Orthorhombic titanium aluminides represent the youngest class of alloys eme
rging out of the group of titanium aluminides. These new materials are base
d on the ordered orthorhombic phase Ti2AlNb, which was discovered for the f
irst time in the late 1980s as a constituent in a Ti3Al-base alloy. In the
1990s primarily simple ternary Ti-Al-Nb orthorhombic alloys were investigat
ed in countries such as the US, UK, India, France, Japan, and Germany. The
drive was mainly provided by jet engine manufacturers and related research
labs looking for a damage-tolerant, high-temperature, light-weight material
. This follows the aim of further extending the use of lower density titani
um-base materials in temperature regimes, where heavy nickel-base superallo
ys are the only alternative today. The present understanding of microstruct
ure-property relationships for orthorhombic titanium aluminides reveals an
attractive combination of low and high temperature loading capabilities. Th
ese involve high room-temperature ductility and good formability, high spec
ific elevated temperature tensile and fatigue strength, reasonable room-tem
perature fracture toughness and crack growth behavior, good creep, oxidatio
n, and ignition resistance combined with a low thermal expansion coefficien
t. This article reviews the aspects of composition-microstructure-property
relationships in comparison to near-alpha titanium, TiAl, and nickel-base a
lloys. Special emphasis is also placed on the environmental degradation of
the mechanical properties.