Title of article :
Influence of boron and oxygen on the microstructure and mechanical properties of high-strength Ti66Nb13Cu8Ni6.8Al6.2 alloys Original Research Article
Author/Authors :
A. Helth، نويسنده , , U. Siegel، نويسنده , , U. Kuhn، نويسنده , , T. Gemming، نويسنده , , W. Gruner and N. Mattern، نويسنده , , S. Oswald، نويسنده , , Michael T. Marr، نويسنده , , J. Freudenberger، نويسنده , , J. Scharnweber، نويسنده , , C.-G. Oertel، نويسنده , , W. Skrotzki، نويسنده , , L. Schultz، نويسنده , , J. Eckert، نويسنده ,
Issue Information :
دوهفته نامه با شماره پیاپی سال 2013
Pages :
11
From page :
3324
To page :
3334
Abstract :
The influence of boron additions and different oxygen contamination levels on the microstructure and the mechanical properties in the Ti66−xNb13Cu8Ni6.8Al6.2Bx (0 ⩽ x ⩽ 1) system were investigated. The alloys were prepared by levitation copper mould casting as rods with a diameter of 5 mm using different grades of starting elements. The alloy without boron exhibits a maximum compressive stress of more than 2500 MPa, associated with a compressive strain of more than 30%. The ultimate tensile stress is ∼1075 MPa with a maximum elongation of 1.6%. Increased oxygen content leads to a rise of yield strength due to solid solution hardening. Boron additions promote grain refinement and reinforce the interdendritic phase compound by forming needle-like TiB precipitates. This change in microstructure increases the yield stress and the Young’s modulus and lowers the plastic strain. The microstructure was analysed in terms of the boron content by means of scanning electron microscopy, Auger electron spectroscopy and transmission electron microscopy. The presented mechanical properties are compared with the compression and tensile properties of the commercially available Ti6Al4V ELI (ELI = extra low interstitial) alloy.
Keywords :
Boron , Oxygen , Titanium alloy , Mechanical properties , Microstructure
Journal title :
ACTA Materialia
Serial Year :
2013
Journal title :
ACTA Materialia
Record number :
1146978
Link To Document :
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