The application discloses an aero-engine blade clamp, which comprises a clamping table, hydraulic cylinders are fixedly installed on both sides of the inner cavity of the clamping table, moving plates are fixedly installed at the output ends of the hydraulic cylinders, clamping pressing blocks are arranged at the upper ends of the sides of the two moving plates, fixed plates are placed at the two ends of the top of the outer surface of the clamping table, and first bolts are inserted into the two ends of the bottom of the fixed plates. Through the arrangement of the fixed plates, side baffles, first bolts, limiting plates and second bolts, auxiliary support and limiting structures around the blade root of the aero-engine blade can be formed on the top of the clamping table, the inclination, deviation or sliding of the blade during clamping can be effectively prevented, manual support of personnel is not needed, through the arrangement of the hydraulic cylinders, the moving plates and the clamping pressing blocks, the clamping and fixing of the blade can be realized, and deviation of the blade during subsequent quality inspection can be avoided.