The invention relates to an alpha +
beta type two-phase
titanium alloy for an aero-engine
fan blade and a preparation method of the alpha +
beta type two-phase
titanium alloy for the aero-engine
fan blade. The preparation method of the alpha +
beta type two-phase
titanium alloy for the aero-engine
fan blade comprises the following steps that S1, the following chemical components are obtained: 4.2%-5.6% of aluminum, 7.5%-8.8% of
vanadium, 0.18%-0.24% of
oxygen, less than or equal to 0.5% of iron, less than or equal to 1% of
niobium, 0.4%-0.8% of
silicon, less than or equal to 0.05% of carbon, less than or equal to 0.05% of
nitrogen, less than or equal to 0.015% of
hydrogen and the balance of titanium and
impurity elements; S2, the
titanium alloy cast
ingot is subjected to first-stage upsetting and drawing; S3, under the conditions of the preset temperature and the preset deformation amount, after reversing is conducted, second-stage upsetting and drawing are conducted on the
titanium alloy cast
ingot; S4, the
titanium alloy cast
ingot is heated to the temperature above the phase transformation point, and then the titanium alloy cast ingot is subjected to third-stage upsetting and drawing; S5, the titanium alloy cast ingot is heated to the temperature below the phase transformation point, then fourth-stage upsetting and drawing are conducted on the titanium alloy cast ingot, and a titanium alloy material is obtained; and S6, the titanium alloy material is subjected to heat treatment. The preparation method is applied to the technical field of titanium alloys.