Chicos Lucia-Antoneta, Pop Mihai Alin, Zaharia Sebastian-Marian, Lancea Camil, Buican George Razvan, Pascariu Ionut Stelian, Stamate Valentin-Marian
Department of Manufacturing Engineering, Transilvania University of Brasov, 500036 Brasov, Romania.
Department of Materials Science, Transilvania University of Brasov, 500036 Brasov, Romania.
Polymers (Basel). 2022 Nov 17;14(22):4988. doi: 10.3390/polym14224988.
Fused Filament Fabrication (FFF) is one of the frequently used material extrusion (MEX) additive manufacturing processes due to its ability to manufacture functional components with complex geometry, but their properties depend on the process parameters. This paper focuses on studying the effects of process parameters, namely infill density (25%, 50%, 75%, and 100%), on the mechanical and thermal response of the samples made of poly(lactic acid) (PLA) reinforced with short glass fibers (GF) produced using FFF process. To perform a comprehensive analysis, tensile, flexural, compression, differential scanning calorimetry (DSC), and thermal gravimetric analysis (TGA) tests were used. The paper also aims to manufacture by FFF process of composite structures of the fuselage section type, as structural elements of an unmanned aerial vehicle (UAV), and their testing to compression loads. The results showed that the tensile, flexural and compression strength of the additive manufactured (AMed) samples increased with the increase of infill density and therefore, the samples with 100% infill density provides the highest mechanical characteristics. The AMed samples with 50% and 75% infill density exhibited a higher toughness than samples with 100% infill. DSC analyses revealed that the glass transition (Tg), and melting (Tm) temperature increases slightly as the infill density increases. Thermogravimetric analyses (TGA) show that PLA-GF filament loses its thermal stability at a temperature of about 311 °C and the increase in fill density leads to a slight increase in thermal stability and the complete degradation temperature of the AMed material. The compression tests of the fuselage sections manufactured by FFF made of PLA-GF composite showed that their stiffening with stringers oriented at an angle of ±45° ensures a higher compression strength than the stiffening with longitudinal stringers.
熔融长丝制造(FFF)是常用的材料挤出(MEX)增材制造工艺之一,因为它能够制造具有复杂几何形状的功能部件,但其性能取决于工艺参数。本文重点研究工艺参数,即填充密度(25%、50%、75%和100%)对采用FFF工艺生产的短玻璃纤维(GF)增强聚乳酸(PLA)制成的样品的力学和热响应的影响。为了进行全面分析,使用了拉伸、弯曲、压缩、差示扫描量热法(DSC)和热重分析(TGA)测试。本文还旨在通过FFF工艺制造机身截面类型的复合结构,作为无人机(UAV)的结构元件,并对其进行压缩载荷测试。结果表明,增材制造(AMed)样品的拉伸、弯曲和压缩强度随填充密度的增加而增加,因此,填充密度为100%的样品具有最高的力学性能。填充密度为50%和75%的AMed样品比填充密度为100%的样品表现出更高的韧性。DSC分析表明,随着填充密度的增加,玻璃化转变温度(Tg)和熔点温度(Tm)略有升高。热重分析(TGA)表明,PLA-GF长丝在约311℃的温度下失去热稳定性,填充密度的增加导致AMed材料的热稳定性和完全降解温度略有增加。由PLA-GF复合材料制成的FFF机身截面的压缩测试表明,与纵向桁条加强相比,以±45°角定向的桁条加强可确保更高的压缩强度。