Abstract
Metal injection moulding (MIM) attracts growing interest as an economic net-shape
manufacturing technique for the processing of titanium and titanium alloys. Even for titaniumaluminides,
intended for high-temperature applications, MIM is seen as a reasonable technique to
overcome processing problems with conventional methods. In this paper, basic requirements in
terms of raw materials, facilities and processing in order to produce high performance components
are presented. Main focus is laid on the well-known Ti-6Al-4V alloy. It is shown that the tensile
properties of specimens after MIM processing can exceed the requirements given by ASTM
standards even without performing an additional HIP process. For an oxygen content ranging from
0.15 to 0.33 wt% plastic elongation yields excellent 14%. Fatigue measurements performed by
means of 4-point-bending tests show that grain size is more important than residual porosity in
order to achieve a high endurance limit. This is shown by addition of boron powder which refines
the microstructure dramatically. The modified alloy Ti-6Al-4V-0.5B yields an endurance limit of
640 MPa compared to 450 MPa of MIM parts made from standard alloy powder. Sintered
components from Ti-45Al-5Nb-0.2B-0.2C (at%) powder made by inert gas atomising (EIGA
technique) and processed by MIM exhibit a residual porosity of only 0.2% and tensile properties
comparable to cast material.