The present application belongs to the field of TiAl
intermetallic compound, and relates to a TiAl
alloy composition and a preparation method of high-performance TiAl
alloy low-pressure
turbine blade. Based on a TiAl
alloy composition, the alloy is first made to have
fine grain structure through reasonable
extrusion + recrystallization annealing process, then the special
molybdenum alloy die and the process method of vacuum isothermal die
forging are adopted, so that the brittle material realizes the forming of blade structure at high temperature and
low speed, and the technical
bottleneck problems such as large blade
machining allowance, serious material waste, uneven blade structure, unstable mechanical properties of parts and the like caused by the need of
machining preform of TiAl alloy at high temperature and preheating at low temperature during the near isothermal forming in the conventional preparation method are solved, and the blade quality is significantly improved and the manufacturing cost is saved. The
machining allowance of the TiAl blade die
forging part of the present application is only 2mm, and the
raw material consumption can be saved by about 30%.