The present invention discloses a flying shear blade. The component has the weight percentage that C is 0.40-0.70, Si is 0.50-1.20, Mn is 0.20-0.50, Cr is 4.00-6.00, Mo is 0.50-2.00, V is 0.30-1.50, P is less than or equal to 0.02, S is less than or equal to 0.02, and Fe and inevitable
impurity are the residual. The present invention provides a manufacture method of electric furnace
smelting, and
ingot casting;
hydrogen removing and annealing treatment, and
forging; preliminary heat treatment, rough
machining,
quenching and
tempering heat treatment (primary
quenching and high temperature
tempering), semi finishing, ultimate heat treatment (secondary
quenching, primary low temperature
tempering, and secondary low temperature tempering), and fine finishing. By effectively controlling the material texture and the morphology, the quantity, the size and the distribution of carbonide, the quenching temperature and the tempering temperature of the quenching and tempering heat treatment, and the quenching temperature and the tempering temperature of the ultimate heat treatment are controlled, the texture
crystal grains are more refined, the carbonide is distributed in a dispersed way, and simultaneously, the
thermal stability and the retentivity are remarkably enhanced, thereby being advantageous for improving the
operational performance of the blade.