703
Publication year
2022
Publication date
2022
Publisher
MDPI AG
e-ISSN
19961944
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
2649024388
Copyright
© 2022 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.