中文核心期刊
CSCD来源期刊
中国科技核心期刊
RCCSE中国核心学术期刊

重庆交通大学学报(自然科学版) ›› 2024, Vol. 43 ›› Issue (6): 124-132.DOI: 10.3969/j.issn.1674-0696.2024.06.16

• 交通装备 • 上一篇    

SLM成形Ti-6Al-4V层状混合点阵结构的力学性能和吸能特性研究

任毅1, 2,冉威1,蒲林1,蔡锶杨1,赵宇成1   

  1. (1.重庆交通大学 航空学院,重庆 400074;2.绿色航空能源动力重庆市重点实验室,重庆 401130)
  • 收稿日期:2023-10-31 修回日期:2024-01-09 发布日期:2024-06-24

Mechanical Properties and Energy Absorption Characteristics of SLM-Formed Ti-6Al-4V Layered Hybrid Lattice Structure

REN Yi1, 2, RAN Wei1, PU Lin1, CAI Siyang1, ZHAO Yucheng1   

  1. (1. School of Aeronautics, Chongqing Jiaotong University, Chongqing 400074, China; 2.Chongqing Key Laboratory of Green Aviation Energy and Power, Chongqing 401130, China)
  • Received:2023-10-31 Revised:2024-01-09 Published:2024-06-24

摘要: 以选区激光熔化(SLM)成形的Ti-6Al-4V钛合金层状混合点阵结构为研究对象。首先设计并制备了由体心立方(BCC)单胞构成的单一点阵结构以及由BCC单胞和面心立方(FCC)单胞组成的2种层状混合点阵结构;其次,利用扫描电子显微镜(SEM)对所制备的点阵结构表面形貌和几何结构进行了表征;再次,采用万能力学试验机对点阵结构进行了准静态单轴压缩试验,并比较了不同点阵结构的力学性能和吸能性能;最后,分析并讨论了单一点阵结构和层状混合点阵结构的变形模式。结果表明:与BCC单一点阵结构相比,层状混合点阵结构TBF-A和TBF-B的弹性模量分别提高27.80%和24.15%,屈服强度分别提高22.96%和18.36%,比吸能分别提高96.01%和33.33%;在变形行为方面,BCC点阵结构沿45°方向整体断裂,而TBF-A和TBF-B层状混合点阵由于增强相(FCC点阵结构)的存在,其断裂仅发生在基体相(BCC点阵结构)区域。

Abstract: The Ti-6Al-4V titanium alloy lattice structure formed by selective laser melting (SLM) was used as the object of study. Firstly, a single lattice structure composed of body-centered cubic (BCC) unit cell and the layered-hybrid lattice structure composed of BCC unit cell and face-centered cubic (FCC) unit cell were designed and prepared. Secondly, the surface morphology and geometry structure of the prepared lattice structures were characterized by using scanning electron microscopy (SEM). Thirdly, quasi-static uniaxial compression tests on the lattice structure were performed by using a universal mechanical testing machine, and the mechanical and energy absorption properties of different lattice structures were compared. Finally, the deformation modes of the single lattice structure and the layered hybrid lattice structure were analyzed and discussed. The results show that the elastic modulus of the layered hybrid lattice structures TBF-A and TBF-B is respectively increased by 27.80% and 24.15%, the yield strength is respectively increased by 22.96% and 18.36%, and the specific energy absorption is respectively increased by 96.01% and 33.33%, compared with the single BCC lattice structure. In addition, in terms of deformation behavior, the BCC lattice structure undergoes overall fracture along the 45° direction, and the fracture of the TBF-A and TBF-B layered hybrid lattice structures occurs only in the region of the matrix phase (BCC lattice structure) due to the presence of the reinforce phase (FCC lattice structure).