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基于精密注射成型的扑翼微型飞行器传动部件最佳加工参数

Optimal Processing Parameters of Transmission Parts of a Flapping-Wing Micro-Aerial Vehicle Using Precision Injection Molding.

作者信息

Huang Huei-Yu, Fan Fang-Yu, Lin Wei-Chun, Huang Chiung-Fang, Shen Yung-Kang, Lin Yi, Ruslin Muhammad

机构信息

Department of Dentistry, Taipei Medical University Shuang Ho Hospital, Taipei Medical University, New Taipei City 23561, Taiwan.

School of Dentistry, College of Oral Medicine, Taipei Medical University, Taipei 11031, Taiwan.

出版信息

Polymers (Basel). 2022 Apr 4;14(7):1467. doi: 10.3390/polym14071467.

Abstract

In this study, we designed and fabricated transmission parts for a flapping-wing micro-aerial vehicle (FW-MAV), which was fabricated by precision injection molding, and analyzed its warpage phenomena. First, a numerical simulation (Moldflow) was used to analyze the runner balance and temperature, pressure, and stress distributions of the base, gears, and linkage of the transmission structures in an FW-MAV. These data were then applied to fabricate a steel mold for an FW-MAV. Various process parameters (i.e., injection temperature, mold temperature, injection pressure, and packing time) for manufacturing transmission parts for the FW-MAV by precision injection molding were compared. The Taguchi method was employed to determine causes of warpage in the transmission parts. The experimental results revealed that the causes of warpage in the transmission parts were, in order of importance, the mold temperature, injection pressure, packing time, and injection temperature. After the transmission parts were assembled on the FW-MAV, experiments revealed that the MAV could achieve a flight time of 180 s. Mass production of the FW-MAV by precision injection molding could potentially produce substantial savings in time, manpower, and cost.

摘要

在本研究中,我们设计并制造了用于扑翼微型飞行器(FW-MAV)的传动部件,该部件通过精密注塑成型制造,并分析了其翘曲现象。首先,使用数值模拟(Moldflow)分析FW-MAV中传动结构的底座、齿轮和连杆的流道平衡以及温度、压力和应力分布。然后将这些数据应用于制造FW-MAV的钢模。比较了通过精密注塑成型制造FW-MAV传动部件的各种工艺参数(即注射温度、模具温度、注射压力和保压时间)。采用田口方法确定传动部件翘曲的原因。实验结果表明,传动部件翘曲的原因按重要性依次为模具温度、注射压力、保压时间和注射温度。将传动部件组装到FW-MAV上后,实验表明该微型飞行器的飞行时间可达180秒。通过精密注塑成型大规模生产FW-MAV可能会在时间、人力和成本方面大幅节省。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/c321/9003489/c72ccd9aaa55/polymers-14-01467-g001.jpg

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