Title of article
Gamma titanium aluminide, TNB
Author/Authors
Voice، نويسنده , , Wayne E. and Henderson، نويسنده , , Michael C. Shelton، نويسنده , , Edward F.J. and Wu، نويسنده , , Xinhua، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2005
Pages
6
From page
959
To page
964
Abstract
A range of mechanical properties for wrought TNB alloy (Ti–45Al–8Nb–0.2C%) and cast Ti4522XD(Ti–45Al–2Nb–2Mn–XD) have been assessed. The influence of notch sensitivity on fatigue strength has been evaluated and compared in terms of different microstructure and alloy composition. The effects of complex loading on fatigue strength have also been investigated with pre-creep deformations of 0.5, 3 and 5%, pre-exposure to 700 °C for 24 and 150 h or pre-low cycle fatigue testing at 700 °C. The tolerance of these materials to foreign object damage (FOD) has also been compared with the nickel alloy IN718. Under most conditions the TNB alloy has shown superior performance to Ti4522XD and its FOD tolerance appears to be better than IN718.
Keywords
G. Aero-engine components , A. Titanium aluminides , based on TiAl , B. Fatigue resistance and crack growth
Journal title
Intermetallics
Serial Year
2005
Journal title
Intermetallics
Record number
1502830
Link To Document