Uyen Tran Minh The, Do Thanh Trung, Minh Pham Son
Faculty of Mechanical Engineering, HCMC University of Technology and Education, Ho Chi Minh City 71307, Vietnam.
Polymers (Basel). 2022 May 30;14(11):2218. doi: 10.3390/polym14112218.
In micro-injection molding, the plastic filling in the cavity is limited by the frozen layer due to the rapid cooling of the hot melt when it comes into contact with the surface of the cavity at a lower temperature. This problem is more serious with composite materials, which have a higher viscosity than pure materials. Moreover, this issue is also more serious with composite materials that have a higher weight percentage of glass filer. In this article, a pre-heating step with the internal gas heating method was used to heat the cavity surface to a high temperature before the filling step to reduce the frozen layer and to improve the filling ability of the composite material (polyamide 6 + 30% glass fiber) in the micro-injection molding process. To heat the cavity surface, an internal gas-assisted mold temperature control (In-GMTC) system was used with a pulsed cooling system. We assessed different mold insert thicknesses (t) and gaps between the gas gate and the heating surface (G) to achieve rapid mold surface temperature control. The heating process was observed using an infrared camera, and the temperature distribution and the heating rate were analyzed. Thereafter, along with the local temperature control, the In-GMTC was used for the micro-injection molding cycle. The results show that, with a gas temperature of 300 °C and a gas gap of 3.5 mm, the heating rate reached 8.6 °C/s. The In-GMTC was also applied to the micro-injection molding process with a part thickness of 0.2 mm. It was shown that the melt flow length had to reach 24 mm to fill the cavity completely. The results show that the filling ability of the composite material increased from 65.4% to 100% with local heating at the melt inlet area when the gas temperature rose from 200 to 400 °C with a 20 s heating cycle.
在微注塑成型中,由于热熔体在较低温度下与型腔表面接触时迅速冷却,型腔内的塑料填充受到冻结层的限制。对于复合材料来说,这个问题更为严重,因为复合材料的粘度比纯材料更高。此外,对于玻璃纤维重量百分比更高的复合材料,这个问题也更为严重。在本文中,采用内部气体加热法的预热步骤,在填充步骤之前将型腔表面加热到高温,以减少冻结层,并提高复合材料(聚酰胺6 + 30%玻璃纤维)在微注塑成型过程中的填充能力。为了加热型腔表面,使用了带有脉冲冷却系统的内部气体辅助模具温度控制系统(In-GMTC)。我们评估了不同的模具镶件厚度(t)以及气闸与加热表面之间的间隙(G),以实现模具表面温度的快速控制。使用红外热像仪观察加热过程,并分析温度分布和加热速率。此后,在局部温度控制的同时,将In-GMTC用于微注塑成型周期。结果表明,在气体温度为300°C和气隙为3.5 mm的情况下,加热速率达到8.6°C/s。In-GMTC还应用于壁厚为0.2 mm的微注塑成型过程。结果表明,熔体流动长度必须达到24 mm才能完全填充型腔。结果表明,当气体温度在20 s加热周期内从200°C升至400°C时,通过在熔体入口区域进行局部加热,复合材料的填充能力从65.4%提高到了100%。