Mechanical Properties of Ti6Al4V Fabricated by Laser Powder Bed Fusion: A Review Focused on the Processing and Microstructural Parameters Influence on the Final Properties

被引:51
作者
Bartolomeu, Flavio [1 ,2 ]
Gasik, Michael [3 ]
Silva, Filipe Samuel [1 ,2 ]
Miranda, Georgina [4 ]
机构
[1] Univ Minho, UMinho, CMEMS, P-4800058 Guimaraes, Portugal
[2] LABBELS Associate Lab, P-4800058 Guimaraes, Portugal
[3] Aalto Univ Fdn, Sch Chem Technol, Dept Mat Sci & Engn, Aalto, Espoo 00076, Finland
[4] Univ Aveiro, Aveiro Inst Mat, CICECO, Dept Mat & Ceram Engn, P-3810193 Aveiro, Portugal
关键词
additive manufacturing; laser powder bed fusion; microstructure; tensile strength; fatigue; ADDITIVELY MANUFACTURED TI-6AL-4V; HEAT-TREATMENT; CELLULAR STRUCTURES; MELTED TI-6AL-4V; FATIGUE PERFORMANCE; CRACK-PROPAGATION; WEAR PERFORMANCE; TITANIUM-ALLOYS; SURFACE DESIGN; BEHAVIOR;
D O I
10.3390/met12060986
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Ti6Al4V alloy is an ideal lightweight structural metal for a huge variety of engineering applications due to its distinguishing combination of high specific mechanical properties, excellent corrosion resistance and biocompatibility. In this review, the mechanical properties of selective laser-melted Ti6Al4V parts are addressed in detail, as well as the main processing and microstructural parameters that influence the final properties. Fundamental knowledge is provided by linking the microstructural features and the final mechanical properties of Ti6Al4V parts, including tensile strength, tensile strain, fatigue resistance, hardness and wear performance. A comparison between Laser Powder Bed Fusion and conventional processing routes is also addressed. The presence of defects in as-built Ti6Al4V parts and their influences on the mechanical performance are also critically discussed. The results available in the literature show that typical Laser Powder Bed-Fused Ti6Al4V tensile properties (>900 MPa yield strength and >1000 MPa tensile strength) are adequate when considering the minimum values of the standards for implants and for aerospace applications (e.g., ASTM F136-13; ASTM F1108-14; AMS4930; AMS6932).
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页数:22
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