上海理工大学 机构 机械工程学院,上海,200093
[ "安星辰,本科生," ]
[ "丁子珊,副教授," ]
纸质出版:2025
移动端阅览
安星辰, 丁子珊, 成国峰, 等. 微重力环境下的FDM熔丝形态研究[J]. 机械科学与技术, 2025,44(12):2136-2145.
安星辰, 丁子珊, 成国峰, et al. Study on FDM Fuse Morphology in Microgravity Environment[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(12): 2136-2145.
安星辰, 丁子珊, 成国峰, 等. 微重力环境下的FDM熔丝形态研究[J]. 机械科学与技术, 2025,44(12):2136-2145. DOI: 10.13433/j.cnki.1003-8728.20230376.
安星辰, 丁子珊, 成国峰, et al. Study on FDM Fuse Morphology in Microgravity Environment[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(12): 2136-2145. DOI: 10.13433/j.cnki.1003-8728.20230376.
针对未来太空加工制造中,熔融沉积成型(Fused deposition modeling
FDM)参数的选择是否会影响熔丝颈部长度和成型件拉伸强度的问题,采用流体有限元软件Fluent对微重力FDM进行堆积成型过程的仿真,分析了不同打印层厚、打印速度和打印温度在不同重力环境下对熔丝叠加黏结时颈部长度的影响,并与FDM成型件的拉伸强度进行关联分析。结果表明,打印层厚的增加会使得熔丝的颈部长度减小,并在0.1 mm时微重力与常重力环境下差距明显,为0.021 mm。打印速度为60 mm/s时的颈部长度最大,当速度过快时,熔丝会因受热不充分导致黏结的效果降低,使得颈部长度降低。微重力则会减小丝材的质量力,进而使颈部长度减小,降低成型件的拉伸强度,且拉伸强度平均低于常重力约7.1%。
Aim at the selection of fused deposition modeling (FDM) parameters affecting the length of the fuse neck and the tensile strength of the molded parts in the future space processing and manufacturing
the fluid finite element software “Fluent” was used to simulate the stacking molding of microgravity FDM. The effects of the printing layer thicknesses
printing speeds and printing temperatures on the neck length of the fuse superposition and bonding under different gravity environments were analyzed
and the tensile strength of the FDM molded parts was analyzed in correlation.The results show that to increase the thickness of the printed layer will reduce the neck length of the fuse
and the difference between the microgravity and the normal gravity environments is obvious at 0.1 mm
which is 0.021 mm.The neck length is maximum when the printing speed is 60 mm/s. When the speed is too fast
the bonding effect of the fuse will be reduced due to insufficient heating
resulting in a reduction in the neck length.Microgravity will reduce the mass force of the wire
thereby reducing the length of the neck and reducing the tensile strength of the molded parts. The averagetensile strength is about 7.1% lower than normal gravity.
0
浏览量
0
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010602201714号