TY - JOUR
T1 - Influence of nitriding on microstructure and fatigue behaviour of a solute-rich beta titanium alloy
AU - Müller, C.
AU - Holzwarth, U.
AU - Gregory, J. K.
PY - 1997
Y1 - 1997
N2 - The solute-rich beta titanium alloy Ti-3Al-8V-6Cr-4Mo-4Zr was subjected to 1500 bar nitrogen pressure at elevated temperatures (500-920°C), leading to a diffusion layer with a high surface hardness. Microstructural, crystallographic and compositional analyses indicate that TiN (δ) and Ti2N (ε) are formed at temperatures exceeding 815°C. The increased concentration of nitrogen, which is a potent α-stabilizer in titanium, also causes α-Ti to form near the surface. The nitriding treatment does not significantly alter the tensile properties or fatigue limit in solution heat treated material. A subsequent ageing treatment of 72 h at 440°C and 16 h at 500°C reduces toughness significantly, allowing cracks induced by nitriding to propagate more easily into the bulk. Tensile ductility and fatigue performance of aged nitrided Ti-3Al-8V-6Cr-4Mo-4Zr are thus significantly lower than in the untreated reference condition.
AB - The solute-rich beta titanium alloy Ti-3Al-8V-6Cr-4Mo-4Zr was subjected to 1500 bar nitrogen pressure at elevated temperatures (500-920°C), leading to a diffusion layer with a high surface hardness. Microstructural, crystallographic and compositional analyses indicate that TiN (δ) and Ti2N (ε) are formed at temperatures exceeding 815°C. The increased concentration of nitrogen, which is a potent α-stabilizer in titanium, also causes α-Ti to form near the surface. The nitriding treatment does not significantly alter the tensile properties or fatigue limit in solution heat treated material. A subsequent ageing treatment of 72 h at 440°C and 16 h at 500°C reduces toughness significantly, allowing cracks induced by nitriding to propagate more easily into the bulk. Tensile ductility and fatigue performance of aged nitrided Ti-3Al-8V-6Cr-4Mo-4Zr are thus significantly lower than in the untreated reference condition.
UR - http://www.scopus.com/inward/record.url?scp=0031355604&partnerID=8YFLogxK
U2 - 10.1111/j.1460-2695.1997.tb01519.x
DO - 10.1111/j.1460-2695.1997.tb01519.x
M3 - Article
AN - SCOPUS:0031355604
SN - 8756-758X
VL - 20
SP - 1665
EP - 1676
JO - Fatigue and Fracture of Engineering Materials and Structures
JF - Fatigue and Fracture of Engineering Materials and Structures
IS - 12
ER -